SYSTEM AND METHOD FOR HARNESSING ENERGY FROM A PRESSURIZED GAS FLOW TO PRODUCE LNG

Abstract

A system includes a heat exchanger including a first inlet for receiving a first pressurized gas stream and a first outlet for outputting a chilled gas stream produced by the heat exchanger cooling the first pressurized gas stream. The system also includes a turbo expander connected to the first outlet of the heat exchanger for receiving the chilled gas stream from the heat exchanger and producing a partially liquified gas stream, the partially liquified gas stream comprising vapors and LNG. The system further includes at least one separator connected to the turbo expander, wherein the partially liquified gas stream is fed into the at least one separator, and the at least one separator separates the vapors from the LNG.

Description

TECHNICAL FIELD

The present invention relates to separators, gas production units and methods for separating gas from liquid, sand and debris being produced from oil and gas wells and more particularly to such devices used to facilitate the production of natural gas and emissions-free or near emissions-free energy for use in the production of LNG (liquid natural gas), CNG (compressed natural gas), electricity, hydrogen and oxygen.

BACKGROUND

Modern natural gas and oil wells generate tremendous pressure during early production, in some cases approaching 20,000 psig. Transporting natural gas via pipeline at these pressures is unfeasible not only because of the enormous wall thickness the pipeline would need, but also because partially depleted wells that share the same pipeline usually cannot produce at these pressures. In the United States, transmission pipelines usually operate at around 1,000 psig, and gathering pipelines often operate at pressures significantly below this. Pipelines, compressors, and processing equipment are commonly designed to handle pressures within this range, and conventional production and flowback equipment is designed to reduce wellhead gas pressure to around 1,000 psig or less; any oil, water, sand or debris is separated from the gas and deposited in tanks on location at near-atmospheric pressure.

A choke valve is conventionally used to reduce the fluid production stream (all the gas and liquids produced by the well) from wellhead pressure to pipeline pressure. At high wellhead pressures, the fluid production stream must be heated before or after the choke to counteract the Joule-Thomson (JT) effect, which would otherwise cause problems downstream (ice and clathrate hydrate formation, low-temperature embrittlement of steel equipment, etc.). This is conventionally accomplished using a glycol-bath heater fueled by a portion of the produced gas; burning this fuel generates undesirable emissions and consumes gas that would otherwise be sold.

Friction causes gas to lose pressure as it travels through a pipeline; transmission pipelines operate booster compressors to counteract this effect, keeping the gas at around 1,000 psig. Yet many compressed natural gas (CNG) facilities take gas from distribution pipelines operating below 100 psig. For a well producing at 3,600 psig or greater, it seems very inefficient to throttle the gas to around 1,000 psig, compress it repeatedly to keep it near 1,000 psig as it travels through the pipeline, throttle it again to less than 100 psig at a pressure letdown station, and then compress it back up to 3,600 psig, the customary pressure of CNG. In the same way, it seems inefficient to heat high-pressure wellhead gas to counteract the JT effect and then chill it from ambient temperature to around −250° F. at a liquefied natural gas (LNG) facility. However, this is all standard practice.

Many natural gas well sites use two primary devices to condition each well's fluid production stream. The first is a sand separator, a vessel that removes sand and debris from the fluid production stream to prevent fouling in (and damage to) downstream equipment. The second is a gas production unit (GPU), which reduces the fluid production stream to pipeline pressure (the aforementioned choke valve and glycol-bath heater are part of the GPU) and separates liquids from the gas. A typical gas production facility including a sand separator 10 and a GPU 20 is shown in FIG. 1.

Existing sand separators and GPUs have many limitations that increase the cost of flowback and production operations. Neither can handle the high rates of sand and liquid produced during flowback, so temporary flowback equipment (usually rented from a third party) must be used before the permanent sand separator and GPU are installed. Sand separators also lack level indication and must be manually drained; because sand production rates are unpredictable, it is impossible to establish an optimized draining schedule for any given well, and sand separators must be drained far more often than would be hypothetically required. Additionally, downstream equipment must be fitted with thicker pipe walls to allow for erosion due to sand carryover in the fluid production stream.

The lack of real-time feedback or precision control of the GPU drain also increases the risk of liquid carryover into the pipeline, which can cause operational problems, as well as gas blowby to production tanks, which creates fugitive emissions and poses a safety hazard. At times, a third “polishing” separation vessel is installed downstream of the GPU to compensate for the GPU's failure to separate all liquids from the produced gas.

In contrast, production equipment would ideally use a single separation vessel, accurate and reliable liquid level indication, and automated drain valves that ensure complete and consistent separation of solids and liquids from the produced gas, even during flowback operations. It would also have a smaller footprint to allow for more flexibility in site design.

