Influence of the palladium coating on the hydrogen embrittlement of Ni61Nb33Zr6 amorphous tapes obtained by melt spinning

G. Thalmaier, I. Vida-Simiti, N. Sechel
{"title":"Influence of the palladium coating on the hydrogen embrittlement of Ni61Nb33Zr6 amorphous tapes obtained by melt spinning","authors":"G. Thalmaier, I. Vida-Simiti, N. Sechel","doi":"10.21741/9781945291999-10","DOIUrl":null,"url":null,"abstract":"The current work is focused towards the properties of Ni61Nb33Zr6 amorphous alloy for use in hydrogen-related energy applications. The master alloys were prepared by arc melting using high purity metals in a Ti-gettered argon atmosphere. The alloys were melted several times to improve homogeneity. The ingots were induction-melted under a argon atmosphere in a quartz tube and a graphite crucible, injected through a nozzle onto a Cu wheel to produce rapidly solidified amorphous ribbons. The characterization of the amorphous ribbons was done by X-ray diffraction, DSC analysis and hardness tests. The hydrogen charging was done electrochemically for low temperature tests and by heating in a hydrogen atmosphere at different temperatures in the case of the high temperature tests. It was found that the palladium plating reduces the hydrogen embrittlement limit by 50 °C. Introduction The amorphous alloys have been proposed for hydrogen separation membranes, because amorphous alloys absorb generally hydrogen without forming metallic hydride and show good mechanical properties. However, since amorphous alloys are thermally unstable, using them as dense, hydrogen permeation membrane at elevated temperatures is very hard. Maintaining an amorphous alloy close to its glass transition temperature will trigger crystallization, decrease of the hydrogen permeability and ultimately its mechanical failure. From this point of view it at utmost importance to have a Tg as high as possible. Generally, Ni-Nb amorphous alloys have high Tx [1] and according to Inoue [2] it could be further improved by adding more elements to the alloy. Zirconium on the other hand has excellent hydrogen permeability and in general improves the glass forming ability of the alloys [3]. On the other hand, increasing the zirconium content will lead to the reduction of the Tg, so, an optimal balance of these two issues must be found. Different nickel niobium alloys are studied [4, 5] which could be used as a separation membrane. The studied alloy has a supercooled liquid region of ~ 50K, which would allow it to be shaped by hot-pressing in this temperature range. The purpose of this paper is to evaluate hydrogel embrittlement behavior of the amorphous Ni61Nb33Zr6 alloy and identifying a temperature range in which the alloy could be used as the hydrogen separation membrane from this point of view. Experimental The master alloy (Ni61Nb33Zr6 ) was prepared by arc melting using high purity materials in a Tigettered argon atmosphere. The alloys were melted several times in order to improve homogeneity. The alloy ingot was induction-melted under a high-purity argon atmosphere in a quartz crucible and injected through a nozzle onto a rotating Cu wheel to produce amorphous Powder Metallurgy and Advanced Materials – RoPM&AM 2017 Materials Research Forum LLC Materials Research Proceedings 8 (2018) 89-94 doi: http://dx.doi.org/10.21741/9781945291999-10 90 tapes. The obtained tapes were 4 mm wide and approximately 50 μm thick. The rotation speed used during the present experiments was 32 m/s. The amorphous nature of the ribbons was investigated by X-ray diffraction using a Shimadzu XRD – 6000 diffractometer and CuKα1 radiation. The samples behavior on heating