Combustor for gas turbine
A combustor for a gas turbine is described which consists of: inner cylinder means for defining a combustion chamber with a plurality of louvers for supplying air into the combustion chamber, the combustion chamber including a head combustion chamber and a main combustion chamber, the main combustion chamber being disposed downstream of the head combustion chamber and having a larger cross-sectional area than the head combustion chamber taken along a plane perpendicular to a longitudinal axis of the combustion chamber; outer housing means for surrounding the inner cylinder means to form an air passage means communicating with the combustion chamber through the louvers; first fuel supply means for supplying a gaseous fuel into the head combustion chamber.
- Assignee:
- Hitachi, Ltd., Tokyo
- Patent Number(s):
- US 4598553
- OSTI ID:
- 5396247
- Country of Publication:
- United States
- Language:
- English
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