Micro combustion chamber with double-walled structure of combustion gas turbine
A micro gas turbine and combustion chamber technology, which is applied in combustion chambers, continuous combustion chambers, combustion methods, etc., can solve the problems of low combustion efficiency, short gas residence time, and poor flame stability of micro combustion chambers, and achieve very high combustion efficiency and The effect of flame stability, temperature reduction, and heat dissipation loss reduction
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[0021] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0022] The combustor of a micro gas turbine with a double-wall structure described in this embodiment uses methane gas fuel. like figure 1 As shown, the combustion chamber is mainly composed of the combustion chamber outer casing 6, the flame cylinder outer ring 12, the flame cylinder inner ring 13, the combustion chamber casing 14, the ignition needle 5, the combustion chamber outlet outer casing 7 and the combustion chamber outlet inner casing 9 constitute. The outer ring 12 of the flame tube is made of porous sintered material, the inner ring 13 of the flame tube, the outer casing 7 of the combustion chamber outlet, and the inner casing 9 of the combustion chamber outlet are made of superalloy materials, and the outer casing 6 of the combustion chamber and the casing 14 of the combustion chamber are made of stainless steel . The compone...
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