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Set of swashplates for controlling the pitch of rotor blades, a rotor and an aircraft having such a set

机译:用于控制旋翼桨距的斜盘组,旋翼和具有该组的飞机

摘要

A set of swashplates having a non-rotary swashplate and a rotary swashplate. The set includes drive means constraining the rotary swashplate and the rotor mast in rotation about the axis of rotation. The drive means are provided with a drive arm driving the rotary swashplate in rotation about the axis of rotation by plane connection means including a fork, the drive arm extending in elevation from a first end to a second end that is fastened to the rotor mast, the first portion being held captive laterally between two lateral branches of the fork, the fork being hinged to the rotary swashplate by movement means giving the rotary swashplate a degree of freedom to move in rotation about a radial direction of the rotary swashplate relative to the fork.
机译:具有非旋转斜盘和旋转斜盘的一组斜盘。该套件包括驱动装置,其限制旋转斜盘和转子桅杆绕旋转轴线旋转。该驱动装置设置有驱动臂,该驱动臂通过包括叉的平面连接装置驱动旋转斜盘绕旋转轴线旋转,该驱动臂从第一端部到第二端部在高度上延伸,该第二端部固定在转子桅杆上,第一部分被横向地俘获在叉的两个侧向分支之间,叉通过运动装置铰接到旋转斜盘,从而使旋转斜盘具有相对于叉绕旋转斜盘的径向旋转运动的自由度。 。

著录项

  • 公开/公告号US9796471B2

    专利类型

  • 公开/公告日2017-10-24

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号US201514687039

  • 发明设计人 FABIEN MASSAL;

    申请日2015-04-15

  • 分类号B64C27/605;

  • 国家 US

  • 入库时间 2022-08-21 13:46:30

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