Patent ID: 9068515
Filing Date: 2015-06-30
Classification: F02C,F05D,Y10T

Abstract:
1. An accessory system for a gas turbine engine comprising: an accessory gearbox which defines an accessory gearbox axis, the accessory gearbox including a first side and a second side; a first geartrain within the accessory gearbox including one or more shafts rotatable about axes perpendicular to the first side of the accessory gearbox; a second geartrain within the accessory gearbox including one or more shafts rotatable about axes perpendicular to the second side of the accessory gearbox; a driven gear set defining an input axis; a first drive gear set driven by the driven gear set about a first drive axis for driving the first geartrain; and a second drive gear set driven by the driven gear set about a second drive axis for driving the second geartrain, wherein the first drive axis and the second drive axis are substantially parallel to the input axis.