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.
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
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