首页> 外国专利> Folding blade rotor for helicopter, has electric cable provided with spare portion wound on reel in S-shape, which is released by withdrawal of reel and blade pin

Folding blade rotor for helicopter, has electric cable provided with spare portion wound on reel in S-shape, which is released by withdrawal of reel and blade pin

机译:直升机用折叠式桨叶旋翼,其电缆上带有备用部分,其备用部分以S形缠绕在渔线轮上,并通过收回渔线轮和桨叶销而释放

摘要

The primary portion (36) of an electric cable connected between a blade (3) and a hub (9), has spare portion (52) wound in S-shape around a pair of reels. The reels are mounted at the ends of a pair of pins (15) so that withdrawal of the blade pin and corresponding reel, releases the spare portion from wound state, to allow the blade to fold back.
机译:连接在叶片(3)和轮毂(9)之间的电缆的主要部分(36)具有以S形缠绕在一对卷轴上的备用部分(52)。这些卷轴安装在一对销钉(15)的端部,以使刀片销钉和相应的卷轴缩回,从而使备用部分脱离缠绕状态,从而使刀片向后折叠。

著录项

  • 公开/公告号FR2810013A1

    专利类型

  • 公开/公告日2001-12-14

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号FR20000007337

  • 发明设计人 POTDEVIN FRANCOIS;

    申请日2000-06-08

  • 分类号B64D15/12;B64C27/50;

  • 国家 FR

  • 入库时间 2022-08-22 00:24:26

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