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Hastelloy C-276合金应力松弛试验及蠕变本构方程 被引量:22

Stress relaxation test of Hastelloy C-276 alloy and its creep constitutive equation
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摘要 对Hastelloy C-276合金分别在不同的温度(750、800、850和900℃)和相应的初始应力(250、250、250和200 MPa)条件下进行了多组应力松弛试验。利用试验测得的应力松弛曲线推导出应力松弛过程中蠕变应变速率与应力之间的关系,建立用于描述Hastelloy C-276合金应力松弛行为的蠕变本构方程,通过对蠕变应变速率—应力曲线进行拟合,得到各温度下蠕变本构方程中的材料常数。将蠕变本构方程带入有限元软件MSC.Marc对Hastelloy C-276合金的应力松弛过程进行模拟,模拟得到的应力松弛曲线与试验测得的应力松弛曲线符合得很好,验证蠕变本构方程的可靠性。 The stress relaxation tests of Hastelloy C-276 alloy were conducted at different temperatures(750,800,850 and 900 ℃) and corresponding initial stress levels(250,250,250 and 200 MPa),respectively.Based on the experimental stress relaxation curves,the relationship between creep strain rate and stress was derived.Then,a set of creep constitutive equations were built for Hastelloy C-276 alloy and the material constants of these equations were determined by fitting the creep strain rate-stress curves.The creep constitutive equations were used to simulate the stress relaxation process of Hastelloy C-276 alloy by integrating these equations into finite element software MSC.Marc.The simulated stress relaxation curves agree well with the experimental ones,which verify the reliability of the creep constitutive equations.
出处 《中国有色金属学报》 EI CAS CSCD 北大核心 2012年第4期1063-1067,共5页 The Chinese Journal of Nonferrous Metals
基金 国家重点基础研究发展计划资助项目(2009CB724307)
关键词 HASTELLOY C-276合金 应力松弛试验 蠕变本构方程 真空热胀形 Hastelloy C-276 alloy stress relaxation test creep constitutive equation vacuum hot bulge forming
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参考文献16

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