航空发动机TC6钛合金尾杆的等温锻造

Isoehermal Forging of the Tc6-Titaniam Alloy Tailrod far Aeroengine

介绍了利用钛合金等温锻造工艺研制航空发动机利用TC_5钛合金尾杆过程,包括坯料准备,模具设计和制备、等温锻造工艺参数的确定及锻件质量分析。

This paper presents isothermal forging of the Tc6-titanium, alloy tail rod for aeroengine, including blank materials preparatioo, die design and manufacture, the determination of paraumeters of isoehermal forging technal ogy and guality analysss of forged piece.