was investigated by differential scanning calorimetry (SETARAM Labsys system) at the heating rate of 40 K/min. The ultimate tensile strength of the tapes was estimated from the Vickers micro-hardness measurements (40 gf. applied for 15 seconds) as UTS = HV*10/3 [MPa]. The palladium layer was deposited by thermal evaporation in a base pressure of 5*10 torr. The hydrogen embrittlement behavior was studied by heating the palladium coated and uncoated samples in flowing hydrogen to different temperatures (250°C, 300°C, 350°C, 400°C, 450°C, 500°C, 540°C and 580°C). Heating to higher temperatures would result in the crystallization of the tapes. The critical bending strain was determined by measuring the radius of curvature at which fracture occurs in a bending test between two parallel plates. The strain is then calculated using the following equation: = t 2r−t ∙ 100 [%] , where r is the bending radius and t is the sample thickness. Results and discussions The amorphous structure of the sample is confined by XRD measurement. The X-ray diffraction pattern shown in Fig. 1a presents a broad maximum (FWHM = 6.3°) characteristic for glassy structures. Fig. 1. X-ray diffraction pattern (a) and DSC curve (b) of the as cast tapes. DSC measurements were performed to determine the thermal transformations that took place in the material and to approximate the thermal stability. The DSC heating curve of an amorphous material presents certain critical temperatures such as: glass transition temperature (Tg), crystallization temperatures (TX and TP) and melting temperature (TS and T1). The amorphous material remains in vitreous state until the TX temperature is reached. The crystallization of the amorphous material is indicated by the presence of exothermic peaks, their number depending on the number of crystallization steps through which the material undergoes. The DSC curve presented in Fig. 1b, shows at 420 °C a structural relaxation followed by a glass transition (Tg at 601 ° C and two crystallization steps (Tx1= 638 °C and Tx2= 702 °C). From the combined analysis we can conclude that these tapes are x-ray amorphous structures. Powder Metallurgy and Advanced Materials – RoPM&AM 2017 Materials Research Forum LLC Materials Research Proceedings 8 (2018) 89-94 doi: http://dx.doi.org/10.21741/9781945291999-10 91 Another advantage of the amorphous structure is the outstanding mechanical properties. Although not as precise, the ultimate tensile strength evaluation from the hardness measurements is a simple and strait forward way to go since even if the samples are prepared by grinding and polishing, there will still remain edges on the margins that act as tension concentrators, leading to an erroneous measurement. In table 1 the microhardness measured using the Vickers method is summarized. Table 1. Microhardness and estimated UTS of the selected tape. HV0.04/15 [daN/mm] Rm","PeriodicalId":20390,"journal":{"name":"Powder Metallurgy and Advanced Materials","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2018-11-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Powder Metallurgy and Advanced Materials","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.21741/9781945291999-10","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
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Abstract

