Combination igniter and fuel atomizer nozzle assembly for a gas

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

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F02C 7264

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active

054919720

ABSTRACT:
An igniter and fuel atomizer nozzle assembly in a gas turbine engine includes an igniter in which a fuel conduit is positioned in a passageway in the igniter between its housing and its electrode for discharging atomized start up fuel from the end of the igniter housing closely proximate to the ignition spark generated by the electrode.

REFERENCES:
patent: 3057159 (1962-10-01), Bennedict
patent: 3073121 (1963-01-01), Baker et al.
patent: 4023351 (1977-05-01), Beyler et al.
patent: 4215979 (1980-08-01), Morishita
patent: 4938019 (1990-07-01), Angell et al.
patent: 5000159 (1991-03-01), Clarke et al.
patent: 5085040 (1992-02-01), Tilston
Lefebvre, Gas Turbine Combustion, Hemisphere Publishing Group (McGraw Hill), 1983, pp. 221-232.

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