Combustion apparatus including an air-fuel premixing chamber

Power plants – Combustion products used as motive fluid – With variable oxidizer control

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60732, 60737, F02C 900, F02G 300

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active

045638756

ABSTRACT:
A combustor for generating a hot gas stream by the combustion of fuel in a pressurized airstream is disclosed including a generally toroidal-shaped combustion chamber of relatively short axial length, an annular orifice providing for the entry of a main airstream into the combustion chamber and a premixing chamber for generating and directing a vapor phase air-fuel premixture into the entering main airstream to form a combustible mixture for burning in the combustion chamber. In a preferred form, the mixture burns along a generally toroidal-helical gas flow path. The combustor is particularly suited for use in a gas turbine engine.

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Wade et al., "Low Emission Combustion for Regenerative Gas Turbine, Part 1," ASME Transactions, Jan. 1974, pp. 33-47.

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