F - Mech Eng,Light,Heat,Weapons – 23 – R
Patent
F - Mech Eng,Light,Heat,Weapons
23
R
F23R 3/28 (2006.01) F23R 3/34 (2006.01)
Patent
CA 2443979
A combustion system for a power generating gas turbine engine which includes at least a combustion chamber with a annular fuel manifold at one end of the combustion chamber and a passageway having a narrow throat downstream of the fuel manifold whereby air passes around the fuel manifold and mixes with fuel and is diffused through the passageway into the burn zone defined in the combustion chamber in an ultimate location.
L'invention concerne un système de combustion destiné à une turbine à gaz génératrice de puissance et comprenant au moins une chambre de combustion dotée, d'une part à une extrémité, d'une rampe de distribution de carburant annulaire et, d'autre part, d'un passage ayant un col étroit en aval de la rampe de distribution de carburant. De l'air contourne la rampe de carburant et se mélange au carburant. Ce mélange est diffusé par le passage dans la zone de combustion définie dans la chambre de combustion dans une position finale.
Norton Rose Or S.e.n.c.r.l. S.r.l./llp
Pratt & Whitney Canada Corp.
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