首页> 外国专利> ROTORCRAFT EQUIPPED WITH AN ANTI-TORQUE REAR ROTOR, SELECTIVELY PARTICIPATING IN LIFT AND PROPULSION IN TRANSLATION OF THE ROTORCRAFT

ROTORCRAFT EQUIPPED WITH AN ANTI-TORQUE REAR ROTOR, SELECTIVELY PARTICIPATING IN LIFT AND PROPULSION IN TRANSLATION OF THE ROTORCRAFT

机译:配备有反扭矩后转子的转辙器,选择性地参与升起和推进转译中的推进

摘要

the invention is directed to a rotorcraft rotor equipped with a back (3) to be the direction of the axis (6) of training which is constant, and the rotor is disposed laterally to the tail boom of the rotorcraft.a mechanism for manoeuvring (14) of the rear rotor blades (8) includes a tray (3) controller (27) with the rotating blade positioned in manceuvrable (8) and by a control rod (21) oriented along the axis of the drill (6) on the rear rotor (3).the set of control (27) is disposed on a mounting plane (mp), causing a continuous constant cyclic variation of rotor blades (8).a man 's rotation of the control rod (21) changes the operation of the cyclic variation of permanent blades (8), providing support and contribution in translation of rotorcraft propulsion according to the angular position of the control plate (27) in the plan of my the tagus (pm).
机译:本发明涉及一种旋翼航空器旋翼,该旋翼航空器的背面(3)沿训练轴线(6)的方向恒定,并且该旋翼相对于旋翼航空器的尾梁横向放置。 14)的后转子叶片(8)包括一个托盘(3)控制器(27),旋转叶片置于可操纵(8)的位置,并且控制杆(21)沿钻头(6)的轴线定向。后转子(3)。这组控制器(27)放置在安装平面(mp)上,导致转子叶片(8)连续不断地周期性变化。控制杆(21)的人为旋转改变了永久叶片(8)周期性变化的操作,根据塔基(pm)平面中控制板(27)的角位置,为旋翼航空器推进的平移提供支持和贡献。

著录项

  • 公开/公告号CA2872810C

    专利类型

  • 公开/公告日2016-05-17

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号CA20142872810

  • 发明设计人 BISTUER OLIVIER;PRUDHOMME-LACROIX PIERRE;

    申请日2014-11-28

  • 分类号B64C27/82;B64C11/46;B64C27/08;B64C27/52;

  • 国家 CA

  • 入库时间 2022-08-21 14:21:34

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