SUMMARY

Embodiments of the present disclosure are generally directed to a system including a heat exchanger, a turbo expander, and at least one separator. In some non-limiting examples, the heat exchanger includes a first inlet for receiving a first pressurized gas stream, and a first outlet for outputting a chilled gas stream produced by the heat exchanger cooling the first pressurized gas stream. The turbo expander is connected to the first outlet of the heat exchanger for receiving the chilled gas stream from the heat exchanger and producing a partially liquified gas stream. The partially liquified gas stream includes vapors and LNG. The at least one separator is connected to the turbo expander. The partially liquified gas stream is fed into the at least one separator, and the at least one separator separates the vapors from the LNG.

In some non-limiting embodiments, the heat exchanger further includes at least one vapor inlet in the heat exchanger connected to the at least one separator for receiving vapors from the at least one separator.

In some non-limiting embodiments, the system further includes: at least one vapor outlet for outputting the vapors from the heat exchanger, and at least one compressor connected between the at least one vapor outlet of the heat exchanger and a pipeline for compressing the vapors output from the heat exchanger to a pressure suitable for the pipeline.

In some non-limiting embodiments, the turbo expander is coupled to the at least one compressor, wherein the turbo expander supplies power to the at least one compressor.

In some non-limiting embodiments, the system further includes a cooler connected between the at least one compressor and the pipeline.

In some non-limiting embodiments, the at least one compressor is a multi-stage compression assembly comprising multiple compressors connected in series, and the at least one separator is a multi-stage separation assembly comprising multiple separators connected in series.

In some non-limiting embodiments, the at least one vapor inlet includes multiple vapor inlets each connected to one of the multiple separators, the at least one vapor outlet includes multiple vapor outlets each connected between a corresponding one of the multiple vapor inlets and a corresponding one of the multiple compressors, and at least one interstage vapor mixer is connected between one of the multiple vapor outlets and the corresponding one of the multiple compressors for mixing vapors output from the one of the multiple vapor outlets with compressed vapors output from an adjacent compressor.

In some non-limiting embodiments, the system further includes: a feed splitter upstream of the heat exchanger for splitting an initial gas stream into the first pressurized gas stream and a second pressurized gas stream, a second turbo expander connected between the feed splitter and a second inlet of the heat exchanger, wherein the second turbo expander receives the second pressurized gas stream and outputs an expanded gas stream to the second inlet, and a pipeline connected to a second outlet of the heat exchanger, the second outlet outputting a heated gas stream produced by the heat exchanger heating the expanded gas stream.

In some non-limiting embodiments, the system further includes at least one compressor connected between the heat exchanger and the pipeline for providing compressed gas to the pipeline, and the heat exchanger further includes: at least one vapor inlet for receiving vapors from the at least one separator, and at least one vapor outlet for outputting the vapors from the heat exchanger, wherein the at least one compressor is connected to the at least one vapor outlet.

In some non-limiting embodiments, the at least one compressor is coupled to one or both of the turbo expander and the second turbo expander, wherein one or both of the turbo expander and the second turbo expander supplies power to the at least one compressor.

Other embodiments of the present disclosure are directed to a method. The method includes receiving a first pressurized gas stream into a heat exchanger, cooling the first pressurized gas stream via the heat exchanger to produce a chilled gas stream output from the heat exchanger, expanding the chilled gas stream via a turbo expander connected to the first outlet to produce a partially liquified gas stream comprising vapors and LNG, and separating the vapors from the LNG via a separator connected to the turbo expander.

In some non-limiting embodiments, the method further includes receiving the vapors from the at least one separator into at least one vapor inlet of the heat exchanger, and cooling the first pressurized gas stream via heat transfer between the first pressurized gas stream and the vapors in the heat exchanger.

In some non-limiting embodiments, the method further includes outputting the vapors from the heat exchanger via at least one vapor outlet of the heat exchanger, and compressing the vapors output from the heat exchanger via at least one compressor to output a compressed gas toward a pipeline at a pressure suitable for the pipeline.

In some non-limiting embodiments, the method further includes supplying power generated by the turbo expander to the at least one compressor for operating the at least one compressor.

In some non-limiting embodiments, the method further includes cooling the compressed gas output from the at least one compressor via a cooler connected between the at least one compressor and the pipeline.

In some non-limiting embodiments, the at least one compressor is a multi-stage compression assembly comprising multiple compressors connected in series, and the at least one separator is a multi-stage separation assembly comprising multiple separators connected in series.

