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Morphing skin for an aircraft

机译:变形飞机的皮肤

摘要

A skin for an aircraft is configured to be disposed on a first rigid member and on a second rigid member. The second rigid member is movable with respect to the first rigid member and a distance is defined between the first rigid member and the second rigid member. A morphing member of the skin extends between the first rigid member and the second rigid member. The morphing member comprises first segments forming a first portion attached to the first rigid member and second segments forming a second portion attached to the second rigid member. The first and second portions are separated along a substantially linear seam in the absence of change in the distance and an orientation between the first rigid member and the second rigid member.
机译:用于飞机的蒙皮被配置为设置在第一刚性构件和第二刚性构件上。第二刚性构件可相对于第一刚性构件移动,并且在第一刚性构件和第二刚性构件之间限定距离。皮肤的变形构件在第一刚性构件和第二刚性构件之间延伸。变形构件包括形成附接到第一刚性构件的第一部分的第一段和形成附接到第二刚性构件的第二部分的第二段。在第一刚性构件和第二刚性构件之间的距离和取向没有变化的情况下,第一部分和第二部分沿着基本线性的接缝分开。

著录项

  • 公开/公告号US10654557B2

    专利类型

  • 公开/公告日2020-05-19

    原文格式PDF

  • 申请/专利权人 BOMBARDIER INC.;

    申请/专利号US201515513439

  • 申请日2015-09-24

  • 分类号B64C3/38;B64C3/40;B64C3/42;B64C3/52;B64C5/10;B64C5/14;B64C3/26;B64C3/44;B64C3/54;

  • 国家 US

  • 入库时间 2022-08-21 11:30:52

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