首页> 外国专利> LAMINATED COMPOSITE STRUCTURES WITH INTERLAMINAR CORRUGATIONS TO IMPROVE IMPACT DAMAGE RESISTANCE, AND SYSTEM AND METHOD OF FORMING THE SAME

LAMINATED COMPOSITE STRUCTURES WITH INTERLAMINAR CORRUGATIONS TO IMPROVE IMPACT DAMAGE RESISTANCE, AND SYSTEM AND METHOD OF FORMING THE SAME

机译:具有层间波纹的叠层复合结构,可提高冲击损伤抵抗力,以及形成该结构的系统和方法

摘要

There is provided a laminated composite structure having improved impact damage resistance and improved strength. The laminated composite structure has a plurality of stacked layers of a composite material. The plurality of stacked layers has one or more interlaminar corrugations formed within the plurality of stacked layers. Each interlaminar corrugation has a substantially sinusoidal shaped profile and has a depth and a length dependent on a size of the laminated composite structure formed. The laminated composite structure with the one or more interlaminar corrugations has improved strength and improved impact damage resistance at an exposed edge of the laminated composite structure, when the exposed edge is subjected to an impact force.
机译:提供了具有改善的耐冲击破坏性和改善的强度的层压复合结构。层压复合结构具有复合材料的多个堆叠层。所述多个堆叠的层具有形成在所述多个堆叠的层内的一个或多个层间波纹。每个层间波纹具有基本正弦形状的轮廓,并且深度和长度取决于所形成的层压复合结构的尺寸。当暴露的边缘受到冲击力时,具有一个或多个层间波纹的层压的复合结构在层压的复合结构的暴露的边缘处具有改善的强度和改善的抗冲击破坏性。

著录项

  • 公开/公告号EP3539764A1

    专利类型

  • 公开/公告日2019-09-18

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20180214713

  • 申请日2018-12-20

  • 分类号B32B3/26;B32B3/28;B29D24;B32B15/08;B32B15/085;B32B15/14;B32B15/20;B32B27/32;B32B37/10;B32B3/02;B32B5/02;B32B5/22;B64C3/20;

  • 国家 EP

  • 入库时间 2022-08-21 12:29:07

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