A yaw control system coupled to a tailboom of a helicopter includes tail rotors. The tail rotors include a clockwise tail rotor and a counterclockwise tail rotor. The clockwise tail rotor is configured to rotate in a first rotational direction. The counterclockwise tail rotor is configured to rotate in a second rotational direction, the second rotational direction opposite of the first rotational direction.
Tail Rotor Configurations for Rotorcraft Yaw Control Systems
02.06.2022
Patent
Elektronische Ressource
Englisch
Tail rotor configurations for rotorcraft yaw control systems
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