An engine reduction gear system includes at least two self-contained, independent engine reduction gearboxes (202a, 202b), each capable of connecting to an aircraft engine. Each of the engine reduction gearboxes (202a, 202b) provides redundant, reduced speed to a main rotor gearbox (208) via a shaft (206a, 206b).


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    Title :

    HIGH SPEED ENGINE REDUCTION GEARBOXES


    Additional title:

    HOCHGESCHWINDIGKEITSMOTORUNTERSETZUNGSGETRIEBE
    BOÎTES DE RÉDUCTION POUR MOTEUR À GRANDE VITESSE


    Contributors:

    Publication date :

    2021-05-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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