Gas turbine engine and method of operating same

Details Gas turbine engine and method of operating same Gas turbine engine and method of operating same

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/72 (2006.01) B64C 9/38 (2006.01)

Patent

CA 2592911

A thrust reverser assembly (100) for a gas turbine aircraft engine is provided. The thrust reverser assembly (100) includes a first plurality of turning vanes (180) for channeling airflow from the gas turbine engine (10) across a surface of an aircraft wing (12) to facilitate increasing lift, and a second plurality of turning vanes (182) for channeling airflow from the gas turbine engine to effect reverse thrust.

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