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Folding protective cover for turbo-engines

机译:涡轮发动机的折叠式防护罩

摘要

The present invention is a folding protective cover primarily for openings which are generally circular in shape, particularly the air inlet and exhaust ducts of a stopped turbo-engine as used by aircraft. The invention is comprised of a generally circular ring shaped frame which is made up of four arc shaped sections of approximately 90 degrees each. Three hinges are mounted between the sections in such a manner that the frame may be folded into an arc of approximately 90 degrees. Affixed to the outer edge of the frame is a resilient gasket and affixed across the center of the frame is a waterproof fabric panel.
机译:本发明是一种折叠保护罩,其主要用于通常为圆形的开口,特别是用于飞机的涡轮发动机的进气道和排气道。本发明包括一个大体上为圆形的环形框架,该框架由每个大约为90度的四个弧形部分组成。三个铰链以使框架可折叠成大约90度的弧形的方式安装在两个部分之间。弹性垫圈固定在框架的外边缘,防水织物面板固定在框架的中心。

著录项

  • 公开/公告号US5143321A

    专利类型

  • 公开/公告日1992-09-01

    原文格式PDF

  • 申请/专利权人 JACKSON;THOMAS H.;

    申请/专利号US19910756349

  • 发明设计人 THOMAS H. JACKSON;

    申请日1991-09-09

  • 分类号B64D33/00;

  • 国家 US

  • 入库时间 2022-08-22 05:22:24

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