Electrodeposition of Iridium-Nickel Thin Films on Copper Foam: Effects of Loading and Solution Temperature on Hydrogen Evolution Reaction Performance of Electrocatalyst in Alkaline Water

In order to better understand the electrodeposition mechanism, the CV measured in electrolytes containing nickel, iridium and both iridium and nickel salts are shown in Figure 1. The reduction peaks of iridium, nickel and iridium-nickel were at −0.56 V, −0.37 V and −0.54 V due to the reduction of Ni(II) to Ni0 and Ir(III) to Ir0, respectively. It can be found that the reduction potentials of iridium-nickel and iridium are very close and their peak currents are much higher than that of nickel, which may lead to much more iridium content in the iridium-nickel deposits. Without the addition of complexing agent in the electrolyte, the reduction potential of Ni2+ ions is higher than that of [Ir(III)Br6]3– ions. Therefore, the deposition of nickel was preferable during the electrodeposition process. The oxidation peak for iridium is present at –0.24 V vs. Ag/AgCl. The oxidation peak was mainly attributed to iridium oxidation, Ir0 → Ir(III). However, the oxidation peak for iridium-nickel is present at around –0.24~–0.15 V vs. Ag/AgCl because the iridium-nickel codeposited film is suggested to be alloyed. There is no oxidation peak for nickel at negative potential. For iridium-nickel film, the current peak at –0.54 V was due to the hydrogen adsorption, while the current peak at around –0.24~–0.15 V was due to the reoxidation of the codeposited deposits. For iridium film, the current peak at –0.56 V was observed due to the hydrogen adsorption, which is higher than the current peak at –0.23 V due to hydrogen desorption. These findings indicate that iridium and iridium-nickel deposits have a significant facility for hydrogen incorporation into the plated deposits (37). The deposition processes of iridium and iridium-nickel films are accompanied by a large amount of hydrogen evolution.

Fig. 1.

Cyclic voltammograms of iridium-nickel electrode in the bath of 26 mM [Ir(III)Br6]3– and 26 mM Ni2+, nickel electrode in the bath of 26 mM Ni2+ and iridium electrode in the bath of 26 mM [Ir(III)Br6]3–

Cyclic voltammograms of iridium-nickel electrode in the bath of 26 mM [Ir(III)Br6]3– and 26 mM Ni2+, nickel electrode in the bath of 26 mM Ni2+ and iridium electrode in the bath of 26 mM [Ir(III)Br6]3–

Figure 2 shows the plots of the mass gain of the specimens deposited in one electrolyte with different deposition times. There is a nonlinear dependence of the mass gain against deposition time. According to CV curves, nickel is preferentially deposited because the deposition potential of nickel is higher than that of iridium. Therefore, the deposition rate for the first specimen, about 2.3 mg min–1 is larger than that of the others. Subsequently, the deposition rate kept stable, and the nickel content in the films decreased. The slope of the second plot is around 0.35, indicating a deposition rate of about 0.35 mg min–1. The atomic composition of the film by EDS is listed in Table II. The iridium content in the deposits increased remarkably from 1 min to 5 min. This result is in agreement with the above discussion.

Fig. 2.

Plots of the mass gain of the specimens

Plots of the mass gain of the specimens

Table II

Atomic Composition (at%) of Iridium-Nickel Thin Films Determined by EDS

Specimen Content, at%
Nickel Iridium
1 min, 2.3 mg cm–2 58 42
3 min, 3.5 mg cm–2 20 80
5 min, 4.2 mg cm–2 12 88

Figure 3 shows the surface morphology of iridium-nickel electrocatalysts and copper foam. Figure 3(a) shows a large number of dendritic structures for copper foam with diameters 30–60 nm. In Figures 3(b) and 3(c), many pores and hollowed topography can be observed. The grain boundary of the copper foam is clearly visible because of the thin layer. With the increase of deposition time, the thickness of the film also increases. It can be clearly seen that the iridium-nickel thin film is attached to the surface of the substrate (see Figure 3(d)). The cross structure and many pores of copper foam can increase the active area of the thin film, which is advantageous for hydrogen evolution performance. Figure 4 shows the EDS spectrum of the iridium-nickel electrocatalysts with different loadings. The chemical composition of iridium and nickel in the thin films is shown in Table II. EDS elemental mapping to probe nickel and iridium presence for Ir80Ni20 and the distribution on the substrate surface is shown in Figure 5. A large amount of copper is evenly distributed on the surface. It can be observed that the amount of iridium is larger than that of nickel in the image. Ir80Ni20 thin film was almost completely covered on the copper foam surface. The phase and crystallographic structure of the films on copper foam were determined by X-ray diffraction (XRD), however the signals of the films were not detected due to small loading, the information of copper foam was only present. The copper foam was composed of polycrystalline structure.

Fig. 3.

SEM images of copper foam: (a) iridium-nickel films; (b) 2.3 mg cm–2; (c) 3.5 mg cm–2; (d) 4.2 mg cm–2

SEM images of copper foam: (a) iridium-nickel films; (b) 2.3 mg cm–2; (c) 3.5 mg cm–2; (d) 4.2 mg cm–2

Fig. 4.

EDS spectra of the iridium-nickel films: (a) 2.3 mg cm–2; (b) 3.5 mg cm–2; (c) 4.2 mg cm–2

EDS spectra of the iridium-nickel films: (a) 2.3 mg cm–2; (b) 3.5 mg cm–2; (c) 4.2 mg cm–2

Fig. 5.

EDS elemental mapping images of Ir80Ni20 thin film in Fig. 3(c): (a) copper-blue; (b) iridium-red; (c) nickel-green

EDS elemental mapping images of Ir80Ni20 thin film in Fig. 3(c): (a) copper-blue; (b) iridium-red; (c) nickel-green

The chemical composition and elemental states of Ir80Ni20 thin films were deeply analysed by XPS technique. The atomic composition of Ir80Ni20 thin films on copper foam is listed in Table III. Figure 6 shows the XPS depth profile for the top surface of iridium-nickel thin films on copper foam. The elements copper, iridium, carbon, oxygen and bromine were determined on the top surface of as-deposited film. Unfortunately, the signal nickel element was not detected, probably due to the low quantities in the film. The large amounts of carbon and oxygen contents were attributed to ordinary adsorption from the environment (see Table III), significant amounts of oxides formed on the surface of the electrode during electrodeposition. The bromine signal was mainly from the electrolytes. The coverage of the Ir80Ni20 thin film on copper foam was not so perfect that the signal copper was determined. Figure 7 shows the high-resolution XPS spectra of as-deposited Ir80Ni20 thin film on copper foam. The binding energies of iridium were located at 63.6 eV and 60.6 eV for Ir0 4f5/2 and 4f7/2, respectively. It was indicated that the film was composed of the metallic state of iridium, although the nickel signal was not detected (Figure 7(a)). The binding energies of Ir0 4f5/2 and 4f7/2 have weak shifts in iridium-nickel thin films in contrast with pure iridium (63.8 eV and 60.8 eV) (38). This is ascribed to the incorporation of nickel into the electronic structures of iridium, demonstrating the changes in the alloyed phase, in turn enhancing the catalytic performance (3941). In the O-1s spectrum (see Figure 7(b)), the main peak at 530.5 eV is attributed to O 1s of the oxides, and the peaks at 531.3 eV and 531.9 eV are usually ascribed to surface species, such as hydroxyls or absorbed water of the film. An additional broader feature peak is present at a higher binding energy of ~533.2 eV.

Table III

Atomic Composition (at%) of Ir80Ni20 Thin Film on Copper Foam Determined by XPS

Elements Chemical composition, at%
Cu2p 24.87
Ir4f 2.91
C1s 34.37
O1s 37.41
Br3d 0.44

Fig. 6.

XPS depth profile for the top surface of Ir80Ni20 thin film on copper foam

XPS depth profile for the top surface of Ir80Ni20 thin film on copper foam

Fig. 7.

High-resolution XPS spectra of Ir80Ni20 thin film: (a) Ir-4f; (b) O-1s

High-resolution XPS spectra of Ir80Ni20 thin film: (a) Ir-4f; (b) O-1s

The electrocatalytic activities for HER of iridium-nickel thin films with different loadings were investigated in 1.0 M KOH solutions. Figure 8 presents the iR-corrected LSV curves and Tafel slopes of the bare copper foam and iridium-nickel samples. As anticipated, the bare copper foam displays a relatively low catalytic activity which requires an overpotential of 502.5 mV to drive a current density of 10 mA cm–2. In contrast, the iridium-nickel catalyst exhibits excellent catalytic activity, demonstrating a negligible onset potential (8.3–18.3 mV) at 1 mA cm–2 for hydrogen evolution in the electrolyte (see Table IV), which are much lower than the onset potential of copper foam. Here, the onset potential should always be defined on the basis of a specific current density, where the Tafel constant can be considered as the onset potential of HER (42, 43). From an electrochemical point of view, the Tafel constant becomes complementary to the Tafel slope.

Fig. 8.

(a) Linear sweep voltammograms obtained in 1 M KOH solution at room temperature and potential scan rate of 5 mV s–1; (b) Tafel plots

(a) Linear sweep voltammograms obtained in 1 M KOH solution at room temperature and potential scan rate of 5 mV s–1; (b) Tafel plots

Table IV

Comparison of the HER Catalytic Performance of Different Catalysts in 1.0 M KOH at 298 K

Samples Onset potential, mV (at 1 mA cm–2) Overpotential, η, mV (at 10 mA cm–2) Tafel slope, mV dec–1 Exchange current density, mA cm–2
Ir42Ni58 8.3 78 49 0.69
Ir80Ni20 11.4 60 40 0.657
Ir88Ni12 18.3 97 43 0.418
Copper foam 336 500 189 0.022
Pt/C (45) 0 40 29.5 0.75

In order to obtain a current density of 10 mA cm–2, Ir42Ni58, Ir80Ni20 and Ir88Ni12 thin films require overpotential of 76.4 mV, 60 mV and 95.4 mV, respectively (see Table IV). These values are already twice the overpotential of 34 mV at the current density of 10 mA cm–2 for the state-of-the-art Pt/C catalyst tested in the same electrolyte. To shed light on insights about the reaction kinetics, a detailed Tafel analysis has been performed. The Tafel equation is as follows (44) (Equation (iii)):

(iii)

where j is the current density, j0 is the exchange current density (i.e. a constant at η = 0 V) and b is the Tafel slope. The equation indicates that excellent catalysts should have both low Tafel slopes and high exchange current densities. The potential-dependency of current density j is related to the interfacial electrocatalytic reaction n, as the following (Equation (iv)):

(iv)

where n is the number of electrons, F is the Faraday’s constant (96,500 mol C–1). Because the current density j is potential-dependent, ν is also potential-dependent and consisted of three elementary steps as the following Equations (v)(vii):

Initial discharge or Volmer step:

(v)

Atom + ion or Heyrovsky step:

(vi)

Atom + atom or Tafel step:

(vii)

The above elementary steps lead to two mechanisms: Volmer-Heyrovsky and Volmer-Tafel. Three rate determining steps, Volmer, Heyrovsky and Tafel are possible for the above two mechanisms. The linear portions of the Tafel plots were fitted to the Tafel equation, the Tafel slope values for Ir42Ni58, Ir80Ni20 and Ir88Ni12 thin films were 49 mV dec–1, 40 mV dec–1 and 43 mV dec–1 respectively, indicating that the Ir80Ni20 electrocatalyst has much higher intrinsic activity than other catalysts for HER while still being less active than the Pt/C catalyst (28mV dec–1) (45). The Tafel slopes indicate the HER process of iridium-nickel film follows a Volmer-Heyrovsky mechanism, where electrochemical desorption of hydrogen is regarded as the rate-limiting step, i.e. the HER rate is determined by both H2O discharge and desorption of H from the catalyst surface (4648). The exchange current density (j0) of iridium-nickel thin films and copper foam were calculated by the Tafel extrapolation method (see Table IV), which reflects the catalytic activity of the electrode material under the reaction thermodynamic equilibrium conditions. The j0 value of the Ir80Ni20 thin film was 87.6% of the Pt/C catalyst (0.75 mg cm–2, 15 wt% Pt) (45). Therefore, an iridium-nickel thin film has highly efficient electrocatalytic activity for HER. In addition, a summary of the hydrogen evolution performance of electrocatalysts in alkaline solutions is listed in detail in Table V (4981). It can be found that the Tafel slope of the iridium-nickel thin film is low, indicating iridium-nickel thin film has excellent electrocatalytic performance.

Table V

Summary of HER Electrocatalysts in Alkaline Solution on Exchange Current Densities, Overpotential and Tafel Slope

Coatings Substrates Methods Alkaline Temperature, °C j0, mAcm–2 η, mV b, mVdec–1 Refs.
Ni-P10 Mild steel Electroless plating 32% NaOH 30 3.6 × 10–3 323(200) 105 (49)
Ni-Mo Mild steel Electrodeposition 6 M KOH 80 185(300) 175 (50, 51)
Ni-Mo Mild steel ditto 6 M KOH 80 1.86 × 10–2 185(300) 105 (5153)
Ni-Mo-Fe Mild steel ditto 6 M KOH 80 187(300) 165 (54, 55)
Ni83P12C5 Copper ditto 1 M NaOH 25 1.54 × 10–3 201.9(250) 95.2 (56, 57)
Ni71Mo27P2 Copper ditto 1 M NaOH 70 3.10 × 10–3 170(250) 89 (58)
Nickel Arc melting 1 M NaOH 25 3.3 × 10–3 121 (59)
NiMo46 Carbon steel Electrodeposition 5 M KOH 25 5.43 215(100) 147 (60)
Ni-Sn Copper ditto 1 M KOH 25 6.939 × 10–3 121 (61)
Ni-Fe-C Copper ditto 3.5% NaCl 90 70(120) (62)
Ni-S Nickel ditto 30% KOH 25 5.385 141(200) 264.4 (63)
NiMn Graphite ditto 30% NaOH 25 0.6 141(100) 130 (64)
NiCoZn Copper ditto 1 M KOH 25 1.62 140(100) 81 (65)
Ni92P8 Copper ditto 1 M NaOH 70 0.24 171(250) 57 (66)
NiTi Steel Thermal arc spraying 1 M NaOH 25 5.25 283 (67)
NiFeZn Carbon steel Electrodeposition 28% KOH 80 3.778 104(135) 67 (68)
Ni-S Carbon steel ditto 28% NaOH 80 4.6 90(150) 80.9 (69)
Ni–CeO2 Carbon steel ditto 1 M NaOH 25 80.71 × 10–3 157 (70)
Ni–LaNi5 Copper ditto 1 M NaOH 25 13.2 330(250) 101 (71)
Co90W10 Arc melting 1 M NaOH 25 76.5 × 10–3 326(250) 102 (72)
CoNiFe Carbon cloth Electrodeposition 1 M NaOH 70 5.85 × 10–4 151 (73)
Co–Mo45 Mild steel ditto 1 M NaOH 30 49.9 × 10–3 103 (74)
Fe82B18 Rapid solidification 1 M KOH 25 47 × 10–3 430(300) 113 (75)
Ni-P Mild steel Electroless plating 32% NaOH 30 3.98 × 10–6 340(250) 147 (76)
Platinum Heat treatment 8 M KOH 85 2.66 × 10–2 460(100) 390 (77)
Nano-Zr67Ni33 Melt-spinning 6 M KOH 25 2.5 × 10–1 1530(50) 121 (78)
Raney Nickel Perforated nickel sheet Plasma spraying 25% KOH 70 4 119(250) 84 (79)
CoFe Nickel foam Electrodeposition 1 M KOH 25 110(10) 35 (80)
Iron Nickel foam ditto 1 M KOH 25 175(10) 48 (80)
Cobalt Nickel foam ditto 1 M KOH 25 180(10) 60 (80)
Nickel foam 1 M KOH 25 260(10) 96 (80)
Platinum Nickel foam Electrodeposition 1 M KOH 25 40(10) 72 (80)
Porous nickel Nickel Spontaneous deposition 1 M NaOH 25 0.32 298(100) 138 (81)
Porous NiIr Nickel ditto 1 M NaOH 25 2.23 274(100) 166 (81)
Porous NiRu Nickel ditto 1 M NaOH 25 7.2 48(100) 42 (81)
Ir80Ni20 Copper foam Electrodeposition 1 M KOH 25 0.657 60(10) 40 (32)
Nickel Copper foam ditto 1 M KOH 25 0.347 170(10) 112 (32)
Iridium Copper foam ditto 1 M KOH 25 0.398 130.1(10) 69 (32)
Ir42Ni58 Copper foam ditto 1 M KOH 25 0.69 78(10) 49 This work
Ir88Ni12 Copper foam ditto 1 M KOH 25 0.418 97(10) 43 This work

The ECSA of the catalyst is proportional to the electrochemical double-layer capacitance (Cdl). As shown in Figure 9, the Cdl values for Ir42Ni58, Ir80Ni20 and Ir88Ni12 were 59.82 mF cm–2, 132.91 mF cm–2 and 70.03 mF cm–2, respectively. It indicates that the high hydrogen evolution performance of Ir80Ni20 catalyst was mainly due to the high exposure of effective active sites. On the other hand, the scanning range of –0.15~0.85V for Ir80Ni20 catalyst is larger than the range of –0.25~0.65 V for other catalysts. In our previous publication (32), the initial CV curve of Ir80Ni20 catalyst was measured at a scanning rate of 10 mV s–1. It was found that iridium oxides are electrochemically formed at high positive potential on the surface of Ir80Ni20 thin film during a positive scanning direction, however the formation of iridium oxides cannot easily be reduced to the metal state (32). The formed iridium oxides could result in a significant decrease of HER activity. Therefore, when the scanning range of Ir42Ni58 and Ir88Ni12 thin films was shifted from –0.25 V to 0.65 V, the obtained Cdl values should be valid. Therefore, it is inferred that the hydrogen evolution performance of Ir88Ni12 film is better than that of Ir42Ni58 film, which might be attributed to the increase in iridium content of the film or electrode surface defects, resulting in increasing the number of effective active sites.

Fig. 9.

CV curves with different scan rates for electrodes in the alkaline solution: (a) Ir42Ni58; (b) Ir80Ni20; (c) Ir88Ni12; (d) differences in current density at 0.05 V vs. RHE (Δi = iaic) plotted against scan rate

CV curves with different scan rates for electrodes in the alkaline solution: (a) Ir42Ni58; (b) Ir80Ni20; (c) Ir88Ni12; (d) differences in current density at 0.05 V vs. RHE (Δi = ia–ic) plotted against scan rate

The large active surface area could be related to the porous structure and hollow architecture with crossed branch structure, which results in a significantly enhanced catalytic activity. The rough texture and the porous structure of copper foam facilitate fast mass transport for the enhanced reaction kinetics (82). However, Ir88Ni12 thin film with a good hydrogen evolution performance has a larger electrochemical surface area than Ir42Ni58 film. The electrocatalytic activity of iridium-nickel catalysts show a loading dependence.

Electrochemical impedance measurements were performed to further investigate the reaction kinetics of the HER process under the experimental conditions. Nyquist plots of copper foam, Ir80Ni22, iridium and nickel thin films as a function of overpotential are shown in Figure 10. The preparation of the iridium and nickel electrocatalysts was addressed (32). According to alternating current (AC) circuit theory, impedance spectra obtained for a given electrochemical system can be correlated to one or more equivalent circuit (83). Thus, different equivalent circuits were suggested to model the present data and the relevant model with the minimum number of electrical elements. The model of Ir80Ni22 film consists of the solution resistance (Rs), the low frequency time constant characterising the double-layer capacitance (Cdl) and charge transfer resistance (Rct). The potential dependencies of the obtained data are shown in Table VI. Due to surface heterogeneity of solid electrodes resulting from surface roughness and formation of porous layers, a constant phase element (CPE) is commonly used to replace the capacitance (C) in a real electrochemical process, which mainly depends on a non-ideal capacitance behaviour (84, 85). Rct values of iridium film and copper foam are 72.34 Ω cm2 and 76.64 Ω cm2, respectively. While the charge transfer resistance of nickel and Ir80Ni22 films are large, about 2642 Ω cm2 and 1312 Ω cm2, indicating that the Rct values of iridium film and copper foam are lower than those of nickel and iridium-nickel films. According to the XPS data, there is no iridium oxide on the catalyst surface for Ir80Ni22 thin films. It can be inferred that the iridium thin film was composed of metallic state. On the other hand, copper foam was immersed in nitric acid solution to activate it before the experiment. The absence of oxides in copper foam may result in a charge transfer resistance that is less than other electrocatalysts as a result. For nickel and Ir80Ni22 thin films, the top surface might be composed of some nickel oxides. The surface of nickel-rich nickel-iridium thin films consisted of lots of nickel oxides, the amount of nickel oxides was much more than that of metal nickel (unpublished data). Therefore, there is a contradiction here. The electrocatalytic performance of the thin film involves various factors, such as surface chemical substances, the number of catalytic active sites per unit area, and the electronic effect of the thin film metal. At the cathode, the process of hydrogen reduction for hydrogen gas requires energy to remove electrons from the metal electrode and connect electrons to protons to produce hydrogen. Therefore, the process of transferring electrons from the electrode to the hydrogen ions in the liquid phase has a certain resistance, which is a charge transfer resistance. Iridium electrode with a low resistance could accelerate the electron transfer during the electrocatalytic reaction.

Fig. 10.

(a) Nyquist plots of Ir80Ni20 film, iridium film and copper foam for the HER in 1M KOH; (b) the corresponding equivalent electric circuit models for all samples

(a) Nyquist plots of Ir80Ni20 film, iridium film and copper foam for the HER in 1M KOH; (b) the corresponding equivalent electric circuit models for all samples

Table VI

Electrical Equivalent Circuit Parameters

Samples Rs, Ω cm2 Cdl, F cm–2 Rct, Ω cm2
Iridium 1.218 0.098 72.34
Ir80Ni20 1.485 0.05076 1312
Nickel 13.6 0.003567 2642
Copper foam 1.89 0.005816 76.64

Figure 11 shows the polarisation curves and Tafel curves of the Ir88Ni12 film at different temperatures. As shown in Figure 11(a), the electrode has the best hydrogen evolution performance at 60°C, with only an overpotential of 186 mV to obtain a current density of 30 mA cm–2. At the temperature of 30°C, an overpotential of 212 mV is required. The performance of hydrogen evolution improves from 30°C to 60°C. Interestingly, the hydrogen evolution performance of the catalyst has decreased from 20°C to 30°C. The effect of temperature is not obvious, and the curves are very close. This result can also be derived from the Tafel slopes (see Figure 11(b)). From 20°C to 60°C, the Tafel slope is 46 mV dec–1, 56 mV dec–1, 52 mV dec–1, 43 mV dec–1 and 40 mV dec–1, respectively. The comparison of the HER catalytic performance at different temperatures is shown in Table VII.

Fig. 11.

(a) Linear sweep voltammograms obtained in 1.0 M KOH solution at different temperatures and potential scanning rate of 5 mV s–1; (b) Tafel plots

(a) Linear sweep voltammograms obtained in 1.0 M KOH solution at different temperatures and potential scanning rate of 5 mV s–1; (b) Tafel plots

Table VII

Comparison of the HER Catalytic Performance in 1.0 M KOH at Different Temperatures

Temperature, °C Onset potential, mV Overpotential, η, mV (at 30 mA cm–2) Tafel slope, mV dec–1 Exchange current density, mA cm–2
20 16 192 46 0.54
30 16 212 56 0.62
40 16 204 52 0.53
50 16 193 43 0.44
60 16 186 40 0.40

To investigate the essence of the improvement of HER activity of the iridium-nickel electrocatalyst, the apparent activation energies (Ea) of the film were determined via the following Arrhenius equations (86) (Equations (viii)(x)):

(viii)

(ix)

(x)

where j0 is exchange current density (A cm–2), F is the Faraday’s constant, k is Kohlrausch coefficient (dimensionless), c is the concentration of reactant (constant), Ea is the apparent activation energy (J mol–1), T is the temperature (K), and R is the gas constant (8.314 J mol–1 K–1). The linear relationship between logj0 and 1/T for Ir88Ni12 thin film is displayed in Figure 12. According to Equations (viii)(x), the apparent activation energy of Ir88Ni12 thin film electrocatalyst is calculated as 7.1 kJ mol–1, by the slopes of lines. Compared with the nickel cathode with about 40 kJ mol–1 in standard electrolyte (87), this result indicates that the Ir88Ni12 thin films can remarkably reduce Ea for HER and accordingly result in higher electrocatalytic activity. Hence, the codeposition process of nickel and iridium species on the copper foam provides a large number of active centres for hydrogen adsorption, with the synergetic effect giving electronic structure suitable for HER.

