Combustion apparatus

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

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Details

431350, F02G 100

Patent

active

040487970

ABSTRACT:
The present invention provides gas turbine reheat combustion apparatus for aircraft propulsion. The apparatus includes means for producing a flame stabilization zone in a stream of combustion supporting gas flowing in a duct, said stabilization zone having a recirculatory flow region therein, an injector for introducing a fluid comprising an inert diluent such as, for example, nitrogen, into the recirculatory flow region, and means for supplying the fluid to the injector.

REFERENCES:
patent: 1536176 (1925-05-01), Aldrich
patent: 2592110 (1952-04-01), Berggren et al.
patent: 3030773 (1962-04-01), Johnson
patent: 3817690 (1974-06-01), Bryce et al.
patent: 3831375 (1974-08-01), Richard et al.

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