Technology Innovation for Molding the Heavy Thickness Whole Wall Panel of Wing

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Technology Innovation for Molding the Heavy Thickness Whole Wall Panel of Wing

更新时间：2026-04-17

- Technology Innovation for Molding the Heavy Thickness Whole Wall Panel of Wing
- Aeronautical Manufacturing Technology Vol. 54, Issue 13, Pages: 54-56(2011)
- 作者机构：
  
  中航工业陕西飞机工业（集团）有限公司工程技术部
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2011.13.014
  CLC：
- Published：2011
- 稿件说明：
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林震宇，林瑜华. 大厚度机翼整体壁板成形工艺技术创新[J]. 航空制造技术, 2011, 54(13): 54-56.

林震宇, 林瑜华. Technology Innovation for Molding the Heavy Thickness Whole Wall Panel of Wing[J]. Aeronautical Manufacturing Technology, 2011, 54(13): 54-56.
林震宇，林瑜华. 大厚度机翼整体壁板成形工艺技术创新[J]. 航空制造技术, 2011, 54(13): 54-56. DOI： 10.16080/j.issn1671-833x.2011.13.014.

林震宇, 林瑜华. Technology Innovation for Molding the Heavy Thickness Whole Wall Panel of Wing[J]. Aeronautical Manufacturing Technology, 2011, 54(13): 54-56. DOI： 10.16080/j.issn1671-833x.2011.13.014.

摘要

事实证明， “以铣代压”创新之路是非常正确的，它既是替代压弯成形工艺的有效途径，也完全符合现代航空制造技术的发展方向。

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