Gas turbine combustor

Details Gas turbine combustor Gas turbine combustor

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/16 (2006.01) F23R 3/00 (2006.01) F23R 3/04 (2006.01) F23R 3/28 (2006.01)

Patent

CA 2392262

A gas turbine combustor is provided with a nozzle extension tube having an inclination outward in a diameter direction of a combustor inner cylinder and in a peripheral direction of the combustor inner cylinder. As a result, the premixed gas is transformed to a spiral flow passing into a combustion chamber while turning, i.e.; an outward turning flow, thereby sufficiently mixing the premixed gas while the premixed gas is flowing in the combustion chamber.

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