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Ground-effect landing gear for aircraft - has flexible enclosure of torus-shaped elements bounding an overpressure space near ground surface

机译:飞机的地效应起落架-圆环形元件的柔性外壳,包围地面附近的超压空间

摘要

The ground-effect landing gear for use on aircraft intended for performing take-off and landing on unprepared soft ground comprises a platform mounting a flexible enclosure constructed in the form of a system of inflatable envelopes bounding an overpressure space near the ground surface. During transition to hovering and during movement of the aircraft the space is kept in communication with a compressed air source. The inner portion of the flexible enclosure is composed of separate torus-shaped elements joined together along chords.
机译:用于打算在未准备好的软地面上起飞和降落的飞机上使用的地效应起落架,包括一个平台,该平台安装了一个柔性外壳,该外壳以可充气包膜系统的形式构造,界定了靠近地面的超压空间。在过渡到悬停期间以及在飞机运动期间,空间保持与压缩空气源连通。柔性外壳的内部由沿着弦连接在一起的单独的圆环形元件组成。

著录项

  • 公开/公告号FR2371327B1

    专利类型

  • 公开/公告日1981-06-12

    原文格式PDF

  • 申请/专利权人 BELOLIPETSKY ALEXEI;

    申请/专利号FR19760034768

  • 发明设计人

    申请日1976-11-18

  • 分类号B60V3/08;

  • 国家 FR

  • 入库时间 2022-08-22 15:06:48

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