Fig. 12.

Dependence on temperature (Arrhenius plots) of the exchange current density for the Ir88Ni12 film

Dependence on temperature (Arrhenius plots) of the exchange current density for the Ir88Ni12 film

AC impedance characterisation of HER on the Ir88Ni12 electrode in 1.0 M KOH with different temperatures is shown in Figure 13. Nyquist plots of Ir88Ni12 film as a function of overpotential are shown in Figure 13(a). Impedance spectra obtained for a given electrochemical system can be correlated to an equivalent circuit (Figure 13(b)). The temperature dependence of Rct and Cdl parameters for the HER of Ir88Ni12 film examined at the temperature range of 20–60°C is present in Table VIII. The Ir88Ni12 electrode exhibited single, ‘depressed’ semicircles (a single-step charge-transfer reaction) at all reaction temperatures, in the explored frequency range, it is noted that a high-frequency semicircle electrode porosity response, which is typically observed in alkaline media, was practically indiscernible (34). The recorded Rs parameter decreased from 1.572 Ω cm2 at 30°C to 1.038 Ω cm2 at 60°C. Simultaneously, the Rct parameter significantly reduced from 48.34 Ω cm2 to 14.75 Ω cm2 for the same temperature range (see Table VIII). The lower Faraday resistance of the Ir88Ni12 electrode surface accelerates the electron transfer during the electrocatalytic reaction. The Cdl parameter was significantly reduced from 0.02515 F cm–2 to 0.02885 F cm–2. The effect most likely results from partial blocking of electrochemically active electrode surface by fresh hydrogen bubbles (34).

Fig. 13.

(a) Nyquist plots of Ir88Ni12 film for the HER in 1M KOH at different temperatures; (b) the corresponding equivalent electric circuit models

(a) Nyquist plots of Ir88Ni12 film for the HER in 1M KOH at different temperatures; (b) the corresponding equivalent electric circuit models

Table VIII

Electrochemical Parameters for the HER on Ir88Ni12 Thin Film Electrode in Contact with 1.0 M KOH, Studied over the Temperature Range of 20-60°C

Parameters 20°C 30°C 40°C 50°C 60°C
Rs, Ω cm2 1.572 1.366 1.126 1.041 1.038
Cdl, F cm–2 0.02515 0.03417 0.02987 0.03334 0.02885
Rct, Ω cm2 48.34 44.74 24.33 20.53 14.75

Apart from the catalytic activity, stability is another important requirement of catalysts for the HER system. In this case, the long-term stability of Ir80Ni20 film electrocatalyst is assessed in 1.0 M KOH at constant current densities of 10 mA cm–2 for 10 h (see Figure 14(a)). A slight increase in the overpotential has been observed in the V-t curve. The result of the long-term hydrogen evolution tests exhibited excellent electrocatalystic stability in alkaline solution. Polarisation curves recorded after 400 cycles testing for Ir88Ni12 film indicate that there is a little decay while the overpotential exceeds 0.068 V, instead, a slight improvement of the electrocatalytic activity of the electrode at low overpotential (see Figure 14(b)). This slight increase in the catalytic activity was possibly owing to the reduction of surface oxides during the initial period of hydrogen evolution, while the observed increase in overpotential as shown in Figure 14(a) could be a result of increased mass exchange resistance due to the continuous gas bubbling (88).

Fig. 14.

(a) Chronoamperometric durability test for Ir80Ni20 film at a constant current density of 10 mA cm–2 for 10 h; (b) polarisation curves of Ir88Ni12 film initially and after 400 cycles vs. RHE at a scan rate of 5 mV s–1 in 1.0 M KOH solution

(a) Chronoamperometric durability test for Ir80Ni20 film at a constant current density of 10 mA cm–2 for 10 h; (b) polarisation curves of Ir88Ni12 film initially and after 400 cycles vs. RHE at a scan rate of 5 mV s–1 in 1.0 M KOH solution

By |2020-12-17T15:23:58+00:00December 17th, 2020|Weld Engineering Services|Comments Off on Electrodeposition of Iridium-Nickel Thin Films on Copper Foam: Effects of Loading and Solution Temperature on Hydrogen Evolution Reaction Performance of Electrocatalyst in Alkaline Water

Lattice Dynamical Study of Platinum by use of Van der Waals Three Body Force Shell Model

Johnson Matthey Technol. Rev., 2021, 65, (1), 87

Introduction

The lattice dynamical study of metallic crystals is an interesting field of research. Platinum group metals are highly valuable transition metals which have many useful properties. The electronic structure of the platinum metals is of impressive theoretical and practical importance. Dependable thermodynamic information is expected to give the crude material from which lattice dynamics, electronic conveyances and energy states can be deduced by genuine understudies of the solid state. In the present manuscript the author has used VTBFSM for theoretical calculation. The pioneering work of Kellerman (1) for ionic interactions in the alkali halides has attracted considerable attention theoretically as well as experimentally. Löwdin’s (2, 3) and Lundqvist’s (46) theory for ionic solids leads to the first important term as many body force which includes the three-body component. The Heitler-London theory and the free-electron approximations will employ the combined effects of VWI and TBI in RSM (7). The effects of VWI and TBI in the framework of ion polarisable RSM (IPRSM) are effective up to the second neighbour with short-range, VWI and TBI interaction. The experimental investigation for the phonon dispersion curve of platinum has been done with coherent inelastic neutron scattering, variation in Debye temperature and Raman spectra (810). The elastic constants and dielectric constants (11), physical and natural properties of platinum have been elucidated by expedient of theoretical models (1216), which has also successfully described their interesting properties. After the failure of the Kellerman rigid-ion model (RIM) then Karo and Hardy (17) used a deformation dipole model, Woods et al. (7) and Dick and Overhauser (18) used a RSM to report lattice properties of alkali halides. The other most prominent model was also proposed by some researchers, among them Schröder’s (19) breathing shell model, Basu and Sengupta’s (20) deformable shell model and the three-body force shell model of Verma and Singh (2123) and Singh et al. (24) for such halides. In consideration of the effect of VWI, reported by Upadhyaya et al. (25), excellent results have been procured between experiment and theory for ionic halides and semiconductors. The betterment of the present model VTBFSM over others can be realised from the fact that in the present model relatively fewer numbers of parameters have been able to interpret numerous and largely divergent physical properties of materials. This has to motivate the author to incorporate this model in the present study.

Theory

Numerical Computations

In the present paper the parameters including (C11, C12 and C44), polarisabilities (α1, α2), and lattice constant by (26) have been theoretically calculated for platinum and given in Table I. By solving Equations (i) and (v) we can obtain the phonon spectra in the first Brillouin zone divided into evenly spaced miniature cells. The theoretical results were obtained by VTBFSM. We have used the computed vibration spectra to study the specific heat and infrared (IR)/Raman spectra in the present paper. The DOS have been obtained by computing the DOS of the frequencies from the knowledge of lattice vibrational frequency spectra. The values of frequencies are compatible with theoretical and experimental peaks and Cauchy-discrepancy for lattice dynamics of platinum.

Table I

Cauchy-Discrepancy and Constant Parameters of Platinum

Input data for platinum Calculated input parameters for platinum
Properties Values for platinum Properties Values for platinum
C11 34.67 (26) C11 32.57
C12 25.07 (26) C12 23.97
C44 7.65 (26) C44 6.35
2a 3.923 (26) 2a 3.923
α1 0.037 α1 0.0487
α2 0.032 α2 0.0368

In the Brillouin zone surface the calculated phonon dispersion curves for platinum are shown in Figure 1 by using first principles along two high symmetry directions (qqq) Г-X-Г. The parallel vibrational modes show real dispersion with a maximum cleave. The upper branch consists of longitudinal modes, while the lower one is the shear‐horizontal mode, along both the Г-X-Г directions. We find that the surface modes for clean platinum (qqq) undergo a few changes in L-T modes on the clean surface, near the zone boundaries and along the X-direction, are replaced only in the dispersion curves. This is because the zone boundaries are moderate and the next two surface modes are strengthened. The experimental reported results for dispersion relation are shown in Figure 1(b) (27). On comparing with the experimental result i.e. Figure 1(a) with Figure 1(b) good agreement can be observed.

Fig. 1.

(a) Phonon dispersion relation curve for platinum by VTBFSM; (b) phonon dispersion relation to platinum along the [ɛ, 0, 0] direction (A) and [ɛ, ɛ, 0] direction (B) (27). Copyright © 2008 Società Italiana di Fisica. Reprinted by permission of Springer Nature

(a) Phonon dispersion relation curve for platinum by VTBFSM; (b) phonon dispersion relation to platinum along the [ɛ, 0, 0] direction (A) and [ɛ, ɛ, 0] direction (B) (27). Copyright © 2008 Società Italiana di Fisica. Reprinted by permission of Springer Nature

The DOS vs. frequency curve for platinum theoretically calculated in the energy range from approximately –7.0 eV to 0.5 eV in bulk is shown as a solid line in Figure 2. The bulk DOS exhibits three main peaks that are accurately produced. The small observed differences are related to the shape of the main peaks. The differences between the calculated and observed values were found and discussed in Figure 2. There are very important features obtained from the DOS vs. frequency curve. The information about the surface and resonance states was found through these differences. Below the Fermi level EF, resonance-states are expected to be obtained, mainly because these energies represent the continuum and few energy gaps exist at these energy values. The experimental reported DOS curve (28) may be compared with the present model i.e. Figure 2(a). Sharp peaks can be seen in Figure 2(a) while in Figure 2(b) the distortion in peaks can be seen which justifies the superiority of the present theoretical study.

Fig. 2.

(a) DOS vs. frequency curve of platinum with present VTBFSM; (b) DOS vs. frequency curve of platinum. Reprinted from (28), with the permission of AIP publishing

(a) DOS vs. frequency curve of platinum with present VTBFSM; (b) DOS vs. frequency curve of platinum. Reprinted from (28), with the permission of AIP publishing

The specific heat and Debye temperature ΘD have been calculated as a function of temperature T from the lattice frequency spectra as shown in Figure 3. Debye temperature ΘD is calculated from different frequency values. The specific heat value of platinum has been measured at extended temperature (0 K to 300 K). The calculated result is in reasonable agreement at moderate temperature and at very low temperature. The comparison can be seen through experimental results (27).

Fig. 3.

(a) Debye temperature curve with VTBFSM; (b) Debye temperature curve by Closs and Shukla (27) Copyright © 2008 Società Italiana di Fisica. Reprinted by permission of Springer Nature

(a) Debye temperature curve with VTBFSM; (b) Debye temperature curve by Closs and Shukla (27) Copyright © 2008 Società Italiana di Fisica. Reprinted by permission of Springer Nature

Discussion

The varying investigated properties are distinctly shown in the present study by successful use of VTBFSM, which has provided the complete lattice description of platinum. It agrees well with the test of anisotropy factor A = 2C44/(C11–C12) > unity and towards the high frequency end the higher peak is found. The determined model parameters in Table I were used to solve the secular equation for specified values of wave vectors in the first Brillouin zone, which is split up in an evenly spaced sample of (1000) wave vectors by Kellerman (1). From the symmetry, these 1000 points are reduced to 48 non-equivalent points at which the vibration frequencies have been obtained by solving the secular determinant. Debye temperature variations at different temperatures by Macfarlane et al. (26) and colossal dielectric constant (CDC) curves for platinum crystals have been computed by using VTBFSM model. By using the sampling technique the corresponding values of ΘD have been compared with available experimental data (2729) and the curve for ΘD vs. absolute temperature (T) was plotted as shown in Figure 1 for platinum. In this temperature range one should take into account the temperature dependence of the frequency spectrum, this requires, however, knowledge of the phonon frequencies at more than one temperature. The variations of ΘD with specific heats have been used to compute phonon frequencies in the first Brillouin zone and data points for different points were reported in Table II. The effect of anharmonicity is excluded so slight discrepancies between theoretical and experimental results at higher temperatures are seen, though the agreement is almost better with VTBFSM. The calculated (ΘD–T) curve for platinum has given excellent agreement with the experimental values (810). The DOS curve is given in Figure 2 and data points are shown in Table III. The two-phonon Raman spectra are sensitised to the high-frequency side while the specific heats are sensitive to its lower side which is stated the reasonableness of VTBFSM for all wavelength range.

Table II

Assignments for the Observed Peak Positions for Phonon Dispersion Relation in Г-X-Г Direction

Г-directions X-directions Г-directions
x-axis y-axis x-axis y-axis x-axis y-axis
0.05283 1.21564 0.4084 5.1927 1.50882 6.4594 2.51486 0.2413
0.09694 1.29258 0.8167 4.3248 1.54589 4.4531 2.58016 0.0742
0.14104 1.29749 1.2251 4.2535 1.54593 4.4548 2.5892 0.3527
0.16361 1.29889 1.9118 4.2383 1.61352 6.3852 2.61588 0.7981
0.1895 1.38452 1.6334 4.5661 1.64652 4.6218 2.633 0.4826
0.19903 1.39083 2.3573 4.4389 1.65054 4.3063 2.67354 1.6334
0.22918 1.39743 1.9861 4.3991 1.67279 4.6961 2.67698 0.7796
0.23438 1.49138 2.7471 6.478 1.70493 6.1439 2.70459 2.0789
0.27413 3.174 1.74195 4.065 2.73415 1.1694
0.27765 2.3944 1.75174 5.0302 2.78695 1.5406
0.30512 3.5638 1.78317 5.8283 2.84847 1.9118
0.33485 2.8028 1.82898 4.9924 2.91871 2.2645
0.34487 3.9907 1.8306 5.29 2.98776 5.5313
0.389 4.4176 1.85263 5.4756 2.99327 2.58
0.39202 3.1926 1.87869 5.4529 3.04495 5.9397
0.42283 3.4153 1.87879 5.4385 3.08086 2.8399
0.42875 4.8445 1.90724 3.5081 3.09402 2.8956
0.47724 5.2715 1.94376 4.9745 3.11517 6.2738
0.48872 3.7865 1.97845 3.8125 3.19451 2.9698
0.53007 5.6798 1.97928 3.6312
0.58951 4.1392 1.98546 3.174
0.59596 6.051 2.03477 4.3619
0.67489 6.3666 2.05494 2.8399
0.68143 4.3619 2.07071 5.29
0.75796 6.478 2.0911 2.8566
0.81252 4.4733 2.09835 2.6172
0.85822 6.348 2.14018 4.9374
0.86919 4.3991 2.14743 3.5824
0.90881 4.6961 2.14883 4.8631
0.95402 6.1253 2.16345 2.2645
0.97385 4.2877 2.19499 3.1555
0.9964 4.9559 2.20077 4.4548
1.03665 5.8283 2.22853 1.8933
1.07096 5.2715 2.24394 4.0093
1.07858 4.2506 2.25891 1.7262
1.1149 5.5313 2.28713 3.5824
1.13663 5.5154 2.32159 3.1555
1.13671 5.5128 2.32399 1.355
1.18774 4.2691 2.35607 2.7471
1.21487 5.123 2.38907 2.2744
2.39051 2.3016
2.44978 0.6125

Table III

Assignments for the Observed Peak Positions for Combined Density of States

x-axis, THz y-axis, arbitrary units x-axis, THz y-axis, arbitrary units
0.0234 3.1403 0.01226 0.23887 1.2142 0.50083
0.1286 3.2455 0.05927 0.28588 1.2586 0.44984
0.2224 3.3964 0.10831 0.32272 1.2914 0.39884
0.3276 3.51 0.15532 0.27586 1.3686 0.29481
0.4213 3.6352 0.20437 0.229 1.4015 0.24381
0.562 3.7489 0.27997 0.18418 1.4459 0.16746
0.6212 3.8852 0.32899 0.12713 1.4788 0.14386
0.692 4.1503 0.38006 0.13548 1.8082 0.00327
0.7512 4.4271 0.42908 0.14791 2.0736 0.01978
0.8219 4.6924 0.48015 0.16033 2.3276 0.03832
0.8811 4.9576 0.52917 0.17072 2.5589 0.06909
0.9518 4.9918 0.5782 0.16054 2.7902 0.09782
1.0111 5.1402 0.62926 0.11778 2.8599 0.11827
1.104 5.2884 0.65177 0.07299 2.9651 0.16528
1.1369 5.4367 0.60077 0.03023 3.0818 0.2123
1.1812 0.54978

Conclusion

The exploration of model parameters, Debye temperature and DOS are reported by use of the present model VTBFSM for platinum. The conformity with experimental data (810) of our theoretical peak is very good for platinum. A successful explanation of spectra has provided the next best test of any model for their higher range of frequency. Small deviations were observed at the higher temperature side due to harmonic approximation in the Debye curve. Better agreement has been obtained with the available experimental data (1620) and theoretical results. The motivation of this work is the availability of experimental (29) and theoretical (30, 31) work on platinum. Therefore, it may be concluded that the incorporation of VWI is requisite for the absolute interpretation of the phonon dynamical behaviour of platinum. Many researchers have also successfully reported theoretical results for alkali halides (3242) by use of the present model. Hence, the present model may be understood to provide a powerful and simple approach for a comprehensive study of the harmonic as well as anharmonic elastic properties of the crystals under consideration. The only constraint of VTBFSM is the knowledge of certain experimental parameters needed that can be used as input data.

  • 1.
  • 2.

    P. O. Löwdin, Ark. Mat. Astr. Fys., 1947, 35A, 30

  • 3.

    P. O. Löwdin, Philos. Mag. Suppl., 1956, 5, (1)

  • 4.

    S. O. Lundqvist, Ark. Fys., 1952, 6, (3), 25

  • 5.

    S. O. Lundqvist, Ark. Fys., 1955, 9, 435

  • 6.

    S. O. Lundqvist, Ark. Fys., 1957, 12, 263

  • 7.
  • 8.
  • 9.
  • 10.
  • 11.
  • 12.
  • 13.
  • 14.
  • 15.
  • 16.
  • 17.
  • 18.
  • 19.
  • 20.
  • 21.
  • 22.
  • 23.
  • 24.
  • 25.
  • 26.
  • 27.
  • 28.
  • 29.
  • 30.

    L. P. Sharma, PhD Thesis, Agra University, Agra, Uttar Pradesh, India, 1979

  • 31.
  • 32.
  • 33.
  • 34.

    U. C. Srivastava and K. S. Upadhyaya, Phys. Rev. Res. Int., 2011, 1, (1), 16

  • 35.
  • 36.
  • 37.
  • 38.
  • 39.
  • 40.

    U. C. Srivastava, J. Sci. Arts, 2017, 2, (39), 309 

  • 41.

    J. P. Dubey, P. K. Pandey and K. S. Upadhyaya, AASCIT J. Phys., 2018, 4, (1), 1

  • 42.

    U. C. Srivastava and M. P. Srivastava, J. Sci. Arts, 2019, 1, (46), 235 

  • The Author


    U. C. Srivastava obtained his MSc (Physics) and PhD (Solid State Physics) degrees from Veer Bahadur Singh Purvanchal University, Jaunpur, Uttar Pradesh, India. He obtained his MTech (Electronics & Telecommunication) degree from Karnataka State Open University, Mysore, India. He currently works as Assistant Professor-III in the Department of Physics, Amity Institute of Applied Sciences, Amity University, India. He has 17 years’ teaching and research experience. His area of research is theoretical lattice dynamical study of ionic crystals. He has published 24 research papers in different national and international journals.

    By |2020-12-15T12:15:39+00:00December 15th, 2020|Weld Engineering Services|Comments Off on Lattice Dynamical Study of Platinum by use of Van der Waals Three Body Force Shell Model

    Different Deformation Behaviour Between Zirconia and Yttria Particles in Dispersion Strengthened Platinum-20% Rhodium Alloys

    Johnson Matthey Technol. Rev., 2021, 65, (1), 112

    Platinum-20% rhodium strengthened by oxides of zirconium and yttrium were prepared by solidification of platinum-rhodium-(zirconium)-yttrium powder which had been internally oxidised. After forging, rolling and annealing, 1 mm plates were obtained. Then the plates were mechanically ground to 50–70 μm from rolling-normal direction, followed by argon ion milling until a hole appeared on the centre of the foil to obtain samples which were characterised by transmission electron microscopy (TEM), combined with thermodynamic analysis. The existence of spherical ZrO2 and Y2O3 particles was verified with platinum and rhodium present as pure metals at the same time. It was found that the deformation behaviour of ZrO2 and Y2O3 particles was quite different during processing, where the former basically maintain their spherical shape and were bonded tightly to matrix, while the latter were compressed along normal direction and form two cracks on both sides of Y2O3 particles along the rolling direction. The differences in hardness and interface bonding properties of these two types of particles are supposed to be the main causes of different deformation behaviour during hot forging and cold rolling.

    1. Introduction

    Platinum and its alloys are very important in industries such as the chemical and glass industries. Some of their main applications are as follows: a functional structural material in the aerospace industry; a catalyst in the nitric acid preparation industry; nozzles for preparing glass fibres; preparing crucibles and utensils that require special properties for use in chemical laboratories. Platinum-rhodium alloys with low rhodium content can also be used as brazing filler metals in metal welding. Although expensive, their high temperature stability and chemical inertia cannot be replaced by other materials (1, 2).

    However, the strength and creep resistance of pure platinum would significantly reduce at high temperature because of sharp grain growth. Therefore, it is crucial to find a way to improve the high temperature creep resistance of platinum alloys (3). Many methods of strengthening platinum materials are known. Among these different methods, the best methods are solid solution strengthening and dispersion strengthening. The addition of rhodium has been found to have the best solid solution strengthening effect in high temperature use of platinum. With increasing rhodium content in platinum-rhodium alloys, the normal temperature strength, high temperature endurance strength, creep rupture life and creep activation energy of the alloy increases greatly, so platinum-rhodium alloys are widely used (4, 5). But the high-temperature mechanical properties of platinum-rhodium alloys fail to satisfy the requirement of industrial production with worsening service conditions. Therefore, dispersion-strengthened platinum-rhodium alloys were subsequently developed in Johnson Matthey, UK (6, 7), Engelhard Corporation, USA (8) and Heraeus, Germany (9) from the 1980s to 1990s. They were prepared by adding zirconium, yttrium or scandium oxide particles into the platinum-rhodium alloy under certain process conditions. At present, dispersion-strengthened platinum alloys such as zirconia grain stabilised (ZGS) platinum and oxide dispersion strengthened (ODS) platinum (10, 11), in which Y2O3 and ZrO2 are two commonly used reinforcement particles, are used in industrial applications. According to the experimental results of Hu et al. (12), as the zirconium concentration increases, the platinum-rhodium alloy’s yield stress (0.2% offset) increases significantly, while the elongation decreases slightly. The work hardening rate of particle-reinforced samples increases with the increase of the volume concentration of dispersed particles, which is a typical behaviour of particle dispersion enhancement. In addition, based on a reformulation of the Orowan stress for particle strengthening and by superposing this stress to the matrix stress, a calculated flow stress is in good accord with the experimental value. Though the strength of these particle strengthened platinum alloys can be significantly improved, the further enhancement of the strength is difficult due to the lack of mechanism research and empirical development in the past (12, 13).

