In-situ observation and finite element analysis of fretting fatigue crack propagation behavior in 1045 steel  

作　　者：Qinan HAN Xusheng LEI Yue SU Shaoshi RUI Xianfeng MA Haitao CUI Huiji SHI 

机构地区：[1]Aero-engine Thermal Environment and Structure Key Laboratory of Ministry of Industry and Information Technology,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China [2]AML,Department of Engineering Mechanics,Tsinghua University,Beijing 100084,China [3]AMPTL,Department of Mechanical Engineering,Tsinghua University,Beijing 100084,China [4]Sino-French Institute of Nuclear Engineering and Technology,Sun Yat-Sen University,Zhuhai 519082,China

出　　处：《Chinese Journal of Aeronautics》2021年第11期131-139,共9页中国航空学报（英文版）

基　　金：financially supported by the National Natural Science Foundation of China(Nos.91860101,11632010,11902370 and 11572171);National Major Science and Technology Projects of China(No.2017-VI-0003-0073)。

摘　　要：In this paper fretting fatigue crack behavior in 1045 steel is studied by in-situ observation and finite element analysis.in-situ fretting fatigue experiments are conducted to capture real-time fretting fatigue crack formation and propagation process.The fretting fatigue tests under different load conditions are carried out,then the lifetime and fracture surface are obtained.The crack propagation rates under different loading conditions are measured by in-situ observations.With in-situ observation,crack initiation location and direction are analyzed.Finite element model is used to calculate J-integral which then is applied to fitting with experimental crack growth rate,and establishing crack growth rate model.From fitted S-N curve,it turns out that smaller load ratio leads to higher lifetime.Crack initiates slightly below the point equivalent to line contact of the contact surface in different test conditions,and crack direction shows no obvious relationship with load parameters.The established crack growth rate model well agrees with the test results.

关 键 词：Crack growth rate Fretting fatigue In-situ observation J-INTEGRAL 1045 steel 

分 类 号：V215.5[航空宇航科学与技术—航空宇航推进理论与工程] V415.5