首页> 外国专利> Aeroplane wing with extending leading edge flap - has tilting strip to avoid exposing sharp wing edge with flap extended

Aeroplane wing with extending leading edge flap - has tilting strip to avoid exposing sharp wing edge with flap extended

机译:带有延伸的前缘襟翼的飞机机翼-具有倾斜条,可避免在襟翼延伸时暴露出锋利的机翼

摘要

The aeroplane wing with an extending leading edge flap is basically conventional. The flap (2) extends forward clear of the wing (1) when in use and it retract into the wing when not in use. To eliminate the aerodynamically disadvantageous sharp leading edge to the wing usually associated with this type of flap a curved strip (3) is fitted, hinged along the wing leading edge and shaped to create an aerodynamically favourable profile when tilted forward. A recess (4) in the wing underside accommodates the retracted strip and flap in such a way that they form a continuous surface with it. To keep this recess short the flap is hinged.
机译:具有延伸的前缘襟翼的飞机机翼基本上是常规的。襟翼(2)在使用时向前伸出机翼(1),在不使用时缩回机翼。为了消除通常与这种类型的襟翼相关联的机翼在空气动力学上不利的锋利的前缘,安装了弯曲的条带(3),其沿机翼的前缘铰接并且成形为当向前倾斜时产生空气动力学上有利的轮廓。机翼下侧的凹槽(4)容纳缩回的条带和襟翼,使它们与其形成连续的表面。为了使该凹口短,活门是铰接的。

著录项

  • 公开/公告号DE1943037B2

    专利类型

  • 公开/公告日1977-12-22

    原文格式PDF

  • 申请/专利权人

    申请/专利号DE19691943037

  • 发明设计人

    申请日1969-08-23

  • 分类号B64C3/50;

  • 国家 DE

  • 入库时间 2022-08-22 22:09:22

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