首页> 外国专利> Variable span aircraft wing - has movable outer portion partly covering inner portion and supported by main spar extension

Variable span aircraft wing - has movable outer portion partly covering inner portion and supported by main spar extension

机译:可变跨度飞机机翼-具有可移动的外部部分覆盖内部并由主翼梁延伸部分支撑

摘要

The varialbe span aircraft wing has a conventional fixed inner portion and a movable outer portion. That part of the latter inboard of the line of action of the resultant aerodynamic force on it when extended is configured to fit closely over the inner portion. - A cantilever-rail extension of the main wing spar projects into the outer portion and carries load-transmitting rollers parallel, and located close to, the line of action. When the wing is fully extended these rollers are up against a stop at the end of the rail.
机译:可变跨度飞机机翼具有常规的固定内部和可移动外部。所得空气动力在其延伸时作用线的后部内侧的那部分在延伸时构造成紧密配合在内部上。 -主翼翼梁的悬臂梁延伸部伸入外部,并承载平行且靠近作用线的载荷传递滚轮。当机翼完全伸展时,这些滚子会抵靠在导轨末端的挡块上。

著录项

  • 公开/公告号DE2102090A1

    专利类型

  • 公开/公告日1972-07-27

    原文格式PDF

  • 申请/专利权人

    申请/专利号DE19712102090

  • 发明设计人

    申请日1971-01-16

  • 分类号B64C3/54;

  • 国家 DE

  • 入库时间 2022-08-23 08:20:46

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