In some non-limiting embodiments, the at least one vapor inlet comprises multiple vapor inlets each connected to one of the multiple separators, the at least one vapor outlet comprises multiple vapor outlets each connected between a corresponding one of the multiple vapor inlets and a corresponding one of the multiple compressors, and the method further includes mixing vapors output from the one of the multiple vapor outlets with compressed vapors output from a compressor adjacent the corresponding one of the multiple compressors.

In some non-limiting embodiments, the method further includes splitting an initial gas stream into the first pressurized gas stream and a second pressurized gas stream, reducing a pressure of the second pressurized gas stream via a second turbo expander to produce an expanded gas stream provided to the heat exchanger, cooling the first pressurized gas stream via heat transfer between the first pressurized gas stream and the expanded gas stream in the heat exchanger, and outputting a heated gas stream produced by the heat exchanger heating the expanded gas stream toward a pipeline at a pressure suitable for the pipeline.

In some non-limiting embodiments, the method further includes receiving vapors from the at least one separator into the heat exchanger, outputting the vapors from the heat exchanger after the vapors are heated, and compressing the vapors output from the heat exchanger via at least one compressor to output a compressed gas toward the pipeline at the pressure suitable for the pipeline.

In some non-limiting embodiments, the method further includes supplying power generated by one or both of the turbo expander and the second turbo expander to the at least one compressor for operating the at least one compressor.

These and other features and characteristics will become more apparent upon consideration of the following description and the appended claims with reference to the accompanying drawings, all of which form a part of this specification, wherein like reference numerals designate corresponding parts in the various figures. It is to be expressly understood, however, that the drawings are for the purpose of illustration and description only and are not intended as a definition of the limits of the disclosure. As used in the specification and the claims, the singular forms of “a”, “an”, and “the” include plural referents unless the context clearly dictates otherwise.

BRIEF DESCRIPTION OF THE DRAWINGS

For a more complete understanding of the present disclosure and its features and advantages, reference is now made to the following description, taken in conjunction with the accompanying drawings, in which:

FIG. 1 is a perspective view of a prior art gas production facility, including a conventional sand separator and GPU;

FIG. 2 is a perspective view of a separator according to an embodiment of the present disclosure;

FIG. 3 is a front view of the separator of FIG. 2;

FIG. 4 is a side view of the separator of FIG. 2;

FIG. 5 is a perspective view of the main body of the separator of FIG. 2;

FIG. 6 is a side cross-sectional view of the separator of FIG. 2;

FIG. 6A is a side cross-section view of a horizontal orientation of the separator of FIG. 2.

FIG. 7 is a detail view of the inlet port of the separator of FIG. 2;

FIG. 7A is a detail view of an alternate embodiment of an inlet port of the separator of FIG. 2;

FIG. 8 is a fluid schematic of the separator of FIG. 2;

FIG. 9 is a fluid schematic of a dual dump valve arrangement for use with the separator of FIG. 2;

FIG. 10 is a schematic partial cross-sectional view of a separator according to another embodiment of the present disclosure;

FIG. 11 is a schematic partial cross-sectional view of a separator according to another embodiment of the present disclosure;

FIG. 12 is a schematic partial cross-sectional view of a separator according to another embodiment of the present disclosure;

FIG. 13 is a perspective view of a gas processing facility according to an embodiment of the present disclosure;

FIG. 14 is a rear view of the line heater and choke of FIG. 13;

FIG. 15 is a flow diagram of a process for operating the separator of FIG. 2;

FIG. 16 is a side cross-sectional view of the separator according to another embodiment of the present disclosure;

FIG. 17 is a schematic diagram illustrating a separator performing flowback operations according to an embodiment of the present disclosure;

FIG. 17A is a schematic diagram illustrating an embodiment employing dual separators for performing flowback operations according to an embodiment of the present disclosure;

FIG. 18 is a schematic block diagram of a system according to an embodiment of the present disclosure using a separator to provide a pressurized gas stream to various downstream components;

FIG. 19 is a schematic block diagram of a system according to another embodiment of the present disclosure using a separator to provide a pressurized gas stream to various downstream components;

FIG. 20 is a schematic block diagram of a system according to yet another embodiment of the present disclosure using a separator to provide a pressurized gas stream to various downstream components;

FIG. 21 is a schematic block diagram of a system according to yet another embodiment of the present disclosure using two separators connected in series to provide a pressurized gas stream to various downstream components;

FIG. 22 is a schematic block diagram of a system according to yet another embodiment of the present disclosure using a pressurized gas stream to perform one or more operations including producing LNG;

FIG. 23 is a detailed schematic diagram of an embodiment of the system in FIG. 22 having one stage of compression; and

FIG. 24 is a detailed schematic diagram of another embodiment of the system in FIG. 22 having multiple compression stages.

