Low emissions gas turbine combustor

Power plants – Combustion products used as motive fluid – Combustion products generator

Patent

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Details

60746, F23R 320, F02C 722

Patent

active

050707000

ABSTRACT:
A combustor for a gas turbine engine includes divergent mixing cones disposed within the combustion chamber proper to provide a flow restriction which separates the combustion chamber into primary and secondary combustion zones. Placement of the mixing cones within the chamber enhances vaporization of the fuel and permits combustion to take place in the primary zone at flame temperature below the stoichiometric temperature thereby reducing formation of nitrous oxides.

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patent: 4356698 (1982-11-01), Chamberlain
patent: 4389848 (1983-06-01), Markowski et al.
patent: 4928481 (1990-05-01), Joshi et al.

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