摘要
进行了TA15合金超塑拉伸试验,在温度920℃和应变速率5.25×10^(-4)s^(-1)时,TA15合金的最大延伸率约为1100%,其应变速率敏感性指数约为0.57。在较佳超塑变形条件930℃和应变速率5.25×10^(-4)s^(-1)附近,TA15合金的超塑本构方程为σ=949ε·^(0.55)。对TA15四层板结构超塑成形过程进行了有限元分析,获得了压力p-时间t曲线。在T=930℃和应变速率5.25×10^(-4)s^(-1)下,成功进行了TA15四层板结构SPF/DB成形试验,试验件的整体质量良好,无沟槽等缺陷,金相组织观测表明,TA15四层SPF/DB试验件扩散连接质量优良。
The optimal superplastic deformation condition of TA15 titanium alloy is determined by tensile test. The maximum elongation of 1100% could be obtained at 920℃ at strain rate of 5.25×10^(-4)s^(-1) and its strain-rate sensitivity index is 0.57. The constitutive equation of TA15 titanium alloy is σ = 949 ε·^(0.55) at 920℃ at strain rate of 5.25×10^(-4)s^(-1). The processes of superplastic forming/diffusion bonding(SPF/DB) of four-sheet structure of TA15 are simulated to obtain the pressure-time curve by the finite element Marc software. The forming test of TA15 titanium alloy four-sheet structure is conducted successfully at 930℃ at strain rate of 5.25×10^(-4)s^(-1). No grooves or other defects are found on the surface of the test pieces. According to metallographic observational, the diffusion bonding is in good quality and attained the metallurgical connection.
出处
《航空制造技术》
2016年第19期88-90,97,共4页
Aeronautical Manufacturing Technology
基金
国家自然科学基金项目(51375396)
关键词
TA15
四层板结构
超塑成形/扩散连接
有限元分析
TA15 titanium alloy
Four-sheet structure
Superplastic forming/diffusion bonding
Finite element analysis