Invention Grant
US09562477B2 Accessory mounting for a gas turbine engine 有权
燃气轮机的配件安装

Accessory mounting for a gas turbine engine
Abstract:
A gas turbine engine assembly is connected to a pylon for mounting the gas turbine engine to an aircraft. The assembly has a frame supporting at least one accessory independently of the gas turbine engine. The frame is attached to the pylon at forward and rearward engine mounting locations. The frame comprises at least one hollow tube and at least one duct is arranged to supply coolant into the at least one hollow tube and the at least one hollow tube is arranged to supply coolant to the at least one accessory.
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