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.


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    Titel :

    ENGAGEMENT AND DISENGAGEMENT OF TAIL ROTOR


    Weitere Titelangaben:

    EIN- UND AUSSERBETRIEBNAHME DES HECKROTORS
    ENGAGEMENT ET DÉSENGAGEMENT DU ROTOR DE QUEUE


    Beteiligte:

    Erscheinungsdatum :

    2020-10-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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