    Zirconium and yttrium have good plasticity and corrosion resistance. Diffusion strengthening improves the metal strength through adding a second phase or multiple phases and the essence is the interaction of the second phase and the dislocation (13). Nevertheless, the two reinforcement particles, i.e. Y2O3 and ZrO2, are usually thought be to the same as strengthening particles based on Orowan’s equation where the strength increment from the non-deformable dispersed particles is positively correlated with the particle spacing (14, 15). When making samples, we tried to add the yttrium content to 0.1%, and found that the ingot will crack during rolling, so we speculate that different deformation behaviours will have a huge impact on alloy strengthening.

    In this study, two kinds of platinum alloys strengthened by Y2O3 and ZrO2, respectively, were prepared and characterised by TEM. A number of differences in deformation behaviour of the two particles during processing were found. These findings are expected to lead to new insights into developing dispersion strengthened high strength platinum alloys.

    2. Experiment

    Nominal composition of the investigated alloys is listed in Table I. The preparation processes have been described in previous research (13) and can be briefly summarised as follows: Pt-20 wt% Rh-0.015 wt% Y without and with 0.1 wt% Zr were smelted in a vacuum induction furnace at 1800–2000°C under argon atmosphere, then cast into a water-cooled copper mould to obtain ingots. The ingots were hot forged to 10 mm plates which were sheared into pieces, followed by mechanical milling to fine powder. The size distribution of the powder was measured using an LS-POP(6) laser particle size analyser (OMEC, China). 97% of the particles were distributed between 5 μm and 60 μm with an average particle size of 25 μm. The powder was sintered and exposed in air to internally oxidise at 1150°C for 4 h. The 30 mm sheets were obtained by hot forging at 1400°C, then rolled to 1 mm sheets at room temperature followed by annealing at 1150°C for 30 min. To prepare the TEM samples, the sheets from rolling-normal direction were mechanically ground to 50–70 μm, followed by argon ion milling at 5 kV until a hole appeared on the centre of the foil. TEM was used to examine the microstructure at 200 kV (JEM-2100 electron microscope (JEOL Ltd, Japan)) and at 300 kV (JEM-3000F field emission electron microscope (JEOL Ltd)). JEM-2100 was used to detect topography of the particles and energy-dispersive X-ray spectroscopy (EDS) was conducted to determine the components; JEM-3000F was used for high-resolution transmission electron microscopy (HR-TEM) observation to determine the structure of the particles. In this paper, Pt-20Rh-0.015Y is referred to as Alloy 1 while Pt-20Rh-0.015Y-0.1Zr is referred to as Alloy 2.

    Table I

    Nominal Compositions of the Investigated Platinum Alloys

    Alloys Zirconium, wt% Yttrium, wt% Others, wt% Rhodium, wt% Platinum, wt%
    1 0.015 ≤0.01 20 Bal.
    2 0.10 0.015 ≤0.01 20 Bal.

    3. Results and Analysis

    3.1 Thermomechanical Analysis

    During preparation processes, especially at high temperature under oxidising atmosphere, the metals in the alloys may be oxidised and the possible oxides are PtO2, Rh2O3, ZrO2 and Y2O3. Their reaction equations are as follows (Equations (i)(vi):

    (i)

    (ii)

    (iii)

    (iv)

    (v)

    (vi)

    According to the Gibbs free energy theorem, a reaction can only occur when the Gibbs free energy is negative and the more negative the Gibbs free energy of a reaction, the more easily the reaction occurs. When the Gibbs free energy is greater than zero, the reaction cannot happen. Figure 1 is the oxidation tendency of platinum, rhodium, zirconium and yttrium, which indicates:

    • ΔG of all the reactions increases as temperature increases

    • Within the temperature range we calculated, ΔG of Y2O3·ZrO2, Y2O3 and ZrO2 are much smaller than those of Rh2O3, Rh2O and RhO, which means the formation of Y2O3·ZrO2, Y2O3 and ZrO2 are much easier during processing

    • ΔG of RhO, Rh2O and Rh2O3 are very close to ΔG = 0 and even greater than 0 at the internal oxidation temperature (1423 K), thus the formation of RhO, Rh2O and Rh2O3 are difficult and can be ignored.

    Fig. 1.

    The oxidation tendency of platinum, rhodium, zirconium and yttrium

    The oxidation tendency of platinum, rhodium, zirconium and yttrium

    For platinum, when the temperature rises from room temperature, platinum will react with oxygen and form a PtO2 film on the metal surface. The thickness of PtO2 would grow with the rise of temperature. When the temperature reaches about 500°C, this process would stop. If the temperature continues to rise, the PtO2 film will be gradually vaporised. Meanwhile, the higher the temperature, the faster the gasification rate. Samples in this experiment were about 1200°C, the PtO2 film formed by oxidation had been basically vaporised. Therefore, PtO2 is not present in the samples.

    Overall, according to the thermomechanical analysis, Y2O3, ZrO2 and Y2O3·ZrO2 are easily formed in the platinum-rhodium-(zirconium)-yttrium alloys. Platinum and rhodium are present as almost pure metals.

    3.2 Microstructure and Energy-Dispersive X-ray Spectroscopy Analysis of Platinum-Rhodium-(Zirconium)-Yttrium

    Figure 2 is the bright field TEM images of Alloy 1 showing the morphology of particles. It shows that some of the particles still maintained spherical shape and each particle was accompanied by two cracks on two sides along the rolling direction, as shown by particle B. One enlarged image of this kind of particle is shown in Figure 2(b). Some particles had been compressed along the normal direction with two cracks along the rolling direction, such as particle A. A small number of fine particles were severely compressed so that the cracks have closed (particles C). Table II shows the EDS analysis results of the particle in Figure 2(b), which indicates that the particle is mainly composed of yttrium and oxygen atoms. A small amount of iron impurity may have come from the TEM equipment.

    Fig. 2.

    Bright-field TEM images in Alloy 1. (a) The overall morphology and distribution of particles; (b) an enlarged particle

    Bright-field TEM images in Alloy 1. (a) The overall morphology and distribution of particles; (b) an enlarged particle

    Table II

    Element Mass, % Atom, %
    Oxygen 7.5 33.7
    Iron 2.9 3.7
    Yttrium 68.3 54.8
    Platinum 21.3 7.8

    Figure 3 is the bright field TEM images of Alloy 2 showing the morphology of the particles. Figure 3(a) shows that the particles (as indicated by red circles) are spherical and uniformly distributed in matrix with a diameter range from 20 nm to 70 nm. Note that the particles show a good bonding with matrix after hot forging and cold rolling during processing. An enlarged image of a particle is shown in Figure 3(b) and its EDS analysis results have been listed in Table III, illustrating that the particle is composed of zirconium and oxygen atoms.

    Fig. 3.

    Bright-field TEM images in Alloy 2. (a) The overall morphology and distribution of particles; (b) an enlarged particle

    Bright-field TEM images in Alloy 2. (a) The overall morphology and distribution of particles; (b) an enlarged particle

    Table III

    Element Mass, % Atom, %
    Oxygen 16.6 53.2
    Zirconium 83.4 46.8

    The particles are so small that it is difficult to characterise them using normal selected area diffraction techniques. Thus, HR-TEM was used to investigate the structure of the particles. Binary monolithic ZrO2 is known to exhibit polymorphic transformations between monoclinic (mP12:P 121/c1, ZrO2-b type), tetragonal (tP6:P42/nmc, ZrO2-type) and cubic (cF12:Fm3m, CaF2-type) (16). The monoclinic phase is stable below 1478 K, while the tetragonal phase is stable between 1478 K and 2650 K. The cubic phase is stable from 1796 K to 2993 K, and exhibits some range of homogeneity. The fast Fourier transform (FFT) diagrams of ZrO2 from different zone axes is shown in Figure 4, and when it is compared with the common ZrO2 structure (17, 18), we find that two crystal structures of ZrO2 were monoclinic and tetragonal. The FFT diagrams of Y2O3 from different zone axes is shown in Figure 4. When it is compared with the common Y2O3 structure (19), we find that the structure of Y2O3 is body-centred cubic.

    Fig. 4.

    TEM and HR-TEM images of ZrO2 particles. (a) Bright-field image; (b) HR-TEM image; (c) FFT diagram of a monoclinic particle with the electron beam approximately parallel to [111] direction; (d) bright-field image; (e) HR-TEM image of the area indicated in (d); (f) FFT diagram of a tetragonal particle with the electron beam approximately parallel to [101]

    TEM and HR-TEM images of ZrO2 particles. (a) Bright-field image; (b) HR-TEM image; (c) FFT diagram of a monoclinic particle with the electron beam approximately parallel to [111] direction; (d) bright-field image; (e) HR-TEM image of the area indicated in (d); (f) FFT diagram of a tetragonal particle with the electron beam approximately parallel to [101]

    Fig. 5.

    TEM and HR-TEM images of Y2O3 particles. (a) Bright-field image; (b) HR-TEM image of the area indicated in (a); (c) FFT diagram of a body-centred cubic particle with the electron beam approximately parallel to [111] direction

    TEM and HR-TEM images of Y2O3 particles. (a) Bright-field image; (b) HR-TEM image of the area indicated in (a); (c) FFT diagram of a body-centred cubic particle with the electron beam approximately parallel to [111] direction

    The volume fractions of particles (ZrO2 and Y2O3) are difficult to measure by X-ray diffraction (XRD) due to low content of the particles or by TEM due to the large atomic mass of platinum and rhodium. It is therefore difficult to measure the thickness of the TEM foil. Thus, we approximately calculated the volume fraction of ZrO2 and Y2O3 as 0.42% and 0.0587%, respectively, based on the weight fraction of zirconium and yttrium. Note also that a small amount of zirconium and yttrium may be present as solute atoms in the matrix ascribed to the extremely low solubility of oxygen atoms in the platinum-rhodium alloy. An oxidation rate of 75% was proved to be reasonable, based on the experimental and calculated yield stress of the alloys (20, 21).

    3.3 Analysis of Deformation Behaviour Between Zirconia and Yttria Particles

    Based on our TEM observations, these two particles have totally different deformation behaviours. Almost all Y2O3 particles have compression deformation along the normal direction with two cracks on the two sides of particles along the rolling direction, while ZrO2 particles basically maintain their spherical shape and are bonded tightly with matrix. The nanoparticle deformation behaviour in particle strengthened metals has been widely researched (2226). By studying the deformation behaviour of dispersion-strengthened particles in steel, Gove et al. (22, 23) claimed that the formation of voids around the particles and the matrix is due to the fact that the steel matrix cannot flow around the particles while maintaining contact with them. The strength of the inclusion-substrate interface is insufficient to withstand the longitudinal tensile stress caused by the deformation of the surrounding steel, so the interface is separated and voids are generated. As the cavity expands in the rolling direction, the vertical compressive stress is no longer balanced, and the combination of vertical and longitudinal stress causes the steel to partially move into the cavity, creating a tapered cavity. Waudby et al. (24) claimed that the combined force of the stress of the steel matrix flowing with the tangential action of the surface of the particle caused and widened the crack and created a void. Luo et al. (25) proposed that if the resolved normal stress at the interface reaches a critical value, peeling occurs and voids are generated by finite element calculation. Belcheko et al. (26) proposed that the flow of the substrate above and below the undeformed inclusions in the rolling direction results in the formation of conical voids. Zhang et al. (27) argued that although there are subtle differences in the mechanism of void formation proposed by different researchers, it is generally believed that the formation of voids is due to the discontinuity of the interface between the particles and the matrix. Therefore, the interfacial strength between particles and the matrix is the main cause of forming of the adjacent interface voids. It is suggested that the interfacial strength between Y2O3 particles and the platinum matrix is not sufficient to withstand the tensile stresses during processing. A crack will form between the particles and the matrix. As the strain continuously increases, the matrix work hardens, and when the hardness of platinum reaches a critical value, the Y2O3 particles will be deformed. In addition, the agglomeration of the reinforcing phase particles causes an increase in the local volume fraction, which increases the internal stress and causes the destruction of the particles. The coarsening of the particles reduces the stress required for particle damage, and the rate of damage of the particles increases with size. As for ZrO2 particles, no voids are observed because the interfacial strength between ZrO2 particles and the platinum matrix is able to withstand the rolling tensile stresses during processing. ZrO2 is also hard enough to stand the stress form matrix so it will keep its spherical shape.

    4. Conclusions

    In platinum-rhodium-(zirconium)-yttrium alloys, yttrium and zirconium are easily oxidised into Y2O3, ZrO2 and Y2O3·ZrO2 and form corresponding oxides while platinum and rhodium are basically present as pure metals. ZrO2 and Y2O3 particles have been observed in platinum-rhodium-zirconium-yttrium and platinum-rhodium-yttrium, respectively, and verified by EDS analysis and HR-TEM observations. The deformation behaviour of these two oxides is quite different during processing, though they have the same deformation history. The ZrO2 particles maintained their spherical shape without any visible deformation, while the Y2O3 particles were compressed along the normal direction with two cracks forming on two sides of the particles. Insufficient hardness of Y2O3 and relatively lower interface strength between Y2O3 particles and matrix were supposed to be responsible for deformation of Y2O3 during processing.

    Acknowledgements

    This work was supported by Chongqing Science and Technology Support Project (No. cstc2017zdcy-zdyfX0070, cstc2018jszx-cyzdX0138) and Fundamental Research Funds for the Central Universities (No. 2019CDCGCL316) and National Undergraduates Training Program for Innovation (No. 201810611054).

    The Authors


    Ziyang Wang received his Bachelor’s degree in 2020 from Chongqing University, China. He entered Chongqing University, majored in Material Forming and Control Engineering in 2016. His interests include light alloys and composite materials.


    Xi Wang received his Bachelor’s degree in 2020 from Chongqing University, China, and he continued to study at Chongqing University for a Master’s degree in the automobile college. Forging and new energy vehicles are his research field.


    Futao Liu received his Bachelor’s degree in 2020 from Chongqing University, China. He entered in Chongqing University, majored in Material Forming and Control Engineering in 2016. His dissertation is about the heat treatment of magnesium-lithium alloys.


    Faping Hu is a PhD candidate from 2017 in Materials Science and Engineering at Chongqing University. He visited the Technical University of Denmark as a guest PhD for two years. His research is the microstructural characterisation of magnesium alloys during plastic deformation.


    Hao Chen is a PhD candidate from 2020 in Materials Science and Engineering at Chongqing University. He studied platinum-rhodium alloys and glass fibre reinforced composites. His current research is on freeze casting.


    Guobin Wei received his PhD in Materials Science and Engineering in 2015 from Chongqing University, China. He is vice professor of the School of Materials Science and Engineering. His interests include magnesium-lithium alloys and the simulation of material forming processes.


    Weiting Liu is a senior engineer and Vice President of Chongqing International Composite Materials Co Ltd, China, supporting and promoting research and manufacture of platinum-rhodium alloy bushings and glass fibre. His professional affiliation includes Deputy Executive Director of the Functional Materials Association and he obtained a Bachelor’s degree in 1993 from the Department of Mechanical Engineering of Chongqing University, China.


    Weidong Xie received his PhD in Materials Science and Engineering in 2008 from Chongqing University, China. He is Vice Dean of the Institute of Scientific Research and Development of Chongqing University and a council member of the Chinese Society for Composite Materials. His interests include light alloys, composite materials, nanomaterials and foundry.

    By |2020-12-15T10:54:15+00:00December 15th, 2020|Weld Engineering Services|Comments Off on Different Deformation Behaviour Between Zirconia and Yttria Particles in Dispersion Strengthened Platinum-20% Rhodium Alloys

    Guest Editorial: Platinum Group Metals for a Greener Future

    Johnson Matthey Technol. Rev., 2021, 65, (1), 2

    Clustered together in the centre of the Periodic Table lie six remarkable elements, six metals without which the world would be a completely different place. Think about the food you eat, your computer, your car, your mobile phone or even the clothes you wear. At some stage during their production one or more of these six rare metals has been utilised, whether as a catalyst or perhaps in the end product itself. The platinum group metals (pgms) play an essential role in our modern lifestyles.

    Platinum, palladium, rhodium, ruthenium, iridium and osmium are rare, expensive and have a unique combination of incredibly useful properties. For example, high thermal stability, corrosion and oxidation resistance and the ability to catalyse a broad range of chemical reactions make them indispensable in processes such as petroleum refining, nitric acid, bulk chemical production and glass manufacture. They are also to be found in a diverse range of products such as the hard disk drives in computers and data storage centres, the airbag in your car or the jet engine that carries you to your holiday destination. Apart from their chemical properties the pgms and platinum and palladium in particular have found favour in both the jewellery and investment markets. Platinum has for many years been marketed as a premium jewellery metal, rarer and more precious even than gold.

    Science and Industrial Applications

    But it is not for the pgms’ aesthetic or investment value that this collection of papers has been collated, rather to highlight the fascinating science of these incredible metals and their wide range of industrial uses. This special edition of the Johnson Matthey Technology Review will examine both the fundamental properties of these metals and their use in a variety of applications and fields.

    The pgms are rare elements, occurring in economic quantities in only a few geographical locations. Demand is generally price inelastic, meaning that consumption volumes are often relatively insensitive to underlying metal prices (1). Importantly, the pgms are widely recovered and recycled; for example, through the recovery of catalytic convertors from end of life vehicles or through a closed-loop system where the catalyst that is installed in a chemical plant is recovered, sent for refining and ultimately reused. Sustainability not only of the metals themselves but also with regard to their end uses is why the pgms are so important, as described in two of the articles – European projects BIORECOVER and PLATIRUS.

    The use of platinum, palladium and rhodium is dominated by the automotive sector where for several decades they have been a vital component in emission control catalysts. These three metals have been fundamental in removing carbon monoxide, hydrocarbons and nitrogen oxides from gasoline and diesel engine exhausts to dramatically improve air quality across the world, as detailed in several publications by one of our authors, Martyn Twigg, who in his long career was at the forefront of autocatalyst development (24).

    In this special edition, Twigg and Emeritus Reader John Burgess from the University of Leicester, UK, have written a two-part commemoration of the late Professor Bob Gillard, discussing his remarkable life, work and contribution to the understanding of transition metal chemistry, particularly the chemistry of rhodium and other platinum group metal complexes.

    The use of pgms by the chemical industry is of vital importance to a huge range of bulk and speciality products. One example of this is the oxidation of ammonia to produce nitric acid which has used platinum and rhodium in catalyst gauze for over 100 years (5). The latest work in this field will be discussed by Ashcroft in this special edition. Interestingly, the use of pgm for chemical catalysts has remained one of the more robust areas of demand during the coronavirus disease (COVID-19) pandemic. Nitric acid is used to manufacture both fertilisers for global crop production and explosives for the mining industry, which are essential for the supply of metals such as nickel and platinum and will be central to the future electrification of the automotive fleet.

    The minor pgms ruthenium, iridium and osmium can often appear somewhat neglected despite their use in a huge number of applications. Iridium is prized for its high melting point which makes it ideal for use in crucibles to produce high purity metal oxide single crystals, used in medical scanners, light-emitting diode production and surface acoustic wave filters, amongst others. The behaviour and properties of iridium are the subject of two papers in this edition. Osmium is perhaps the least known of the metals given its more limited applications. However, Arblaster has remedied that with a paper discussing the thermodynamic properties of the densest element in the Periodic Table.

    The Most Useful Elements

    The pgms are among the most invaluable elements discovered. To sum up all their useful properties in one key attribute is that they enable the world to be a more sustainable place. Globally we are starting to undergo a monumental change in energy use and production, away from reliance on fossil fuels towards a cleaner, greener, more sustainable model (6). The move to hydrogen as an energy source is vital in the move to a net zero economy, a key example of which is the fuel cell vehicle. Johnson Matthey actually provided the platinum to William Grove when he demonstrated the first fuel cell in 1839 (7). Aside from the use of pgm in the catalyst of the vehicle itself, the production of hydrogen of suitable purity makes use of one of the key properties of palladium. Palladium has an intrinsic selectivity for hydrogen, which makes it an ideal choice for purification membrane technology. In this issue, Faizal et al. discuss the use of palladium in this vital application for the growing hydrogen economy.

    The pgms: six of the rarest elements in the Periodic Table that have and continue to change the world around us. Metals that are driving forward sustainable technology and the move towards net zero, metals that will help drive the clean energy revolution, provide food to billions and facilitate communication and data sharing and storage across the globe to enable a more connected society.

    By |2020-12-15T10:04:47+00:00December 15th, 2020|Weld Engineering Services|Comments Off on Guest Editorial: Platinum Group Metals for a Greener Future

    Comprehensive Review on High Hydrogen Permselectivity of Palladium Based Membranes: Part I

    Johnson Matthey Technol. Rev., 2021, 65, (1), 64

    1. Introduction and Background

    Hydrogen purification by palladium-based membrane is one of the most well-known techniques for supplying high purity hydrogen to low temperature operated (1) PEFC in various electronic devices such as tablets, laptop computers and small vehicles. The compact methanol steam reformer that consists of a catalytic burner, reformer and hydrogen purification device in a single package was developed almost two decades ago (2). Over the years, various integrated systems, operating conditions and geometries have been investigated to obtain the optimum operating conditions for reliable performance (39). As a result, the compact reformer has several advantages (i.e. simple and compact) compared to complex systems with separated units (10).

    Due to the difficulty and high risk of exposure to accidents, the transportation and storage of gaseous hydrogen are undesirable. Alternatively, the utilisation of alcohols is more practical due to their existence in a liquid form at ambient conditions. Methanol for instance has a relatively high hydrogen:carbon ratio and moderate reaction temperature compared to other alcohols (10, 11). Based on the two step equations of methanol steam reforming, the reaction between vaporised methanol and steam produces hydrogen and carbon dioxide along with carbon monoxide. However, the concentration of carbon monoxide in the electrode of PEFC must be equal to or less than 10 ppm (12). Otherwise, the carbon monoxide could deteriorate the electrode performance by reducing the active surface area for reaction and lowering the partial pressure of hydrogen (1315).

    Hydrogen purification by palladium based membrane is preferable rather than selective carbon monoxide methanation and selective carbon monoxide oxidation (16), in which very high purity of hydrogen and very high permeation flux can be obtained (1719). PSA is an alternative technique to produce very high purity hydrogen (20). However, the high costs of installing PSA is not economical for small size (or small capacity) applications (21). In addition to the well-known inhibitive carbon monoxide produced from the aforementioned methanol steam reforming, carbon dioxide and excessive methanol from the same reaction (22), hydrogen sulfide (23, 24) and trace amounts of ammonia (20, 25) from coal gasification process, dehydrogenated methanol and ethanol (26) also affect adversely the performance of palladium membranes through its inhibitive mechanism.

    Alloying palladium with other metals such as silver and copper is necessary during membrane fabrication to prevent embrittlement when the membrane is used under hydrogen atmosphere and below 573 K and 2 MPa (10). It was found that the maximum amount of permeated hydrogen is obtained when the silver content is 23% (27). In addition, the palladium/silver membrane shows better performance compared to the palladium/copper membrane from the viewpoint of hydrogen permeability. Consequently, there is growing interest in the palladium/silver membrane. In addition to these two types of alloys, the palladium-yttrium membrane has also been previously examined due to its superior hydrogen permeability. However, this type of membrane is not commercialised due to the expensive processes required to convert the palladium-yttrium alloy into the functional separation membrane (28).

    Hydrogen permeation through palladium based membranes is based on the solution-diffusion mechanism (29). When a membrane with sufficient thickness is operated at sufficiently high temperature, the diffusion of hydrogen atoms through the metallic lattice becomes dominant, thus permeation flux can be estimated accurately by using Sieverts’ Law (30, 31) that is quantified in Fick’s First Law as follows, Equation (i):

    (i)

    where f is the hydrogen permeation mole flux, q is the hydrogen permeance coefficient, d is the membrane thickness, PH2,1 is the hydrogen partial pressure at membrane surface of upstream (or retentate) side and PH2,2 is the hydrogen partial pressure at membrane surface of downstream (or permeate) side. The Sieverts’ equation as shown by Equation (i) states that hydrogen permeation is governed by the difference in the square root of the hydrogen partial pressure between the upstream and downstream side.

