Ejector controlled twin air source gas turbine pressurizing...

Details Ejector controlled twin air source gas turbine pressurizing... Ejector controlled twin air source gas turbine pressurizing...

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 3/13 (2006.01) B64D 13/02 (2006.01) F01D 17/00 (2006.01)

Patent

CA 2582075

A passive pressurizing air system for a gas turbine engine comprises a flow path for directing an air flow having a low temperature and low pressure, extending through a cavity to a pressurized area of the engine. The cavity contains pressurized air having a high temperature and high pressure. Means are provided for adding the pressurized air from the cavity into the flow path to provide a mixed air flow having an intermediate temperature and intermediate pressure.

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