The current work is focused towards the properties of Ni61Nb33Zr6 amorphous alloy for use in hydrogen-related energy applications. The master alloys were prepared by arc melting using high purity metals in a Ti-gettered argon atmosphere. The alloys were melted several times to improve homogeneity. The ingots were induction-melted under a argon atmosphere in a quartz tube and a graphite crucible, injected through a nozzle onto a Cu wheel to produce rapidly solidified amorphous ribbons. The characterization of the amorphous ribbons was done by X-ray diffraction, DSC analysis and hardness tests. The hydrogen charging was done electrochemically for low temperature tests and by heating in a hydrogen atmosphere at different temperatures in the case of the high temperature tests. It was found that the palladium plating reduces the hydrogen embrittlement limit by 50 °C. Introduction The amorphous alloys have been proposed for hydrogen separation membranes, because amorphous alloys absorb generally hydrogen without forming metallic hydride and show good mechanical properties. However, since amorphous alloys are thermally unstable, using them as dense, hydrogen permeation membrane at elevated temperatures is very hard. Maintaining an amorphous alloy close to its glass transition temperature will trigger crystallization, decrease of the hydrogen permeability and ultimately its mechanical failure. From this point of view it at utmost importance to have a Tg as high as possible. Generally, Ni-Nb amorphous alloys have high Tx [1] and according to Inoue [2] it could be further improved by adding more elements to the alloy. Zirconium on the other hand has excellent hydrogen permeability and in general improves the glass forming ability of the alloys [3]. On the other hand, increasing the zirconium content will lead to the reduction of the Tg, so, an optimal balance of these two issues must be found. Different nickel niobium alloys are studied [4, 5] which could be used as a separation membrane. The studied alloy has a supercooled liquid region of ~ 50K, which would allow it to be shaped by hot-pressing in this temperature range. The purpose of this paper is to evaluate hydrogel embrittlement behavior of the amorphous Ni61Nb33Zr6 alloy and identifying a temperature range in which the alloy could be used as the hydrogen separation membrane from this point of view. Experimental The master alloy (Ni61Nb33Zr6 ) was prepared by arc melting using high purity materials in a Tigettered argon atmosphere. The alloys were melted several times in order to improve homogeneity. The alloy ingot was induction-melted under a high-purity argon atmosphere in a quartz crucible and injected through a nozzle onto a rotating Cu wheel to produce amorphous Powder Metallurgy and Advanced Materials – RoPM&AM 2017 Materials Research Forum LLC Materials Research Proceedings 8 (2018) 89-94 doi: http://dx.doi.org/10.21741/9781945291999-10 90 tapes. The obtained tapes were 4 mm wide and approximately 50 μm thick. The rotation speed used during the present experiments was 32 m/s. The amorphous nature of the ribbons was investigated by X-ray diffraction using a Shimadzu XRD – 6000 diffractometer and CuKα1 radiation. The samples behavior on heating was investigated by differential scanning calorimetry (SETARAM Labsys system) at the heating rate of 40 K/min. The ultimate tensile strength of the tapes was estimated from the Vickers micro-hardness measurements (40 gf. applied for 15 seconds) as UTS = HV*10/3 [MPa]. The palladium layer was deposited by thermal evaporation in a base pressure of 5*10 torr. The hydrogen embrittlement behavior was studied by heating the palladium coated and uncoated samples in flowing hydrogen to different temperatures (250°C, 300°C, 350°C, 400°C, 450°C, 500°C, 540°C and 580°C). Heating to higher temperatures would result in the crystallization of the tapes. The critical bending strain was determined by measuring the radius of curvature at which fracture occurs