Turbofan engine cowl assembly and method of operating the same

Details Turbofan engine cowl assembly and method of operating the same Turbofan engine cowl assembly and method of operating the same

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/68 (2006.01) F01D 17/10 (2006.01) F02C 9/16 (2006.01)

Patent

CA 2609282

A thrust reverser assembly (100) for a turbofan engine assembly (10), the engine assembly including a core gas turbine engine (20), a core cowl (22) which circumscribes the core gas turbine engine (20), a nacelle (24) positioned radially outward from the core cowl, a fan nozzle duct (26) having an area defined between the core cowl and a portion of the nacelle, and a thrust reverser positioned within a portion of the nacelle. The thrust reverser assembly includes a first cowl (104), a second cowl (102) repositionable with respect to the first cowl for varying the area of the fan nozzle duct, and at least one flow directing member (133, 137) coupled to the second cowl to selectively impede airflow from flowing through a cavity (156) defined between the first cowl and the second cowl.

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