Exhaust duct with bypass channel

Details Exhaust duct with bypass channel Exhaust duct with bypass channel

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/30 (2006.01) F01D 25/24 (2006.01) F02K 1/78 (2006.01)

Patent

CA 2638661

An exhaust duct for directing a stream of exhaust gases in a gas turbine engine is provided. The exhaust duct comprises an inlet for receiving the stream of exhaust gases from a turbine section of the gas turbine engine; an outlet in fluid communication with the inlet; and a transition portion defining a passage between the inlet and the outlet. The passage comprises an annular region having a first side portion and a second side portion that are separated by a flow splitter. At least one bypass channel interconnects the first side portion and the second side portion of the annular region.

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