Research on Flange Instability During Heat Conventional Spinning of Titanium Alloy Thin - Wall Cabin

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Research on Flange Instability During Heat Conventional Spinning of Titanium Alloy Thin - Wall Cabin

更新时间：2026-04-17

- Research on Flange Instability During Heat Conventional Spinning of Titanium Alloy Thin - Wall Cabin
- Aeronautical Manufacturing Technology Vol. 54, Issue 16, Pages: 40-42(2011)
- 作者机构：
  
  航天特种材料及工艺技术研究所
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2011.16.021
  CLC：
- Published：2011
- 稿件说明：
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吕昕宇，雷鹍，许沂. 钛合金薄壁舱段热普旋过程凸缘失稳现象研究[J]. 航空制造技术, 2011, 54(16): 40-42.

吕昕宇, 雷鹍, 许沂. Research on Flange Instability During Heat Conventional Spinning of Titanium Alloy Thin - Wall Cabin[J]. Aeronautical Manufacturing Technology, 2011, 54(16): 40-42.
吕昕宇，雷鹍，许沂. 钛合金薄壁舱段热普旋过程凸缘失稳现象研究[J]. 航空制造技术, 2011, 54(16): 40-42. DOI： 10.16080/j.issn1671-833x.2011.16.021.

吕昕宇, 雷鹍, 许沂. Research on Flange Instability During Heat Conventional Spinning of Titanium Alloy Thin - Wall Cabin[J]. Aeronautical Manufacturing Technology, 2011, 54(16): 40-42. DOI： 10.16080/j.issn1671-833x.2011.16.021.

摘要

旋压道次与轨迹及排布决定 TC4 钛合金热普旋零件的成形精度。道次多、旋压时间长，整个热旋系统的膨胀会较难控制，道次少，变形量大易引起不均匀变形导致零件失稳，因此优化 TC4 钛合金热普旋的道次与轨迹尤为重要。

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