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Helicopter main rotor head - has gimbal mounted, rigidly linked main blade attitude controlled by pivoted blade shape weights angled from swashplate

机译:直升机主旋翼机头-装有万向架,刚性连接的主桨叶姿态由与斜盘成角度的枢转桨叶形状配重控制

摘要

The main-rotor head for a helicopter has a gimbal mounting on the end of a motor-driven shaft, carrying main blades rigidly linked with a constant pitch relationship plus stabilising weights and controllable via a swashplate and a rod-plus lever linkage. For unmanned equipment-carrying, helicopters the stabilising weights are given the form of (conventional) relatively heavy auxiliary blades (6) carried by a rod (3) passing through the gimbal-mounting's centre and rotatable via the swashplate (9) and linkage (7,8). The linkage greatly amplifies swashplate tilting movement. (DS).
机译:直升机的主旋翼头在万向轴的末端装有一个万向架,以恒定的螺距关系刚性地连接主叶片,并具有稳定的重量,并可以通过斜盘和杆加杠杆连杆进行控制。对于无人驾驶设备,直升飞机的稳定重物采用(常规)相对较重的辅助叶片(6)的形式,由杆(3)穿过万向支架底座的中心并通过斜盘(9)和连杆可旋转( 7,8)。连杆极大地增加了斜盘的倾斜运动。 (DS)。

著录项

  • 公开/公告号DE2045913A1

    专利类型

  • 公开/公告日1972-03-23

    原文格式PDF

  • 申请/专利权人

    申请/专利号DE19702045913

  • 发明设计人

    申请日1970-09-17

  • 分类号B64C27/625;

  • 国家 DE

  • 入库时间 2022-08-23 08:21:52

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