发明名称 |
Altitude and speed assist control circuit for helicopter has sensors for speed and altitude for comparison to reference values for power correction |
摘要 |
The altitude and speed control assist for a helicopter (2) has a sensor circuit (22) to deliver signals dependent on the altitude and speed values and a stored value memory (26) for predetermined altitude and speed levels. A circuit (20) controls the sensed values to correspond to the stored values . The circuit automatically varies the pitch and or power developed by the aircraft engines to cause the signals to correspond.
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申请公布号 |
FR2844607(A1) |
申请公布日期 |
2004.03.19 |
申请号 |
FR20020011454 |
申请日期 |
2002.09.16 |
申请人 |
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE CNRS |
发明人 |
FRANCESCHINI NICOLAS;RIFFIER FRANCK;VIOLLET STEPHANE;BOYRON MARC |
分类号 |
B64D43/00;G05D1/06;G05D1/08;(IPC1-7):G05D1/10;B64C13/16 |
主分类号 |
B64D43/00 |
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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