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Prediction of combined cycle fatigue life of TC11 alloy based on modified nonlinear cumulative damage model
Institution:1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjinj University of Aeronautics and Astronautics, Nanjing 210016, China;2. 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
Abstract:The nonlinear cumulative damage model is modified to have high prediction accuracy when the high-low cycle stress frequency ratio m is large (m ≥ 500). The low cycle fatigue (LCF) tests, high cycle fatigue (HCF) tests and combined high and low cycle fatigue (CCF) tests of TC11 titanium alloy were carried out, and the influencing factors of CCF life were analysed. The CCF life declines with the decrease of the ratio of high-low cycle stress frequency m. Both linear and nonlinear cumulative damage models are used to predict the CCF life. The CCF life prediction error of the linear cumulative damage model is great and the predictions tend to be overestimated, which is dangerous for engineering application. The accuracy is relatively high when the high-low cycle stress frequency ratio m ≤ 500. The accuracy of nonlinear cumulative damage model is higher than that of linear model when the high-low cycle stress frequency ratio m ≥ 500. Based on the relationship between high cycle average stress σmajor and material yield limit σp,0.2, a correction term is added to the nonlinear cumulative damage model and verified, which made the modified model more accurate when m ≥ 500.
Keywords:Combined cycle  Damage accumulation  High-cycle fatigue  Low-cycle fatigue  Prediction method
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