Helicopter rotor
    1.
    发明授权
    Helicopter rotor 失效
    直升机转子

    公开(公告)号:US4808075A

    公开(公告)日:1989-02-28

    申请号:US123605

    申请日:1987-11-20

    IPC分类号: B64C27/37 B64C27/32 B64C27/38

    CPC分类号: B64C27/322

    摘要: A helicopter rotor on which each blade is connected in articulated manner to a center hub by means of a fork, the vertical plane movement of which is limited, below a given speed of the rotor, by a pair of limit rocker arms located between the hub and a ring nut mounted for rotation on the fork and angularly integral with the hub by means of a rod of variable length connected in articulated manner to a slide supported on the hub and arranged substantially horizontally and crosswise in relation to the blade.

    摘要翻译: 一种直升机转子,每个叶片通过叉子以铰接的方式连接到中心毂,其垂直平面运动受到转子的给定速度的限制,位于毂之间的一对限位摇臂 以及环形螺母,其安装成用于在叉上旋转并且通过可变长度的杆以与铰接的方式成角度地成一体的环形螺母连接到支撑在轮毂上的滑块,并且相对于叶片基本上水平且横向地设置。

    Helicopter rotor
    2.
    发明授权
    Helicopter rotor 失效
    直升机转子

    公开(公告)号:US4652211A

    公开(公告)日:1987-03-24

    申请号:US830543

    申请日:1986-02-18

    CPC分类号: B64C27/322

    摘要: Helicopter rotor on which each blade is connected in articulated manner to a center hub by means of a forkthe vertical plane movement of which, at rotor speeds below a given set value, is limited by a pair of limit rocker arms located between the hub and a ring nut mounted in rotary manner on the forkand rendered angularly integral with the hub by means of a compass drive.

    摘要翻译: 直升机转子,每个叶片通过叉子以铰接方式连接到中心毂,其转子速度低于给定设定值的垂直平面运动由一对位于轮毂和 环形螺母以旋转方式安装在叉上,并通过罗盘驱动器与轮毂成角度地成一体。