Creep performance characterization for Haynes 282TM using the deformation-mechanism-based true stress model

被引:6
|
作者
Ding, Y. P.
Wu, X. J. [2 ]
Liu, R. [3 ]
Zhang, X. Z. [3 ]
Khelfaoui, F. [1 ,4 ]
机构
[1] Zhejiang A&F Univ, Jiyang Coll, Sch Engn & Technol, Zhuji 311800, Peoples R China
[2] Natl Res Council Canada, Aerosp Res Ctr, Struct & Mat Performance Lab, Ottawa, ON K1A 0R6, Canada
[3] Carleton Univ, Dept Mech & Aerosp Engn, 1125 Colonel By Dr, Ottawa, ON K1S 5B6, Canada
[4] Velan Inc, 300 McArthur Ave, Montreal, PQ H4T 0A2, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Haynes; 282; alloy; Deformation-mechanism-based true-stress; creep model; Creep rate; Creep life; Microstructure-based creep mechanism; TENSILE PROPERTIES; HEAT-TREATMENT; MICROSTRUCTURE; BEHAVIOR;
D O I
10.1016/j.tsep.2022.101603
中图分类号
O414.1 [热力学];
学科分类号
摘要
The deformation-mechanism-based true-stress (DMTS) creep model is used to analyze short-term (<10000 h) creep test data for nickel-based alloy Haynes 282 in this research. The deformation mechanisms are delineated in terms of power-laws for grain boundary sliding (GBS), intragranular dislocation glide (IDG) and intragranular dislocation climb (IDC), with a deformation mechanism map developed, which shows the regions of IDG, IDC and GBS-dominance. It is found that the DMTS model is capable of describing the entire creep curve consisting of the primary, secondary, and tertiary stages before unstable deformation (necking) occurs. The predictions from the model are in very good agreement with the experimental observations. Coupled with a two-parameter failure criterion, the model demonstrates the effectiveness of predicting the creep failure mode and rupture life of Haynes 282 with an average coefficient of determination R2 = 0.93.
引用
收藏
页数:19
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