Combustion chamber for a gas turbine

Details Combustion chamber for a gas turbine Combustion chamber for a gas turbine

2005-10-25

2005-10-25

Kim, Ted (Department: 3746)

Power plants

Combustion products used as motive fluid

Combustion products generator

C060S755000, C060S756000, C239S132300

Reexamination Certificate

active

06957538

ABSTRACT:
The invention relates to a combustion chamber for a gas turbine having at least one closed-circuit-cooled burner insert which can be disposed in an inlet opening of the combustion chamber for the purpose of feeding and/or igniting a combustible gas/air mixture, and having an outlet opening.The object of the present invention is therefore to create an arrangement enabling simplified manufacture and assembly to be achieved.To achieve this object there is proposed according to the invention a combustion chamber for a gas turbine having at least one closed-circuit-cooled burner insert which can be disposed in an inlet opening of the combustion chamber for the purpose of feeding and/or igniting a combustible gas/air mixture, and having an outlet opening, at least one hot-gas-path component, specifically a component of an inner wall of the combustion chamber, forming on its outer side opposite the hot-gas-path side (55), in conjunction with a planar shaped element disposed thereabove, at least one channel which is fluidically connected to a coolant source on the feed side and to a channel arrangement of the burner insert on the discharge side.

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patent: 0 725 253 (1996-08-01), None
patent: WO 97/14875 (1997-04-01), None

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