An exemplary rotorcraft (10) includes a propulsion system (22) including a prime mover (26) and a drive shaft (32) coupled to the prime mover (26), the drive shaft (32) including a coupling (36) separating the drive shaft (32) into an input shaft (38) and an output shaft (40), the coupling (36) operable between an engaged position rotationally coupling the input shaft and the output shaft and a disengaged position rotationally disengaging the output shaft from the input shaft, a main rotor (18) coupled to the prime mover, a secondary rotor (18') attached to the output shaft, and a motor (56) coupled to the output shaft.
ENGAGEMENT AND DISENGAGEMENT OF TAIL ROTOR
EIN- UND AUSSERBETRIEBNAHME DES HECKROTORS
ENGAGEMENT ET DÉSENGAGEMENT DU ROTOR DE QUEUE
2020-10-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Modeling and Simulation of Rotor Engagement and Disengagement During Shipboard Operations
British Library Conference Proceedings | 2004
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