MAO You-sheng 1 , LI Tong 1 , JIA Wen-bin 1,2 , LI Xin 1 , LIU Fei-long 1 , FANG Lei 1.Multiaxial Thermo-mechanical Viscoplastic Constitutive Model and Verification of GH4169 Alloy[J].航空发动机,2024,50(3):160-168
Multiaxial Thermo-mechanical Viscoplastic Constitutive Model and Verification of GH4169 Alloy
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Key Words:GH4196  multiaxial fatigue  thermo-mechanical fatigue  Chaboche model  Lemaitre damage model  critical plane theory  viscoplastic potential function correction coefficient
Author NameAffiliation
MAO You-sheng 1 , LI Tong 1 , JIA Wen-bin 1,2 , LI Xin 1 , LIU Fei-long 1 , FANG Lei 1 1. College of Energy and Power Engineering Nanjing University of Aeronautics and Astronautics Nanjing 210016 China 2. College of Energy Engineering Zhejiang Universtity Hangzhou 310027 China 
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Abstract:In order to describe the multiaxial thermo-mechanical behavior of GH4169 alloy more accurately, based on the Chaboche viscoplastic constitutive model, by introducing the Lemaitre damage model, the non-proportional strengthening factor based on critical plane theory, and the viscoplastic potential function correction coefficient, a multiaxial thermo-mechanical fatigue viscoplastic constitu? tive model suitable for GH4169 alloy was proposed to describe cyclic softening, non-proportional hardening, and non-Masing behavior of the material, and the method for obtaining the parameters of the constitutive model was provided. This constitutive model was used to simulate the multiaxial and thermo-mechanical behavior of GH4169 alloy. The results show that at 20 ℃, for the simulations of the hysteresis loops of the 200th cycle under five loading conditions (axial loading, torsional loading, proportional loading, 45 ° non- proportional loading, and 90 ° non-proportional loading), the results of the axial stress peaks and valleys are consistent with the experimental results; at 650 ℃, for the simulation of the hysteresis loops of the 200th cycle under three loading conditions (proportional loading, 45 ° non proportional loading, and 90 ° non proportional loading), the results are basically consistent with the experimental results, proving that the established model is suitable for high temperature conditions; for the simulations of the hysteresis loops of uniaxial axial loading and circular path loading at 300 ℃, 550 ℃, and 650 ℃, the results are basically consistent with the experimental values; for the simulations of the hysteresis loops of the 200th cycle under in-phase and antiphase loading conditions, the simulated values of the corrected constitutive model are in good agreement with the experimental values.
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