Lean premixed combustion chamber for gas turbine
A gas turbine and combustor technology, applied in lean premixed combustion premixed fuel injection structure, lean premixed combustor field, can solve problems such as inability to achieve uniform air mixing
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[0031] The technical problem to be solved by the present invention is to improve the mixing effect of the premixed fuel and air in the gas turbine lean premixed combustor, reduce the NO X emission.
[0032] Technical scheme of the present invention is realized like this:
[0033] A cylindrical gas turbine combustor for burning gaseous fuel, comprising five parts in total, including a casing, a flame cylinder, a nozzle swirler assembly, a swirl cup assembly and an igniter.
[0034]The combustion chamber is generally divided into two layers, the outer side is the casing, and the inner side is the flame tube. A secondary channel of air is formed between the casing and the flame tube. There are a large number of circular holes on the wall of the rear of the casing, and the air from the compressor enters the secondary channel through these circular holes. The total area of the circular holes will be greater than twice the cross-sectional area of the two passages, to ensure th...
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