F - Mech Eng,Light,Heat,Weapons – 23 – R
Patent
F - Mech Eng,Light,Heat,Weapons
23
R
F23R 3/28 (2006.01) F23D 14/06 (2006.01) F23R 3/12 (2006.01) F23R 3/54 (2006.01)
Patent
CA 2509895
A gas fuel nozzle for mounting in a combustor wall of a gas turbine engine, with an at least partially radially-directed array of gas fuel outlets extending beyond an air flow head having an array of compressed air jet apertures around the gas fuel outlets. The air flow head also has a deflector for creating an axial flow of air for deflecting in an axial direction the radially-injected gas fuel.
L'invention concerne un injecteur de combustible gazeux à monter dans une paroi de chambre de combustion d'une turbine à gaz. Un jeu d'orifices de combustible gazeux dirigé radialement au moins partiellement s'étend au-delà d'une tête d'écoulement d'air qui possède des ouvertures de jet d'air comprimé autour des orifices de carburant gazeux. La tête d'écoulement d'air présente également un déflecteur servant à créer un flux d'air axial de manière à dévier dans une direction axiale le carburant gazeux injecté radialement.
Mccaldon Kian
Oskooei Saeid
Norton Rose Or S.e.n.c.r.l. S.r.l./llp
Pratt & Whitney Canada Corp.
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