Methods and apparati for quickset gas lift separation and liquid storage
The present disclosure provides methods and apparati for separating liquids from production gases and recovering the liquids. The methods and apparati of the present disclosure can reduce or eliminate emissions compared to standard methods and devices and also eliminate the need for haul away of liquids by collecting compressor system liquids in charge vessel(s). The methods and apparati of the present disclosure can also be used to fuel the engines which operate the compressor systems using gas from the compressor drains and the gas used to drain the charge vessel(s).
1. An apparatus comprising:
a first charge vessel comprising:
a first liquid inlet configured to receive liquids,
a first charge gas valve configured to be fluidically connected to a high pressure gas source in a compressor system, wherein the compressor system comprises at least one engine, and further configured to deliver high pressure gas to drain the first charge vessel when the first charge gas valve is in an open configuration,
a liquid outlet fluidically connected to a first dump valve, the first dump valve allowing liquid from the first charge vessel to flow out of the first charge vessel when the dump valve is in an open position and preventing the flow of liquid from the first charge vessel when the first dump valve is in a closed position,
a gas outlet configured to be fluidically connected to the at least one engine, and
a gas de pressure outlet,
wherein the at least one engine is capable of being operated using gas from the gas outlet as fuel, and
wherein the first liquid inlet of the first charge vessel is configured to be fluidically connected to the compressor system to receive liquids from the compressor system.
2. The apparatus of claim 1 , the first charge vessel further comprising a second liquid inlet configured to be fluidically connected to the compressor system to receive liquids from the compressor system.
3. The apparatus of claim 1 , wherein the first liquid inlet is configured to receive liquids from at least one source chosen from an inlet or suction scrubber, a fuel filter, an interstage scrubber and environmental drains of the compressor system.
4. The apparatus of claim 2 , wherein the second liquid inlet is configured to receive liquids from at least one source chosen from an inlet or suction scrubber, a fuel filter, an interstage scrubber and environmental drains of the compressor system.
5. The apparatus of claim 1 , wherein the high pressure gas source is a gas source with a pressure greater than the pressure in the first charge vessel.
6. The apparatus of claim 1 , wherein the high pressure gas source is chosen from a first interstage scrubber, a second interstage scrubber, a third interstage scrubber and a final discharge of gas from the compressor system.
7. The apparatus of claim 1 , wherein the high pressure gas source is a second stage interstage scrubber of the compressor system.
8. The apparatus of claim 1 , further comprising a fuel filter comprising:
a gas inlet,
a liquid outlet, and
a gas outlet configured to be fluidically connected to the at least one engine the fluidic connection between the gas outlet and the at least one engine comprising a pressure control valve configured to allow a suitable pressure of fuel gas to the at least one engine to operate the at least one engine,
wherein the gas inlet of the fuel filter is fluidically connected to the gas outlet of the first charge vessel.
9. The apparatus of claim 8 , further comprising a pressure sensor configured to detect a pressure to the at least one engine, configured to be positioned between the pressure control valve and the compressor system, the fuel filter being configured to be fluidically connected to a gas make up outlet, the fluid connection between the gas make up outlet and the fuel filter comprising a fuel gas make up valve, the fuel gas make up valve being configured to allow sufficient fuel gas to flow to the fuel filter to maintain a pressure suitable to operate the at least one engine, the pressure sensor being operatively connected to the gas make up valve and configured to open or close the gas make up valve sufficiently to deliver a suitable pressure of fuel gas to the at least one engine to operate the at least one engine.
10. The apparatus of claim 1 , further comprising a charge gas pressure regulator fluidically connected to the first charge gas valve, the charge gas pressure regulator being configured to be fluidically connected to the high pressure gas source between the high pressure gas source and the first charge gas valve, the charge gas pressure regulator being configured to deliver a target charge gas pressure.
11. The apparatus of claim 1 , further comprising a first level controller operatively connected to the first charge vessel, the de pressure valve, the first charge gas valve and the first dump valve,
the first level controller being configured to close the de pressure valve, open the first charge gas valve and open the first dump valve when a liquid level in the first charge vessel exceeds a first target liquid level, and
the first level controller being configured to open the de pressure valve, close the first charge gas valve, and close the first dump valve when the liquid level in the first charge vessel is less the first target liquid level.
12. The apparatus of claim 1 , further comprising a second charge vessel, the second charge vessel comprising:
at least one liquid inlet configured to be fluidically connected to the compressor system to receive liquids from the compressor system,
a second charge gas valve configured to be fluidically connected to the high pressure gas source in said compressor system and further configured to deliver high pressure gas to drain the second charge vessel when the second charge gas valve is in an open configuration,
a liquid outlet fluidically connected to a second dump valve, the second dump valve allowing liquid from the second charge vessel to flow out of the second charge vessel when the second dump valve is in an open position and preventing the flow of liquid from the second charge vessel when the second dump valve is in a closed position.
13. The apparatus of claim 12 , the second charge vessel being configured to receive liquids from a second interstage of the compressor system.
14. The apparatus of claim 12 , further comprising a second level controller operatively connected to the second charge vessel, the second charge gas valve and the second dump valve,
the second level controller being configured to open the second charge gas valve and open the second dump valve when a liquid level in the second charge vessel exceeds a second target liquid level, and
the second level controller being configured to close the second charge gas valve, and close the second dump valve when the liquid level in the second charge vessel is less than the second target liquid level.
15. The apparatus of claim 1 , further comprising the compressor system.
16. The apparatus of claim 2 , further comprising the compressor system.
17. The apparatus of claim 8 , further comprising the compressor system.
18. A method for recovering a gas lift gas and liquids from production gas, comprising:
providing an apparatus according to claim 1 ,
allowing fuel gas from the first charge vessel to flow into the at least one engine in the compressor system, the gas outlet of the first charge vessel being fluidically connected to the at least one engine, the fuel gas being suitable to operate the at least one engine.
19. The method of claim 18 , further comprising:
allowing a first portion of liquids generated by the compressor system to flow into the first charge vessel, wherein the first charge vessel is fluidically connected to a source of the first portion of liquids generated by the compressor system; and
pushing the liquid in the first charge vessel out of the first charge vessel using the high pressure gas source from the compressor system, the first charge vessel being fluidically connected to the high pressure gas source.