Method of operating catalytically supported thermal combustion s

Details Method of operating catalytically supported thermal combustion s Method of operating catalytically supported thermal combustion s

1974-04-24

1976-03-02

Freeh, William L.

Power plants

Combustion products used as motive fluid

60 3902, 431 7, F02C 316, F02C 726

Patent

active

039409236

ABSTRACT:
An improved method is provided for more efficiently operating a catalytically supported thermal combustion gas turbine system, and at the same time provide low emissions of unburned hydrocarbons, carbon monoxide, and nitrogen oxides. In the adiabatic combustion of the fuel and air admixture at least a portion of the thermal combustion of the fuel takes place in the expansion zone of the gas turbine to counteract the cooling effect of the expansion of the gases.

REFERENCES:
patent: 2243467 (1941-05-01), Jendrassik
patent: 2632296 (1953-03-01), Houdry
patent: 3191659 (1965-06-01), Weiss
patent: 3705492 (1972-12-01), Vickers
patent: 3890088 (1975-06-01), Ferri
Haslam et al., Fuels and Their Combustion, N.Y., 1926, pp. 266, 282, 287-288.
Smith I. E., (editor), Combustion in Advanced Gas Turbine Systems, Pergamon Press, 1967, pp. 14-15.

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