    Membrane temperature (22, 32) and membrane thickness (3335) are among the important parameters that determine compliance with Sieverts’ Law. When the temperature of the membrane is sufficiently high, the adsorption and dissociation of hydrogen atoms at the membrane surface are very fast. Therefore, the diffusion of hydrogen atoms through the metallic lattice becomes a controlling step for permeation. In this case, the hydrogen permeation flux is found to be linear with respect to the difference in the square root of hydrogen partial pressures between the upstream and downstream side. For the case of the palladium/copper membrane, Ma found that Sieverts’ Law is valid only when the membrane temperature is set above 573 K (32), whereas for the palladium/silver membrane, the law can be applied even if the temperature is lower than 500 K (22).

    The different findings by several groups of researchers had proven that there is no exact value of thickness that can be set as a limit for compliance with Sieverts’ Law. Ward and Dao (33) and Federico et al. (34) found that the membrane thickness should be higher than 10 μm in order to apply the Sieverts’ equation (Equation (i)). Other research groups discovered that the Sieverts’ Law is still valid even though the membrane thickness is below 10 μm (22, 35). These contrary findings are supposed to be caused by difficulty in quantifying various uncontrolled factors such as surface processes (36), surface poisoning (37) and grain boundaries (38).

    For the case of pure hydrogen, hydrogen permeation is found to follow the correlation of Sieverts’ equation regardless of feed flow rate. However, for mixtures, when the feed flow rate of hydrogen becomes sufficiently high, the hydrogen permeation ratio (fraction of fed hydrogen that permeates membrane) (39) becomes low. Therefore, the hydrogen permeation flux can be predicted accurately by Sieverts’ equation (Equation (i)). Further, the term PH2,1 in Equation (i) can be predicted from the bulk value of hydrogen mole fraction at the upstream side, which indicates that hydrogen partial pressures at the membrane surface and the bulk flow are uniform, as illustrated by Line 1 in Figure 1.

    Fig. 1.

    Schematic diagram of hydrogen partial pressure profile

    Schematic diagram of hydrogen partial pressure profile

    When a mixture of hydrogen with relatively low feed flow rate (or high permeation ratio) is used, the direct substitution of inlet hydrogen partial pressure (PH2,in) value into the Sieverts’ equation causes an overestimation of PH2,1 from the actual permeation flux. This indicates there is a nonuniformity of hydrogen mole fraction in the boundary layer near to membrane surface, as illustrated by Line 2 in Figure 1. In this case, several research groups (3941) mentioned that the hydrogen permeation flux could start to affect the hydrogen concentration at the membrane surface, thus could trigger the phenomenon of concentration polarisation.

    The concentration polarisation phenomenon causes the accumulation of the less permeable species and the depletion of the more permeable species in the boundary layer adjacent to the membrane, thus generating a concentration gradient in the boundary layer (42). Therefore, in such situation, an additional elementary step is essential for the solution-diffusion mechanism of the membrane. This involves the transportation of molecular hydrogen from (to) the bulk gas phase to (from) the gas layer adjacent to the surface at the upstream (downstream) side (33). As a consequence, if the inlet hydrogen partial pressure is directly substituted into the Sieverts’ equation (Equation (i)), the hydrogen partial pressure at the membrane surface of upstream side is overestimated, which causes a significant deviation from the actual permeation flux. Chen et al. observed that such deviation implies the level of concentration polarisation for a palladium based membrane (41). Based on the analytical study for multicomponent hydrogen mixtures, Caravella et al. confirmed that such deviation is caused by the effect of multicomponent external mass transfer (such as concentration polarisation) in addition to non-ideal diffusion through the membrane (43).

    Technological advances in membrane materials, modification and fabrication (42) since the end of the 20th century have stimulated the fabrication of very thin membranes in order to substantially improve the permeation performance. Therefore, the phenomenon of concentration polarisation could not be avoided due to the use of membranes with minimal thickness. However, some researchers (44) have recommended installation of baffles in the membrane reactor to decrease the polarisation effect. For palladium based membranes, concentration polarisation has been extensively investigated in the past decade (40) although concentration polarisation had been investigated in the 1990s for separation of a gas-vapour mixture (45). Therefore, significant research interest in the theoretical understanding of the phenomenon has resulted in numerous methods for estimating hydrogen flux for such conditions.

    Therefore, a comprehensive review of the transport phenomena for palladium based membranes is performed, particularly on concentration polarisation. In addition to the background of the scenario related to palladium based membranes already highlighted, current information on various parametric studies and theoretical approaches for predicting hydrogen permeation flux under the influence of concentration polarisation are covered. Therefore, this review presents critical scientific knowledge and current research on concentration polarisation. The coverage of the present review is significantly different from the published works of Adhikari and Fernando (46), Rei (47), Gallucci et al. (21), Al-Mufachi et al. (28), Li et al. (48), Conde et al. (49) and Peters and Caravella (50). Adhikari and Fernando comprehensively reviewed the classification of hydrogen purification membranes, along with the advantages and disadvantages of each type of membrane (46). The study emphasised the superior quality of palladium based membranes in producing ultra-high purity hydrogen due to very high selectivity (46). Similarly, Rei (47) reviewed the advances in permeation through palladium based membranes for the case of a hydrogen mixture based on case studies in Taiwan. Several discoveries on new phenomena of hydrogen permeation such as perturbation of hydrogen permeation due to palladium lattice expansion and hydrogen spillover in the membrane reactor have been described (47). Gallucci et al. also highlighted the problem of concentration polarisation in the membrane reactor, although this was not the main topic of the study (21). The authors mainly focused on the route of commercialisation and application of various types of membranes (21). The review of several palladium alloy membranes was presented by Al-Mufachi et al. (28). The paper highlighted the advantages and disadvantages of each type of membrane in terms of hydrogen permeability, tensile strength and fabrication costs (28). Subsequently, Li et al. reviewed the thermal and chemical stability of palladium based membranes which are considered the two most critical issues for the commercialisation of the membranes (48). In 2017, a review on palladium based membranes was performed by Conde et al. (49). The paper presented a review of the alloying elements for palladium based membranes and their effect on the membrane properties. Finally, a most recent overview by Peters and Caravella (50) has covered the scopes of manufacturing process of palladium membranes, membrane materials, membrane modules and reactor design, as well as applications of palladium based membranes.

    Based on these published review articles, it can be said that the subject of transport phenomena, particularly on the concentration polarisation, is the novelty for the present review. This paper presents coverage of recent research features and technological advances on the transport phenomena of palladium based membranes. It also presents the various prediction methods applicable to hydrogen permeation under the influence of concentration polarisation that could serve as a future reference for researchers and industrial practitioners.

    2. Factors Affecting Concentration Polarisation in Palladium Based Membranes

    In this section, a review of case studies on concentration polarisation is presented. The various studies and types of membrane used for each study are presented in Table I, whereas the parameters considered for studying such phenomena are listed in Table II. Based on Table I, it is evident that most common membranes are tubular, as illustrated by the various configurations in Figures 2(a)–2(c). The studies by Faizal et al. (55, 60) examined the phenomenon of concentration polarisation for flat sheet type membranes, which are widely used in compact reformers for hydrogen production (45, 6566). The common configuration for a flat sheet type membrane is illustrated by Figure 2(d). It is interesting to note that various configurations and fluid flow conditions have been considered for studying concentration polarisation. Based on Table II, it is evident that the most common varied parameters for concentration polarisation are operating pressure, hydrogen mixture composition, feed flow rate and Reynolds number as well as membrane temperature. However, several studies have focused on geometry improvement to suppress concentration polarisation, as elaborated in this section.

    Table I

    Types of Study and Membranes Used for Investigation on Concentration Polarisation Phenomena

    No. References Type of study for concentration polarisation Membrane
    Type Thicknessa, μm
    1. Zhang et al. (51) Experiment and modelling Porous ceramic tube supported palladium membrane
    2. Pizzi et al. (52) Experiment and analytical Palladium/20 wt% silver tubular membranes deposited on ceramic supports 2.5
    3. Catalano et al. (40) Experiment and analytical Palladium/20 wt% silver tubular membrane with ceramic support 2.5
    4. Caravella et al. (53) Modelling and analytical Tubular type self-supported palladium based membrane 1–150
    5. Coroneo et al. (44) Simulation and experiment Tubular palladium/silver membrane deposited on tube 3
    6. Caravella et al. (54) Modelling and analytical Self-supported tubular palladium based membrane 60
    7. Chen et al. (39) Numerical simulation Self-supported tubular type palladium based membrane
    8. Chen et al. (41) Numerical simulation Self-supported tubular type palladium based membrane
    9. Faizal et al. (55) Experiment and analytical Self-supported circular flat sheet type palladium/23 wt% silver membrane 25
    10. Chen et al. (56) Numerical simulation Self-supported tubular palladium membrane
    11. Chen et al. (57) Experiment Palladium and palladium/copper membrane with porous stainless steel support 6.5–7.0
    12. Chen et al. (58) Numerical simulation Self-supported tubular palladium membrane
    13. Nekhamkina and Sheintuch (59) Analytical Self-supported tubular palladium membrane
    14. Zhao et al. (23) Experiment Palladium/copper tubular membrane with ceramic substrate 5
    15. Faizal et al. (60) Experiment and analytical Self-supported circular flat sheet type palladium/23 wt% silver membrane 25
    16. Nakajima et al. (61) Experiment and numerical Tubular palladium/silver membrane with ceramic support
    17 Caravella and Sun (62) Analytical and simulation (for case study of water-gasshift reaction) Self-supported tubular palladium based membrane
    18. Kian et al. (63) Experiment Palladium layer deposited on yttria stabilised zirconia (YSZ) support (tubular) 11
    Palladium/gold layer deposited on YSZ deposited on Al2O3 substrate (tubular) 8
    19. Helmi et al. (64) Simulation and experiment Pd0.85Ag0.15 based tubular membrane supported on Al2O3 porous in fluidised membrane reactor 4.5

    Table II

    Varied Parameters for Studying the Effect on Concentration Polarisation

    Reference Parameters
    Zhang et al. (51) Feed flow rate: 0–5.1 × 10−5 m3 s−1. Pressure: 101.3–405.3 kPa (difference in total pressure). Temperature: 623–773 K
    Pizzi et al. (52) Pressure: 20–600 kPa (difference in total pressure). Inlet H2 concentration: 88 vol% and 50 vol%
    Catalano et al. (40) Feed flow rate (m3 s−1): (1.67–5.00) × 10−5 m3 s−1 (at normal condition). Pressure: up to 600 kPa (difference in total pressure). Inlet H2 concentration: 50 vol% and 88 vol%. Temperature: 673–773 K. Binary (H2:N2, H2:CH4) and ternary mixtures (H2:N2:CH4)
    Caravella et al. (53) Membrane thickness: 1–150 μm. Permeance: 0.1–20 mmol m−2 s−1 Pa−0.5. Reynolds Number: 2100–8000. Upstream total pressure: 200–1000 kPa. Downstream total pressure: 100–800 kPa. Inlet H2 concentration: 0–1 molar fraction. Temperature: 573–773 K
    Coroneo et al. (44) 0, 2 and 3 (number of baffles)
    Caravella et al. (54) Total upstream pressure: 400–1000 kPa. CO partial pressure: 0–1000 kPa. Inlet H2 concentration: 0–1 molar fraction. Ternary (H2:CO:N2) and binary mixture (H2:CO)
    Chen et al. (39) Permeance: 10−3–1 mmol m−2 s−1 Pa−0.5. Reynolds number: 20–2000. Pressure: 506.5–3039 kPa. Inlet H2 concentration: 0.20–0.80 molar fraction
    Chen et al. (41) Feed flow rate: 2.713 × 10−4–4.3408 × 10−3 mol s−1. Reynolds number: 10–50 (retentate side) and 2–2000 (permeate side). Flow pattern: countercurrent and cocurrent modes. Position of the feed flow: in lumen or shell side
    Faizal et al. (55) Feed flow rate: 1.489 × 10−5–2.976 × 10−4 mol s−1. Upstream total pressure: 200–300 kPa
    Chen et al. (56) Reynolds number: 20–2000 (permeate side) and 20–800 (retentate). Pressure difference: 506.5–3039 kPa. Shell diameter: 25–100 mm
    Chen et al. (57) Feed flow rate: 1.67–3.33 × 10−6 m3 s−1. Pressure: 50.7–405.2 kPa (H2 partial pressure difference). Inlet H2 concentration: 50–100 vol%
    Chen et al. (58) Baffle patterns, positions at shell wall, ratio of baffle length to radius (0–0.75)
    Nekhamkina and Sheintuch (59) Pressure: 31.62–632.46 Pa0.5 (initial driving force). Inlet H2 concentration: 0.50–0.88 (molar fraction). Separation parameter, Γ(<29)
    Zhao et al. (23) Feed flow rate: 4.17 × 10−6–4.00 × 10−3 m3 s−1. Inlet H2 concentration: 0.50–0.90 (molar fraction). Temperature: 673–773 K. H2S concentration: 7–35 ppm
    Faizal et al. (60) Feed flow rate: 2.78 × 10−5–2.50 × 10−4 mol s−1. Inlet H2 concentration: 0.70–0.80 (molar fraction). Various species in H2 mixture (H2:N2, H2:Ar, H2:He and H2:CO2)
    Nakajima et al. (61) Feed flow rate: 5.0 × 10−4–1.5 × 10−3 Nm3 s−1 m−2. Internal diameter of reactor vessel: 1.66–2.39 × 10−2 m
    Kian et al. (63) Total upstream pressure: 150–600 kPa. Various ternary and quaternary mixtures as well as a senary mixture → H2:Ar, H2,He,H2:CH4, H2:H2O, H2:CO:He (example of ternary mixture), H2:CO2:CO:He (example of quaternary mixture), H2:CO2,H2O:CH4:CO:He. Gas hourly space velocity (GHSV): 221–882 h−1. Flow rates: 276–1078 ml min−1
    Helmi et al. (64) Relative fluidisation velocity: 1.3–3.3. H2 mole fraction: 0.1, 0.25 and 0.45

    Fig. 2.

    (a) Tubular type membrane configuration (feed flow is issued through shell side); (b) tubular type membrane configuration (feed flow is issued through lumen side); (c) tubular type membrane with ‘finger-like’ configuration (front view); (d) circular flat sheet type membrane configuration (front view)

    (a) Tubular type membrane configuration (feed flow is issued through shell side); (b) tubular type membrane configuration (feed flow is issued through lumen side); (c) tubular type membrane with ‘finger-like’ configuration (front view); (d) circular flat sheet type membrane configuration (front view)

    In the early 21st century, Hou and Hughes were among the earliest groups who observed the concentration polarisation during an experiment involving hydrogen permeation with a palladium based membrane (67). The authors confirmed the existence of the concentration polarisation phenomenon during their experiment for a membrane with a thickness of 5 μm to 6 μm. However, the effect was not severe due to the relatively high feed gas velocity, which was a 5% decrease in hydrogen concentration for the various mixing ratios of the binary mixture of hydrogen and nitrogen (67).

    Zhang et al. (51) were one of the pioneer groups who comprehensively investigated the concentration polarisation phenomenon specifically for palladium based membranes. The effect of various parameters such as pressure, temperature, feed gas flow rate and permeability was investigated experimentally. Also, the parameters were interpreted through mathematical modelling particularly for tubular membranes with porous ceramic supports. The authors found that when the feed gas flow rate is increased, the concentration polarisation is weakened, resulting in higher hydrogen permeation. For instance, for the case of membrane temperature of 723 K, when the feed flow rate was 5 ml s−1 (equivalent to 5 × 10−6 m3 s−1), the concentration polarisation degree for hydrogen (ratio of hydrogen permeation flux with concentration polarisation to hydrogen permeation flux without concentration) was around 0.54. However, when the feed flow rate was increased to around 14 ml s−1 (equivalent to 14 × 10−6 m3 s−1), the concentration polarisation degree for hydrogen became 1, that is no effect of concentration polarisation on hydrogen permeation flux was found. Furthermore, the authors reported that the observed phenomena are mainly due to the higher removal rate of accumulated nitrogen in the boundary layer at higher feed flow rates (51). However, an increase in pressure at the retentate or upstream side (at constant permeated pressure) increases concentration polarisation, as clearly described by the mathematical modelling developed in the study. Based on their study, at constant temperature of 723 K, for the case of pressure of 2 atm (equivalent to 202.6 kPa), the concentration polarisation degree for hydrogen already reached a value of 1 (no effect of concentration polarisation) when the feed flow rate was around 14 ml s−1 (equivalent to 14 × 10−6 m3 s−1). However, for the case of higher pressure of 4 atm (equivalent to 405.2 kPa), the concentration polarisation degree for hydrogen still not reached value of 1 even though feed flow rate was increased to 32 ml s−1 (equivalent to 32 × 10−6 m3 s−1). Based on the model, the observed trend is related to the proportional relation between the mass transfer coefficient of the retentate side and the diffusion coefficient, which is reciprocal to operating pressure (51). Therefore, the findings of Zhang et al. corroborated the previous findings by Morguez and Sanchez (68), which reported that the effect of selectivity is less significant compared to feed gas flow rate, pressure and permeability (68). The authors also observed that the temperature range used in their experiment did not trigger the concentration polarisation phenomenon. However, the authors did not rule out the possibility of concentration polarisation when the hydrogen permeation rate is enhanced due to the increase in temperature (51).

    Pizzi et al. performed an experimental study for ultra-thin (~2.5 μm thickness) palladium/silver membranes deposited on ceramic supports. The authors observed that pronounced concentration polarisation occurred regardless of the composition mixture (52). As a result, the phenomenon was evident despite the concentration of nitrogen in a binary mixture of H2:N2 being relatively very low (12 vol%) (52). For this case, it was found that when Sieverts’ driving force is set to 0.8 bar0.5 (equivalent to 253 Pa0.5), the hydrogen permeate flux is only 0.26 mol s−1 m−2, that is significantly lower if compared to the permeate flux obtained when the concentration polarisation effect is negligible (permeate flux of 0.68 mol s−1 m−2).

    The lack of extensive studies on the detailed mechanism of concentration polarisation specifically for palladium based membranes prompted Catalano et al. (40) to explore this research area. The findings of Catalano et al. demonstrated a similar trend with that of Zhang et al. (51) in terms of the effect of feed flow rate, and Pizzi et al. (52) in terms of the effect of mixture composition on the concentration polarisation phenomena. Compared to previous research, a fundamental investigation on the ternary mixture of H2:N2:CH4 (volume ratio of 50:25:25) was also conducted for the first time. The findings showed that the permeation flux was marginally less than the flux for the binary mixture of H2:N2 (volume ratio of 50:50) but almost similar to the H2:CH4 (volume ratio of 50:50) mixture. Therefore, the findings reveal that there was a very slight decrease in permeation flux, which occurred when nitrogen was replaced with methane (40). In this case, previous researchers have confirmed that the inhibitive effect caused by methane is very minimal, thus can be neglected (69). Based on the findings of Catalano et al. (40) and Jung et al. (69), it is evident that the severity level of concentration polarisation is independent on number of species (binary or ternary) in the non-inhibitive hydrogen mixture. Catalano et al. also have interpreted the level of concentration polarisation for various operating conditions using a dimensionless polarisation number, which is defined as the ratio of gas phase to membrane sensitivity factor (40). The polarisation number of much higher than 1 (S>>1) means concentration polarisation is dominant, whereas when the number is much less than 1 (S<<1), resistance by the metal membrane controls the entire permeation process. The authors discovered that for both cases of ternary and binary hydrogen mixtures with feed flow rates of 1 Nl min−1 to 3 Nl min−1 and relatively low inlet hydrogen concentration (50 vol% H2), the concentration polarisation becomes dominant, that is S>>1. However the value of S is reduced when hydrogen concentration or feed flow rate is increased. As example, for the case of binary mixture of H2:N2 (50 vol% H2 and 50 vol% N2) with operating temperature and total pressure of 673 K and 600 kPa, respectively, when the feed flow rate was increased from 1 Nl min−1 to 3 Nl min−1, S reduced significantly from 6 to 2.5.

    Most of the studies on concentration polarisation elaborated previously used palladium based membrane with support that influences the hydrogen permeation process (70). Conversely, Caravella et al. (53) examined the concentration polarisation phenomenon on self-supported palladium-based membrane in which case the effect of support was eliminated. In addition to the previous studies, other researchers (40, 5152), have analysed the broader range of upstream hydrogen molar fraction, total upstream pressure, downstream total pressure, operating membrane temperature, membrane thickness and permeability to develop polarisation maps as a very useful guide for membrane reactor designer. The term concentration polarisation coefficient (CPC) was introduced in the maps as a demonstration for the level of concentration polarisation. Here, when the value of CPC is 0, it means no polarisation occurs while the value of 1 indicates the occurrence of total or maximum polarisation. Additional parameters were considered in this study that were not covered by the other previous researchers, namely: operating temperature, permeance, total downstream pressure and membrane thickness. Furthermore, the analysis demonstrated that the severity of concentration polarisation increases when the temperature and permeance are increased whereas the total downstream pressure and membrane thickness are reduced (53). As example, when Reynolds number, hydrogen retentate molar fraction, temperature, pressure at retentate side and pressure at permeate side were set to 2100, 0.40, 500°C, 1000 kPa and 200 kPa, respectively, the CPC increased significantly from around 0.13 to around 0.65 (thus concentration polarisation effect become stronger) when membrane thickness was reduced from 50 μm to 5 μm. Similar to the assertion by Morgues et al. (68), Caravella et al. (53) also found that the hydrogen flux itself plays a significant role during concentration polarisation.

    Caravella et al. extended their analytical study to cover the concentration polarisation phenomena for a hydrogen mixture that contains well-known inhibitive species of carbon monoxide (22, 7176). In this study (54), the authors simultaneously considered the effects of concentration polarisation and inhibition by carbon monoxide by merging their previously introduced approach (53) and the approach by Barbieri et al. (77). Similar to their previous study (53), the authors introduced a parameter so-called permeation reduction coefficient (PRC) that includes both polarisation and carbon monoxide inhibitive effects simultaneously. Interestingly, it was found that when the polarisation and carbon monoxide inhibition occur at the same time, the hydrogen permeation flux obtained is lower compared to the flux obtained when both phenomena occurred separately. This is mainly due to the polarisation of the inhibitor carbon monoxide toward the membrane surface, which increases the carbon monoxide partial pressure at the surface (54). The researchers found that for binary mixture of hydrogen and carbon monoxide, when operating temperature, membrane thickness, Reynolds number, hydrogen upstream molar fraction, total upstream pressure and downstream pressure are set to approximately 647 K, 60 μm, 1200, 0.60, 1000 kPa and 200 kPa, respectively, the permeating flux for the cases of polarisation only, inhibition by carbon monoxide only, and simultaneous polarisation and inhibition are around 85 mmol m−2 s−1, 71.5 mmol m−2 s−1 and 67 mmol m−2 s−1 (54). The inhibition of carbon monoxide under the influence of concentration polarisation is expected since the low feed flow rate is generally applied, for instance, during steam reforming for application in small portable electrical devices (8, 66).

