Combustor for gas turbine

Details Combustor for gas turbine Combustor for gas turbine

1993-01-13

1994-06-28

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Combustion products generator

60749, 60760, F02C 0100

Patent

active

053236149

ABSTRACT:
A premixed combustor for a gas turbine, comprises, a combustion chamber for burning a fuel with an air therein, at least two premixed fuel/air mixture outlets which are juxtaposed with each other, and through each of which a premixed fuel/air mixture flows out into the combustion chamber, and a flow deflection member arranged between the premixed fuel/air mixture outlets, urging the permixed fuel/air mixture from one of the premixed fuel/air mixture outlets to go away from another one of the premixed fuel/air mixture outlets, and terminating in the combustion chamber so that the premixed fuel/air mixture from the one of the premixed fuel/air mixture outlets is permitted to move toward the premixed fuel/air mixture flowing out from the another one of the premixed fuel/air mixture outlets after going away from the another one of the premixed fuel/air mixture outlets.

REFERENCES:
patent: 3817690 (1974-06-01), Bzyce et al.
patent: 3921391 (1975-11-01), Hall et al.
patent: 4445337 (1984-05-01), Davis, Jr. et al.
patent: 4898001 (1990-02-01), Kuroda et al.
patent: 5054280 (1991-10-01), Ishibashi
patent: 5069029 (1991-12-01), Kuroda et al.
patent: 5121597 (1992-06-01), Urushidani et al.

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