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Variable pitch rotor blade for shrouded rotors, in particular helicopter rotors

机译:用于带罩转子,特别是直升机转子的变桨转子叶片

摘要

The blade includes a current part (1) having an aerodynamic profile enclosing a spar (7) and extending from blade tip (4) to a blade root (3) provided with a pitch sleeve (21), through which twisting arm (6) passes and protrudes beyond blade root (3), and having a first part of a bundle (5) of superimposed and elongated metal strips, current part (1) including a block (13) based on synthetic material molded in form in a single piece around spar (7), and a second part of bundle (5) extending in line with the first part forming the twisting arm (6) and cooperating with the anchoring devices (14, 17) of the block (13) based on synthetic material around the spar (7).
机译:叶片包括当前部分( 1 ),该部分具有空气动力学轮廓,包围翼梁( 7 ),并从叶片尖端( 4 )延伸至叶片。带有桨距套筒( 21 )的桨叶根( 3 ),扭臂( 6 )穿过并伸过桨叶根(< B> 3 ),并且具有叠加的细长金属带束( 5 )的第一部分,当前部分( 1 )包括块( 13 )是基于合成材料,以合成材料的形式模制成单根( 7 ),而束的第二部分( 5 )延伸与形成扭臂( 6 )的第一部分成一直线,并与块( 13 )的锚定装置( 14、17 )配合使用)基于翼梁( 7 )周围的合成材料。

著录项

  • 公开/公告号US7040863B2

    专利类型

  • 公开/公告日2006-05-09

    原文格式PDF

  • 申请/专利权人 BRUNO GUIMBAL;

    申请/专利号US20040860745

  • 发明设计人 BRUNO GUIMBAL;

    申请日2004-06-04

  • 分类号B64C11/20;

  • 国家 US

  • 入库时间 2022-08-21 21:41:12

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