Systems and methods utilizing turbine compressor discharge for hydrostatic manifold purge
Embodiments of systems and methods for air recovery are disclosed. The diverted pressurized air may be used to supply a hydrostatic purge to the unutilized portion of a turbine engine fuel manifold circuit to ensure that exhaust gases from the utilized side of the fuel manifold circuit do not enter the portion of the alternative fuel manifold circuit rack. The assembly used to remove compressor section pressurized air may include a flow control orifice, line pressure measuring instrumentation, non-return valves, isolation valves and hard stainless-steel tubing assemblies. In some embodiments, a turbine compressor section diverter system may include a small air receiver used to increase the volume of air supplying the manifold to aid in potential pressure and flow disruptions from a turbine engine compressor section.
1. A manifold pressurization system comprising:
a purge inlet configured to receive purge air from a compressor of a dual fuel engine positioned to operate on a liquid fuel and a gaseous fuel;
a common purge line connected at an upstream end to the purge inlet, the common purge line configured to provide the purge air at a purge pressure and including 1) one or more backflow prevention valves configured to prevent backflow within the common purge line, and 2) a pneumatic intensifier configured to increase the purge pressure of the purge air;
a first purge line connected at a downstream end thereof to a manifold of the dual fuel engine via a first fuel circuit, the first fuel circuit connected to a supply of the liquid fuel;
a second purge line connected at a downstream end thereof to the manifold via a second fuel circuit, the second fuel circuit connected to a supply of the gaseous fuel; and
a control valve connected to a downstream end of the common purge line, an upstream end of the first purge line, and an upstream end of the second purge line, the control valve having a first position in which the control valve connects the common purge line with the second purge line such that the supply of the liquid fuel is in fluid communication with the purge air at the manifold, thereby to prevent backflow from the manifold into the second fuel circuit, and the control valve having a second position in which the control valve connects the common purge line with the first purge line such that the supply of the gaseous fuel is in fluid communication with the purge air at the manifold, thereby to prevent backflow from the manifold into the first fuel circuit;
wherein the one or more backflow prevention valves are upstream of the pneumatic intensifier; and
wherein the common purge line includes a pressure sensor configured to provide a signal indicative of a pressure of the common purge line, and the manifold pressurization system further comprising a control system configured to receive the signal from the pressure sensor and control a position of the purge inlet in response to the signal from the pressure sensor.
2. The system according to claim 1 , wherein the common purge line includes an orifice, the orifice configured to limit a volume of the purge air within the common purge line.
3. The system according to claim 2 , wherein the orifice is a fixed orifice.
4. The system according to claim 3 , wherein the fixed orifice has size in a range of 1/64 to ¼ of an inch.
5. The system according to claim 3 , wherein the fixed orifice is replaceably received within an orifice fitting such that a size of the fixed orifice is variable.
6. The system according to claim 1 , wherein the common purge line includes a plenum configured to store the purge air.
7. The system according to claim 1 , wherein the control valve has a third position in which control valve closes the downstream end of the common purge line, the upstream end of the first purge line, and the upstream end of the second purge line.
8. The system according to claim 1 , wherein the purge inlet is positioned at a P3 point of the compressor.
9. The system according to claim 1 , wherein the position of the purge inlet has a closed position in which the purge air is prevented from entering the common purge line and an open position in which the purge air is allowed to enter the common purge line.
10. The system according to claim 1 , wherein the dual fuel engine operates on one or more of gasoline, natural gas, well gas, field gas, or diesel.
