An accessory drive system for an aircraft gas turbine engine is disclosed. The system may comprise an engine case including a core engine cowl and at least a first accessory drive gearbox disposed within the core engine cowl. The at least first accessory drive gearbox may be operatively connected to one or more accessories remotely located therefrom.


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    Title :

    DISTRIBUTED ENGINE ACCESSORY DRIVE


    Additional title:

    VERTEILTER ANTRIEB VON TRIEBWERK ANBAUGERÄTEN
    PRISE D'ENTRAÎNEMENT DES ACCESSOIRES DE MOTEUR RÉPARTI


    Contributors:

    Publication date :

    2019-02-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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