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
2019-05-21
Patent
Electronic Resource
English
GASKET - ENGINE ACCESSORY DRIVE
SAE Technical Papers | 2014
GASKET - ENGINE ACCESSORY DRIVE
SAE Technical Papers | 2004
GASKET - TYPE XIII ENGINE ACCESSORY DRIVE
SAE Technical Papers | 2004