Variable geometry combustor apparatus

Power plants – Combustion products used as motive fluid – With variable oxidizer control

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Details

60733, 60742, F02C 314

Patent

active

045451966

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: 2856755 (1958-10-01), Szydlowski
patent: 2999359 (1961-09-01), Murray
patent: 3026675 (1962-03-01), Vesper et al.
patent: 3124933 (1964-03-01), Stram et al.
patent: 3961475 (1976-06-01), Wood
patent: 4192139 (1980-03-01), Buchheim
patent: 4420929 (1983-12-01), Jorgensen et al.
Carlstrom et al., Improved Emissions Performance in Today's Combustion System, paper presented at AEG/SOA Seminar; Athens, Greece; Jun. 1978.

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