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Model aircraft rudder control system - is operated by rod system connected to two rudder adjustment machines and servo mechanism

机译:飞机模型舵控制系统-由连接到两个舵调节机和伺服机构的杆系统操作

摘要

The installation for controlling rudder movements of model aircraft, has a rod system connected to two rudder adjustment machines. The adjustment link is moved to a varying degree through one or more levers. One or both rudder adjustment machines have in addition a connection with a further adjustment link to be moved. One lever has its bearing on a servo, preferably a linear servo and a further rudder adjustment machine is fitted to one end of the lever, whilst the other end of the lever has a connection to the adjustment link to be actuated.
机译:用于控制模型飞机的舵运动的装置具有连接至两个舵调节机的杆系统。调节连杆通过一个或多个操纵杆以不同程度移动。一个或两个方向舵调节机还具有与另一条要移动的调节连杆的连接。一个杠杆将其轴承支承在伺服机构上,优选地是线性伺服机构,并且另一操纵舵调节机安装到该杠杆的一端,而杠杆的另一端具有与要致动的调节连杆的连接。

著录项

  • 公开/公告号DE2803506A1

    专利类型

  • 公开/公告日1979-10-04

    原文格式PDF

  • 申请/专利权人 NEUHIERLHERMANNDIPL.-CHEM.DR.;

    申请/专利号DE19782803506

  • 发明设计人 NEUHIERLHERMANNDIPL.-CHEM.DR.;

    申请日1978-01-27

  • 分类号A63H27/02;

  • 国家 DE

  • 入库时间 2022-08-22 19:47:00

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