首页> 外国专利> A TWIST MECHANISM FOR TWISTING A ROTOR BLADE FOR A ROTORCRAFT, AND A BLADE

A TWIST MECHANISM FOR TWISTING A ROTOR BLADE FOR A ROTORCRAFT, AND A BLADE

机译:旋翼桨叶旋转叶片的扭曲机理和叶片

摘要

PURPOSE: A twist mechanism for twisting a rotor blade for a rotorcraft and a blade are provided to twist a rotor blade through an extended surface of a rotor blade and to have high reliability and accuracy. CONSTITUTION: A twist mechanism for twisting a rotor blade for a rotorcraft comprises a mounting structure(7), a twist member(8), and a driving assembly. The mounting structure installs the twist mechanism in a blade(2). The twist member comprises a coupling unit(9) which is coupled to the blade. The driving assembly moves the twist member and comprises an actuator(11) and a power transmission unit(12). The power transmission unit transmits moving force generated by the actuator to the twist member.
机译:目的:提供一种用于使旋翼飞机的转子叶片扭转的扭转机构和叶片,以使转子叶片通过转子叶片的延伸表面扭转并且具有高可靠性和准确性。构成:一种用于使旋翼飞行器的旋翼桨叶扭曲的扭曲机构,包括安装结构(7),扭曲构件(8)和驱动组件。该安装结构将扭转机构安装在叶片(2)中。扭转构件包括联接至叶片的联接单元(9)。驱动组件使扭转构件运动并且包括致动器(11)和动力传递单元(12)。动力传递单元将由致动器产生的移动力传递到扭转构件。

著录项

  • 公开/公告号KR20120134027A

    专利类型

  • 公开/公告日2012-12-11

    原文格式PDF

  • 申请/专利权人 유로꼽떼르;

    申请/专利号KR20120055664

  • 发明设计人 허쉬 장-프랑소와;

    申请日2012-05-24

  • 分类号B64C27/46;F16H25/20;

  • 国家 KR

  • 入库时间 2022-08-21 16:28:28

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