    The phenomenon of concentration polarisation was featured by the two-dimensional numerical method for tubular type (39) and flat sheet type (78) membranes. In general, for permeation with tubular type membrane under concentration polarisation influence, the direction of hydrogen concentration decrease for binary mixture of H2:N2 is from the region around the leading edge (inlet part) to the tailing edge (outlet part) (39). This phenomenon is featured by Figure 3, in which dimensionless hydrogen concentration gradient decreases from the leading edge to the tailing edge of the membrane surface regardless of hydrogen volume percentage. However, for the case with vertical flow towards flat sheet type membrane surface, the hydrogen concentration is highest at the centre of the membrane, and decreases in radial direction, as shown by Figure 4 (78). These studies investigated the hydrogen concentration distribution around the membrane surface for various important parameters such as operating pressure, hydrogen molar fraction, feed flow rate (or Reynolds number) and membrane permeance. The qualitative simulated results reveal that the hydrogen concentration decreases at the membrane surface due to the effect of hydrogen flux itself during the phenomena. However, the severity level of concentration polarisation for the various parameters above is generally similar to the values described quantitatively by previous experimental and analytical studies (40, 5154). Chen et al. introduced an important parameter called hydrogen permeation ratio (HPR) to indicate the level of concentration polarisation (39). The HPR is defined as the ratio of hydrogen permeation rate across the membrane to the hydrogen feed rate at the inlet. The authors concluded that a decrease in value of HPR indicates that the severity of concentration polarisation is diminished. As an example, for the case of binary mixture of H2:N2 (H2 mole fraction of 0.50) with pressure difference and membrane permeance of 30 atm and 10−4 mol m−2 s−1 Pa−0.5, respectively, HPR decreased from 96 to 3 when Reynolds number was increased from 20 to 2000, thus severity of concentration polarisation is significantly reduced (39). It is interesting to note that when the aforementioned four important parameters (operating pressure, hydrogen molar fraction, feed flow rate and membrane permeance) were set in such a way to cause the effect of concentration polarisation to become very significant, the hydrogen concentration gradient is very high at the leading edge of the membrane (in the region near to the inlet) and then decays faster. Due to this phenomenon, there was almost no driving force for permeation in most of the remaining membrane length, as demonstrated by Figure 5 (refer to the case of permeance (K) of 10−3) (39). Figure 5 also demonstrates that when the permeance is increased, the tendency for concentration polarisation to occur increases. Based on Nagy et al. (79), a convex shape can be observed for the hydrogen concentration curve in a boundary layer during concentration polarisation phenomena, once the convective flow starts to play a role in the diffusive flow of the layer (80, 81). Based on these numerical simulation studies, Chen et al. also asserted that the concentration polarisation phenomenon is not significant when the hydrogen permeation ratio (H2 permeation rate:H2 feed rate) is less than 30%. It is important to note that even if the concentration polarisation can be improved (and more hydrogen flux can be obtained), the HPR that indicates hydrogen recovery becomes smaller, and this becomes a shortcoming for the membrane performance (39).

    Fig. 3.

    Dimensionless hydrogen concentration gradient from the leading edge (Z = 0.025 m) to the tailing edge (Z = 0.175 m) of the membrane surface, for the case of Reynolds number of 200, pressure difference of 30 atm and permeance of 10−3 Reprinted from (39) Copyright (2011), with permission from Elsevier

    Dimensionless hydrogen concentration gradient from the leading edge (Z = 0.025 m) to the tailing edge (Z = 0.175 m) of the membrane surface, for the case of Reynolds number of 200, pressure difference of 30 atm and permeance of 10−3 Reprinted from (39) Copyright (2011), with permission from Elsevier

    Fig. 4.

    Radial profile of hydrogen concentration on the membrane surface as a function of mean mole flux (feed flow rate divided by effective membrane surface area) for the case of inlet hydrogen mole fraction of 0.75, membrane temperature of 623 K, total upstream pressure of 0.25 MPa and total downstream pressure of 0.10 MPa (78)

    Radial profile of hydrogen concentration on the membrane surface as a function of mean mole flux (feed flow rate divided by effective membrane surface area) for the case of inlet hydrogen mole fraction of 0.75, membrane temperature of 623 K, total upstream pressure of 0.25 MPa and total downstream pressure of 0.10 MPa (78)

    Fig. 5.

    Distributions of concentration contour for various hydrogen permeance values (H2:N2 mixture, inlet H2 = 50%, Reynolds number = 200 and pressure difference = 30 atm). Reprinted from (39) Copyright (2011), with permission from Elsevier

    Distributions of concentration contour for various hydrogen permeance values (H2:N2 mixture, inlet H2 = 50%, Reynolds number = 200 and pressure difference = 30 atm). Reprinted from (39) Copyright (2011), with permission from Elsevier

    Subsequently, Chen et al. extended their numerical simulation to the tubular type membrane with simultaneous use of feed flow and sweep flow (41) under concentration polarisation influence. The advantage of using sweep flow to improve hydrogen permeation flux (and to abate concentration polarisation) has been confirmed by previous researchers (6, 7, 8284). When the sweep flow rate at the permeated side is increased, the hydrogen partial pressure at the membrane surface of the permeated side can be reduced, thus hydrogen permeation flux increases (and concentration polarisation is weakened) due to increase in hydrogen partial pressure difference (7, 83). For instance, in the case of countercurrent mode with the use of sweep gas in the shell side (outside tubular membrane and inside shell), the improvement in hydrogen flux was improved by 12.3% when the sweep flow rate was increased from 2.713 mol s−1 to 4.3408 mol s−1, thus indicating the importance of sweep flow rate in improving hydrogen flux. In this case, the optimum flow rate of sweep gas can be estimated from the arctangent function (41, 85) of feed gas flow rate, once the flow rate or Reynolds number of the feed gas is specified. Here, the flow rate of sweep gas is considered optimum when the flow rate can give the maximum hydrogen permeation flux and sufficiently high hydrogen recovery (up to 95% H2 recovery) could be maintained (41). It is interesting to note that the coupling between feed gas and sweep gas will give better separation performance when countercurrent mode is applied (5, 41). It is also interesting to note that whether the feed gas is issued in the lumen side (inside tubular membrane) or the shell side (outside tubular membrane and inside the shell) during countercurrent mode, the difference in hydrogen flux for both configurations is negligible. Therefore, this implies the independence of hydrogen flux on the position of the feed flow. Also, the difference in hydrogen permeation flux between cocurrent mode and countercurrent mode can be reduced by increasing the feed flow rate. Similar to the feed flow rate, a decrease in the sweep flow rate causes the effect of concentration polarisation to become stronger.

    Part II (86) continues the discussion and provides the conclusions.

    The Authors


    Mohd Faizal Hasan currently is working at the Faculty of Engineering, Universiti Teknologi Malaysia (UTM). He obtained his PhD degree in Engineering from Keio University, Japan. He is actively doing research on densification, torrefaction and gasification of palm biomass, characteristics of hydrogen permeation through palladium/silver purification membranes for fuel cell applications and methanol steam reforming for hydrogen production. In addition to research activities, he is currently teaching Thermodynamics and Applied Thermodynamics.


    Bemgba B. Nyakuma obtained his doctoral degree from UTM and currently works at the School of Chemical and Energy Engineering, UTM Skudai Campus, Johor Bahru, Malaysia. He is actively doing research and producing articles in biomass and coal related pretreatment, conversion and utilisation technologies.


    Mohd Rosdzimin Abdul Rahman currently is working at the Faculty of Engineering, Universiti Pertahanan Nasional Malaysia. He obtained his PhD degree in Engineering from Keio University, Japan. He is actively doing research on thermal and reactive fluid dynamics.


    Md. Mizanur Rahman obtained his PhD in Mechanical Engineering from Aalto University School of Engineering, Finland; MSc in Sustainable Energy Engineering from Royal Institute of Technology (KTH), Sweden; and BSc in Mechanical Engineering from Khulna University of Engineering and Technology, Bangladesh. His research interests include energy economics, renewable energy technologies, biomass digestion and gasification, multicriteria-based rural electrification, energy policy, modelling and optimisation and sustainable energy systems.


    Natrah Kamaruzaman obtained her undergraduate level degree from University of The Ryukyus, Japan. Then she obtained Master and Doctoral Degrees from UTM. Currently, she is specialising in microelectronic cooling and heat transfer. Her research interests are focusing on heat transfer, computational fluid dynamics, fluid flow and microchannel and microneedle areas.


    Syahrullail Samion is currently working at the Faculty of Engineering, UTM. He obtained his undergraduate, master and doctoral degrees from Kagoshima University, Japan. His areas of expertise are tribology in metal forming, friction and wear tests (tribotester), biolubricants, palm oil as lubricant and fluid mechanics. He is also teaching mechanics of fluids (undergraduate course) and research methodology (master course).

    By |2020-12-08T12:42:19+00:00December 8th, 2020|Weld Engineering Services|Comments Off on Comprehensive Review on High Hydrogen Permselectivity of Palladium Based Membranes: Part I

    Comprehensive Review on High Hydrogen Permselectivity of Palladium Based Membranes: Part II

    Johnson Matthey Technol. Rev., 2021, 65, (1), 77

    1. Factors Affecting Concentration Polarisation in Palladium Based Membranes

    Miguel et al. examined the decrease in the hydrogen concentration along the membrane length of a finger-like configuration (13) for the case of binary hydrogen mixtures with inhibitive carbon monoxide or carbon dioxide, by replacing the terms of feed partial pressure of inhibitive species and the difference in the square root of hydrogen partial pressure in the Sieverts’ Langmuir equation (4) with the average partial pressure of inhibitive species and logarithm mean driving force (5), respectively. In this case, the authors obtained an excellent concordance between the predicted results obtained from their rearranged Sieverts’ Langmuir equation with the actual hydrogen permeation flux (2), which proved the existence of concentration polarisation during the permeation.

    With the apparent advantage of using sweep gas during hydrogen permeation (6), Chen et al. have further investigated the concentration polarisation phenomena under sweep gas and baffles implementation (7). The flows of feed gas and sweep gas were in the form of countercurrent mode. It is interesting to note that higher hydrogen flux can be obtained from the membrane when a smaller diameter of the shell (smaller distance between the shell and tubular membrane) is used. As an example, when the pressure difference, temperature, mass flow rate of feed gas and Reynolds number of flow at the permeate side were set to 9 atm, 623 K, 267.48 mg s−1 and 1000, respectively, the hydrogen flux for the cases of large, medium and small shell were 0.88 mol m−2 s−1, 0.96 mol m−2 s−1 and 1.03 mol m−2 s−1, respectively. This is due to the reduction of boundary layer thickness, as demonstrated by the numerical results (7). Besides, the introduction of baffles to the shell side causes disturbance to the boundary layer and more hydrogen is directed towards the membrane surface. Therefore, concentration polarisation is weakened and more permeated hydrogen can be obtained. Interestingly, due to the trade-off between the installation cost and slight improvement in permeation performance when more baffles are installed, one baffle installation has been recommended (7). In this case, Coroneo et al. also have asserted there should be an optimum number of baffles installed after observing just a slight improvement in permeated flow when the number of baffles is increased, from around 38% (two baffles configuration) to just around 46% (three baffles configuration) (8).

    Further investigation by Chen et al. (9) then discovered the optimum baffles configuration for minimising concentration polarisation while obtaining maximum hydrogen recovery. In this case, the authors emphasised the importance of concentrating hydrogen at the membrane surface through the flow contraction mechanism. The optimum conditions for baffle installations are as follows: (a) installation of single baffle at shell wall; (b) installation at the leading edge of the membrane and (c) use of a sufficiently high ratio of baffle length to shell radius (ratio of 0.75) (9).

    Faizal et al. (10) investigated the effect of hydrogen partial pressure and feed flow rate on the level of concentration polarisation for flat sheet palladium/silver membrane, despite widespread research interest in tubular type membranes. A third degree polynomial equation has been introduced as a tool to predict hydrogen permeation flux for such geometry. Based on the predicted profile of hydrogen mole fraction at the membrane surface, the difference between the predicted average hydrogen mole fraction at the membrane surface and hydrogen mole fraction at the inlet becomes larger at higher inlet hydrogen partial pressure. For the case of a binary mixture of H2:N2 (inlet hydrogen mole fraction of 0.75), when operating temperature, feed mole flux and hydrogen partial pressure at downstream (permeate) side were set to 623 K, 0.40 mol m−2 s−1 and 0.10 MPa, respectively, the aforementioned difference increased from 9% to 20% when inlet hydrogen partial pressure was increased from 0.150 MPa to 0.225 MPa. Therefore, the concentration polarisation was strengthened. Compared to the previous studies, the changes in the concentration polarisation level concerning the inlet hydrogen partial pressure and feed flow rate are similar qualitatively (10).

    Chen et al. performed experimental studies on a H2:N2 mixture permeation test using high permeance tubular palladium based membranes (palladium and palladium/copper membrane with porous stainless steel) (11). Here, the thickness applied was from 6–7 μm. Similar to the previous study on ultrathin high permeance palladium/silver membrane with ceramic support (thickness of 2.5 μm) (12), the authors revealed that concentration polarisation was most affected by the concentration of the hydrogen feed, notably when the hydrogen concentration was decreased from 75 vol% to 50 vol%. The severity of concentration polarisation becomes higher even though the hydrogen partial pressure difference has been set to the same value. In this case, it can be noticed that in order to obtain the same hydrogen partial pressure difference, when the hydrogen partial pressure at the permeated side is set constant, higher total upstream pressure is necessary for smaller feed hydrogen fraction, and this increases the levels of concentration polarisation. Within their selected operating condition, feed flow rate and hydrogen partial pressure difference cause concentration polarisation as well, but with minor influence compared to the feed hydrogen concentration factor (11). Zhao et al. performed a permeation test for a mixture that was almost similar to coal gasification product (<40% H2 and <40 ppm H2S) to simultaneously determine the effect of sulfur contamination and concentration polarisation. The authors found that the influence of concentration polarisation was dominant for the mixture with lower hydrogen composition (50% mole fraction) especially at a low feed flow rate due to the minor effect of sulfur poisoning in the specified condition (13).

    As a continuation of their previous study (10), Faizal et al. (14) investigated the concentration polarisation phenomena for various binary hydrogen mixtures with different inlet hydrogen mole fraction (0.70–0.80) and species (nitrogen, argon, helium and carbon dioxide). It is interesting to note that a mixture of hydrogen and argon was used due to different chemical characteristics, whereas the mixture of hydrogen and helium was used due to the different binary diffusivity compared to the hydrogen mixture that contained nitrogen (14). The authors compared the analytical results calculated by using their previously introduced theoretical equation that takes into account the effect of hydrogen permeation itself (10) with the actual hydrogen permeation flux. The study demonstrated an excellent concordance between the estimated hydrogen permeation flux and the actual flux regardless of inlet hydrogen mole fraction and species, thus elucidates the significant effect of hydrogen permeation itself on the decrease in hydrogen concentration at the membrane surface during concentration polarisation. Therefore, it is interesting to note that the severity of concentration polarisation is determined by feed flow rate and inlet hydrogen mole fraction, but not the different chemical characteristics and binary diffusivity of the mixtures (14).

    Nakajima et al. reduced the boundary layer thickness to abate concentration polarisation by improving physical geometry of a reactor vessel containing a tubular palladium/silver membrane (15). In this case, the reduction of boundary layer thickness was performed by narrowing the path between the membrane surface and the inner surface of the vessel shell (15). For instance, by narrowing the path from 23.9 mm to 16.6 mm, the amount of produced hydrogen can be improved by around 25% even though there is only a 2% increment in methane conversion during hydrogen production from natural gas (for feed flow rate of 9 Nml min−1 cm−2) (15). Such improvement is due to the reduction in distance between the inner surface of the vessel and the membrane surface, which has also been observed through the previous numerical simulation performed by Chen et al. (7).

    As an alternative to the numerical simulation technique performed by Chen et al. (6, 16), the profiles of average axial concentration and concentration at the membrane surface can also be obtained by determining an analytical solution of the governed ordinary differential equation (ODE) (17). Further discussion on the analytical solution is presented in the following section.

    In 2018, Kian et al. investigated the concentration polarisation phenomenon for the case of various ternary mixtures (18). They found the hydrogen permeation behaviour for ternary mixtures is similar to the case of binary mixtures, in which competitive adsorption becomes dominant when strong inhibitive carbon monoxide is used in the ternary hydrogen mixture (H2:CO2:CO) while concentration polarisation starts to play a significant role when methane is used instead of carbon monoxide. In the same year, Helmi et al. also proved the concentration polarisation phenomenon for the case of a fluidised membrane reactor (19). The good agreement between the developed model that considers concentration polarisation (so called ‘1D/kd’) with experimental results elucidates that this phenomenon becomes more significant when lower inlet hydrogen mole fraction and higher inlet velocity are used (19). Based on the comprehensive review of the research scenarios in the previous paragraphs, it is evident that concentration polarisation is an undesirable phenomenon. This is because the ability of the membrane to permeate a very high amount of hydrogen cannot be fully utilised. However, it is unavoidable due to the advances in membrane technology that cause the fabrication of very thin membranes. Consequently, the external mass transfer becomes the permeation controlling step instead of diffusion in the metallic lattice. Although the development of compact devices with sufficiently high hydrogen recovery is possible, the concentration polarisation level becomes high due to the significant effect of permeation itself during the permeation.

    In brief, several techniques have been introduced to address such disadvantages and effectively reduce the severity of concentration polarisation. For example, baffles may be implemented (7, 8) in the membrane reactor and the path between membrane surface and inner vessel wall may be narrowed (7, 15) to reduce the boundary layer at the membrane surface (15). The implementation of a spherical particles bed between tubular membranes in a membrane reactor has been confirmed to reduce the effect of concentration polarisation, due to the increase in the interparticle velocity and the increase in the Reynolds number between the particles and membrane surfaces (20). Helmi et al. have used fluidising particles inside a fluidised membrane reactor to significantly reduce the concentration polarisation effect due to better mixing of gases (21). The permeation system with microchannel configuration (22, 23) also has been suggested as a technique for concentration polarisation abatement due to the ability to decrease boundary layer thickness near to the membrane surface (22, 24). The combined usage of baffles and perforated pipe to reduce concentration polarisation effect has been demonstrated by Peters et al. (25) due to the creation of turbulence. Recently, an integrated compact system that consists of combustor, prereformer, reformer and hydrogen separator (palladium membrane) in a single module was developed by Wunsch et al. for small hydrogen demand applications (26). Since the height of the integrated system was relatively very small (12.4 mm) with eleven plates arranged in a stack, the concentration polarisation effect could be minimised, thus improving hydrogen yield as well as hydrogen productivity (26).

    2. Estimation Methods for Hydrogen Permeation under Concentration Polarisation Influence

    In 2008, Chen et al. introduced a constant concentration method with the aim to characterise the membrane by eliminating the effect of concentration polarisation (27). Based on this method, the tubular membrane reactor was filled with non-H2 species first and followed by H2 to obtain the desired hydrogen partial pressure without allowing any permeation. Once permeation began, the hydrogen that permeated out of the membrane was made up or replaced by the fresh hydrogen from the pressurised tank to maintain the hydrogen partial pressure at the retentate side. Therefore, the variation of hydrogen concentration at the membrane surface could be eliminated (27). However, this technique is not practical for industrial application since the flow stream at the upstream side of industrial membrane reactor is usually in plug flow, and not perfectly mixed flow, in which concentration polarisation usually could be triggered.

    Extensive studies on concentration polarisation phenomena have been performed by Caravella et al. (28) and Catalano et al. (12). Caravella et al. (28) have created concentration polarisation maps which are very useful for hydrogen purification system design. Here, the maps are a two-dimensional graph of concentration polarisation coefficient versus hydrogen retentate molar fraction that was derived based on Equation (i):

    (i)

    where H2flux (elementary steps) is the hydrogen permeation flux that is calculated by considering all the permeation elementary steps (external mass transfer, superficial adsorption, diffusion through the palladium-based bulk and superficial desorption) (29), in which in this case, involved complex procedures. Meanwhile, the concentration polarisation coefficient (CPC) is a concentration polarisation coefficient that becomes as an indicator for concentration polarisation level. The values of CPC were obtained by solving Equation (i) for various operating conditions and the values were plotted with respect to hydrogen retentate molar fraction. Here, when the value of CPC is 0, it means no concentration polarisation occurs while the CPC value of 1 indicates maximum level of concentration polarisation that has been defined as ‘total polarisation’ in their study. ΠMembrane is the membrane permeance that can be obtained from permeation test for pure hydrogen. Meanwhile, DFBulk is bulk driving force that can be obtained from the difference in square root of hydrogen partial pressure between the feed side and permeate side when the effect of concentration polarisation is negligible. For those who want to evaluate the concentration polarisation level by using these maps, only knowledge of the operating condition of the membrane reactor is required. The CPC can be determined manually from the maps. Finally, hydrogen permeation flux can be predicted by substitution of the CPC value into Equation (i) and followed by solving the equation. Despite the simplicity of this prediction method, the determined CPC actually does not account for the remaining length (and remaining area) of the tubular membrane where no permeation occurs anymore due to very fast decay of driving force at the region around the inlet. This situation occurs when concentration polarisation becomes significant (16), thus hydrogen concentration is overestimated when the aforementioned CPC value is used. This weakness was then solved through the introduction of the powerful parameter so called effective average CPC (EAC) (30). The determination of EAC is stated as follows, Equation (ii):

    (ii)

    where L, z and CPC are the membrane length, membrane axial abscissa and concentration polarisation coefficient, respectively. Here, the local value of CPC for each position on the membrane in z-direction is determined analogously as was introduced previously (28). Meanwhile, the hydrogen concentration profile and the respective profile of hydrogen permeation flux can be obtained by simultaneously solving the external mass transfer and hydrogen permeation equations (30). Here, the calculation of mass transfer coefficient is as reported by Caravella et al. (29). Finally, Equation (ii) can be solved to obtain the value of EAC. Based on the previous individual elaboration on the prediction techniques using CPC (28) and EAC (30), it can be said that the use of EAC is more desirable, since it has the ability to represent the real behaviour of a hydrogen permeation device. It is interesting to note that once the EAC maps have been prepared, similar to the previous technique of using the CPC maps (28), the hydrogen permeation flux can be estimated by simply substituting the value of the EAC obtained from the maps into Equation (ii).

    Similarly, Catalano et al. (12) concluded the existence of non-negligible resistance to hydrogen transport in the gaseous phase itself, in addition to resistance caused by the membrane. For the case of a hydrogen mixture, the authors demonstrated a significant deviation from Sieverts’ Equation (Equation (iii)) when the hydrogen partial pressure of the bulk gas is substituted into the equation. To compensate for this situation, semi-empirical equations were developed for a tubular type membrane (membrane thickness of 2.5 μm) as follows (12), Equations (iv) and (v):

    (iii)

    (iv)

    (v)

    where NH2,int is the hydrogen flux crossing the membrane interface and is defined as the hydrogen flux within the gas-metal interface, kG is the mass transport coefficient, pret is the pressure at the retentate side, pH2,int is the hydrogen partial pressure at gas-metal interface, pH2,ret is the hydrogen partial pressure at retentate side, pH2,per is the hydrogen partial pressure at permeate side and is the hydrogen permeance obtained from pure hydrogen experiment. It is interesting to note that once the value of kG is obtained by solving Equations (iv) and (v) simultaneously and by using experimental data of NH2,int, the same value of kG can then be used to estimate hydrogen permeation flux for the cases with different hydrogen partial pressure difference.

    As a continuity of the previous study (28), Caravella et al. (31) considered simultaneously both concentration polarisation and inhibition by carbon monoxide species in their model, by introducing the permeation reduction coefficient. Similar to the prediction technique introduced previously (28), the permeation reduction coefficients were plotted for different operating conditions, or so called ‘permeation reduction maps’. The simple relation for the permeation reduction coefficient as shown by Equation (vi) was derived from definitions of CPC and inhibitive coefficient (IC), that were obtained from previous studies by Caravella et al. (28) and Barbieri et al. (4), respectively through complex calculation steps, Equation (vi):

    (vi)

    where PRC is the permeation reduction coefficient, CPC is the concentration polarisation coefficient and IC is the inhibition coefficient. To predict the hydrogen permeation flux for certain operating conditions, the value of PRC is determined manually from the ‘permeation reduction maps’ and then the value is substituted into Equation (vii) as follows:

    (vii)

    where JH2 is the hydrogen permeation flux, PRC is the permeation reduction coefficient, ΠSieverts is the permeance which is similar to the hydrogen permeance coefficient, obtained from pure-hydrogen test. Meanwhile, is the bulk driving force for hydrogen permeation, that is bulk difference in square root of hydrogen partial pressures between the retentate and permeate side.

