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Large aircraft critical surface covers

机译:大型飞机关键表面罩

摘要

A cover and method for applying the cover unto the wing comprising a flexible material to cover the top surface of said wing, said material having a leading edge to cover the leading edge of said wing and a trailing edge to cover trailing edge of said wing; a first set of spaced apart attachment straps each said first attachment strap extending from said trailing edge of said cover under said wing for quick release attachment to said leading edge of said cover, so as to attach and quickly release said cover to said wing; a second set of spaced apart removal straps, each said straps extending from said leading edge of said cover over said wing for quick release attachment to said trailing edge of said cover so as to remove said cover from said leading edge to said trailing edge of said wing by pulling said removal straps.
机译:一种覆盖物和用于将覆盖物施加到机翼上的方法,包括柔性材料以覆盖所述机翼的顶表面,所述材料具有覆盖所述机翼的前边缘的前缘和覆盖所述机翼的后缘的后缘。第一组间隔开的连接带,每个所述第一连接带从所述机盖下方的所述机盖的所述后缘延伸到所述机翼下方,以快速释放附接到所述机盖的所述前缘,从而将所述机盖附着并快速释放至所述机翼;第二组间隔开的去除带,每个所述带从所述机盖的所述前缘在所述机翼上延伸,以便快速释放附接至所述机盖的所述后缘,以便将所述机盖从所述前缘移除至所述机壳的所述后缘。机翼通过拉动所述拆卸带。

著录项

  • 公开/公告号US5845873A

    专利类型

  • 公开/公告日1998-12-08

    原文格式PDF

  • 申请/专利权人 MILLARD;CARL W.;

    申请/专利号US19960610858

  • 发明设计人 CARL W. MILLARD;

    申请日1996-03-05

  • 分类号B65D85/68;

  • 国家 US

  • 入库时间 2022-08-22 02:09:22

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