US 6,598,383 B1Granted

Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels

AssigneeGeneral Electric Company

InventorsChristian L. Vandervort, Richard S. Bourgeois

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Abstract

A nozzle configuration and control methodology adapted to provide a compact means for configuring and operating an industrial gas turbine on either gaseous or liquid fuel while utilizing fuel staging to achieve very low emissions. More specifically, the outer fuel nozzles are used for delivery of a portion of the premix gaseous fuel and all liquid fuel, but not diffusion gaseous fuel. Water injection for emissions control on liquid fuel and atomizing air for the liquid fuel are also supplied entirely by the outer fuel nozzles. The central fuel nozzle is thus used for the supply of both premix gaseous fuel and all diffusion gaseous fuel. The disclosed configuration reduces the number of required fluid passages thus simplifying the endcover structure while enabling fuel staging to achieve very low emissions on gaseous fuel.

Claims4

Dependent claims

A method of operating a combustor wherein the combustor has a plurality of outer fuel nozzles in an annular array arranged about a center axis and a center nozzle located on the center axis, and wherein the annular array is selectively supplied with premix fuel, liquid fuel, water and atomizing air, and further wherein the center nozzle is selectively supplied with diffusion fuel and premix fuel, the method comprising the steps of:

a) at start-up, supplying the center fuel nozzle with diffusion fuel;
b) as the unit load is raised, supplying premix fuel to at least one of the outer nozzles in the annular array;
c) at part load, ceasing diffusion fuel flow to the center nozzle and redirecting a corresponding percentage of fuel to at least one of the outer nozzles in the annular array, thereby to maintain fuel flow constant;
d) after load is further increased, initiating premix fuel supply to the center nozzle without adding to the supply of premix fuel to the outer fuel nozzles in the annular array;
and then
e) selectively supplying additional premix fuel to all of the fuel nozzles in the annular array and to the center nozzle as the turbine load increases.

3 more elements

Dependencies are inferred from the claim text.