The application relates to the technical field of micro-scale
combustion, in particular to a
micro combustion chamber with a regenerative structure. The
micro combustion chamber with the regenerative structure is used for a gas
turbine and comprises a fluid passage, the fluid passage can circulate air and fuel, the fluid passage is provided with an outer exhaust passage, an outer ring cavity, a
flame tube inner cavity, an inner ring cavity, an inner exhaust passage and a
fuel gas collecting cavity, the air flows into the
flame tube inner cavity through the outer ring cavity and the inner ring cavity in sequence, the fuel can flow into the
flame tube inner cavity through the
fuel gas collecting cavity, the air and the fuel are combusted in the flame tube inner cavity to form high-temperature
fuel gas, and the high-temperature fuel gas flows into the outer exhaust passage through the inner exhaust passage; the high-temperature fuel gas in the inner exhaust passage and the flame tube inner cavity can exchange heat with the air in the inner ring cavity, and the high-temperature fuel gas in the outer exhaust passage and the flame tube inner cavity can exchange heat with the air in the outer ring cavity. In this way, the air is preheated by the high-temperature fuel gas, the total heat cycle
thermal efficiency is improved, and the
combustion chamber performance is improved.