陈明和
Professor
Education Level:南京航空航天大学
Degree:Doctoral Degree in Engineering
School/Department:College of Mechanical and Electrical Engineering
Discipline:Aeronautical and Astronautical Manufacturing Engineering. Material Process Engineering
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Affiliation of Author(s):机电学院
Journal:RARE METAL MATERIALS AND ENGINEERING
Key Words:TA32 titanium alloy stress relaxation constitutive equation
Abstract:Stress relaxation experiments under different combinations of temperatures (775, 800, 825 degrees C), initial stresses (150, 200 MPa) and pre-strains (7.85%, 15.7%) were performed for TA32 titanium alloy to study the influences of the process parameters on its stress relaxation behavior. The microstructures of the specimen after the experiments at different temperatures were observed to investigate the temperature effects on the microstructure evolution. The stress relaxation curves were fitted with the quadratic delay function. And the creep constitutive equation at the high temperature was established and applied to define the stress relaxation behavior of TA32 titanium alloy in the finite element analysis. The results show that the stress drops rapidly with high stress relaxation rate in the first 200 s of the stress relaxation. The stress tends to be stable and finally reaches the limit of stress relaxation after 3600 s. The stress relaxation rate increases with increasing the temperature while the stress relaxation limit decreases. And the initial stress and pre-strain have little effect on the stress relaxation behavior. The equiaxed and grown grains can enhance the plasticity with the increase of temperature. The simulation results and experimental stress relaxation curves are in good correlation which validates the reliability of the creep constitutive equation.
ISSN No.:1002-185X
Translation or Not:no
Date of Publication:2019-10-01
Co-author:Wu Ronghua,xls,Su Nan,sax,Chen Can
Correspondence Author:cmh