DETAILED DESCRIPTION

For purposes of the description hereinafter, the terms “upper”, “lower”, “right”, “left”, “vertical”, “horizontal”, “top”, “bottom”, “lateral”, “longitudinal”, and derivatives thereof shall relate to the disclosure as it is oriented in the figures. However, it is to be understood that the disclosure may assume alternative variations and step sequences, except where expressly specified to the contrary. It is also to be understood that the specific devices and processes illustrated in the attached drawings and described in the following specification are simply exemplary aspects of the disclosure. Hence, specific dimensions and other physical characteristics related to the aspects disclosed herein are not to be considered as limiting.

As used herein, the term “psi” means pounds per square inch.

As used herein, the term “at least one of” is synonymous with “one or more of”. For example, the phrase “at least one of A, B, and C” means any one of A, B, and C, or any combination of any two or more of A, B, and C. For example, “at least one of A, B, and C” includes one or more of A alone; or one or more B alone; or one or more of C alone; or one or more of A and one or more of B; or one or more of A and one or more of C; or one or more of B and one or more of C; or one or more of all of A, B, and C. Similarly, as used herein, the term “at least two of” is synonymous with “two or more of”. For example, the phrase “at least two of D, E, and F” means any combination of any two or more of D, E, and F. For example, “at least two of D, E, and F” includes one or more of D and one or more of E; or one or more of D and one or more of F; or one or more of E and one or more of F; or one or more of all of D, E, and F.

Referring to FIGS. 2-7, embodiments of the present disclosure are directed to a sand and liquid separator 1000 (hereinafter “separator 1000”) particularly adapted for use at natural gas wells. The main body 1100 of the separator 1000 is generally a hollow vessel which defines an interior chamber 1010. In the embodiment shown in the FIGS. 2-8, the main body 1100 is constructed of an upper vessel section and a lower vessel section, which together define a continuous interior chamber 1010. However, it is to be understood that the main body 1100 could be constructed from any number of sections, including one continuous, unitary section as shown in FIGS. 10-12 and 16. The main body 1100 is preferably constructed from a strong, rigid material such as steel designed, configured, or rated to operate at an incoming pressure of gas flowing directly or indirectly (e.g. through a choke) from the wellbore. In some embodiments, the separator 1000 may be rated, designed, or configured for, or be capable of, operating at gas pressures greater than approximately 1500 psi, or greater than approximately 2,500 psi, or greater than approximately 5,000 psi. In some embodiments, the separator 1000 may be rated, designed, or configured for, or be capable of, operating at gas pressures as high as or greater than an unregulated pressure at which gas flows from the wellbore. For example, unregulated gas pressure at the wellhead of Marcellus Shale formation wells may be approximately 5,000 psi, and unregulated gas pressure at the wellhead of Utica Shale formation wells may be approximately 10,000 psi. In other embodiments, the separator 1000 may be rated, designed, or configured for, or be capable of, operating at regulated gas pressures. For example, the gas pressure of a Utica Shale formation well may be regulated down from approximately 10,000 psi at the wellhead to approximately 5,000 psi before being fed to the separator 1000. Such a pressure regulation, which may be utilized to prevent damage to or failure of the various components of the separator 1000 described herein, may be achieved by a choke or other device disposed inline between the wellbore and the separator 1000. In some embodiments, the separator 1000 and the various components thereof may be designed to meet various industry standards for pressure vessels or pressure and/or technical limitations associated with instrumentation described herein. As those of ordinary skill in the art will appreciate, modifications to existing instruments and other system components (e.g., the main body 1100 of the separator 1000) can be made to accommodate the high pressures of formations such as the Utica Shale formation without the need of equipment to regulate the pressure down from that coming out of the wellbore. As those of ordinary skill in the art will appreciate, the separator 1000 can be oriented horizontally rather than vertically, as shown in FIG. 6A.

In addition, the disclosed separator 1000 allows for separation of fluid, sand and debris from the gas stream at pressures available at the wellbore, prior to gas pressure reduction. It is advantageous to maintain high gas pressure of the gas removed of fluid, sand, and debris, as this pressurized stream of gas may be used for the production of compressed natural gas (CNG), liquefied natural gas (LNG), electricity, hydrogen and/or oxygen. These products may be produced individually or simultaneously in any combination without compression and free of emissions, with or without also providing natural gas to a pipeline.

In embodiments in which the main body 1100 is constructed of multiple sections, the various sections may be connected to one another using any suitable fastening method or device, such as mechanical fasteners (e.g. bolts or rivets), a welded joint, or the like. The connection between the various sections should be sufficiently tight to prevent the escape of high pressure gas and other materials from the interior chamber 1010 to the outside environment. The main body 1100 may be supported in a generally vertical position by a frame 1002.

