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TC1钛合金端盖零件热拉深成形工艺研究
引用本文:张志,李鹏亮,孙宾,李均红.TC1钛合金端盖零件热拉深成形工艺研究[J].航空制造技术,2017(8).
作者姓名:张志  李鹏亮  孙宾  李均红
作者单位:1. 中国航空制造技术研究院,北京100024;塑性成形技术航空科技重点实验室,北京100024;数字化塑性成形技术及装备北京市重点实验室,北京100024;2. 四川成发航空科技股份有限公司,成都,610503
摘    要:针对TC1钛合金端盖零件的结构特点,分析了零件的成形难点,对热拉深工艺的模具材料、温度、压边间隙、拉深速度等对零件成形性能的影响进行了研究,提出了合理的工艺参数。结果表明,该工艺方法可实现薄壁、大拉深比的TC1钛合金零件的精确成形,采用空气脱模的方式可获得平面度满足设计要求的零件,为类似零件的取件提供了工艺参考。

关 键 词:TC1钛合金  热拉深工艺  薄壁  大拉深比  空气脱模

Study on Thermal Deep-Drawing Process of TC1 Titanium Alloy Cover Part
ZHANG Zhi,LI Pengliang,SUN Bin,LI Junhong.Study on Thermal Deep-Drawing Process of TC1 Titanium Alloy Cover Part[J].Aeronautical Manufacturing Technology,2017(8).
Authors:ZHANG Zhi  LI Pengliang  SUN Bin  LI Junhong
Abstract:According to the feature of TC 1 titanium alloy cover part,the processing property of the part is analyzed.The influence of some factors such as mould material,temperature,blank holder gap and drawing rate on the drawing formability of TCl titanium alloy cover part are discussed,meanwhile the appropriate parameters are optimized.The results indicate that the proposed technological method is feasible for the integral forming of thin-walled TC1 titanium alloy with large drawing ratios.Moreover,parts with high quality of flatness can be successfully formed by using air-demoulding method.It provides a technical reference for picking off the similar parts.
Keywords:TC1 titanium alloy  Thermal deep drawing technology  Thin-wall  Large drawing ratio  Air-demould
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