11. A method of operating a dual fuel engine positioned to operate on a liquid fuel and a gaseous fuel, the method comprising:
supplying a first fuel to a combustion chamber of the dual fuel engine through a manifold and a first fuel circuit when no fuel is supplied to the manifold through a second fuel circuit such that the dual fuel engine is in a first mode of operation;
switching the dual fuel engine to a second mode of operation such that a second fuel is supplied to the combustion chamber through the manifold and the second fuel circuit when no fuel is supplied to the manifold through the first fuel circuit;
supplying combustion air to the combustion chamber with a primary compressor of the dual fuel engine;
diverting purge air from the primary compressor into a common purge line including 1) one or more backflow prevention valves configured to prevent backflow within the common purge line, and 2) a pneumatic intensifier configured to increase the purge pressure of the purge air from the primary compressor of the dual fuel engine through a purge inlet during operation of the dual fuel engine, the purge air being separated from the combustion air before the combustion chamber;
positioning a directional control valve in a first position when the dual fuel engine is in the first mode of operation such that the purge air flows into the manifold via the second fuel circuit at a purge pressure equal to or greater than a pressure within the combustion chamber such that backflow from the combustion chamber into the second fuel circuit is prevented; and
positioning the directional control valve in a second position when the dual fuel engine is in the second mode of operation such that the purge air flows into the manifold via the first fuel circuit at a purge pressure equal to or greater than a pressure within the combustion chamber such that backflow from the combustion chamber into the first fuel circuit is prevented;
wherein the one or more backflow prevention valves are upstream of the pneumatic intensifier; and
wherein the common purge line includes a pressure sensor configured to provide a signal indicative of a pressure of the common purge line, and the dual fuel engine further comprising a control system configured to receive the signal from the pressure sensor and control a position of the purge inlet in response to the signal from the pressure sensor.
12. The method according to claim 11 , further comprising
selecting a fixed orifice based on a pressure of the primary compressor; and
fitting the fixed orifice in the common purge line to limit a volume of the purge air diverted from the primary compressor.
13. The method according to claim 12 , wherein selecting the fixed orifice includes selecting a fixed orifice in a range of 1/64 to ¼ of an inch.
14. The method according to claim 11 , wherein diverting the purge air from the primary compressor includes diverting the purge air from a P3 point of the primary compressor.
15. The method according to claim 11 , wherein supplying the first fuel to the combustion chamber includes supplying the liquid fuel to the combustion chamber through the manifold and the first fuel circuit.
16. The method according to claim 15 , wherein supplying the second fuel to the combustion chamber includes supplying the gaseous fuel to the combustion chamber through the manifold and the second fuel circuit.
17. The method according to claim 11 , further comprising driving a hydraulic fracturing pump with the dual fuel engine, the hydraulic fracturing pump and the dual fuel engine mounted to a mobile trailer.
18. The method according to claim 11 , wherein the dual fuel engine operates on one or more of gasoline, natural gas, well gas, field gas, or diesel.
19. A manifold pressurization system comprising:
a purge inlet configured to receive purge air from a compressor of a dual fuel engine positioned to operate on a liquid fuel and a gaseous fuel;
a common purge line connected at an upstream end to the purge inlet, the common purge line configured to provide the purge air at a purge pressure and including 1) one or more backflow prevention valves configured to prevent backflow within the common purge line, and 2) a pneumatic intensifier configured to increase the purge pressure of the purge air, wherein a position of the purge inlet has a closed position in which the purge air is prevented from entering the common purge line and an open position in which the purge air is allowed to enter the common purge line;
a first purge line connected at a downstream end thereof to a manifold chamber of the dual fuel engine via a first fuel circuit;
a second purge line connected to at a downstream end thereof to the manifold chamber via a second fuel circuit; and
a control valve connected to a downstream end of the common purge line, an upstream end of the first purge line, and an upstream end of the second purge line, the control valve having a first position in which the control valve connects the common purge line with the second purge line, thereby to prevent backflow from the manifold chamber into the second fuel circuit, and the control valve having a second position in which the control valve connects the common purge line with the first purge line, thereby to prevent backflow from the manifold chamber into the first fuel circuit;
wherein the one or more backflow prevention valves are upstream of the pneumatic intensifier;
wherein the common purge line includes a pressure sensor configured to provide a signal indicative of a pressure of the common purge line, and the manifold pressurization system further comprising a control system configured to receive the signal from the pressure sensor and control the position of the purge inlet in response to the signal from the pressure sensor.
20. The system according to claim 19 , wherein the dual fuel engine operates on one or more of gasoline, natural gas, well gas, field gas, or diesel.