A plurality of inlets and outlets (e.g., in the form of connecting ports and/or flanges) may be provided in the main body 1100 to facilitate flow of liquid, sand, and other debris through the separator 1000. An inlet (e.g., inlet port 1020 provided in the main body 1100) may allow flow into the interior chamber 1010 from a wellbore. The inlet port 1020 may be fluidly connected to the wellbore by rigid or flexible pipe, and flow to the inlet port 1020 may be regulated by one or more valves or the like (see FIG. 8). As shown in FIGS. 6-7, the inlet port 1020 may include a tube 1022 extending into the interior chamber 1010, with a terminal end of the tube 1022 being partially obstructed by a baffle 1024. Gas, liquid, sand and other debris entering the interior chamber 1010 flows through the tube 1022, in the direction of arrow A, and any solid and/or liquid contaminants carried by the gas may be deflected by the baffle 1024 toward a bottom of the interior chamber 1010. Such contaminants may include, for example, sand, water, oil, rock, and metal fragments.

An outlet (e.g., liquid, sand, and debris outlet port 1030) may be provided at or near a lower portion of the interior chamber 1010. The outlet port 1030 may be fluidly connected to a valve 2000 which may be periodically and/or continuously opened and closed to drain liquid and solid contaminants collected at the bottom of the interior chamber 1010. The valve 2000 may be mounted remotely from the separator 1000 by rigid or flexible pipe. The valve 2000 may feed into a waste holding tank 3000 (see FIG. 8), also via rigid or flexible pipe, for holding contaminants removed from the gas until the contaminants can be safely processed for disposal.

As shown in FIG. 8, the holding tank 3000 may be fluidly coupled to one or more pieces of downstream processing equipment 3002. The downstream processing equipment may include, for example, one or more separation components used to separate the different constituents of the liquid, sand, and/or debris output from the separator 1000. The downstream processing equipment 3002 may, in certain embodiments, comprise a dedicated sand vessel configured to remove sand from the waste fluid, a gun barrel-type separator, or a pressurized four-phase (e.g., gas, sand, water and oil) separation skid equipped with a sand removal device. Use of a pressurized four-phase separation skid may allow the well pressure to provide the motive force for removing fluid from the well pad, instead of diesel transfer pumps.

The valve 2000 may be a dump valve, and more particularly a hardened dump valve 2000. It should be noted, however, that any desired type of valve 2000 may be used to output liquid, sand, and/or debris from the lower portion of the interior chamber 1010. The valve 2000 may be a piston valve, a ball valve, a butterfly valve, a gate valve, a choke valve, a needle valve or the like suitable for operation at pressures up to, for example, 5,000 psi. The valve 2000 may include an electrical, hydraulic, or pneumatic actuator such as an electric motor, solenoid, hydraulic actuator, pneumatic actuator, or combinations thereof such that opening and closing of the valve 2000 can be performed automatically by an electronic controller 4000 (see FIG. 8). As such, the valve 2000 may be an electronically controlled valve. In certain embodiments, the valve 2000 may include a fast-acting electrically actuated linear valve actuator used to rapidly transition the valve 2000 between open and closed positions and/or to one or more intermediate positions between the open and closed positions. The valve actuator may be capable of transitioning the valve 2000 between a fully open position and a fully closed position in less than 2.0 seconds, more particularly less than 1.0 second, or more particularly less than 0.5 seconds.

In some embodiments, the valve 2000 may be configured to be selectively operated in a hand mode. In some embodiments, the controller that controls the valve 2000 may be programmed to allow operation of the valve 2000 in a hand mode. “Hand mode” is a manual operation mode by which the valve 2000 may be selectively opened or closed manually either by rotating the wheel handle or by the user pressing buttons on the valve to open and close it. This may allow for equalization across the valve 2000 to drain the line segment for maintenance of the valve. In some embodiments, the valve 2000 may be equipped with a bleed valve for performing maintenance on the valve 2000.

In some embodiments, the valve 2000 may be equipped with or coupled to a pressure pilot device configured to automatically initiate closure of the valve 2000 upon encountering pressure in the valve line above a predetermined threshold. This may prevent high pressure from damaging the holding tank 3000 and/or other downstream components 3002, for example, in the case of gas breaking through the liquid, sand, and debris outlet 1030 of the separator 1000. The pressure pilot device associated with the valve 2000 may thus provide a failsafe for the separator system. In other embodiments, a pressure transducer 4053 may be disposed in the valve line downstream of the valve 2000 and configured to detect pressure in the line and communicate the detected pressure to the controller 4000, as shown in FIG. 8. The controller 4000 may then send an electronic command to close the valve 2000 to prevent high pressure from damaging downstream components. Both an active pilot safety valve and/or pressure transducer may be used. Because of the critical nature of this operation, redundant pilot safety valves and/or pressure transmitters may be used.