in a bending test between two parallel plates. The strain is then calculated using the following equation: = t 2r−t ∙ 100 [%] , where r is the bending radius and t is the sample thickness. Results and discussions The amorphous structure of the sample is confined by XRD measurement. The X-ray diffraction pattern shown in Fig. 1a presents a broad maximum (FWHM = 6.3°) characteristic for glassy structures. Fig. 1. X-ray diffraction pattern (a) and DSC curve (b) of the as cast tapes. DSC measurements were performed to determine the thermal transformations that took place in the material and to approximate the thermal stability. The DSC heating curve of an amorphous material presents certain critical temperatures such as: glass transition temperature (Tg), crystallization temperatures (TX and TP) and melting temperature (TS and T1). The amorphous material remains in vitreous state until the TX temperature is reached. The crystallization of the amorphous material is indicated by the presence of exothermic peaks, their number depending on the number of crystallization steps through which the material undergoes. The DSC curve presented in Fig. 1b, shows at 420 °C a structural relaxation followed by a glass transition (Tg at 601 ° C and two crystallization steps (Tx1= 638 °C and Tx2= 702 °C). From the combined analysis we can conclude that these tapes are x-ray amorphous structures. Powder Metallurgy and Advanced Materials – RoPM&AM 2017 Materials Research Forum LLC Materials Research Proceedings 8 (2018) 89-94 doi: http://dx.doi.org/10.21741/9781945291999-10 91 Another advantage of the amorphous structure is the outstanding mechanical properties. Although not as precise, the ultimate tensile strength evaluation from the hardness measurements is a simple and strait forward way to go since even if the samples are prepared by grinding and polishing, there will still remain edges on the margins that act as tension concentrators, leading to an erroneous measurement. In table 1 the microhardness measured using the Vickers method is summarized. Table 1. Microhardness and estimated UTS of the selected tape. HV0.04/15 [daN/mm] Rm
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钯涂层对熔体纺丝Ni61Nb33Zr6非晶带氢脆的影响
目前的工作重点是Ni61Nb33Zr6非晶合金在氢相关能源应用中的性能。采用高纯度金属在含钛氩气气氛中弧熔法制备了中间合金。合金经过多次熔化以改善均匀性。在石英管和石墨坩埚中,在氩气气氛下感应熔化铸锭,通过喷嘴注入铜轮,以产生快速凝固的非晶态带。通过x射线衍射、DSC分析和硬度测试对非晶带进行了表征。氢气充注是在低温试验中用电化学方法进行的,在高温试验中用不同温度的氢气气氛加热。结果表明,镀钯使合金的氢脆极限降低了50℃。由于非晶合金一般能吸收氢而不形成金属氢化物,且具有良好的力学性能,因此提出用非晶合金作为氢分离膜材料。然而,由于非晶合金热不稳定,在高温下使用它们作为致密的氢透膜是非常困难的。保持非晶合金接近其玻璃化转变温度会引发结晶,降低氢渗透率,最终导致其机械失效。从这个角度来看,Tg越高越重要。一般来说,Ni-Nb非晶合金具有较高的Tx[1],根据Inoue[2],可以通过在合金中添加更多的元素来进一步提高Tx。另一方面,锆具有优异的透氢性,总体上提高了合金的玻璃化形成能力[3]。另一方面,锆含量的增加会导致Tg的降低,因此,必须找到这两个问题的最佳平衡。研究了不同的镍铌合金[4,5]作为分离膜。所研究的合金具有~ 50K的过冷液体区,这将允许在该温度范围内通过热压成形。本文的目的是评价非晶Ni61Nb33Zr6合金的水凝胶脆化行为,并从这个角度确定该合金可以用作氢分离膜的温度范围。实验以高纯度材料为原料,在tigeti氩气气氛中采用电弧熔炼法制备了中间合金Ni61Nb33Zr6。合金经过多次熔化以改善均匀性。合金锭在石英坩埚中高纯度氩气气氛下感应熔化,并通过喷嘴注入旋转的铜轮上,以生产非晶粉末冶金和先进材料- RoPM&AM 2017材料研究论坛LLC材料研究论文集8 (2018)89-94 doi: http://dx.doi.org/10.21741/9781945291999-10 90 tapes。得到的磁带宽4mm,厚约50 μm。本实验中使用的旋转速度为32米/秒。采用岛津XRD - 6000衍射仪和CuKα1辐射对带的无定形性质进行了研究。采用差示扫描量热仪(SETARAM Labsys系统)在40 K/min的加热速率下研究样品的加热行为。胶带的极限抗拉强度由维氏显微硬度测量(40gf)估算。施加15秒),UTS = HV*10/3 [MPa]。在5*10 torr的基压下热蒸发沉积钯层。通过在不同温度(250℃、300℃、350℃、400℃、450℃、500℃、540℃和580℃)下加热钯包覆和未包覆样品,研究了氢脆行为。加热到更高的温度会导致磁带结晶。临界弯曲应变是通过测量两个平行板在弯曲试验中发生断裂的曲率半径来确定的。然后用如下公式计算应变:= t 2r−t∙100[%],其中r为弯曲半径,t为试样厚度。结果与讨论用XRD测定样品的非晶态结构。图1a所示的x射线衍射图显示出玻璃结构的最大宽(FWHM = 6.3°)特征。图1所示。铸带的x射线衍射图(a)和DSC曲线(b)。进行DSC测量以确定材料中发生的热转变并近似计算热稳定性。非晶材料的DSC加热曲线呈现出一定的临界温度,如:玻璃化转变温度(Tg)、结晶温度(TX和TP)和熔融温度(TS和T1)。在达到TX温度之前,非晶态材料保持玻璃态。
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