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A system includes a gas turbine engine having a combustor, a liquid fuel supply coupled to the combustor, and a water supply coupled to the liquid fuel supply. The water supply is configured to flow water through the liquid fuel supply while the liquid fuel supply is not in use to flow a liquid fuel

A system includes a gas turbine engine having a combustor, a liquid fuel supply coupled to the combustor, and a water supply coupled to the liquid fuel supply. The water supply is configured to flow water through the liquid fuel supply while the liquid fuel supply is not in use to flow a liquid fuel.

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1. A system, comprising: a gas turbine engine having a combustor;a liquid fuel supply coupled to the combustor, wherein the liquid fuel supply is configured to supply a liquid fuel to the combustor;a water supply coupled to the liquid fuel supply, wherein the water supply is configured to flow water

1. A system, comprising: a gas turbine engine having a combustor;a liquid fuel supply coupled to the combustor, wherein the liquid fuel supply is configured to supply a liquid fuel to the combustor;a water supply coupled to the liquid fuel supply, wherein the water supply is configured to flow water through the liquid fuel supply to displace the liquid fuel and to maintain a pressure of the water in the liquid fuel supply after the liquid fuel is displaced while the liquid fuel supply is not in use to flow a liquid fuel; anda mixing valve disposed in the liquid fuel supply upstream of the combustor, wherein the mixing valve is configured to substantially block flow of the water from entering the combustor. 2. The system of claim 1, wherein the water supply comprises a water manifold configured to couple to a plurality of combustors, and the liquid fuel supply comprises a liquid fuel manifold configured to couple to the plurality of combustors. 3. The system of claim 1, wherein the water supply comprises a check valve configured to block backflow of the liquid fuel into the water supply. 4. The system of claim 1, wherein the water supply comprises a water vent valve configured to vent a first gas from the water supply, and the liquid fuel supply comprises a liquid vent valve configured to vent a second gas from the liquid fuel supply. 5. The system of claim 1, comprising a controller configured to cause a flow of the liquid fuel to be blocked and to cause flow of the water through the liquid fuel supply to displace the liquid fuel. 6. The system of claim 5, wherein the controller is configured to monitor a water pressure of the liquid fuel supply and to cause an increase of water pressure if a sensed water pressure in the liquid fuel supply is below a threshold level. 7. A system, comprising: a liquid fuel manifold configured to couple to a gas turbine combustor to route a liquid fuel to the gas turbine combustor via a liquid fuel supply line;a water manifold configured to couple to the gas turbine combustor to route water to the gas turbine combustor via a water supply line coupled to the liquid fuel supply line;a liquid fuel supply valve configured to selectively supply the liquid fuel to the liquid fuel manifold;a water supply valve configured to selectively supply water to the liquid fuel manifold via the water manifold to displace the liquid fuel from the liquid fuel manifold and to maintain a first pressure of the water in the liquid fuel manifold after the liquid fuel is displaced when the liquid fuel supply valve is closed; anda mixing valve disposed in the liquid fuel supply line, wherein the mixing valve is configured to substantially block flow of the water from entering the gas turbine combustor. 8. The system of claim 7, comprising: a pilot fuel manifold configured to couple to the gas turbine combustor to route a pilot fuel to the gas turbine combustor via a pilot fuel supply line; wherein the water supply line is coupled to the pilot fuel supply line; anda pilot fuel supply valve configured to supply the pilot fuel to the pilot fuel manifold, wherein the water supply valve is configured to selectively supply water to the pilot fuel manifold via the water manifold to displace the pilot fuel from the pilot fuel manifold and to maintain a second pressure of the water in the pilot fuel manifold after the pilot fuel is displaced when the pilot fuel supply valve is closed. 9. The system of claim 7, comprising a water controller configured to transmit a first signal to cause the liquid fuel supply valve to close, a second signal to cause the water supply valve to open to displace the liquid fuel from the liquid fuel manifold with water, and a third signal to adjust the water supply valve to increase a water pressure in the liquid fuel manifold if a sensed water pressure in the liquid fuel manifold is below a threshold level. 10. The system of claim 7, comprising a water pressure sensor disposed in the liquid fuel manifold and configured to transmit an input signal indicative of a sensed water pressure in the liquid fuel manifold to the water controller. 11. The system of claim 7, comprising a check valve coupled to the water manifold and configured to block backflow of the liquid fuel into a supply of water to the water manifold. 12. The system of claim 7, wherein the water manifold comprises a water vent valve configured to vent a first gas from the water manifold, and the liquid fuel manifold comprises a liquid vent valve configured to vent a second gas from the liquid fuel manifold. 13. The system of claim 7, comprising the gas turbine combustor. 14. The system of claim 7, wherein the water comprises demineralized water, steam condensate, or a combination thereof. 15. A system, comprising: a water controller configured to transmit a first signal to a water flow control to flow water from a water supply through a liquid fuel supply coupled to a combustor of a gas turbine engine to displace a liquid fuel and to maintain a pressure of the water in the liquid fuel supply after the liquid fuel is displaced while the liquid fuel supply is not in use to flow a liquid fuel, and a fourth signal to a mixing valve disposed in the liquid fuel supply upstream of the combustor to substantially block flow of the water from entering the combustor. 16. The system of claim 15, wherein the water controller is configured to transmit a second signal to a liquid fuel flow control to block a flow of a liquid fuel through the liquid fuel supply prior to transmitting the first signal. 17. The system of claim 15, wherein the water controller is configured to transmit a third signal to cause the water flow control to increase a water pressure in the liquid fuel supply if a sensed level of the water pressure in the liquid fuel supply is below a threshold level. 18. The system of claim 17, comprising a water pressure sensor disposed in the liquid fuel supply and configured to transmit an input signal indicative of the sensed water pressure in the liquid fuel supply to the water controller. 19. The system of claim 17, wherein the threshold level of the water pressure is greater than approximately 1700 kilopascals. 20. The system of claim 17, wherein the water pressure controller is configured to transmit the third signal to the water flow control if a ratio of the sensed level of the water pressure to a combustion pressure of the combustor is less than approximately 1.03.