Starting means for a gas turbine engine

Details Starting means for a gas turbine engine Starting means for a gas turbine engine

1981-07-29

1983-11-29

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Different fluids

60742, 60746, F02C 7264

Patent

active

044174390

ABSTRACT:
Improvement to the starting characteristics of an annular combustor for a gas turbine engine that employs dual fuel nozzles (primary and secondary fuel flow systems) by redistributing the total fuel admitted to the nozzles in an asymmetrical pattern to deliver the requisite amount of fuel to the igniter by the primary flow system feeding fuel to that igniter.

REFERENCES:
patent: 2540642 (1951-02-01), Allen et al.
patent: 2969925 (1961-01-01), Burgess et al.
patent: 3763650 (1973-10-01), Hussey et al.
patent: 4062183 (1977-12-01), Davies et al.

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