A gearbox system for a dual coaxial counter rotating rotor assembly includes an input shaft to input a first torque into the gearbox system and a transfer shaft operably connected to the input shaft to transfer the first torque therethrough. Two gear sets are operably connected to the transfer shaft. Each gear set includes a first output gear to transfer a second torque acting in a first direction to a first rotor of a rotor assembly and a second output gear to transfer the second torque acting in a second direction opposite the first direction to a second rotor of the rotor assembly. The second torque transferred by each gear set of the two gear sets is substantially equal.


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    Titel :

    ROTARY WING AIRCRAFT WITH A TORQUE SPLIT GEARBOX


    Weitere Titelangaben:

    DREHFLÜGELFLUGZEUG MIT EINEM LEISTUNGSVERZWEIGUNGSGETRIEBE
    AÉRONEF À VOILURE TOURNANTE AVEC UN BOÎTE DE VITESSES À COUPLE DIVISÉ


    Beteiligte:
    GARCIA TODD A (Autor:in)

    Erscheinungsdatum :

    2019-06-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16H Getriebe , GEARING



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