As illustrated in FIG. 8, in some embodiments a valve position sensor 4050 may be disposed proximate or incorporated into the valve 2000. The valve position sensor 4050 may include at least one of a visual detection sensor, a motion sensor, a pressure sensor, a strain gauge, or any other type of sensor configured to indicate either a relative position of the valve 2000, or simply whether the valve 2000 is fully closed. The valve position sensor 4050 may indicate an operational position of the valve 2000. The valve position sensor 4050 may be connected to the controller 4000 to provide feedback of the operational position of the electronically controlled valve 2000 to the controller 4000. This valve position feedback may be used by the controller 4000 to identify the presence of an obstruction to the valve 2000 (e.g., in the event that the valve 2000 fails to completely close). Upon identifying an obstruction to the valve 2000, the controller 4000 may output a notification to a user interface 4002 coupled to the controller 4000 so that a user may manually remove the obstruction or switch operation of the valve 2000 to a backup valve. In other embodiments, the controller 4000 may output a command to a piece of equipment designed to automatically remove obstructions from the valve 2000. The obstruction can be cleared by initiating a rapid open/close cycle. In at least one embodiment, the feedback to the controller 4000 can be used to detect wash out (erosion) where the valve is closed but fluid is still leaking past the valve. A second valve or emergency shutdown (“ESD”) valve 4057 may be located downstream of valve 2000.

In some embodiments, two or more valves 2000 may be provided in parallel to one another due to the critical nature of this component. If one of the two valves 2000 fails, leaks, erodes or is nonoperational (e.g. undergoing maintenance), the second valve 2000 may be used to operate the separator 1000. FIG. 9 schematically illustrates the arrangement of two valves 2000A and 2000B in parallel. The primary valve 2000A and secondary valve 2000B may be identical valves, so that fewer maintenance components and spare parts are needed to perform maintenance and repairs on the valves 2000. As illustrated, the valves 2000A and 2000B may be coupled to independent strainers (or junk catchers) 4110A and 4110B, respectively, provided upstream of the valves 2000A and 2000B to capture debris. The valves 2000A and 2000B may feed into the same waste holding tank 3000, as illustrated, or into different waste holding tanks. Both valves 2000A and 2000B may be electronically controlled and connected to the controller 4000. The valves 2000A and 2000B may be electronically controlled by the controller 4000 to provide a fixed flow rate, e.g., 150 barrels of water per hour rather than controlled to maintain a certain level of liquid in the interior chamber 1010 of the vessel. As those of ordinary skill in the art will appreciate, this method of operation may be employed, e.g., where little to no gas is present.

Turning back to FIGS. 2-8, in some embodiments, a plurality of bridle ports 1040a-1040d may be provided in the upper vessel section 1100 and may be configured to connect to a bridle 1300. The bridle 1300 may include a tube 1310 and a plurality of connecting flanges 1320a-1320d. As illustrated, the tube 1310 may be a vertical tube 1310 (i.e., the tube axis is oriented vertically). Each of the connecting flanges 1320a-1320f may connect to a corresponding one of the bridle ports 1040a-1040f, such that fluid can flow freely between the tube 1310 and any of the bridle ports 1040a-1040f via the connecting flanges 1320a-1320f. Because fluid can flow freely between the interior chamber 1010 and the bridle 1300 via the bridle ports 1040a-1040f, a liquid level in the tube 1310 of the bridle 1300 self-equalizes with a liquid level in the interior chamber 1010. As such, the liquid level in the interior chamber 1010 may be ascertained by measuring the liquid level in the bridle 1300. The bridle 1300 also helps to protect the instruments from gas bubbles in the interior chamber 1010, which can cause the instruments to record inaccurate readings.

