Combustion chamber for gas turbine engines, particularly an igni

Details Combustion chamber for gas turbine engines, particularly an igni Combustion chamber for gas turbine engines, particularly an igni

1978-05-08

1980-05-27

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Combustion products generator

60 3982S, F02G 300

Patent

active

042044049

ABSTRACT:
A combustion chamber for gas turbine engines, particularly aircraft turbojet engines, which is constituted of an outer casing, at least one flame tube inserted therein, and incorporating at least one ignition device for the produced, respectively, supplied fuel-air mixture. The ignition device comprises two high-capacity ignition or spark plugs which are presently arranged in series in a single axial plane in the flame tube, and further including an ignition fuel nozzle, whose fuel injection spray cone will simultaneously encompass the ignition spark zones of both high-capacity spark plugs.

REFERENCES:
patent: 2496502 (1950-02-01), Steensma
patent: 3264825 (1966-08-01), Halls et al.

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