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SLAT, WING OF AIRCRAFT, FLIGHT CONTROL SURFACE OF AIRCRAFT, AND AIRCRAFT

机译:机翼,飞机机翼,飞机飞行控制面和飞机

摘要

A flight control surface such as a slat capable of keeping and achieving a minimum basic functions even when it is damaged by collisions of birds or the like, and a wing using the same are provided. Both ends of one wire cable 15 or more are fixed to paired ribs 10A and 10B provided in a short direction of the slat. This wire cable 15 is placed so as to pass through a through-hole 13 formed in each of the ribs 10 positioned between the paired ribs 10A and 10B. Even if birds or the like collide with slat 3 at the time of a flight of the aircraft to damage and deform not only a skin 4 of the slat 3 but also any rib 10, the wire cable 15 between the paired ribs 10A and 10B prevents the slat 3 from being broken into pieces.
机译:提供了一种飞行控制表面,例如即使在受到鸟等的碰撞而损坏时也能保持并实现最低限度基本功能的板条,以及使用该飞行控制表面的机翼。一根或多于一根电缆 15 的两端固定在沿板条短边方向设置的成对的肋 10 A和 10 B上。放置该电缆 15 ,以使其穿过形成在位于成对的肋 10 中的每个肋 10 中的通孔 13 。 B> 10 A和 10 B。即使鸟类等在飞机飞行时与板条 3 碰撞,不仅会损坏板条 3 4的皮肤并使其变形, 3 / B>以及任何肋骨 10 ,成对肋骨 10 A和 10 B之间的电缆 15 防止板条 3 破碎成碎片。

著录项

  • 公开/公告号US2014166818A1

    专利类型

  • 公开/公告日2014-06-19

    原文格式PDF

  • 申请/专利权人 HIDEAKI TANAKA;

    申请/专利号US201214126291

  • 发明设计人 HIDEAKI TANAKA;

    申请日2012-08-21

  • 分类号B64C3/50;

  • 国家 US

  • 入库时间 2022-08-21 16:09:34

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