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Composite material, a structural element comprised of the composite material, an airplane wing spar and their methods of production

机译:复合材料,由该复合材料组成的结构元件,飞机翼梁及其制造方法

摘要

Disclosed is to a composite material, a structural element comprised of the composite material, an airplane wing spar and their methods of production. Some embodiments of the present invention include composite materials comprised of multiple layers of arrays of metallic bodies separated by layers of non-metallic material, wherein the orientation of metallic bodies in some metallic layers is structurally complementing to the orientation of metallic layers in adjacent metallic layers. Other embodiments of the present invention include structural elements, such as an airplane wing spar, comprised of the composite material.
机译:公开了一种复合材料,由该复合材料构成的结构元件,飞机翼梁及其制造方法。本发明的一些实施例包括由非金属材料层隔开的多层金属体阵列组成的复合材料,其中一些金属层中金属体的取向在结构上与相邻金属层中金属层的取向在结构上互补。本发明的其他实施例包括由复合材料构成的结构元件,例如飞机翼梁。

著录项

  • 公开/公告号US9006119B2

    专利类型

  • 公开/公告日2015-04-14

    原文格式PDF

  • 申请/专利权人 ZIGMUND BLUVBAND;VIKTOR SHKATOV;

    申请/专利号US20100833985

  • 发明设计人 ZIGMUND BLUVBAND;VIKTOR SHKATOV;

    申请日2010-07-11

  • 分类号B32B15/14;B23B3/22;B32B27/36;B64C3/20;B64C3/18;B32B5/12;B32B3/18;

  • 国家 US

  • 入库时间 2022-08-21 15:20:29

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