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Studies on Notch Tensile Properties of Ti-5Al-2.5Sn ELI at Cryogenic Temperature for Hydrogen Embrittlement Effect

机译:氢气脆性效应低温温度下Ti-5A2.5SN ELI的缺口拉伸性能研究

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Ti-5Al-2.5Sn alloy is widely used in aerospace applications due to its high specific strength, low coefficient of thermal expansion and good corrosion resistance. Presence of interstitial elements in the alloy has some significant effects on its properties. However the high notch toughness and cryogenic ductility attracts the usage of Ti-5Al-2.5Sn for usage at cryogenic temperatures even at 20K. For hydrogen embrittlement studies and for investigating notch sensitivity of Ti-5Al-2.5Sn alloy, the notched and smooth specimens from ELI grade of Ti-5Al-2.5Sn alloy were subjected to LH2 exposure and tensile test at 20K (-253°C) and at 77K (-196°C). The tensile properties obtained from different specimens were compared and analyzed. Also the notch to smooth tensile strength ratio (NSR) were compared and analysed. The obtained NSR was above unity which confirms the low notch brittleness. The tensile strength values between LH_2 exposed and unexposed specimen at 20K and 77K were compared and it revealed greater compatibility of Ti-5Al-2.5Sn-ELI with liquid hydrogen environment.
机译:Ti-5Al-2.5Sn合金广泛用于航空航天应用,由于其高比强度,低热膨胀系数和良好的耐腐蚀性。合金中间质要素的存在对其性质产生了一些显着影响。然而,高凹口韧性和低温延展性也吸引了Ti-5Al-2.5sn的使用,即使在20K时也能在低温温度下使用使用。对于氢脆性研究和研究Ti-5Al-2.5Sn合金的缺口敏感性,将来自Ti-5Al-2.5Sn合金的ELI等级的缺口和平滑标本进行LH2暴露和拉伸试验,在20K(-253°C)在77k(-196°C)。比较和分析了从不同样品获得的拉伸性质。还比较和分析了凹口对平滑拉伸强度比(NSR)的凹口。获得的NSR高于统一,证实了低缺口脆性。比较了LH_2曝光和未曝光标本的拉伸强度值,并比较了20K和77K的抗曝光标本,并揭示了Ti-5Al-2.5sn-Eli与液态氢气环境的更大相容性。

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