Multiple passage cooling circuit method and device for gas turbi

Power plants – Combustion products used as motive fluid – Combustion products generator

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60742, 60746, 2391325, F02G 722

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active

055705804

ABSTRACT:
A gas turbine fuel nozzle and method of fuel flow provide resistance to coking of the fuel by means of a multiple passage heat transfer cooling circuit. Fuel streams to primary and secondary sprays of pilot and main nozzle tips are arranged to transfer heat between the pilot primary fuel stream and each of the main secondary fuel stream and the pilot secondary fuel stream. This protects the fuel in the streams from coking during both low flow, lower engine heat conditions and high flow, high engine heat conditions. This nozzle and flow can protect engines with both single tip and dual tip nozzles.

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International Search Report from WIPO completed Jan. 7, 1994.

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