Airplane front wing servo acting system and servo control method thereof

The invention belongs to a flight control technology and relates to an airplane front wing servo acting system and a servo control method thereof. The servo acting system comprises an electro-hydraulic combined steering engine (1), a spring pull rod (3), a support (2), a rocker arm (6), a pull rod (...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	XU WENLIANG, CHU BING, ZHAO DONGBAI, ZHOU JINGXIANG, PANG ZHIJUN
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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