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Pitch control swash plate assembly of a main rotor as well as a rotor with such an assembly

机译:主转子的变桨控制斜盘组件以及具有这种组件的转子

摘要

The assembly (10) has a non-rotary swashplate (12) retained against rotation about a rotational axis (AX) and a rotary swashplate (11) rotating around the rotational axis. A drive unit (100) connects the rotary swashplate and a rotor mast (2) of a main rotor (1) in rotation around the axis. An annular linear connection unit (200) is integrated to the rotary swashplate. A drive arm has an end (110) connected to the rotary swashplate by the annular linear connection unit and another end (120) connected to the rotor mast by a slideway connection unit of the drive unit. An independent claim is also included a rotor of a rotorcraft with a rotor mast rotationally driving blades around a rotational axis.
机译:组件(10)具有非旋转斜盘(12)和旋转斜盘(11),该非旋转斜盘(12)绕旋转轴(AX)旋转而保持旋转。驱动单元(100)将旋转斜盘和主转子(1)的转子杆(2)绕轴线旋转连接。环形线性连接单元(200)集成到旋转斜盘上。驱动臂的一端(110)通过环形线性连接单元连接到旋转斜盘,另一端(120)通过驱动单元的滑道连接单元连接到转子桅杆。独立的权利要求还包括旋翼飞机的旋翼,该旋翼飞行器的旋翼具有绕旋转轴线旋转驱动叶片的旋翼桅杆。

著录项

  • 公开/公告号EP2314507A1

    专利类型

  • 公开/公告日2011-04-27

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号EP20100009658

  • 发明设计人 GIRARD VINCENT;

    申请日2010-09-16

  • 分类号B64C27/605;

  • 国家 EP

  • 入库时间 2022-08-21 17:54:34

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