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Title:Forming process of rotary skin with curved generatrix for TC4 titanium alloy
Authors: Zhu Shiqiang  Wang Dagang  Wang Xinyu  Zhang Sicong  Wang Hailun  Li Weihong  Liu Kai 
Unit: Capital Aerospace Machinery Corporation Limited 
KeyWords: TC4 titanium alloy rotary body with curved generatrix skin thermoforming stress relaxation thermal sizing 
ClassificationCode:V461
year,vol(issue):pagenumber:2020,45(6):107-110
Abstract:

For the rotary skin with curved generatrix in aerospace, the technological scheme of first split thermoforming and then thermal sizing was developed by analyzing the skin structure, and the temperatures of thermoforming and thermal sizing were selected as 700 ℃. Then, based on the analysis and calculation of the linear expansion coefficient of material, the design dimensions of the thermoforming and thermal sizing dies were obtained respectively, and the forming process parameters were optimized by the thermoforming and thermal sizing experiments. The results show that when the heat and pressure holding time during the thermoforming is 1000 s, the gap between the arc of formed part and the template is less than 0.3 mm, which meets the subsequent welding needs. Furthermore, the comparison test results of different preloads and heat holding times show that the die applies a certain preload to the product during the thermal sizing process, and after thermal sizing of 30 min, the dimensional accuracy of the manufactured skin product reaches ±0.3 mm, which proves the feasibility of this process.

Funds:
中国运载火箭技术研究院工艺改进基金(GYGJ14-211-30)
AuthorIntro:
祝世强(1978-),男,硕士,高级工程师 E-mail:hitzsq@126.com 通讯作者:王大刚(1987-),男,硕士,工程师 E-mail:wdgnba@163.com
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