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Twist mechanism for twisting a rotor blade for a rotorcraft, and a blade

机译:用于使旋翼飞行器的旋翼桨叶扭曲的扭曲机构和桨叶

摘要

A twist mechanism for twisting a rotary-wing blade (2). A twist member (8) is movable by an actuator (11) of the centrifugal force type, which twist member has at least one flyweight (14) for driving a rotary member (13) about a pivot axis (A). The flyweight (14) is radially movable on the rotary member (13) by movement means. The centrifugal force FC to which the flyweight (14) is subjected as a result of the blade (2) being caused to rotate induces drive torque CM for causing the rotary member (13) to pivot, thereby causing the twist member (8) to be moved. The twist member (8) is in engagement with the blade (2) at its free end and is connected to the rotary member (13) via remote mechanical transmission means (12).
机译:用于扭转旋翼叶片( 2 )的扭转机构。扭转元件( 8 )可通过离心力类型的执行器( 11 )移动,该致动器具有至少一个飞锤( 14 >),用于绕枢轴(A)驱动旋转构件( 13 )。飞锤( 14 )可通过移动装置在旋转部件( 13 )上径向移动。由于叶片( 2 )旋转而导致飞重( 14 )受到的离心力FC产生驱动转矩CM,从而导致旋转部件( 13 )枢转,从而使扭曲构件( 8 )移动。扭转构件( 8 )在其自由端与刀片( 2 )啮合,并与旋转构件( 13 )连接通过远程机械传动装置( 12 )。

著录项

  • 公开/公告号US9162759B2

    专利类型

  • 公开/公告日2015-10-20

    原文格式PDF

  • 申请/专利权人 JEAN-FRANCOIS HIRSCH;

    申请/专利号US201213478426

  • 发明设计人 JEAN-FRANCOIS HIRSCH;

    申请日2012-05-23

  • 分类号B64C27/54;B64C27;B64C27/72;

  • 国家 US

  • 入库时间 2022-08-21 15:22:51

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