F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/22 (2006.01) F23R 3/28 (2006.01)
Patent
CA 2604636
A gas turbine engine (10) internal fuel manifold (22) has a plurality of airblast fuel nozzles (26) in communication with an air source such that nozzle core air does not pass through the manifold (22).
Le collecteur de combustible interne (22) d~une turbine à gaz (10), selon l~invention, comporte une pluralité d~injecteurs de carburant à air comprimé (26) communiquant avec une source d~air de telle sorte que l~air au centre de la buse ne traverse pas le collecteur (22).
Kojovic Aleksandar
Prociw Lev Alexander
Shafique Harris
Norton Rose Or S.e.n.c.r.l. S.r.l./llp
Pratt & Whitney Canada Corp.
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