As shown in the accompanying drawings, a representative embodiment of the separator 1000 includes six bridle ports 1040a-1040f and six corresponding connecting flanges 1320a-1320f. As those of ordinary skill in the art will appreciate, the bridle 1300 may include more than six bridle ports or a lesser number. The bridle port third from the top 1040c may correspond to a high liquid level within the interior chamber 1010, and the lowermost bridle port 1040f may correspond to a low liquid level within the interior chamber 1010. During operation, the valve 2000 may be periodically and/or continuously opened and closed, or modulated between an opened and closed position, to maintain the liquid level within the interior chamber 1010 at a desired level, for example between the bridle port third from the top 1040c and the lowermost bridle port 1040f. The two intermediate bridle ports 1040d, 1040e between the bridle port third from the top 1040c and the lowermost bridle port 1040f may facilitate equalization of the liquid level in the interior chamber 1010 with the liquid level in the bridle 1300. The bridle port 1040a prevents the formation of a gas pocket from forming at the top of the bridle 1300 and allowing the liquid level sensor 1400 to take measurements along the entire length of the bridle 1300 and vessel. The bridle ports 1040a-f may be spaced vertically apart from one another and be of sufficient cross-sectional area to ensure that the liquid level within the bridle 1300 can rapidly equalize with the liquid level in the interior chamber 1010. That is, the bridle ports 1040a-f allow sufficient liquid flow into the bridle 1300 to minimize time delay in equalization of the liquid level within the bridle 1300 to the liquid level in the interior chamber 1010. It is to be understood that the separator 1000 may include more or fewer bridle ports, and a corresponding number of connecting flanges, than are shown in the drawings in order to reduce liquid level equalization time in the bridle 1300. Moreover, the bridle ports may have increased cross sectional area in order to reduce liquid level equalization time in the bridle 1300. The bridle 1300 may include a cleanout valve 1330 that may be used to evacuate sand or other particulate material that may become trapped in the bridle 1300. The cleanout valve 1330 may be coupled to a drain line 1332 extending from the bridle 1300. In FIGS. 2-4, 6, and 6A, the drain line 1332 is illustrated as leading back into the interior chamber 1010 of the separator. In other embodiments (e.g., as shown in FIG. 8), the drain line 1332 may be a flow path extending from the bridle 1300 to a location downstream of the valve 2000 for outputting the sand or other particulate material to the waste holding tank 3000 or another downstream location.

In some embodiments, the drain line 1332 of the bridle 1300 may be at least partially tilted with respect to a vertical direction, as shown in FIG. 10. In at least one example the drain line 1332 is installed at a 45° angle from the vertical axis of the bridle 1300. As shown in FIGS. 8 and 10, the lower drain line 1332 may be tilted back into the interior chamber 1010 of the separator 1000. The tilted drain line 1332 of the bridle 1300 may prevent buildup of sand or other particulate material in the bridle 1300, since the tilted axis of the drain line 1332 and its intersection with the interior chamber 1010 automatically urges any sand or particulate material to settle back into the bottom of the interior chamber 1010 for eventual release through the outlet 1030.

In some embodiments, the bridle may be equipped with cleanout out ports or plugs, 1340a-1340f, as shown in FIG. 6. These ports allow for the cleaning of the equalization ports/piping, in the event sand or debris collects in the horizontal pipe segments associated with equalization ports 1320a-f.

A liquid level sensor 1400 may be inserted in the tube 1310 of the bridle 1300 to determine the liquid level in the tube 1310 which, as noted above, is automatically equalized with the liquid level in the interior chamber 1010, by flow through the bridle ports 1040c, 1040d, 1040e, 1040f. The liquid level sensor 1400 may be in electronic communication with the controller 4000 that actuates the valve 2000. In particular, the controller 4000 may open and close the valve 2000, and in particular modulate between open and closed states, based on the measured liquid level in the bridle 1300. In an embodiment, the liquid level sensor 1400 may be a guided wave radar sensor including a probe that extends generally parallel to an axis of the tube 1310 so as to be immersed in any liquid within the bridle 1300. Examples of suitable, commercially available guided wave radar sensors include the Eclipse® Model 706 by Orion® Instruments. In other embodiments, the liquid level sensor 1400 may be a capillary tube, a differential pressure sensor, an ultrasonic sensor, or the like. However, guided wave radar may be desired as that technology can determine differences as fine as 0.10 inches of water column in real-time and is effective throughout the life of the well down to, for example, 2 psi. In comparison to a differential pressure sensor, the guided wave radar may be desired because it is unaffected by the ever-changing gravity of the fluid. In some embodiments, the liquid level sensor 1400 may be configured to determine a stratification level between water and oil in the bridle 1300.

In some embodiments, the separator 1000 may not include a bridle at all. For example, as shown in FIG. 11, the separator 1000 may include a liquid level sensor 1400 inserted directly into an upper portion of the interior chamber 1010 of the separator 1000 to determine the liquid level in the separator 1000. The liquid level sensor 1400 may be a guided wave radar sensor, as described above. In still other embodiments, the separator 1000 may include both a bridle 1300 with a first liquid level sensor 1400 disposed therein (as shown in FIG. 8) and a second liquid level sensor 1400 disposed in the interior chamber 1010 (as shown in FIG. 11) to provide redundant measurements of the liquid level in the separator 1000.