    As one of the solutions for the difficulty in obtaining a general relation that consists of several interdependent parameters as has been mentioned by Morgues et al. (32), Faizal et al. (10, 14, 33) have introduced a theoretical approach for hydrogen permeation through a flat sheet palladium based membrane after observing a significant deviation between the actual permeation flux and the estimated flux by Sieverts’ equation (Equation (iii)) when inlet hydrogen concentration was used (33). As asserted by previous researchers on the significant effect of permeation flux during concentration polarisation phenomena (6, 12, 16), the term of hydrogen partial pressure at membrane surface of upstream side in the Sieverts’ equation (Equation (iii)) has been modified to consider the effect of hydrogen permeation flux during permeation. The modification of Equation (iii) leads to the formation of Equation (viii) as follows (14):

    (viii)

    where fp is the estimated hydrogen permeation mole flux, q is the hydrogen permeance coefficient, d is the membrane thickness, fH2,in is the mole flux of hydrogen from inlet (feed flow rate of hydrogen divided by effective membrane surface area), fin is the mole flux of the mixture from inlet (feed flow rate of mixture divided by effective membrane surface area), Pin is the total pressure at inlet (total upstream pressure) and pH2,2 is the hydrogen partial pressure at membrane surface of the downstream side. In order to predict fp, the values of operating parameters are substituted into Equation (viii) and followed by solving the equation for fp. Surprisingly, the modified equation as shown by Equation (viii) can estimate accurately hydrogen permeation flux for any noninhibitive binary hydrogen mixture with different chemical characteristics and binary diffusivity, along with any hydrogen concentration and with any mole flux of mixture from the inlet. For instance, when the mole flux of mixture from the inlet is increased, the effect of concentration polarisation is weakened. Therefore, the estimated flux obtained from Equation (viii) approaches the flux obtained from Equation (iii) due to the weaker effect of fp. The introduced method is supposed to be very useful for reactors with similar type of membrane used (3436).

    To prevent membrane damage due to mechanical stress, the palladium/silver tubular membrane was created in the form of a ‘finger-like’ configuration, thus allowing the free elongation and contraction of the membrane (2). For this kind of configuration, the way to predict hydrogen permeation flux is supposed to be similar to that for the tubular type membrane with common configurations (Figures 2(a) and 2(b) in Part I (37)) because the hydrogen mixture similarly flows horizontally along the membrane length for both cases. In the research performed by Miguel et al. (2), a model to simultaneously consider both concentration polarisation and inhibition by carbon monoxide or carbon dioxide has been introduced based on the logarithm-mean driving force (for considering concentration polarisation effect) and correction factor due to inhibitive effect (4). Compared to the approach by Barbieri et al. (4), the model introduced by Miguel et al. could provide more accurate results for the simultaneous occurrence of both phenomena. This is because the previous approach by Barbieri et al. (4) only considers the feed hydrogen partial pressure for prediction. However, the model introduced by Miguel et al. is semi-empirical and therefore, experimental data is necessary in order to determine certain parameters in the correction factor. The combination of correction factor and rearranged Sieverts’ equation forms the rearranged Sieverts’-Langmuir equation as shown below (2), Equation (ix):

    (ix)

    where the term is the correction factor due to adsorption of inhibitive species on the membrane surface and the term is the rearranged Sieverts’ equation.

    Here, is the hydrogen permeation flux, α is the Sieverts’-Langmuir reduction factor, Ki is the Langmuir’s adsorption constant for species (CO or CO2), is the average partial pressure of species (CO or CO2) between the feed and retentate sides, LH2 is the hydrogen permeance or hydrogen permeation coefficient, δ is the membrane thickness and ΔPln is the logarithm mean driving force that is determined based on theory of heat exchanger for parallel flow case (2, 5). It is important to note that the values of α and Ki for carbon monoxide and carbon dioxide are dependent on operating temperature, thus these values need to be fitted with experimental data first before using Equation (ix) to estimate hydrogen permeation flux.

    A prediction method for hydrogen permeation capacity (length of membrane for hydrogen permeation) has been introduced by Xie et al. (38) through computer programming. The investigation was performed analytically for seven important scenarios with a different flow pattern on both sides (upstream and downstream side). In this case, the concept is similar to that performed by Faizal et al. (10, 14, 33), in which the effect of hydrogen permeation rate is taken into account when determining hydrogen partial pressure at the membrane surface of the upstream side, as shown by the following Equation (x) (example for the scenario with plug flow at upstream side, and no sweep gas):

    (x)

    where PH (x) is the hydrogen partial pressure of an infinitesimal permeation capacity (infinitesimal membrane length for permeation), dx in the high pressure (upstream) side, M1 is the feed flow rate of hydrogen at upstream side, M2 is the feed flow rate of nonpermeable gas at upstream side, P1 is the total pressure of upstream side and Mx is the hydrogen permeation rate through a membrane for length from 0 to x. Then, the local hydrogen permeation rate through the infinitesimal permeation capacity dx can be predicted by substituting Equation (x) into the Sieverts’ equation as follows, Equation (xi):

    (xi)

    where C is the constant for membrane and P2 is the total pressure of downstream side. In their study, Equation (xi) is rearranged and then followed by integration of x with respect to Mx in order to predict the permeation capacity (membrane length for separation) x as shown by Equation (xii):

    (xii)

    Differently to other techniques, the technique introduced by Xie et al. (38) is used to estimate the value of x instead of Mx.

    Recently, algebraic functions that can be used to predict the profiles of hydrogen permeation flux under the influence of the concentration polarisation phenomenon have been introduced (17). Concentration polarisation is accounted through the use of an effectiveness factor which was derived in the previous study (39). The effectiveness factor is the ratio of actual permeation flux over the calculated flux based on the average concentration, and it is a function of separation parameter that represents the ratio of diffusive to permeation flux. The effectiveness factor and separation parameter that obeys Sieverts’ Law can be expressed as Equation (xiii) and Equation (xiv), respectively (2):

    (xiii)

    (xiv)

    where (Equation (xv)):

    (xv)

    Here, η is the effectiveness factor, is the hydrogen partial pressure at membrane surface of retentate side,  is the hydrogen partial pressure at membrane surface of permeate side, is the average hydrogen partial pressure at retentate side, Γ is the separation parameter, D is the diffusion coefficient of hydrogen in the gaseous phase, Sh is the Sherwood number, d is the characteristic length, pret is the pressure at retentate side, KH2 is the hydrogen permeability and ctot is the total molar density. To predict the profile of hydrogen permeation flux, the algebraic functions presented by Nekhamkina et al. (17) need to be solved.

    3. Conclusions

    The background of the scenarios related to palladium based membranes has been elaborated. It was found that concentration polarisation becomes unavoidable in parallel with advances in membrane technology. The scenario of parametric studies on the concentration polarisation phenomenon specifically for palladium based membranes was reviewed comprehensively. Based on the present review, it is evident that an increase in total upstream pressure, membrane temperature and permeance promotes concentration polarisation. The same trend is also achieved when the feed flow rate, inlet hydrogen concentration, total downstream pressure and membrane thickness are reduced. When the ratio of hydrogen permeation rate to hydrogen feed rate at the inlet becomes sufficiently high, the effect of hydrogen permeation flux on the hydrogen concentration decrease at the membrane surface becomes significant, thus concentration polarisation becomes strong. Therefore, it can be said that an increase in hydrogen recovery percentage leads to a stronger tendency for concentration polarisation to occur, and as a consequence, larger deviation from the hydrogen permeation flux estimated by Sieverts’ equation could be observed. For both tubular type and flat sheet type membranes, when concentration polarisation is triggered, the hydrogen concentration decreases in the horizontal direction (from the leading edge to the tailing edge) and radial direction, respectively. Furthermore, the existence of inhibitive species such as carbon monoxide in the hydrogen mixture somehow causes the membrane performance in terms of hydrogen permeation flux to become worse due to the simultaneous occurrence of concentration polarisation and inhibition by carbon monoxide. Meanwhile, the concentration polarisation level does not depend on the number of noninhibitive species, chemical characteristics of noninhibitive species or binary diffusivity in the hydrogen mixture (binary or ternary mixture).

    Several techniques have been identified to effectively abate concentration polarisation such as coupling of upstream flow with sweep flow in countercurrent mode, installation of baffles in the appropriate number, size and position, and by narrowing the space for upstream flow, that is reduction of the distance between the shell and membrane. Basically, the aforementioned techniques were implemented to increase the hydrogen concentration at the membrane surface of upstream side, thus concentration polarisation could be reduced.

    Finally, several estimation methods for hydrogen permeation flux have been reported for different membrane configurations. Several methods are empirical, in which experimental data is necessary to obtain certain coefficients while some of the methods can be used by just substituting the operating parameters into the introduced equation.

    For future work, it is suggested that the methods to estimate hydrogen permeation flux for the application of steam reforming should be intensively developed for various operating conditions. In this case, the detailed chemical kinetics must be considered to obtain the accurate mixture composition near the membrane surface. The competitive adsorption by excessive steam and excessive vaporised alcohols (methanol for instance) in addition to carbon monoxide during the occurrence of steam reforming reaction should also be taken into account in the future development of estimation methods.

    The Authors


    Mohd Faizal Hasan currently is working at the Faculty of Engineering, Universiti Teknologi Malaysia (UTM). He obtained his PhD degree in Engineering from Keio University, Japan. He is actively doing research on densification, torrefaction and gasification of palm biomass, characteristics of hydrogen permeation through palladium/silver purification membranes for fuel cell applications and methanol steam reforming for hydrogen production. In addition to research activities, he is currently teaching Thermodynamics and Applied Thermodynamics.


    Bemgba B. Nyakuma obtained his doctoral degree from UTM and currently works at the School of Chemical and Energy Engineering, UTM Skudai Campus, Johor Bahru, Malaysia. He is actively doing research and producing articles in biomass and coal related pretreatment, conversion and utilisation technologies.


    Mohd Rosdzimin Abdul Rahman currently is working at the Faculty of Engineering, Universiti Pertahanan Nasional Malaysia. He obtained his PhD degree in Engineering from Keio University, Japan. He is actively doing research on thermal and reactive fluid dynamics.


    Md. Mizanur Rahman obtained his PhD in Mechanical Engineering from Aalto University School of Engineering, Finland; MSc in Sustainable Energy Engineering from Royal Institute of Technology (KTH), Sweden; and BSc in Mechanical Engineering from Khulna University of Engineering and Technology, Bangladesh. His research interests include energy economics, renewable energy technologies, biomass digestion and gasification, multicriteria-based rural electrification, energy policy, modelling and optimisation and sustainable energy systems.


    Natrah Kamaruzaman obtained her undergraduate level degree from University of The Ryukyus, Japan. Then she obtained Master and Doctoral Degrees from UTM. Currently, she is specialising in microelectronic cooling and heat transfer. Her research interests are focusing on heat transfer, computational fluid dynamics, fluid flow and microchannel and microneedle areas.


    Syahrullail Samion is currently working at the Faculty of Engineering, UTM. He obtained his undergraduate, master and doctoral degrees from Kagoshima University, Japan. His areas of expertise are tribology in metal forming, friction and wear tests (tribotester), biolubricants, palm oil as lubricant and fluid mechanics. He is also teaching mechanics of fluids (undergraduate course) and research methodology (master course).

    By |2020-12-08T12:26:50+00:00December 8th, 2020|Weld Engineering Services|Comments Off on Comprehensive Review on High Hydrogen Permselectivity of Palladium Based Membranes: Part II

    Optimising Metal Content in Platinum Group Metal Ammonia Oxidation Catalysts

    Johnson Matthey Technol. Rev., 2021, 65, (1), 44

    1. Introduction and History

    The production of nitric acid, a key industrial process, requires the synthesis of nitric oxide as a precursor to the desired end product. Nitric acid, with a current annual production of 65.9 million tonnes, is primarily used in the production of ammonium nitrate for fertiliser applications, with the remainder (around 20%) used in industrial applications including the production of explosives (1).

    Johnson Matthey has manufactured pgm ammonia oxidation catalysts for over 100 years, selling the first platinum gauze pack to the UK Munitions Invention department in October 1916. This pack contained woven wires manufactured from pure platinum and required 1 kg of platinum to manufacture 1 tonne of nitric acid (2). In the century that followed, a number of technological advances resulted in lighter and more efficient catalyst packs and reduced the installed metal content per tonne of nitric acid produced from kilograms to milligrams.

    The first advancement in technology was the substitution of pure platinum with a 10% rhodium 90% platinum alloy, first patented by DuPont, USA, in 1929 (3). Rhodium increased the mechanical strength of the alloy and reduced in situ metal loss, allowing the catalyst to be operated at higher temperatures and benefit from the associated increase in selectivity to nitric oxide (4).

    Despite the reduction in metal loss from the optimisation in alloy, the metal lost from the catalyst in situ remained high and formed a significant part of the plant operating costs. To reduce the cost of the metal loss, gauzes comprising woven palladium-alloy wires were developed in 1968, using a gold-palladium alloy, with up to 20% gold (5). This catchment pack sacrificially collects platinum whilst losing palladium, reducing the cost of the total metal loss. Further research to reduce the cost of the catchment system resulted in the development of nickel-palladium and tungsten-palladium alloys (6, 7) with research showing that a low concentration of the base metal was required for high collection efficiency (8). As a result, alloys used in catchment systems today typically contain 95% palladium.

    The 1990s saw a significant change in the design and manufacture of pgm catalysts, with Johnson Matthey introducing new technology where knitted gauzes superseded woven. As well as introducing more flexibility to catalyst design, the new technology was observed to have a positive impact on the catalyst selectivity to nitric oxide (6). This technology is now the standard for ammonia oxidation catalysts and is offered by all major catalyst suppliers.

    Gauze manufacturers make use of different technologies, i.e. warp and weft knitting, to manufacture the catalyst gauzes. Recent advances driven by knitting include the manufacture of very high-density gauzes to concentrate metal towards the top of the pack. There are different methods to achieve this: Johnson Matthey has achieved this by minimising the open area of a weft-knitted gauze, using high density structures that increase the metal content per gauze by over 90% compared to the basic knit structure. Other manufacturers such as Umicore, Belgium, limited to greater open areas, have developed three-dimensional knit structures to achieve a high-density gauze (9).

    The mid-2000s saw a fundamental change in ammonia oxidation catalyst design, with ternary rhodium-platinum-palladium alloys, containing high concentrations of palladium, replacing traditional rhodium-platinum alloys in the lower portion of the pack. Johnson Matthey developed ECO-CATTM gauzes using these principles, and this new technology saw a reduction in installed weight required to produce a set amount of nitric acid. The length of time the plant could run with a catalyst pack (known industrially as the ‘campaign’) was increased. Lower density palladium-based alloys in the lower layers collect volatilised platinum from the top layers, with the captured platinum being used later in the campaign as the reaction progresses further into the pack. Variations on this technology are now the standard offering by most catalyst suppliers for medium-pressure nitric acid plants.

    Historically, catalyst packs were designed using rules of thumb and best estimates. An increased understanding of ammonia oxidation and primary metal losses within pgm catalysts has resulted in the creation of bespoke design tools, which allow Johnson Matthey to optimise the metal content and distribution required within a catalyst pack. Using these tools, catalyst designs can be tailored to plant operating conditions and KPIs. A tailored design can result in higher selectivity to nitric oxide, along with increased campaign lengths and reduced metal content in catalyst packs.

    Improvements have also been observed in nitric acid plant designs over the last 100 years. The first industrial nitric acid plants operated at atmospheric pressure and were restricted to low production rates. In the late 1920s, nitric acid plants were constructed that could operate under pressure, resulting in more compact plants that could achieve higher rates (10).

    Today, new nitric acid plants are typically dual-pressure plants or ultra-high mono-pressure plants (10). Dual-pressure plants utilise a low operating pressure for the ammonia oxidation reactor to ensure high selectivity to nitric oxide (typically 3–6 barg) and increase the pressure in the downstream absorption column to improve the column efficiency. Ultra-high mono-pressure plants operate at a single pressure, typically 10–13 barg, benefiting from lower capital costs but achieving lower plant efficiencies.

    2. Understanding Ammonia Oxidation

    2.1 Reaction Fundamentals

    Ammonia reacts with oxygen to produce nitric oxide, nitrogen and nitrous oxide. The selectivity of ammonia to each reactant is dependent on process conditions and catalyst specification. Nitrogen is the favoured product at lower temperatures, whilst nitric oxide formation is favoured at higher temperatures and at lower pressures. At low temperatures, NO is formed but is bound strongly to the platinum surface. This allows the NO to react with ammonia to form N2 which will then desorb. At high temperatures, the NO formed will desorb from the catalyst surface before this secondary reaction occurs, increasing the catalyst selectivity to NO (11).

    In industrial production, the reaction is mass transfer limited due to the relatively slow diffusion of reactants to the wire surface compared to the almost instantaneous surface kinetics (12). In industrial operation, the catalyst operates between 850–930°C and plant operating pressures range from atmospheric pressure to 13 barg. Typical selectivity to nitric oxide ranges from 90–97% (Equations (i)(iii)):

    (i)

    (ii)

    (iii)

    In addition to these primary reactions, ammonia can react with nitric oxide to produce nitrogen and nitrous oxide, which reduces the efficiency of the plant (Equations (iv) and (v)):

    (iv)

    (v)

    As a result, an effective catalyst will be designed to convert 100% of ammonia in the top few layers of the catalyst pack at the beginning of a campaign; although the reaction will progress further through the pack as platinum is lost and the top layers of the catalyst lose activity.

    The surface chemistry and metallurgy of the catalyst used impacts the selectivity achieved. Several precious metals have been shown to catalyse the ammonia oxidation reaction, including platinum, rhodium, palladium (13), silver and iridium (14). Platinum has the greatest selectivity to nitric oxide, making it the most suitable catalyst for nitric acid plants. Rhodium-platinum alloys, containing 3–10% rhodium, are the most common alloys offered in ammonia oxidation catalysts today, although often in conjunction with a rhodium-platinum-palladium alloy.

    While rhodium-containing alloys are primarily used to increase the alloy strength during manufacture and operation (15), rhodium-platinum alloys have been observed to have a higher selectivity to nitric oxide than pure platinum (4), and palladium-containing alloys have a reduced selectivity to nitrous oxide at all temperatures as demonstrated through ab initio modelling of the selectivity of ammonia oxidation to NO, NO2, N2 and N2O on pure platinum and palladium-platinum alloys (Figure 1). The benefit of lower selectivity to N2O is partially offset by an increase in selectivity to N2: palladium-based alloys can help reduce N2O emissions but at the cost of reduced selectivity to NO (16). The benefit of using palladium-based alloys has been demonstrated within the nitric acid industry, with catalyst packs using ECO-CATTM technology or other catalyst manufacturers ternary alloy technologies, shown to reduce N2O emissions by up to 30% compared to standard rhodium-platinum catalyst packs (17).

    Fig. 1

    In-house modelling by Johnson Matthey using ab initio kinetics and density functional theory (DFT) demonstrates the significant reduction in selectivity to N2O for: (a) a pure platinum alloy; (b) a palladium-doped platinum alloy across a range of temperatures. An increase in selectivity to N2 at higher temperatures is also demonstrated (16)

    In-house modelling by Johnson Matthey using ab initio kinetics and density functional theory (DFT) demonstrates the significant reduction in selectivity to N2O for: (a) a pure platinum alloy; (b) a palladium-doped platinum alloy across a range of temperatures. An increase in selectivity to N2 at higher temperatures is also demonstrated (16)

    2.2 In situ Restructuring and Metal Loss

    When exposed to the ammonia-air feed gas, the pgm wires begin to restructure, forming high-surface-area dendritic multiplanar crystal growths, known in the industry as ‘cauliflowers’. The formation of cauliflowers results in a significant increase in the specific surface area of the wire, with 10 to 20-fold increases in surface area observed after industrial operation, with the initial period of restructuring taking several days (1820). After initial restructuring, cauliflower formation is greatest in the top layer of the catalyst (Figure 2), as this is exposed to the greatest concentration of ammonia, with layers further down the pack seeing little to no restructuring until later in the campaign.

    Fig. 2

    (a) layer 1; (b) layer 3 and (c) layer 5 of a catalyst pack composed of 5% rhodium 95% platinum alloy after 5 days operation at 4 barg showing a high level of restructuring and cauliflower growth in the top layer and negligible restructuring on the bottom layer. Images are at 4000 × magnification (21)

    (a) layer 1; (b) layer 3 and (c) layer 5 of a catalyst pack composed of 5% rhodium 95% platinum alloy after 5 days operation at 4 barg showing a high level of restructuring and cauliflower growth in the top layer and negligible restructuring on the bottom layer. Images are at 4000 × magnification (21)

    The restructuring mechanism is poorly understood, with several mechanisms suggested for the production of cauliflower structures at the surface of platinum alloy wires. The prevailing theory is that the adsorption and subsequent reaction of NHx species results in localised areas of high temperature which promotes the dissociation of surface PtOx and RhOx; the presence of gas phase platinum species during ammonia oxidation has been demonstrated by mass spectrometry (22). The hotspots occur close to surface defects, such as grain boundaries, and this is where the restructuring process is observed to begin (14). As these gaseous species contact regions of the gauze where the reaction is slower, condensation occurs due to reduced temperatures, which forms new crystallites (23). These colder regions can be found very close to the hotspots, which results in a localised temperature gradient that drives the chemical vapour transport of the metal oxides. Some of these metal oxides will condense on the wire surface in these colder regions; further ammonia oxidation then occurs at this deposition and this rapidly results in the growth of cauliflower structures observed in activated and spent gauzes (18).

    Whilst this vapour-phase mechanism results in capture of a proportion of the metal, some is lost downstream of the gauze pack. The addition of palladium and rhodium will reduce the overall metal loss from the pack, as these alloys see a reduction in platinum volatility compared to pure platinum (14). Catalyst packs will typically lose half of the installed pgm content at the end of a campaign.

    The movement and loss of metal within the catalyst pack is a key constraint during the pack design phase, and it is critical to ensure sufficient metal is installed to maintain a high selectivity for the desired campaign length. As the campaign progresses, the catalyst begins to lose a significant amount of platinum in the top gauze layers, with the wires becoming enriched with rhodium. Post-campaign analyses of catalysts have observed surface rhodium levels of over 40% in extreme cases that suffered mechanical loss of platinum, with further research observing 33% rhodium enrichment in non-damaged gauzes (14). As a result of the platinum deficiency, full conversion of ammonia is no longer achieved in these top layers and the reaction zone stretches further into the catalyst. Lower gauze layers will be exposed to the ammonia oxidation reaction and begin restructuring.

    The design of the lower half of the catalyst pack is key to maintaining a high selectivity to nitric oxide in the later stages of the campaign: installing too many catalyst gauzes or not correctly distributing the metal within the pack can result in residual ammonia reacting with nitric oxide. These reactions result in both a reduction in selectivity to nitric oxide and an increase in unwanted side products, N2 and N2O. These reactions are suppressed in the presence of excess oxygen (24), and as a result are more likely to occur in lower layers of the pack. Conversely, if too few layers are installed then 100% conversion of ammonia may not be achieved as the campaign progresses, resulting in ammonia slip downstream of the catalyst.

    The use of ternary rhodium-platinum-palladium alloys in the lower portion of the catalyst pack is a key feature of ECO-CATTM packs. The concentration of palladium in the alloy can vary from low levels to constituting the majority of the alloy and allows the lower half of the pack to function as part catalyst, part catchment. During operation, volatilised platinum from the top rhodium-platinum layers is captured on the lower layers, increasing the platinum content on the surface of the wire, while palladium is lost from the catalyst. A successful ECO-CATTM catalyst will have a wire surface covered in platinum at the point the ammonia begins to break through and react on the layer, and selectively react to produce mostly nitric oxide.

    The restructuring mechanism within ECO-CATTM packs differs from rhodium-platinum cauliflower formation. Surface growths are more block-like (Figure 3), showing a resemblance to catchment restructuring (Figure 4) and the lower layers will fuse together during operation; a similar mechanism has been observed with catchment gauzes which are always separated with steel layers to prevent this. As a result of this formation, the gauze open area is reduced, and the pressure drop over the system increases.

