首页> 外国专利> Aircraft wing, method for operating an aircraft wing, and use of a pivotable trailing edge on a main wing of an aircraft, for adjusting the shape and width of an air gap

Aircraft wing, method for operating an aircraft wing, and use of a pivotable trailing edge on a main wing of an aircraft, for adjusting the shape and width of an air gap

机译:飞机机翼,操作飞机机翼的方法以及在飞机主机翼上使用可枢转的后缘以调节气隙的形状和宽度

摘要

An aircraft wing comprises a main wing with a pivotable trailing edge and a lift-assisting flap on the rear of the wing. The lift-assisting flap is coupled to the main wing and is designed in such a way that in its retracted state, the lift-assisting flap abuts the main wing and in an extended state, the lift-assisting flap forms an air gap with the main wing. The pivotable trailing edge is pivotable in such a way that, by pivoting the pivotable trailing edge, the shape and the width of the air gap are adjustable.
机译:飞机机翼包括具有可枢转后缘的主机翼和位于机翼后部的升力辅助翼。助力襟翼与主翼相连,其设计方式是,在其缩回状态下,助力襟翼邻接主翼,在伸展状态下,助力襟翼与主翼形成气隙。主翼。可枢转的后缘以如下方式可枢转:通过枢转可枢转的后缘,气隙的形状和宽度是可调节的。

著录项

  • 公开/公告号US7520471B2

    专利类型

  • 公开/公告日2009-04-21

    原文格式PDF

  • 申请/专利权人 DANIEL RECKZEH;ADRIAN R. DYKE;

    申请/专利号US20050246859

  • 发明设计人 DANIEL RECKZEH;ADRIAN R. DYKE;

    申请日2005-10-07

  • 分类号B64C3/50;B64C9;

  • 国家 US

  • 入库时间 2022-08-21 19:30:40

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