Combustor having enhanced weak extinction characteristics for a

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

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60756, F02C 100

Patent

active

054903890

ABSTRACT:
A gas turbine engine combustor (16) is provided with an airspray fuel injector (24), the downstream end of which is coplanar with a heat shield (38) provided at the upstream end of the combustor (16). The fuel injector (24) injects a fuel and air mixture into the combustion chamber (16a) defined within the combustor (16) which is in the form of a cone having an angle greater than 130.degree.. The combustor (16) has enhanced weak extinction characteristics.

REFERENCES:
patent: 3851462 (1974-12-01), Vranos
patent: 4122670 (1978-10-01), Reider
patent: 4246757 (1981-01-01), Heberling
patent: 4695247 (1987-09-01), Enzaki et al.
patent: 5012645 (1991-05-01), Reynolds
patent: 5094082 (1992-03-01), Thompson et al.

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