FAN Rong,LI Xiu-hong,LI Wen-hui,YANG Sheng-qiang.Fatigue Life Simulation and Experiment of TC4 Titanium Alloy Board Based on ABAQUS/FE-SAFE[J],46(1):158-163
Fatigue Life Simulation and Experiment of TC4 Titanium Alloy Board Based on ABAQUS/FE-SAFE
Received:September 03, 2016  Revised:January 20, 2017
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DOI:10.16490/j.cnki.issn.1001-3660.2017.01.025
KeyWord:titanium alloy  surface roughness  residual stress  barrel finishing  fatigue life  prediction model
           
AuthorInstitution
FAN Rong 1.School of Mechanical Engineering, Taiyuan University of Technology, Taiyuan , China; 2.Shanxi Key Laboratory of Precision Machining, Taiyuan , China
LI Xiu-hong 1.School of Mechanical Engineering, Taiyuan University of Technology, Taiyuan , China; 2.Shanxi Key Laboratory of Precision Machining, Taiyuan , China
LI Wen-hui 1.School of Mechanical Engineering, Taiyuan University of Technology, Taiyuan , China; 2.Shanxi Key Laboratory of Precision Machining, Taiyuan , China
YANG Sheng-qiang 1.School of Mechanical Engineering, Taiyuan University of Technology, Taiyuan , China; 2.Shanxi Key Laboratory of Precision Machining, Taiyuan , China
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Abstract:
      The work aims to establish a fatigue life prediction model for titanium alloy and verify feasibility of this model in predicting titanium alloy fatigue life after barrel finishing by virtue of experimental study. Influencing law of roughness and residual stress on TC4 titanium alloy fatigue life was studied by virtue of finite element simulation and multivariate regression orthogonal experiment. Relation equation among fatigue life, roughness and residual stress was simulated, correctness of the simulation results and equation were further validated by experiments. After the barrel finishing, the roughness of TC4 board changed from Rz=3.16 to Rz=1.69. The initial residual tensile stress turns into compressive residual stress from 50 MPa to 228 MPa. The fatigue life increases from 28,083 to 39,510 times and has increased by 40.6%. Compared with the results of simulation, the error is about 5%, testifying feasibility of simulation results. Therefore, a fatigue life prediction model is provided for titanium alloys subject to barrel finishing.
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