F - Mech Eng,Light,Heat,Weapons – 23 – R
Patent
F - Mech Eng,Light,Heat,Weapons
23
R
F23R 3/20 (2006.01) F02K 3/10 (2006.01)
Patent
CA 2586431
A fuel shield (68) is configured for use in the afterburner (34) of a turbofan aircraft engine (10). The shield (68) includes wings (72,74) obliquely joined together at a nose (76) to conform with the leading edge region (52) of a flameholder vane (42). A hood (78) is joined to the wings (72,74) and extends obliquely therefrom to conform with a supporting outer shell (44) of the flameholder (34).
Mayer Jeffrey Carl
Roberts Brian Benscoter
Company General Electric
Craig Wilson And Company
LandOfFree
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