发明授权
US5242130A Method and device for the reduction of the oscillations of a divergent nature of the fuselage of a helicopter 失效
用于减少直升机的融合的多种性质的振荡的方法和装置

Method and device for the reduction of the oscillations of a divergent
nature of the fuselage of a helicopter
摘要:
Method and device for the reduction of the oscillations of a divergent nature induced in the fuselage (2) of a helicopter (1) by its rotary wings (3) when they are turning. According to the invention, the oscillations are detected (at 17, 18) and they are converted (at 19, 20) into electrical signals, which are used (at 13) in order to produce pitch variations of the blades (4) of the rotary wings (3), in such a way that a rotating torque vector opposing said oscillations results.
公开/授权文献
信息查询
0/0