    Fig. 3

    Scanning electron microscopy (SEM) at 250 × magnification showing the top layer of the fused structure at the bottom of an ECO-CATTM pack which had been installed in a high-medium pressure plant

    Scanning electron microscopy (SEM) at 250 × magnification showing the top layer of the fused structure at the bottom of an ECO-CATTM pack which had been installed in a high-medium pressure plant

    Fig. 4

    SEM at 250 × magnification showing the top layer of a catchment pack in a high-medium pressure plant. The observed low open area results in a high pressure drop as the gas passes through this gauze layer

    SEM at 250 × magnification showing the top layer of a catchment pack in a high-medium pressure plant. The observed low open area results in a high pressure drop as the gas passes through this gauze layer

    Platinum capture is also possible through the use of palladium-based catchment gauzes and glass-wool platinum filters. Glass-wool filters see recovery rates of 10–20% (5), and catchment packs can recover from 25% to 95% of platinum lost in the catalyst gauzes depending on the weight and distribution of palladium installed (6). 95% palladium alloys used in the catchment pack exhibit a different end of life morphology than the rhodium-platinum and rhodium-platinum-palladium catalyst gauzes, with the observed restructuring driven by the collection of platinum. However, palladium and palladium-based alloys can catalyse the ammonia oxidation reaction, and if exposed to the NH3-O2 containing gas, will restructure to produce cauliflower structures similar to those observed in rhodium-platinum alloys (14).

    2.3 Industrial Operation

    Industrial ammonia oxidation is carried out at high temperatures (ranging from 850–930°C) and at pressures ranging from atmospheric pressure to 14 barg. Depending on the daily acid production, the flux of ammonia (known in industry as the nitrogen loading) can range from 3–100 tonnes of nitrogen per m2 of cross sectional area of the ammonia oxidation burner per day (teN m−2 day−1; units are based on nitrogen from ammonia, excluding air).

    At industrial operating conditions, the selectivity to nitric oxide can range from 90–97%, with the large range due primarily to the reduction in efficiency caused when operating at higher pressures. In addition to reduced selectivity, higher pressure plants also see an increased rate of metal loss from the catalyst in situ.

    Nitric acid plants in industry have a wide range of operating conditions; however, they can broadly be defined in four categories. These categories are derived from plotting ammonia oxidation pressure against nitrogen loading (Figure 5).

    • Atmospheric plants, with nitrogen loadings of <10 teN m−2 day−1 and pressures of <1 barg, were the first type of nitric acid plants to be built industrially, and benefit from high selectivity to nitric oxide. However, due to the low nitrogen loading, the acid production rates are low

    • Low-medium pressure plants, which include most dual-pressure plants. These plants continue to benefit from relatively high selectivity to nitric oxide, with efficiencies of up to 96.5% observed. Operating at higher pressure allows for a significant increase in daily acid production and, due to relatively low metal losses, campaign lengths of up to one year can be achieved

    • High-medium pressure plants have a wide range of operating conditions. Some of these plants will benefit from similar design principles to low-medium pressure plants, while others from those for ultra-high-pressure plants

    • Ultra-high-pressure plants operate at high pressures (10–13 barg) and high temperatures (920–930°C). The selectivity to nitric oxide of around 90% is significantly lower than other plant types. The intrinsic rate of metal loss is substantially higher, limiting campaigns to around 100 days. As a result of the metal loss, the catalyst designs for these plants have the highest level of installed pgm weight per tonne of acid.

    Fig. 5

    Plotting individual nitric acid plant operating pressure against nitrogen loading gives rise to four distinct categories of plants. The majority of nitric acid plants will have operating conditions that lie within one of the four operating ranges illustrated here

    Plotting individual nitric acid plant operating pressure against nitrogen loading gives rise to four distinct categories of plants. The majority of nitric acid plants will have operating conditions that lie within one of the four operating ranges illustrated here

    In addition to the catalyst selectivity and metal loss, the pressure drop over the catalyst and catchment pack can also have an effect on industrial operation. This is most pronounced for ultra-high-pressure plants: a high system pressure drop will put strain on the compressor and the plant will not be able to operate at maximum production rates. The pressure drop over binary rhodium-platinum catalysts is relatively low, with higher pressure drops observed when operating ECO-CATTM catalysts due to the high palladium layers fusing together and reducing the system open area. The catchment system will create the greatest pressure drop as the physical collection of platinum can reduce the gauze open area. Post-campaign analysis by Johnson Matthey has observed the open area of used catchment gauzes to be as low as 2%.

    3. Designing the Optimal Pack

    The reaction fundamentals, restructuring and loss of metal and constraints in industrial operation must all be considered when designing a catalyst pack for ammonia oxidation in a nitric acid plant. The variables available to a catalyst designer and manufacturer include optimising the metal content and metal placement within the pack and selecting the most appropriate alloys and optimising their placement in the pack.

    3.1 Metal Content

    The optimal metal content installed in a catalyst pack is determined by the expected levels of metal loss during the campaign, which is modelled as a function of the burner operating pressure and nitrogen loading. For standard packs, the pack will be designed such that around 50% of the installed metal content remains after the completion of the campaign. For optimised packs utilising high-palladium alloys, the remaining metal content can be as low as 30% of the installed weight.

    A catalyst pack with an insufficient mass of pgm installed can lead to ammonia slip, where the reaction fails to complete within the catalyst pack. The introduction of ammonia downstream can result in the formation of ammonium nitrite and ammonium nitrate, which can pose an explosion hazard. Ammonium nitrite can form when NO2, NO and NH3 are present; significant levels of NO2 form downstream of the gauzes as NO undergoes oxidation, so avoiding ammonia slip downstream of gauze is crucial. Ammonium nitrite is highly unstable and can undergo explosive decomposition, which can result in the detonation of any ammonium nitrate present (25).

    Defining the required mass of pgm required for the catalyst pack is critical, however thought must also be given to the distribution of metal within the pack to achieve high selectivity to nitric oxide. The underlying kinetics of the reaction require that the ammonia oxidation is completed within as few gauze layers as possible to minimise the side reactions between ammonia and nitric oxide.

    Modifying the metal concentration within the pack is achieved by varying the densities of the gauzes. Johnson Matthey manufactures multiple knit structures of varying density which are combined with wire diameters ranging from 60 μm to 120 μm, as well as a range of different binary and ternary alloys. There are hundreds of configurations possible for each layer within the catalyst pack, and possible densities range from 300 g m−2 to over 1200 g m−2.

    To ensure the installed metal content is correct, Johnson Matthey uses theoretical and empirical models to estimate the primary loss expected from a catalyst at the required operating pressure and nitrogen loading. Distribution of the metal within the catalyst is also dependent on the plant category, and can be evaluated using an ammonia oxidation kinetic model, in conjunction with the expected primary losses, to determine where the majority of the reaction is carried out at different stages in the campaign (Figure 6) and ensure sufficient metal is installed to prevent ammonia slip later in the campaign.

    Fig. 6

    Kinetic model output for a gauze design for a low-medium pressure plant showing achieved ammonia conversion throughout the gauze pack at the start of the campaign and nine days into the campaign. This shows sufficient metal has been installed to prevent significant levels of ammonia slip on start-up (zero days) and to carry out the majority of the reaction in the top two gauze layers after nine days online

    Kinetic model output for a gauze design for a low-medium pressure plant showing achieved ammonia conversion throughout the gauze pack at the start of the campaign and nine days into the campaign. This shows sufficient metal has been installed to prevent significant levels of ammonia slip on start-up (zero days) and to carry out the majority of the reaction in the top two gauze layers after nine days online

    3.2 Alloy Selection

    The selection and placement of different alloys within the catalyst pack is critical to achieving high performance, with some alloys suited to the top part of the pack (the catalytic ‘engine’) and others providing benefits when installed at the bottom of the pack. Having a high platinum content in the top layer reduces the temperature at which the reaction begins to progress, in turn reducing the time between start-up and reaching peak efficiency. This can be achieved through a combination of alloy choice, selecting a binary alloy with <5% rhodium and increasing the metal concentration at the top of the pack by using high density knit structures. Experimental data has demonstrated a reduction in the light-off temperature of around 100°C, and Johnson Matthey has developed specific products for plants that struggle with light-off.

    A range of rhodium concentrations are available in binary rhodium-platinum alloys. Lower levels of rhodium are advised when plants suffer from rhodium oxide formation (Figure 7), which is significantly less selective to nitric oxide (26), to minimise or prevent such formation. Plants operating at low temperatures (<850°C) are at higher risk of rhodium oxide formation, and the risk increases for catalysts with significant levels of iron contamination. Interest in low-rhodium alloys has increased following the substantial increase in rhodium price, peaking at almost US$12,000 per troy oz in early 2020 (27).

    Fig. 7

    SEM image of a gauze wire at 4000 × magnification, showing the formation of characteristic rhodium oxide needles. Optimising rhodium content and placement within the gauze pack can reduce the likelihood of formation

    SEM image of a gauze wire at 4000 × magnification, showing the formation of characteristic rhodium oxide needles. Optimising rhodium content and placement within the gauze pack can reduce the likelihood of formation

    Palladium proves a beneficial addition in the lower part of the catalyst pack, and the introduction of ternary alloys within the pack of Johnson Matthey’s ECO-CATTM catalyst results in a significant reduction in the primary N2O generated by the catalyst pack (17). The catalyst pack achieves a higher efficiency towards the end of the expected campaign length due to the capture and recycling of volatilised platinum, allowing for campaign lengths to be extended, where maintenance schedules permit, while maintaining or even reducing the installed metal content. As a result of this technology, campaigns of up to one year are now commonplace in low-medium pressure plants.

    There are a range of ternary alloys used in ECO-CATTM catalysts. Initial developments of ECO-CATTM used only one high-palladium alloy, but further work has shown that the average campaign efficiency can be improved through use of a gradient of palladium in the pack. This has been demonstrated industrially, with an increase in the average efficiency of up to 1% reported by nitric acid plants, along with a reduction in N2O emissions.

    The optimal level of palladium is influenced by both plant performance and the relative price difference between platinum and palladium, balancing the cost of the installed metal, the net metal loss and any financial implications resulting from a change in N2O emissions.

    3.3 Catchment System

    In addition to the catalyst gauze pack, a palladium-alloy catchment (or getter) system will often be installed below the catalyst to minimise the metal loss from the catalyst through platinum capture and palladium loss.

    Recent changes to the pgm market have reduced the profitability of catchment systems. Palladium prices have continued to rise steadily since 2017, whilst platinum remained relatively flat. For 2020, the platinum market is expected to move into surplus and the palladium market to fall further into deficit (27), which has further implications for the optimal catchment pack design. The optimal catchment design is a function of the price differential and acceptable pressure drop.

    4. Case Study

    Optimisation of metal content is applicable to all categories of nitric acid plants and Johnson Matthey continually reviews existing catalyst designs to ensure they are optimal for plant operation and prevailing pgm market conditions. In recent years, significant steps have been taken to optimise metal content for ultra-high-pressure plants, with design options tailored to the key drivers of each plant, for example maximising daily production rates or maximising plant efficiency from a set level of ammonia feed.

    For a significant proportion of nitric acid producers operating ultra-high-pressure plants, the key driver is to produce the maximum amount of nitric acid from a gauze pack. In these cases, the introduction of palladium alloys is not recommended due to the increased pressure drop. The catalyst pack is instead optimised by increasing the platinum weight at the top of the pack by using larger wire diameters in the top layers. To maintain a constant pack weight, the total number of layers within the pack is reduced. As a result, ammonia oxidation is completed higher in the pack and the N2 and N2O-producing side reactions are reduced. In addition to selectivity benefits, increasing the wire diameter in the top layers provides sufficient metal for further cauliflower formation in the event of mechanical metal loss following a plant trip.

    For other ultra-high-pressure producers, typically operating in locations with higher raw material costs, the key driver is to maximise the efficiency of the gauze pack over a set campaign length. As a slight increase in pressure drop is tolerable for these plants, pack optimisation includes the use of ECO-CATTM design principles. Initial design optimisation work for a plant in this category combined the use of high-density knit structures in the top portion of the pack with high palladium alloys in the lower portion of the pack. The changes resulted in improving the conversion efficiency towards the end of the campaign, and as a result increasing the average campaign efficiency. Further design changes, including the reduction of palladium content whilst increasing the concentration of palladium higher in the pack, resulted in a reduction in N2O emissions from the gauze system.

    5. Conclusion

    The catalysis of ammonia oxidation using pgm gauzes has been used industrially for over 100 years. Step changes in performance have been achieved throughout the decades, reducing the required pgm metal content required in a catalyst pack and introducing a range of alloys and knitted structures from which to construct a catalyst pack. Research into ammonia oxidation has continued to support the development of catalysts with higher selectivity to NO and reduced N2O emissions, giving rise to the current binary and ternary alloys used in catalysts today.

    The underlying reaction kinetics and metal movement provide a basis for designing the optimal ammonia oxidation catalyst and have been used within Johnson Matthey to develop plant category specific design rules. Achieving a high selectivity to nitric oxide can be achieved by promoting near 100% ammonia conversion in the top layers, and the use of ternary alloys in the lower catalyst layers promotes recycling of platinum to maintain a high efficiency towards the end of the campaign. A wide range of knit structures, wire diameters and alloys are available to tailor the catalyst to the plant operating conditions and to distribute the metal within the pack in a way that promotes the highest selectivity to NO throughout the campaign. The concentration of rhodium and palladium in the top catalyst layers can be optimised to address plant-specific issues, including the formation of rhodium oxide and helping the catalyst to light-off at a lower temperature.

    Other factors influence the optimal design, with the acceptable pressure drop over the catalyst pack being key. Despite having significant benefits, including reduced N2O emissions, ECO-CATTM and catchment technologies are not always suitable for ultra-high-pressure plants due to the increased pressure drop.

    Optimisation of metal content within the catalyst pack is now the expected standard for all medium-pressure plants, with the development of high-density knit structures and ECO-CATTM technology resulting in improvements to conversion efficiency, reduction in installed metal content and the extension of campaign lengths. In recent years, further progress has been made in optimising catalyst packs for ultra-high-pressure nitric acid plants operating at >10 bar and with nitrogen loading values in excess of 60 teN m−2 day−1, designing the pack to minimise unwanted side reactions. While the high intrinsic metal loss continues to constrain the maximum campaign length for these plants, the optimisation of pgm content within the pack has resulted in an improvement in plant efficiency and, where targeted, a reduction in N2O emissions.

    Despite being a mature and conservative industry, the operational targets for nitric acid plants continue to increase to support the global demand for fertiliser. Many plants will seek to operate in excess of the nameplate capacity and carry out de-bottlenecking studies to support this. Changing operational targets should always be communicated to the catalyst supplier, as a change in plant loading, temperature or pressure is likely to require an updated catalyst design. The dynamic pgm market also influences the optimal pack design; catchment packs see a reduction in profitability when the price of palladium exceeds that of platinum. Additionally, at the time of writing rhodium was seeing extremely high prices which form a significant portion of the pack cost, leading to increasing interest in low-rhodium alloys.

    The optimisation of a catalyst pack is never a complete process, and continual monitoring of catalyst performance and an open dialogue between plant operator and catalyst supplier are critical in creating and maintaining an optimal pack design.

    ECO-CATTM is a trademark of Johnson Matthey PLC.

    By |2020-12-01T11:44:16+00:00December 1st, 2020|Weld Engineering Services|Comments Off on Optimising Metal Content in Platinum Group Metal Ammonia Oxidation Catalysts

    A Re-assessment of the Thermodynamic Properties of Osmium

    Johnson Matthey Technol. Rev., 2021, 65, (1), 54

    Introduction

    The thermodynamic properties of osmium were reviewed by the author in 1995 (1) with a further review in 2005 (2) to estimate a most likely value for the melting point at 3400 ± 50 K to replace the poor quality experimental values which were being quoted in the literature. More recently Burakovsky et al. (3) have estimated a value of 3370 ± 75 K in good agreement with the above selected value. In the 1995 review the enthalpy of fusion was unknown but was estimated from a relationship between the entropy of fusion and the melting point which showed a high degree of correlation for the platinum group metals (pgms). However the derived entropy of fusion value for osmium was based on values for the other pgms available at that time but since then the values for both palladium and platinum have been revised so that the entropy of fusion value for osmium would also be revised leading to a new estimate of 68.0 ± 1.7 kJ mol−1 for the enthalpy of fusion. This would then require the thermodynamic properties of the liquid phase to also be updated. A comment is included on an independent much lower estimate of the enthalpy of fusion. Wherever possible measurements have been corrected to the International Temperature Scale (ITS-90) and to the currently accepted atomic weight of 190.23 ± 0.03 (4).

    Low Temperature Solid Phase

    Selected values in the normal and superconducting states are based on the specific heat measurements of Okaz and Keesom (0.18 K to 4.2 K) (5) including a superconducting transition temperature of 0.638 ± 0.002 K, an electronic specific heat coefficient (γ) of 2.050 ± 0.003 mJ mol−1 K−2 and a limiting Debye temperature (ΘD) of 467 ± 6 K. Specific heat values up to 5 K in both the normal and superconducting states are given in Table I.

    Table I

    Low Temperature Specific Heat Data Up To 5 K

    Temperature, K Cºsa, mJ mol−1K−1 Cºnb, mJ mol−1K−1 Temperature, K Cºp, mJ mol−1 K−1
    0.2 0.093 0.410 1.0 2.07
    0.3 0.525 0.616 2.0 4.25
    0.4 1.19 0.821 3.0 6.67
    0.5 1.94 1.03 4.0 9.43
    0.6 2.79 1.23 5.0 12.7
    0.638 3.14 1.32

    Above 4 K selected specific heat values are initially based on the measurements by Naumov et al. (6 K to 316 K) (6). However above 280 K these measurements show an abrupt increase of 0.5 J mol−1 K−1 and a further abrupt increase of 0.3 J mol−1 K−1 above 300 K. Naumov et al. attempted to accommodate these values but the selected specific heat curve showed an unnatural sharp change in slope above 270 K. Therefore the selected values of Naumov et al. above 250 K were rejected and instead specific heat values to 298.15 K were obtained by joining smoothly with the high temperature enthalpy measurements of Ramanauskas et al. (7). In the original review of the low temperature data only the specific heat values were given consisting above 50 K of 10 K intervals to 100 K and then 20 K intervals above this temperature as well as the value at 298.15 K. This minimalist approach is now considered to be unsatisfactory and therefore comprehensive low temperature thermodynamic data are now given at 5 K intervals from 5 K to 50 K and at 10 K intervals above this temperature up to 290 K and then the value at 298.15 K as given in Table II.

    Table II

    Low Temperature Thermodynamic Data Above 5 K

    Temperature, K pa, J mol−1K−1 T – Hº0 Kb, J mol−1 Tc, J mol−1 K−1 −GºT – Hº0 Kd, J mol−1 −(GºT – Hº0 K)/Td, J mol−1 K−1
    5 0.0127 0.0286 0.0111 0.0266 0.00532
    10 0.0417 0.153 0.0272 0.119 0.0119
    15 0.116 0.519 0.0559 0.319 0.0213
    20 0.290 1.475 0.110 0.719 0.0360
    25 0.636 3.704 0.208 1.490 0.0596
    30 1.252 8.302 0.374 2.910 0.0970
    35 2.104 16.61 0.628 5.376 0.154
    40 3.139 29.65 0.975 9.346 0.234
    45 4.322 48.25 1.412 15.27 0.339
    50 5.604 73.03 1.933 23.60 0.472
    60 8.205 142.2 3.186 48.99 0.817
    70 10.563 236.2 4.631 87.96 1.257
    80 12.661 352.6 6.182 142.0 1.775
    90 14.448 488.4 7.780 211.8 2.353
    100 15.939 640.6 9.381 297.6 2.976
    110 17.182 806.4 10.961 399.3 3.630
    120 18.231 983.6 12.502 516.7 4.305
    130 19.132 1170 13.997 649.2 4.994
    140 19.912 1366 15.445 796.4 5.689
    150 20.577 1568 16.842 957.9 6.386
    160 21.085 1777 18.187 1133 7.082
    170 21.533 1990 19.479 1322 7.774
    180 21.975 2207 20.722 1523 8.459
    190 22.377 2429 21.921 1736 9.136
    200 22.695 2655 23.078 1961 9.804
    210 22.928 2883 24.191 2197 10.463
    220 23.178 3113 25.263 2445 11.111
    230 23.441 3346 26.928 2702 11.749
    240 23.715 3582 27.302 2970 12.377
    250 23.929 3820 28.275 3248 12.993
    260 24.119 4061 29.217 3536 13.599
    270 24.290 4303 30.130 3832 14.195
    280 24.444 4546 31.017 4138 14.780
    290 24.584 4791 31.877 4453 15.355
    298.15 24.688 4992 32.560 4715 15.816

    High Temperature Solid Phase

    In the high temperature region, after correction for temperature scale and atomic weight, the enthalpy measurements of Ramanauskas et al. (1155 K to 2961 K) (7) were fitted to the following equation with an overall accuracy of ± 200 J mol−1 (0.4%) (Equation (i)):

    (i)

    This equation was used to represent selected enthalpy values from 298.15 K to 3400 K. Equivalent specific heat and entropy equations corresponding to the above equation are given in Table III, the free energy equations in Table IV, transitions values associated with the free energy functions in Table V and derived thermodynamic values in Table VI. The actual equation given by Ramanauskas et al. to represent the enthalpy measurements over the experimental temperature range agrees with Equation (i) to within 0.2%.

    Table III

    Thermodynamic Equations Above 298.15 K

    Solid: 298.15 K to 3400 K
    pa, J mol−1 K−1 = 26.1938 + 2.64636 × 10−4 T + 1.15788 × 10−6 T2 + 1.599912 × 10−10 T3 – 150378/T2
    T – Hº298.15 Kb, J mol−1 = 26.1938 T + 1.32318 × 10−4 T2 + 3.85960 × 10−7 T3 + 3.99978 × 10−11 T4 + 150378/T – 8336.36
    Tc, J mol−1 K−1 = 26.1938 ln(T) + 2.64636 × 10−4 T + 5.78940 × 10−7 T2 + 5.33304 × 10−11 T3 + 75189/T2 – 117.6597
    Liquid: 3400 K to 5600 K
    pa, J mol−1 K−1 = 50.0000
    T – H298.15 Kb, J mol−1 = 50.0000 T + 816.2
    Tc, J mol−1 K−1 = 50.0000 ln(T) – 281.5442

    Table IV

    Free Energy Equations Above 298.15 K

    Solid: 298.15 K to 3400 K
    T – Hº298.15 Ka, J mol−1 = 143.8535 T – 1.32318 × 10−4 T2 – 1.92980 × 10−7 T3 – 1.33326 × 10−11 T4 + 75189/ T – 26.1938 T ln(T) – 8336.36
    Liquid: 3400 K to 5600 K
    T – Hº298.15 K, J mol−1 = 331.5442 T – 50.0000 T ln(T) + 816.2

    Table V

    Transition Values Involved with the Free Energy Equations

    Transition Temperature, K ΔHM, J mol−1 ΔSM, J mol−1 K−1
    Fusion 3400 68005.00 20.0014

    Table VI

    High Temperature Thermodynamic Data for the Condensed Phases

    Temperature, K pa, J mol−1 K−1 T – Hº298.15 Kb, J mol−1 Tc, J mol−1 K−1 −(GºT – Hº298.15 K)/Td, J mol−1 K−1
    298.15 24.688 0 32.560 32.560
    300 24.711 46 32.712 32.560
    400 25.555 2564 39.951 33.541
    500 26.034 5145 45.709 35.419
    600 26.386 7767 50.488 37.543
    700 26.694 10,421 54.579 39.692
    800 26.994 13,105 58.163 41.781
    900 27.301 15,820 61.360 43.782
    1000 27.626 18,566 64.253 45.687
    1100 27.975 21,346 66.902 47.497
    1200 28.351 24,162 69.352 49.217
    1300 28.757 27,017 71.637 50.855
    1400 29.196 29,914 73.784 52.417
    1500 29.669 32,857 75.814 53.909
    1600 30.178 35,849 77.745 55.339
    1700 30.724 38,894 79.591 56.712
    1800 31.308 41,996 81.363 58.033
    1900 31.932 45,157 83.073 59.306
    2000 32.597 48,383 84.727 60.536
    2100 33.303 51,678 86.335 61.726
    2200 34.053 55,045 87.902 62.880
    2300 34.846 58,490 89.432 64.002
    2400 35.684 62,016 90.933 65.093
    2500 36.568 65,628 92.407 66.156
    2600 37.499 69,331 93.859 67.193
    2700 38.478 73,130 95.293 68.208
    2800 39.506 77,028 96.710 69.200
    2900 40.583 81,032 98.115 70.173
    3000 41.712 85,147 99.510 71.128
    3100 42.892 89,377 100.897 72.066
    3200 44.125 93,727 102.278 72.988
    3300 45.412 98,203 103.655 73.897
    3400 (solid) 46.751 102,811 105.031 74.792
    3400 (liquid) 50.000 170,816 125.032 74.792
    3500 50.000 175,816 126.482 76.249
    3600 50.000 180,816 127.890 77.664
    3700 50.000 185,816 129.260 79.040
    3800 50.000 190,816 130.594 80.379
    3900 50.000 195,816 131.892 81.683
    4000 50.000 200,816 133.158 82.954
    4100 50.000 205,816 134.393 84.194
    4200 50.000 210,816 135.598 85.403
    4300 50.000 215,816 136.774 86.585
    4400 50.000 220,816 137.924 87.738
    4500 50.000 225,816 139.047 88.866
    4600 50.000 230,816 140.146 89.969
    4700 50.000 235,816 141.222 91.048
    4800 50.000 240,816 142.274 92.104
    4900 50.000 245,816 143.305 93.139
    5000 50.000 250,816 144.306 94.152
    5100 50.000 255,816 145.311 95.146
    5200 50.000 260,816 146.276 96.120
    5300 50.000 265,816 147.229 97.075
    5400 50.000 270,816 148.164 98.012
    5500 50.000 275,816 149.081 98.933
    5600 50.000 280,816 149.982 99.836

    The only other enthalpy measurements were obtained by Jaeger and Rosenbohm (693 K to 1877 K) (8) and compared to the selected values vary from 1.6% low at 693 K to an estimated 1.2% low at 1600 K to 1.4% low at 1877 K.

