Dual-fuel feed system for a gas turbine engine

Details Dual-fuel feed system for a gas turbine engine Dual-fuel feed system for a gas turbine engine

1975-06-19

1976-11-16

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Using special fuel or oxidizer

60 3974B, 431 60, 431181, 137604, 137606, F02C 722, F17D 104

Patent

active

039915611

ABSTRACT:
The dual-fuel feed system for a gas turbine engine, having a plurality of fuel nozzles arranged to effect admixture of air and fuel in a combustor of the engine for combustion of fuel, comprises a fuel feed conduit means communicating with each of the fuel nozzles and separate sources of different fuels and flow control means for alternating flow of fuel from one source or the other to the fuel nozzles.

REFERENCES:
patent: 2637334 (1953-05-01), Starkey
patent: 2771741 (1956-11-01), Barnard
patent: 2854819 (1958-10-01), Walker
patent: 2931429 (1960-04-01), Brown
patent: 3139724 (1964-07-01), Nerad et al.
patent: 3267676 (1966-08-01), Sneeden
patent: 3517679 (1970-06-01), Williamson
patent: 3766734 (1973-10-01), Jones

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