| 发明名称 |
Model aircraft rudder control system - is operated by rod system connected to two rudder adjustment machines and servo mechanism |
| 摘要 |
<p>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.</p> |
| 申请公布号 |
DE2803506(A1) |
申请公布日期 |
1979.10.04 |
| 申请号 |
DE19782803506 |
申请日期 |
1978.01.27 |
| 申请人 |
NEUHIERL,HERMANN,DIPL.-CHEM.DR. |
发明人 |
NEUHIERL,HERMANN,DIPL.-CHEM.DR. |
| 分类号 |
A63H27/20;(IPC1-7):63H27/02 |
主分类号 |
A63H27/20 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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