Method and system for reliable gas to liquid transfer
A method and system for transitioning a gas turbine from burning gaseous fuel to liquid fuel and purging the liquid fuel therefrom after transfer back to the gaseous fuel are disclosed herein. The method includes pressurizing a volume of liquid fuel in an accumulator with a first volume of motive gas. A valve is opened in response to low gaseous fuel pressure in the gas turbine to permit the volume of liquid fuel to flow through a conduit to the gas turbine. A volume of flushing medium is pressurized in the accumulator with a second volume of motive gas. The valve is opened to permit at least a portion of the volume of flushing medium to flow through the conduit to flush any of the volume of liquid fuel remaining in the conduit after the gas turbine consumes the volume of liquid fuel.
1. A fuel transfer system comprising:
an accumulator tank for alternatively storing a first combination of a volume of liquid fuel and a first volume of motive gas and a second combination of a volume of flushing medium and a second volume of motive gas;
a conduit for coupling the accumulator tank to a gas turbine;
a motive gas source for providing the first volume of motive gas and the second volume of motive gas to the accumulator tank; and
a valve that opens in response to low gaseous fuel pressure in the gas turbine to permit the volume of liquid fuel to flow through the conduit to the gas turbine and opens to permit at least a portion of the volume of flushing medium to flow through the conduit to flush any of the volume of liquid fuel remaining in the conduit after the volume of liquid fuel has been consumed by the gas turbine.
2. The fuel transfer system of claim 1 , wherein the flushing medium is demineralized water and the liquid fuel is diesel.
3. The fuel transfer system of claim 1 , wherein the motive gas source is a compressor of the gas turbine.
4. The fuel transfer system of claim 1 , wherein the motive gas source is a pump separate from the gas turbine.
5. The fuel transfer system of claim 1 , further comprising a controller that opens the valve in response to low gaseous fuel pressure in the gas turbine.
6. The fuel transfer system of claim 5 , wherein the controller modulates a motive gas conduit valve in response to a pressure in the accumulator tank measured by a pressure sensor.
7. The fuel transfer system of claim 5 , wherein the controller modulates the pump in response to a pressure in the accumulator tank measured by a pressure sensor.
8. A method for transferring fuel with a fuel transfer system having an accumulator tank for alternatively storing a first combination of a volume of liquid fuel and a first volume of motive gas and a second combination of a volume of flushing medium and a second volume of motive gas, the method comprising: pressurizing the volume of liquid fuel in the accumulator tank with the first volume of motive gas from a motive gas source;
opening a valve in response to low gaseous fuel pressure in a gas turbine to permit the volume of liquid fuel to flow from the accumulator tank through a conduit to the gas turbine; pressurizing the volume of flushing medium in the accumulator tank with the second volume of motive gas from the motive gas source; and
opening the valve to permit at least a portion of the volume of flushing medium to flow through the conduit to flush any of the volume of liquid fuel remaining in the conduit after the volume of liquid fuel has been consumed by the gas turbine.
9. The method of claim 8 , further comprising closing the valve after the volume of flushing medium flows through the conduit to flush any of the volume of liquid fuel remaining in the conduit.
10. The method of claim 8 , further comprising pressurizing a second volume of liquid fuel with a third volume of motive gas in the accumulator tank after closing the valve.
11. The method of claim 8 , wherein the flushing medium is demineralized water.