Variable geometry combustor apparatus and associated methods

Power plants – Combustion products used as motive fluid

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60733, 60742, F02C 700, F02C 722

Patent

active

045677247

ABSTRACT:
The fuel nozzles in a variable geometry combustor cooperate with an inwardly projecting liner wall section to define a sheltered pilot combustion zone within the liner. Simultaneously operable inlet valves are provided for admitting a selectively variable quantity of combustion air into the pilot zone.

REFERENCES:
patent: 2227666 (1941-01-01), Noack
patent: 4192139 (1980-03-01), Buchheim
patent: 4420929 (1983-12-01), Jorgensen et al.
patent: 4459803 (1984-07-01), Marshall
Carlstrom et al., "Improved Emissions Performance in Today's Combustion System", paper presented at AEG/SOA International Seminar; Athens, Greece, Jun. 1978.

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