Annular type gas turbine combustor

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

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60751, F23R 326

Patent

active

059184590

ABSTRACT:
An annular type gas turbine combustor which can regulate air flow distribution without being influenced by high temperature flames and with a desired fuel-air ratio for reducing the generation of NO.sub.x etc. A slide duct (10), for regulating air flow distribution, is disposed slidably in an axial direction at a terminal end of a diffuser (1). And as the slide duct (10) is moved, air flow supplied downstream to a swirler (4) is regulated so as to obtain a desired fuel-air ratio.

REFERENCES:
patent: 2655787 (1953-10-01), Brown
patent: 3905192 (1975-09-01), Pierce et al.
patent: 4202170 (1980-05-01), Meyer

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