摘要
采用有限元软件对芯板的超塑成形过程进行了分析,获得了壁厚分布规律曲线和气压加载p–t曲线。在温度为920℃时,制得Ti60/TA15四层结构舵面样件,并对舵面进行了壁厚分析。结果显示,最小壁厚为1.24mm,最大壁厚为1.80mm。采用三维扫描对Ti60/TA15合金四层结构舵面的型面进行分析。结果表明,90%以上型面的公差在±0.2mm以内,整体型面的公差不超过±0.5mm。对扩散连接界面进行了金相分析。得出在温度为920℃时,TA15同种材料之间以及Ti60/TA15异种材料之间的扩散连接界面基本消失,3种扩散连接界面处已经看不出空洞。
The superplastic forming process of the core was simulated by using the finite element software, to obtain the thickness distribution and the pressure-time curves. The four-sheet structure rudder of Ti60/TA15 alloy was obtained at 920℃. The thickness of the rudder was investigated. The results show that the minimum thickness is 1.24 mm and the maximum thickness is 1.80 mm. The moulding surface for the four-sheet structure rudder of Ti60/TA15 alloy was measured by using the 3D scanning. The results show that the tolerance of more than 90% is less than ±0.2 mm, and the global is less than ±0.5 mm. The interface of diffusion bonding was investigated by the metallograph observation. The results show that at 920℃, interfaces of diffusion bonding between the same materials of TA15 and between the different materials of TA15 disappear basically, and no holes can be seen at the three diffused interfaces.
作者
李保永
刘伟
秦中环
蒋少松
薛杰
李信
LI Baoyong;LIU Wei;QIN Zhonghuan;JIANG Shaosong;XUE Jie;LI Xin(School of Material Science and Engineering,Harbin Institute of Technology,Harbin 150001,China;Beijing Hangxing Machine Manufacturing Co.,Ltd.,Beijing 100013,China)
出处
《航空制造技术》
2019年第8期76-80,共5页
Aeronautical Manufacturing Technology
基金
装备预研基金(6144290902417)