F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
F - Mech Eng,Light,Heat,Weapons
02
K
F02K 3/02 (2006.01) F01D 17/00 (2006.01) F02C 9/18 (2006.01) F02K 1/78 (2006.01)
Patent
CA 2545761
A nozzle assembly (100) for an engine (10) including a core engine (40) and at least one bypass duct (52) for channeling airflow around the core engine includes a liner (110) comprising an inner surface and an outer surface, wherein the inner surface confines airflow within a nozzle bypass duct (108), and the outer surface confines airflow discharged from the core engine. A plurality of strut members (106) are coupled to and support the liner. A plurality of fairings (104) are in flow communication with the at least one bypass duct, and each fairing is upstream from a respective one of the plurality of strut members to facilitate directing a portion of the airflow from the bypass duct past the plurality of strut members.
Jumper Matthew Wilson
Renggli Bernard James
Company General Electric
Craig Wilson And Company
LandOfFree
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