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Phase controller for helicopter, has connector moved by drive shaft so that connecting rods are rotated to operate controller of helicopter, where rotational axes of connecting rods run vertically to longitudinal direction of fuselage

机译:直升机的相位控制器,其连接器通过驱动轴移动,从而使连杆旋转以操作直升机的控制器,其中连杆的旋转轴垂直于机身的纵向方向

摘要

The controller has a drive shaft (12) vertically protruding from a front side of a fuselage (1). A cam plate (15) lies on the front side of the fuselage and is implemented in a middle of the driveshaft. A connector (31) is arranged on a side of the cam plate. The connector is moved by the drive shaft so that connecting rods (32, 33) are rotated to operate the controller of a helicopter, where rotational axes of the connecting rods run vertically to a longitudinal direction of the fuselage.
机译:控制器具有从机身(1)的前侧竖直地突出的驱动轴(12)。凸轮板(15)位于机身的前侧,并安装在驱动轴的中间。连接器(31)布置在凸轮板的一侧。连接器通过驱动轴移动,从而使连杆(32、33)旋转以操作直升机的控制器,其中连杆的旋转轴垂直于机身的纵向方向延伸。

著录项

  • 公开/公告号DE202007001203U1

    专利类型

  • 公开/公告日2007-08-09

    原文格式PDF

  • 申请/专利权人 THUNDER TIGER CORP.;

    申请/专利号DE202007001203U1

  • 发明设计人

    申请日2007-01-26

  • 分类号B64C27/59;

  • 国家 DE

  • 入库时间 2022-08-21 20:28:58

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