The
gas turbines of the present invention have multiple
combustion chambers, and within each chamber are multiple fuel nozzles. Each
nozzle has its own fuel control valve to control the fuel flowing to the nozzles. To minimize the pressure drop through the fuel
control valves, multiple manifolds are employed. Each manifold supplies at least one fuel
nozzle in multiple
combustion chambers with fuel. The fuel
control valves are mounted on the manifolds such that the weight of the fuel
control valves and nozzles are carried by the manifolds, not the multiple
combustion chambers. A plurality of thermocouples for measuring
exhaust gas from said multiple combustion chambers are employed to sense gas exhaust temperature. In carrying out the methods of the present invention for tuning a gas
turbine, it is essential to note that the most efficient gas
turbine is one which has the least nitrous oxides, the least amount of unburned hydrocarbons, and the least amount of
carbon monoxide for a specified energy output. In order to tune the gas
turbine to accomplish these objectives, it is desirable that each
combustion chamber in the gas turbine be well balanced relative to the remaining combustion chambers. It is an aim of the present invention to tune each of the multiple combustion chambers such that no specific
combustion chamber is rich or lean, and all are operating within about 1% of the remaining combustion chambers.