Gas turbine with atomizer nozzle

Details Gas turbine with atomizer nozzle Gas turbine with atomizer nozzle

1980-07-25

1983-11-15

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Combustion products generator

60737, 60751, 415DIG1, F02C 722

Patent

active

044148151

ABSTRACT:
A gas turbine engine which includes a combustion chamber adapted to be supplied with fuel by at least one atomizer nozzle. The gas turbine engine includes an air compressor for supplying compressed air to the combustion chamber, with the compressor including a secondary guide vane set having a plurality of ducts. At least one of the ducts of the secondary guide vane set is connected to the atomizer nozzle by means of a conduit. The at least one duct is equipped with a boundary layer bleed-off.

REFERENCES:
patent: 3362629 (1968-01-01), Papapanu
patent: 4081957 (1978-04-01), Cox, Jr.
patent: 4131389 (1978-12-01), Perrone et al.
patent: 4182117 (1979-01-01), Exley et al.

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