Method of distributing fuel flow to an annular burner for starti

Power plants – Combustion products used as motive fluid

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60 39141, F02C 726

Patent

active

045480320

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: 2701164 (1955-02-01), Purchas, Jr. et al.
patent: 3158998 (1964-12-01), Robinson et al.
patent: 3763650 (1973-10-01), Hussie et al.
patent: 4062183 (1977-12-01), Davies et al.
patent: 4417439 (1983-11-01), Sepulveda et al.

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