航空制造技术
航空製造技術
항공제조기술
Aeronautical Manufacturing Technology
2015年
17期
107-109
,共3页
张智鑫%庞洪%陈海涛%王红武
張智鑫%龐洪%陳海濤%王紅武
장지흠%방홍%진해도%왕홍무
TC4钛合金%冷轧加工率%热处理%显微组织%超塑性
TC4鈦閤金%冷軋加工率%熱處理%顯微組織%超塑性
TC4태합금%랭알가공솔%열처리%현미조직%초소성
TC4 titanium alloy plate%Cold rolling reduction%Heat treatment%Microstructure%Super-plastic property
通过观察和测试不同冷轧和热处理工艺超塑用TC4板材的组织和力学性能,研究了冷轧加工率和热处理温度对TC4钛合金组织和性能的影响,优化了TC4板材的显微组织并测试了其超塑性能。研究结果表明:增加冷轧加工率,840~860℃热处理,有利于超塑用TC4板材得到均匀、无畸变、细小的再结晶组织,其室温强度可达到1060~1048MPa,延伸率为18%~18.5%;经组织优化后的超塑TC4板材在870℃,应变速率为2.4×10-3/s-1时,延伸率可达到894%。
通過觀察和測試不同冷軋和熱處理工藝超塑用TC4闆材的組織和力學性能,研究瞭冷軋加工率和熱處理溫度對TC4鈦閤金組織和性能的影響,優化瞭TC4闆材的顯微組織併測試瞭其超塑性能。研究結果錶明:增加冷軋加工率,840~860℃熱處理,有利于超塑用TC4闆材得到均勻、無畸變、細小的再結晶組織,其室溫彊度可達到1060~1048MPa,延伸率為18%~18.5%;經組織優化後的超塑TC4闆材在870℃,應變速率為2.4×10-3/s-1時,延伸率可達到894%。
통과관찰화측시불동랭알화열처리공예초소용TC4판재적조직화역학성능,연구료랭알가공솔화열처리온도대TC4태합금조직화성능적영향,우화료TC4판재적현미조직병측시료기초소성능。연구결과표명:증가랭알가공솔,840~860℃열처리,유리우초소용TC4판재득도균균、무기변、세소적재결정조직,기실온강도가체도1060~1048MPa,연신솔위18%~18.5%;경조직우화후적초소TC4판재재870℃,응변속솔위2.4×10-3/s-1시,연신솔가체도894%。
Effect of cold rolling reduction and heat treatment on microstructure and mechanical prop-erty of TC4 titanium sheet is studied through observing and testing the microstructure and property of TC4 plates with different cold rolling and heat treatment processes. The microstructure of TC4 is optimizing, and the super-plastic property of TC4 plates is tested. The result shows that uniform, non-distorted and fine microstructures of TC4 plates are obtained by increasing cold rolling reduction and annealing at 840~860℃. Its strength can reach to 1060~1048MPa, and its elongation can reach to 18%~18.5%. In the parameters of 870 ℃ and strain rate 2.4×10-3/s-1, the elongation of microstructure optimized TC4 plates can reach to 894%.