发明名称 PRIMARY FLIGHT CONTROLS
摘要 PURPOSE: A main steering device is provided to implement a power-up and built-in test by inspecting the control ability of the main steering device with a smart interface actuator before flight. CONSTITUTION: A main steering device(10) comprises a steering wheel, a flight control computer(1), an electric motor(5), and a mechanical linkage(7). At least one pilot deals the steering wheel. The flight control computer is connected to the steering wheel. The electric motor is formed on a main rotary blade and a tail rotary blade. The flight control computer transmits electric signals to the electric motor. The mechanical linkage connects the electric motor to a hydraulic servo actuator(8) for controlling the main rotary blade and the tail rotary blade.
申请公布号 KR20130006322(A) 申请公布日期 2013.01.16
申请号 KR20120072461 申请日期 2012.07.03
申请人 EUROCOPTER DEUTSCHLAND GMBH;EUROCOPTER 发明人 CHADUC BRUNO;GROHMANN BORIS;TEMPIER CHRISTOPHE
分类号 B64C27/68;B64C13/50;B64C27/64 主分类号 B64C27/68
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