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Rotor head for helicopter - includes bidirectional joint centre of which takes weight instead of needle-roller bearings

机译:直升机旋翼头-包括双向关节中心,该中心关节承担重量而不是滚针轴承

摘要

The helicopter rotor head includes four blades propelled by jets of pressurised cold air passing through an integral distributor. The head contains a cross (CR) the arms (CRa-CRd) of which run in needle-roller bearings. One pair of opposing arms (CRa,CRb) is connected into the distributor and the other into an upper shell. The centre of the cross has upper (CRe) and lower (CRf) spherical parts which contact concave supports (CMa,CMb) one attached to the upper shell (E2) and the other to the distributor (E1). The supports (CMa,CMb) take the weight of the upper shell instead of the needle-roller bearings, ensuring greater longevity.
机译:直升机旋翼头包括四个叶片,这些叶片由穿过整体分配器的加压冷空气射流推动。头部包含一个十字(CR)臂(CRa-CRd),该臂在滚针轴承中运行。一对相对的臂(CRa,CRb)连接到分配器,另一对连接到上壳。十字形的中心具有上球形(CRe)和下球形(CRf),它们与凹形支撑(CMa,CMb)接触,一个附接到上壳(E2),另一个附接到分配器(E1)。支撑件(CMa,CMb)承担上壳体的重量,而不是滚针轴承的重量,从而确保更长的使用寿命。

著录项

  • 公开/公告号FR2477501A1

    专利类型

  • 公开/公告日1981-09-11

    原文格式PDF

  • 申请/专利权人 DECHAUX CHARLES;

    申请/专利号FR19800005145

  • 发明设计人

    申请日1980-03-07

  • 分类号B64C27/37;

  • 国家 FR

  • 入库时间 2022-08-22 15:01:30

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