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
2023-10-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Tail Rotor Configurations for Rotorcraft Yaw Control Systems
European Patent Office | 2022
|European Patent Office | 2016
|European Patent Office | 2019
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