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.
DISTRIBUTED ENGINE ACCESSORY DRIVE
VERTEILTER ANTRIEB VON TRIEBWERK ANBAUGERÄTEN
PRISE D'ENTRAÎNEMENT DES ACCESSOIRES DE MOTEUR RÉPARTI
2019-02-06
Patent
Electronic Resource
English
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