Creep-Fatigue Behaviors and Life Assessments in Two Nickel-Based Superalloys

Author:

Wang Run-Zi1,Wang Ji1,Gong Jian-Guo1,Zhang Xian-Cheng2,Tu Shan-Tung3,Zhang Cheng-Cheng4

Affiliation:

1. Key Laboratory of Pressure Systems and Safety, Ministry of Education, East China University of Science and Technology, Shanghai 200237, China

2. Key Laboratory of Pressure Systems and Safety, School of Mechanical and Power Engineering, Ministry of Education, East China University of Science and Technology, Meilong Road 130, Xuhui District, Shanghai 200237, China

3. Key Laboratory of Pressure Systems and Safety, School of Mechanical and Power Engineering, Ministry of Education, East China University of Science and Technology, Meilong Road 130, Xuhui District, Shanghai 200237, China e-mail:

4. AECC, Commercial Aircraft Engine Co. LTD., Shanghai Engineering Research Center for Commercial Aircraft Engine, Shanghai 201108, China e-mail:

Abstract

The aim of this paper is to investigate different factors, including dwell time, strain range, and strain ratio on creep-fatigue endurances in nickel-based Inconel 718 and GH4169 superalloys. We also summarize classic approaches for life assessments based on the generalizations of Coffin–Manson equation, linear damage summation (LDS), and strain-range partitioning (SRP) method. Each approach does have some degree of success in dealing with a specific set of creep–fatigue data. In order to evaluate the prediction capabilities of the validated approaches, a Bayesian information criterion (BIC) allowing for maximum likelihood and principle of parsimony is used to select the best performing model.

Funder

National Natural Science Foundation of China

China National Funds for Distinguished Young Scientists

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Safety, Risk, Reliability and Quality

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