| 摘要 |
An accessory system (60) for a gas turbine engine includes an accessory gearbox which defines an accessory gearbox axis (L) and comprises four gear sets (84B, A, F, E) comprising each a drive gear ( 86B, A, F E) and a spur gear (88B, A, F, E), wherein the first and second spur gears (88A, B) are meshed, the third and fourth spur gears (88E, and 88F) are meshed and a crossover gear set (92) having a crossover drive gear (86D) meshed with the first and the third drive gears (86B, F).
Gas turbine engine comprising an engine case section (44) and an accessory gearbox.
An accessory system (60) for a gas turbine engine includes an accessory gearbox which defines an accessory gearbox axis (L). A crossover gear set (92) generally along the accessory gearbox axis (L) interconnects a first gear set (84C) and a second gear set (84E). |
