Patent ID: 8459037

Claim:
A system for feeding a gas turbine engine, comprising: a. a base fuel delivery line in fluid communication with a fuel tank to supply fuel to a gas turbine combustor; b. a conditioned fuel solution delivery line in fluid communication with the fuel tank to supply a conditioned fuel solution to the gas turbine combustor; c. an ejector mixer in fluid communication with exhaust gases from the gas turbine combustor and gas from a gas supply pump; d. a fuel conditioner in fluid communication with the conditioned fuel solution delivery line and the ejector mixer to produce the conditioned fuel solution; e. control valves for selectively supplying the fuel to the base fuel delivery line and the conditioned fuel solution delivery line; and f. an incombustible evaporative liquid-gas solution delivery line in fluid communication with an incombustible liquid absorber to supply an incombustible evaporative liquid-gas solution to the gas turbine combustor.