Gas turbine combustor fed by a plurality of primary combustion c

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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60 3965, 60 3969R, 60 3982P, F02C 914, F02G 300

Patent

active

040731340

ABSTRACT:
The system has a plurality of small primary combustion chambers which lead into a larger secondary combustion chamber in order to reduce the amount of nitrous oxides produced during combustion and thus, lower, pollution. The primary combustion chambers are arrayed in a spherical pattern to eliminate the need for individual ignition devices and to provide a better mixing effect and a more uniform temperature distribution within the secondary combustion chamber.

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Wade et al., "Low Emissions Combustion for Regenerative Gas Turbine," ASME Paper, No. 73-6T-11, Dec. 1973, pp. 33, 34, 44, 45.

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