Gas turbine engine stored energy combustion system

Power plants – Combustion products used as motive fluid – With combustible gas generator

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60 39142, 60 3921, F02C 314, F23R 330

Patent

active

050690310

ABSTRACT:
Improved starting for turbine engines operating at low fuel flows and at high altitudes is accomplished in an engine 10 having an annular combustion 12 by utilizing a stored energy combustion system 28 which includes a source of oxidant 36 and a fuel source 38 both of which are in fluid communication with an auxiliary combustion space 32 of an auxiliary combustor 30 for combusting the oxidant and fuel to generate a gaseous fuel including secondary gases of combustion which are directed to the annular combustor 12 through a fuel injector 24 as a reactive, gaseous fuel ignitable therewithin.

REFERENCES:
patent: 2916367 (1959-12-01), Stokes
patent: 4092824 (1978-06-01), Friedrich
patent: 4759178 (1988-07-01), Joy
patent: 4819423 (1989-04-01), Vershure, Jr. et al.
patent: 4899536 (1990-02-01), Vershure

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