发明授权
US09527577B2 Rotorcraft with a fuselage and at least one main rotor 有权
转子陀飞轮与机身和至少一个主转子

Rotorcraft with a fuselage and at least one main rotor
摘要:
A rotorcraft with a fuselage and at least one main rotor, the at least one main rotor being drivable for controlling an associated pitch attitude of the rotorcraft in operation, and the fuselage being equipped with at least one passive wing-type aerodynamic device that is adapted for generating independently of the associated pitch attitude a lift force acting on the fuselage, the lift force being oriented perpendicular to an air flow that is directed in operation of the rotorcraft against the passive wing-type aerodynamic device.
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