    Liquid Phase

    Selected values of the enthalpies and entropies of fusion of the Groups 8 to 10 elements with a close-packed structure are given in Table VII. Only the enthalpy of fusion of osmium is unknown. References (1014) represent the latest reviews on the thermodynamic properties of the pgms by the present author. From an evaluation of the entropies of fusion of the elements, Chekhovskoi and Kats (15) proposed that the entropy of fusion (ΔSºM) and the melting point (TM) could be related by the equation ΔSºM = A TM + B. In the previous review (1) different values were proposed for the entropies of fusion of palladium (8.80 J mol−1 K−1) and platinum (10.45 J mol−1 K−1) leading to an estimate of the entropy of fusion for osmium of 20.6 J mol−1 K−1. With the revised values it is clear that, although of the right order, the entropy of fusion of nickel is discrepant and has therefore been disregarded. The other six values were fitted to the equation with A = 6.6954 × 10−3 and B = −2.7630 and a standard deviation of the fit of ± 0.193 J mol−1 K−1. However in order that the derived entropy of fusion of osmium has a similar accuracy to those of the input values then the accuracy is expanded to a 95% confidence level leading to an entropy of fusion of 20.0014 ± 0.387 J mol−1 K−1 and based on a melting point 3400 ± 50 K to an enthalpy of fusion of 68,005 ± 1653 J mol−1. Based on neighbouring elements then a liquid specific heat of 50 J mol−1 K−1 was proposed in the original paper (1) and therefore the enthalpy of liquid osmium can now be expressed as Equation (ii):

    (ii)

    Table VII

    Enthalpies and Entropies of Fusion for the Groups 8 to 10 Elements

    Element Melting point, K Enthalpy of fusion, J mol−1 Entropy of fusion, J mol−1 K−1 Reference
    Cobalt 1768 16056 ± 369 9.08 ± 0.21 (9)
    Nickel 1728 17042 ± 376 9.86 ± 0.22 (9)
    Ruthenium 2606 39040 ± 1400 14.98 ± 0.54 (10)
    Rhodium 2236 27295 ± 850 12.21 ± 0.38 (11)
    Palladium 1828.0 17340 ± 730 9.48 ± 0.40 (12)
    Iridium 2719 41335 ± 1128 15.20 ± 0.41 (13)
    Platinum 2041.3 22110 ± 940 10.83 ± 0.46 (14)

    Equivalent specific heat and entropy equations corresponding to the above equation are given in Table III, the free energy equation in Table IV and derived thermodynamic values in Table VI. It should now be possible to accurately determine the melting point and enthalpy of fusion of osmium since the metal is available in high purity in a coherent form whilst the enthalpies of fusion of other high melting point elements such as rhenium (3458 K) and tungsten (3687 K) have been successfully determined.

    Gas Phase

    Based on a standard state pressure of 1 bar the thermodynamic properties of the monatomic gas were calculated from the 295 energy levels listed by Van Kleef and Klinkenberg (16) and Gluck et al. (17) using the method outlined by Kolsky et al. (18) together with the 2018 Fundamental Constants (19). Derived thermodynamic values are given in Table VIII.

    Table VIII

    Thermodynamic Properties of the Gaseous Phase

    Temperature, K pa, J mol−1 K−1 T – Hº298.15 Kb, J mol−1 Tc, J mol−1 K−1 −(GºT – Hº298.15 K)/ Td, J mol−1 K−1
    298.15 20.788 0 192.579 192.579
    300 20.788 38 192.707 192.579
    400 20.810 2118 198.689 193.394
    500 20.901 4203 203.341 194.936
    600 21.102 6302 207.168 196.665
    700 21.432 8428 210.444 198.404
    800 21.887 10,592 213.334 200.093
    900 22.453 12,809 215.944 201.712
    1000 23.104 15,086 218.342 203.256
    1100 23.812 27,431 220.577 204.731
    1200 24.545 29,849 222.680 206.140
    1300 25.278 22,340 224.674 207.489
    1400 25.988 24,904 226.574 208.785
    1500 26.659 27,537 228.390 210.032
    1600 27.283 30,234 230.130 211.234
    1700 27.854 32,991 231.802 212.395
    1800 28.374 35,803 233.409 213.518
    1900 28.844 38,665 234.956 214.606
    2000 29.269 41,571 236.446 215.661
    2100 29.656 44,517 237.884 216.685
    2200 30.009 47,501 239.272 217.681
    2300 30.337 50,518 240.613 218.649
    2400 30.642 53,567 241.911 219.591
    2500 30.931 56,646 243.167 220.509
    2600 31.207 59,753 244.386 221.404
    2700 31.473 62,887 245.569 222.277
    2800 31.732 66,047 246.718 223.130
    2900 31.986 69,233 247.836 223.962
    3000 32.234 72,444 248.925 224.776
    3100 32.480 75,680 249.986 225.573
    3200 32.722 78,940 251.021 226.352
    3300 32.961 82,224 252.031 227.115
    3400 33.197 85,532 253.019 227.862
    3500 33.430 88,864 253.984 228.595
    3600 33.660 92,218 254.929 229.313
    3700 33.885 95,596 255.855 230.018
    3800 34.107 98,995 256.761 230.710
    3900 34.323 102,417 257.650 231.389
    4000 34.535 105,860 258.522 232.057
    4100 34.742 109,324 259.377 232.713
    4200 34.943 112,808 260.217 233.357
    4300 35.138 116,312 261.041 233.992
    4400 35.327 119,835 261.851 234.616
    4500 35.510 123,377 262.647 235.230
    4600 35.687 126,937 263.429 235.834
    4700 35.858 130,514 264.199 236.430
    4800 36.023 134,108 264.956 237.016
    4900 36.182 137,719 265.700 237.594
    5000 36.325 141,345 266.432 238.164
    5100 36.483 144,986 267.153 238.725
    5200 36.625 148,641 267.863 239.278
    5300 36.762 152,311 268.562 239.824
    5400 36.895 155,993 269.251 240.363
    5500 37.022 159,689 269.929 240.894
    5600 37.145 163,398 270.597 241.419

    Enthalpy of Sublimation

    No temperature scales were given with the measurements of the vapour pressures by Panish and Reif (20) and Carrera et al. (21). Normally the experimental temperature values would therefore be accepted but in the case of such values above 2000 K the difference from the current scale, ITS‐90, becomes significant. Since the measurements were carried out in 1962 and 1964 then they would ultimately be associated with the International Practical Temperature Scale (IPTS-1948) and were therefore corrected to the ITS-90 scale on this basis. Derived enthalpies of sublimation are given in Table IX. The selected enthalpy of sublimation of 788 ± 4 kJ mol−1 is basically an unweighted average but slightly biased towards the measurements of Carrera et al. (21).

    Table IX

    Enthalpies of Sublimation at 298.15 K

    Authors Reference Methoda Temperature range, Kb ΔHº298.15 K (II)c, kJ mol−1 ΔHº298.15 K (III)c, kJ mol−1
    Panish and Reif (19) L 2376–2718 807 ± 35 784.3 ± 1.3
    Carrera et al. (20) L 2159–2595 773 ± 13 790.7 ± 0.7
    Selected 788 ± 4

    Vapour Pressure Equations

    The vapour pressure equations are given in Table X. For the solid the evaluation was for free energy functions for the solid and the gas at 50 K intervals from 1700 K to 3400 K and for the liquid at 50 K intervals from 3400 K to 5600 K and were fitted to Equation (iii):

    (iii)

    Table X

    Vapour Pressure Equationsa

    Phase Temperature range, K A B C D E
    Solid 1700–3400 26.82612 −1.17464 −95030.60 5.68917 × 10−4 −6.25849 × 10−8
    Liquid 3400–5600 45.02206 −3.41958 −93542.51 2.64385 × 10−4 −5.78416 × 10−9

    A review of the vapour pressure data is given in Table XI.

    Table XI

    Vapour Pressure

    Temperature, K Pressure, bar ΔGºTa, J mol−1 ΔHºTb, J mol−1 Pressure, bar Temperature, K
    298.15 2.03 × 10−130 740,290 788,000 10−15 1780
    300 1.44 × 10−129 739,994 787,992 10−14 1861
    400 2.81 × 10−95 724,059 787,554 10−13 1950
    500 1.03 × 10−74 708,242 787,058 10−12 2048
    600 5.14 × 10−61 692,527 786,535 10−11 2156
    700 3.09 × 10−51 676,901 786,007 10−10 2277
    800 6.59 × 10−44 661,350 785,487 10−9 2411
    900 3.28 × 10−38 645,863 784,989 10−8 2563
    1000 1.18 × 10−33 630,430 784,520 10−7 2736
    1100 6.23 × 10−30 615,043 784,085 10−6 2934
    1200 7.88 × 10−27 599,693 783,687 10−5 3163
    1300 3.31 × 10−24 584,375 783,323 10−4 3435
    1400 5.86 × 10−22 569,084 782,990 10−3 3792
    1500 5.19 × 10−20 553,816 782,680 10−2 4235
    1600 2.62 × 10−18 538,568 782,385 10−1 4804
    1700 8.32 × 10−17 523,338 782,097 1 5559.70
    1800 1.80 × 10−15 508,126 781,807 NBPc 5564.74
    1900 2.81 × 10−14 492,929 781,508
    2000 3.33 × 10−13 477,749 781,188
    2100 3.12 × 10−12 462,586 780,839
    2200 2.38 × 10−11 447,439 780,456
    2300 1.52 × 10−10 432,312 780,028
    2400 8.32 × 10−10 417,204 779,551
    2500 3.97 × 10−9 402,117 779,018
    2600 1.68 × 10−8 387,052 778,422
    2700 6.36 × 10−8 372,012 777,757
    2800 2.19 × 10−7 356,998 777,019
    2900 6.92 × 10−7 342,011 776,201
    3000 2.02 × 10−6 327,054 775,297
    3100 5.51 × 10−6 312,129 774,303
    3200 1.41 × 10−5 297,237 773,213
    3300 3.39 × 10−5 282,381 772,021
    3400 (solid) 7.75 × 10−5 267,563 770,721
    3400 (liquid) 7.75 × 10−5 267,563 702,716
    3500 1.58 × 10−4 254,788 701,048
    3600 3.08 × 10−4 242,061 699,402
    3700 5.78 × 10−4 229,380 697,780
    3800 1.05 × 10−3 216,742 696,179
    3900 1.84 × 10−3 204,146 694,601
    4000 3.15 × 10−3 191,590 693,044
    4100 5.23 × 10−3 179,073 691,508
    4200 8.48 × 10−3 166,593 689,992
    4300 1.34 × 10−2 154,148 688,496
    4400 2.08 × 10−2 141,739 687,019
    4500 3.15 × 10−2 129,363 685,561
    4600 4.69 × 10−2 117,018 684,121
    4700 6.84 × 10−2 104,706 682,698
    4800 9.87 × 10−2 92,422 681,292
    4900 0.140 80,169 679,903
    5000 0.195 67,943 678,529
    5100 0.269 55,745 677,170
    5200 0.365 43,574 675,820
    5300 0.490 31,428 674,495
    5400 0.651 19,307 673,177
    5500 0.854 7,210 671,873
    5559.70 1.000 0 671,100
    5600 1.110 −4,863 670,582

    Discussion of Alternative Estimates of the Enthalpy of Fusion of Osmium

    Based on various assumptions Fokin et al. (22) proposed that the enthalpy of fusion for osmium was only in the range 30 kJ mol−1 to 40 kJ mol−1 or half of the above derived value. One of the main arguments was that by using the Chekhovskoi-Kats equation the entropy of fusion for rhenium was estimated to be 20.0 J mol−1 K−1 whereas the actual value is only 9.85 J mol−1 K−1 (23) and therefore if the estimate for rhenium was so completely wrong then it would also be possible that the estimate for the neighbouring element osmium at 19.0 J mol−1 K−1 could also be wrong. However, Fokin et al. completely misunderstood how the estimated values were arrived at. It was initially assumed that Group 7 rhenium would behave like Groups 8 to 10 (the pgms) whereas all that the experimental value proved was that Group 7 elements behaved completely independently of Groups 8 to 10 and therefore showed the same deviations as other transition metal groups. For example, the entropies of fusion of Group 5 elements vanadium, niobium and tantalum at 10.46 J mol−1 K−1, 11.13 J mol−1 K−1 and 10.25 J mol−1 K−1 (24) showed no trend with temperature whilst the entropies of fusion of the Group 6 elements chromium, molybdenum and tungsten at 13.89 J mol−1 K−1, 13.53 J mol−1 K−1 and 13.66 J mol−1 K−1 (24) were virtually identical. Therefore it would not be surprising if Group 7 elements would also behave completely independently. In fact for the transition metals only the Groups 8 to 10 elements showed a high degree of correlation with the Chekhovskoi-Kats equation. However in order to prove their point that osmium does behave differently to the other pgms, Fokin et al. used the equation: σM = Z ΔHM ρSM d where σM is the surface tension at the melting point, ΔHM is the enthalpy of fusion, ρSM is the density of the solid at the melting point and d is the interatomic distance. This equation was applied to a number of elements but there is virtually no correlation for the values of Z with values varying between 1.2 to 3.3. For osmium Fokin et al. selected an arbitrary rounded value of Z = 2 for osmium and values of surface tension and liquid density determined by Paradis et al. (25) to arrive at an enthalpy of fusion of only 32 kJ mol−1 which is considerably less than the value of 39.0 ± 1.4 kJ mol−1 (9) selected for the analogue element ruthenium whereas for the other pgms the enthalpy of fusion is always greater for the heavier analogue. This much lower value for the enthalpy of fusion would suggest that the thermal properties of osmium should then be distinct from those of the other pgms but this is not the case. For example, the specific heat values of ruthenium (10) and osmium at reduced temperature (T/TM) as indicated in Figure 1 are very similar and show virtually the same behaviour suggesting that they are genuine analogues of each other whilst the extrapolated melting point of osmium obtained by applying the same incremental difference as between iridium and platinum agrees closely with the selected value and again suggesting a common Groups 8 to 10 behaviour.

    Fig. 1

    The specific heat values of ruthenium and osmium at reduced temperature (T/TM)

    The specific heat values of ruthenium and osmium at reduced temperature (T/TM)

    Further, the chemical properties of ruthenium and osmium are virtually identical forming the same type of compounds with similar properties. These are examples where osmium behaves exactly like the other pgms and on these grounds it is suggested that the very low value for the enthalpy of fusion as suggested by Fokin et al. is inconsistent with this behaviour and that osmium would obey the same periodic trend as suggested by the other pgms and that its entropy of fusion can be determined by the Chekhovskoi-Kats equation. This would suggest anomalies in the input values selected by Fokin et al., especially in the selection of Z = 2 for osmium since the value for the analogue ruthenium is only 1.5 whilst the value for the neighbouring element iridium is only 1.2 where the selection of such values would lead to higher enthalpies of fusion for osmium. It is suggested that in view of the lack of any real correlation for Z that the value for osmium may well be independent and could even be 1.0 leading to an enthalpy of fusion similar to that obtained from the Chekhovskoi-Kats equation. Therefore until the actual enthalpy of fusion of osmium is determined it is assumed that it behaves as a normal Groups 8 to 10 element.

    Conclusions

    Estimated entropy and enthalpy values of fusion of osmium have been revised leading to corrections of the thermodynamic properties of the liquid phase and therefore to the vapour pressure curve above the melting point. The revisions are based on the assumption that osmium behaves as a normal Group 8 to 10 element and contradicts recent suggestions that its behaviour could be abnormal.

  • 1.
  • 2.
  • 3.
  • 4.
  • 5.
  • 6.

    V. N. Naumov, I. E. Paukov, G. Ramanauskas and V. Ya. Chekhovskoi, Zh. Fiz. Khim., 1988, 62, (1), 25, translated into English in Russ. J. Phys. Chem., 1988, 62, (1), 12

  • 7.

    G. Ramanauskas, V. D. Tarasov, V. Ya. Chekhovskoi, N. L. Korenovskii and V. P. Polyakova, Vysokochist. Veshchestva., 1988, (4), 149, in Russian

  • 8.

    F. M. Jaeger and E. Rosenbohm, Proc. R. Acad. Amsterdam, 1931, 34, (1), 85

  • 9.
  • 10.
  • 11.
  • 12.
  • 13.
  • 14.
  • 15.

    V. Ya. Chekhovskoi and S. A. Kats, High Temp.–High Pressures, 1981, 13, (6), 611

  • 16.
  • 17.
  • 18.

    H. G. Kolsky, R. M. Gilmer and P. W. Gilles, “The Thermodynamic Properties of 54 Elements Considered as Ideal Monatomic Gases”, LA 2110, US Atomic Energy Commission, Washington, USA, 15th March, 1957, 138 pp

  • 19.
    E. Tiesinga, P. J. Mohr, D. B. Newell and B. N. Taylor, ‘The CODATA Internationally Recommended 2018 Values of the Fundamental Physical Constants’, NIST Standard Reference Database 121, Version 8.0, National Institute of Standards and Technology, Gaithersburg, USA, May, 2019 LINK https://physics.nist.gov/cuu/Constants/index.html
  • 20.
  • 21.
  • 22.
  • 23.
  • 24.
  • 25.
  • By |2020-11-26T12:54:40+00:00November 26th, 2020|Weld Engineering Services|Comments Off on A Re-assessment of the Thermodynamic Properties of Osmium

    Professor Robert D. Gillard: Transition Metal Chemist 1936–2013: Part II


    Professor Robert D. Gillard: Transition Metal Chemist 1936–2013: Part II | Johnson Matthey Technology Review















    Johnson Matthey Technol. Rev., 2021, 65, (1), 23

    doi:10.1595/205651320×15864407040223

    Professor Robert D. Gillard: Transition Metal Chemist 1936–2013: Part II

    From the University of Cardiff to retirement interests and scientific legacy

    • John Burgess
    • Department of Chemistry, University of Leicester, Leicester LE1 7RH, UK
    • Martyn V. Twigg*
    • Twigg Scientific & Technical Ltd, Caxton, Cambridge CB23 3PQ, UK
    SHARE THIS PAGE:

    Article Synopsis

    The second part of this commemoration covers the final stage of Robert Gillard’s career as Professor of Inorganic Chemistry at Cardiff University and his time in retirement. At Cardiff he built on earlier work while extending his scientific interests still further into mineralogical and archaeological chemistry, and even into forensic dentistry. Coordination chemistry research continued and included the polysulfide S5 chain as a bidentate ligand in the all-inorganic cyclic PtS5 unit and the rhodium(III) complex [Rh(S5)3]3–. His penchant for discussion led him into several controversies, particularly over his ‘covalent hydration’ hypothesis of coordinated nitrogen-carbon double bonds in metal complexes which included those with platinum and 2,2’-bipyridine. He travelled widely attending international conferences and giving lectures. Research collaborations continued throughout his time at Cardiff and in particular he had many strong links with Portugal, both with colleagues there and as supervisor of Portuguese higher degree students at Cardiff. His years in retirement were spent in finalising his research legacy, in continuing to read historical literature, both chemical and otherwise, and in following his musical interests that had included many years singing in the Cwmbach Male Voice Choir

    **The complete article is available by downloading the PDF. Full text HTML is coming soon!**

    BACK TO TOP

    View Part I to download the Supplementary Information

    Read more from this issue »

    BACK TO TOP

    SHARE THIS PAGE:


    By |2020-10-20T15:47:27+00:00October 20th, 2020|Weld Engineering Services|Comments Off on Professor Robert D. Gillard: Transition Metal Chemist 1936–2013: Part II

    Professor Robert D. Gillard: Transition Metal Chemist 1936–2013: Part I


    Professor Robert D. Gillard: Transition Metal Chemist 1936–2013: Part I | Johnson Matthey Technology Review















    Johnson Matthey Technol. Rev., 2021, 65, (1), 4

    doi:10.1595/205651320×15864407040160

    Professor Robert D. Gillard: Transition Metal Chemist 1936–2013: Part I

    From early life to the University of Kent at Canterbury

    • John Burgess
    • Department of Chemistry, University of Leicester, Leicester LE1 7RH, UK
    • Martyn V. Twigg*
    • Twigg Scientific & Technical Ltd, Caxton, Cambridge CB23 3PQ, UK
    SHARE THIS PAGE:

    Article Synopsis

    This first part of a two-part commemoration of the life and work of Robert D. Gillard begins with a biographical outline which provides a context for his chemical achievements. He was awarded a State Scholarship and after his National Service in the Royal Air Force he went up to St Edmund Hall, Oxford, to read Chemistry. There follows a chronological account of his career in Chemistry starting with his undergraduate days in Oxford, where a Part II project with Dr Harry Irving on alkaline earth and cobalt complexes proved seminal. His PhD research at Imperial College, London in the Geoffrey Wilkinson group broadened his experience into the then poorly developed chemistry of rhodium and other platinum group metal complexes. Gillard next went to Sheffield University as a Lecturer where he developed independent research while continuing to work on earlier topics. There followed a move to Canterbury as a Reader at the University of Kent. In his particularly productive seven years there with a large research group he widened his experience further, expanding his interests in such areas as the optical properties of transition metal complexes, considering biological and medical relevance, and increasing the range of metals and ligands he investigated. His subsequent time at Cardiff and then into retirement will be covered in the second part of this commemoration.

    **The complete article is available by downloading the PDF. Full text HTML is coming soon!**

    BACK TO TOP

    Download the Supplementary Information (PDF, 394 KB)

    Read more from this issue »

    BACK TO TOP

    SHARE THIS PAGE:


    By |2020-10-20T15:02:14+00:00October 20th, 2020|Weld Engineering Services|Comments Off on Professor Robert D. Gillard: Transition Metal Chemist 1936–2013: Part I
    Go to Top