(US5693201-A)      An aero-derivative gas turbine power system (70) includes an electrochemical converter (72) and a gas turbine assembly. The gas turbine comprises a compressor (76), a turbine (80) and a generator (84). Air from a source (73) is introduced to the compressor where it is compressed and thus heated and is then discharged to the electrochemical converter. Fuel (74) is introduced to a preheater (68) where it is heated to an elevated temp.    The heated air and fuel function as input reactants and power the electrochemical converter. The converter (72) heats the compressed air and the fuel to produce a high temp. exhaust which is fed to the gas turbine to drive the generator.    ADVANTAGE -   Integrates an electrochemical converter and a gas turbine to create a high efficiency power system.    (JP11503860-W)      An aero-derivative gas turbine power system (70) includes an electrochemical converter (72) and a gas turbine assembly. The gas turbine comprises a compressor (76), a turbine (80) and a generator (84). Air from a source (73) is introduced to the compressor where it is compressed and thus heated and is then discharged to the electrochemical converter. Fuel (74) is introduced to a preheater (68) where it is heated to an elevated temp.    The heated air and fuel function as input reactants and power the electrochemical converter. The converter (72) heats the compressed air and the fuel to produce a high temp. exhaust which is fed to the gas turbine to drive the generator.    ADVANTAGE -   Integrates an electrochemical converter and a gas turbine to create a high efficiency power system.    (EP776529-B1)      An aero-derivative gas turbine power system (70) includes an electrochemical converter (72) and a gas turbine assembly. The gas turbine comprises a compressor (76), a turbine (80) and a generator (84). Air from a source (73) is introduced to the compressor where it is compressed and thus heated and is then discharged to the electrochemical converter. Fuel (74) is introduced to a preheater (68) where it is heated to an elevated temp.    The heated air and fuel function as input reactants and power the electrochemical converter. The converter (72) heats the compressed air and the fuel to produce a high temp. exhaust which is fed to the gas turbine to drive the generator.    ADVANTAGE -   Integrates an electrochemical converter and a gas turbine to create a high efficiency power system.    (US5976332-A)      An aero-derivative gas turbine power system (70) includes an electrochemical converter (72) and a gas turbine assembly. The gas turbine comprises a compressor (76), a turbine (80) and a generator (84). Air from a source (73) is introduced to the compressor where it is compressed and thus heated and is then discharged to the electrochemical converter. Fuel (74) is introduced to a preheater (68) where it is heated to an elevated temp.    The heated air and fuel function as input reactants and power the electrochemical converter. The converter (72) heats the compressed air and the fuel to produce a high temp. exhaust which is fed to the gas turbine to drive the generator.    ADVANTAGE -   Integrates an electrochemical converter and a gas turbine to create a high efficiency power system.    (JP2000311698-A)      An aero-derivative gas turbine power system (70) includes an electrochemical converter (72) and a gas turbine assembly. The gas turbine comprises a compressor (76), a turbine (80) and a generator (84). Air from a source (73) is introduced to the compressor where it is compressed and thus heated and is then discharged to the electrochemical converter. Fuel (74) is introduced to a preheater (68) where it is heated to an elevated temp.    The heated air and fuel function as input reactants and power the electrochemical converter. The converter (72) heats the compressed air and the fuel to produce a high temp. exhaust which is fed to the gas turbine to drive the generator.    ADVANTAGE -   Integrates an electrochemical converter and a gas turbine to create a high efficiency power system.