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An aerofoil

机译:机翼

摘要

An aerofoil has a main portion of aerofoil cross section and a trailing edge portion (12) movable with respect to the main portion by an actuating device (14), the trailing edge portion (12) is movable at or about an area/point of flexion A, the area/point of flexion A is located at or adjacent a pressure or suction surface of the aerofoil, the trailing edge portion (12) is connected to the main portion by first and second connection members (18, 20), the first connection member (18) extends inwardly away from the area/point of flexion A and has an end which is directly or indirectly connected to the main portion, the first and second connection members (18, 20) are flexible.
机译:翼型件具有翼型横截面的主要部分和后缘部分(12),后缘部分(12)可通过致动装置(14)相对于该主体部分运动,后缘部分(12)可在或围绕该区域/点运动。弯曲A,弯曲A的面积/点位于机翼的压力或吸力表面处或附近,后缘部分(12)通过第一和第二连接构件(18、20)连接到主体部分,第一连接构件(18)从弯曲部A的区域/点向内延伸,并且具有直接或间接连接到主体部分的端部,第一和第二连接构件(18、20)是柔性的。

著录项

  • 公开/公告号GB2537630B

    专利类型

  • 公开/公告日2020-11-04

    原文格式PDF

  • 申请/专利权人 AGUSTAWESTLAND LIMITED;

    申请/专利号GB20150006739

  • 发明设计人 SIMON STACEY;ANDREW CAVE;

    申请日2015-04-21

  • 分类号B64C27/615;B64C27/467;B64C27/54;B64C27/72;F01D5/16;F01D5/26;

  • 国家 GB

  • 入库时间 2022-08-21 10:59:42

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