Purged flameholder fuel shield

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

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Details

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).

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