An example gas turbine engine (20) includes, among other things, a nacelle (66) having an inner wall (70) providing a bypass duct (78) of a gas turbine engine (20), and an outer wall (74); an accessory gearbox (86) is received between the inner wall (70) and the outer wall (74) of the nacelle (66); and an accessory drive (D4, D5) of the accessory gearbox (86) is configured to rotate about an accessory drive axis (AT) that is transverse to a central axis (A) of the gas turbine engine (20).
GAS TURBINE ENGINE ACCESSORY GEARBOX
HILFSGETRIEBE FÜR EINEN GASTURBINENMOTOR
BOÎTE DE VITESSES ACCESSOIRE DE MOTEUR À TURBINE À GAZ
2024-05-01
Patent
Electronic Resource
English