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Method for eliminating wrinkles or bridging in composite laminate corners or bends

机译:消除复合层压板拐角或弯曲的皱纹或桥接的方法

摘要

A method of manufacturing a composite part having a curved or radiused corner to avoid wrinkling or bridging of outer-most composite plies during consolidation and cure, including laying up composite material on male or female tooling to form two flanges extending at a first angle relative each other and a curved or radiused corner extending between the two flanges. Then the method may include changing an orientation of one or both of the flanges of the composite material, such that the two flanges extend at a second included angle relative each other. The second included angle is smaller than the first angle. The method may also include a step of consolidating the composite material before, after, or during the step of changing the orientation of the composite material to the second angle, as well as a step of curing the composite material oriented at the second angle.
机译:一种制造具有弯曲或倒圆角的复合零件的方法,以避免在固结和固化过程中最外面的复合层起皱或桥接,包括将复合材料铺在凸模或凹模上以形成两个相对于每个以第一角度延伸的凸缘另一个是在两个法兰之间延伸的弯曲或倒圆角。然后,该方法可以包括改变复合材料的一个或两个凸缘的取向,使得两个凸缘相对于彼此以第二夹角延伸。第二夹角小于第一夹角。该方法还可以包括在将复合材料的取向改变为第二角度的步骤之前,之后或之中固结复合材料的步骤,以及固化以第二角度取向的复合材料的步骤。

著录项

  • 公开/公告号US10786953B2

    专利类型

  • 公开/公告日2020-09-29

    原文格式PDF

  • 申请/专利权人 SPIRIT AEROSYSTEMS INC.;

    申请/专利号US201816050061

  • 发明设计人 MARK ANTHONY WADSWORTH;

    申请日2018-07-31

  • 分类号B29C70/34;B29C70/44;B29C43/56;B29C65;B29C70/06;B29C43/12;B29K105/06;

  • 国家 US

  • 入库时间 2022-08-21 11:29:51

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