With continued reference to FIGS. 2-7, a gas outlet (e.g., gas outlet port 1050) may be provided in the main body 1100 through which gas may flow out of the separator 1000 to downstream components of the facility, such as a line heater or molecular dryer. The gas outlet port 1050 may be fluidly connected to the downstream components, for example, by rigid or flexible pipe. The gas outlet port 1050 may be located vertically above the uppermost bridle port 1040a, and therefore above the intended liquid level of the interior chamber 1010, such that no liquid flows out of the gas outlet port 1050 during normal operation. In some embodiments, a mist extractor 1052 may be provided within the interior chamber 1010 below the outlet port 1050 to prevent very fine water droplets/aerosols from reaching the outlet port 1050 and exiting the separator 1000. In some embodiments, a diffuser 1054 (see FIG. 6) may be provided within the interior chamber 1010 to allow gas to more easily travel upward within the interior chamber 1010.

In some embodiments, the gas outlet port 1050 may extend through a top of the main body 1100 of the separator 1000, as shown in FIGS. 2-7, thereby enabling a maximum length of the bridle 1300 and/or a maximum length between the upper and lower limits for the liquid level in the separator 1000. In other embodiments, as shown in FIG. 12, the gas outlet port 1050 may extend through a side wall 1056 of the main body 1100 of the separator 1000.

In some embodiments, a gas measurement device 1057, as shown in FIG. 8 may be installed to measure gas volumes exiting separator 1000. The measurement device may be an ultrasonic, orifice, VCone, or any device capable of measuring gas volumes exiting the separator 1000. By measuring the gas flow immediately downstream of separator 1000, gas from other wells that have been measured can be comingled. This is of particular importance where each of the wells are on different gas leases or have different gas ownership. This also allows multiple wells to be tied together to collectively harness their energy through common downstream equipment.

An upper sensor port 1060 may be provided in the main body 1100 of the separator 1000 and may receive an upper limit sensor 1064, such as a limit switch, float switch, thermal dispersion switch, or the like. The upper sensor port 1060 may be located vertically above the uppermost bridle port 1040a and vertically below the gas outlet port 1050. In some embodiments, the upper limit sensor 1064 may be located above an uppermost point at which the liquid level sensor 1400 can detect liquid. The upper limit sensor 1064 may be used to detect the presence of liquid, and may thus serve as an auxiliary device, in addition to the liquid level sensor 1400, for determining if the liquid level is above a predetermined high point in the interior chamber 1010. The upper limit sensor 1064 may be in electronic communication with the controller 4000, and the controller 4000 may be programmed or configured to initiate a shutdown procedure if liquid is detected by the upper limit sensor 1064.

Similarly, a lower sensor port 1064 may be provided in the main body 1100 of the separator 1000 and may receive a lower limit sensor 1066, such as a limit switch, float switch, thermal dispersion switch, or the like. The lower sensor port 1062 may be located vertically below the lowermost bridle port 1040f and vertically above the inlet port 1020. In some embodiments, the lower limit sensor 1066 may be located below a lowermost point at which the liquid level sensor 1400 can detect liquid. The lower limit sensor 1066 may be used to detect the presence of liquid, and may thus serve as an auxiliary device, in addition to the liquid level sensor 1400, for determining if the liquid level is below a predetermined low point in the interior chamber 1010. The lower limit sensor 1066 may be in electronic communication with the controller 4000, and the controller 4000 may be programmed or configured to initiate a shutdown procedure if liquid is not detected by the lower limit sensor 1066.

In the embodiments shown in FIGS. 2-6 and 8, the upper sensor port 1060 and the lower sensor port 1064 are provided in the main body 1100 of the separator 1000. FIG. 16 shows an alternative embodiment in which the upper sensor port 1060 and the lower sensor port 1064 are provided in the bridle 1300. The functionality of the upper sensor port 1060 and the lower sensor port 1064, along with the associated upper and lower limit sensors 1064, 1066, are the same in the embodiment shown in FIGS. 2-6 and 8 and the embodiment shown in FIG. 16.

With reference to FIG. 8, a density sensor port may be provided in the main body 1100 of the separator 1000 and may receive a density sensor 4052, such as a Coriolis meter or the like. The density sensor port may be located vertically above the lower sensor port 1064 and vertically below the lowermost bridle port 1040f The density sensor 4052 may be used to detect the density or specific gravity of the fluid (liquid) in the main body 1100 of the separator 1000. The density sensor 4052 may be in electronic communication with the controller 4000, and the controller 4000 may be programmed or configured to open, close, or modulate the shutoff valve 4120 depending on the detected flow rate and/or sand concentration of the liquid, sand, and debris in the separator 1000.

A second density sensor 4054 may be ported to the valve line upstream of the valve 2000, as illustrated in FIG. 8. The second density sensor 4054 may comprise the same type of sensor (e.g., a Coriolis meter) as the density sensor 4052 in the separator 1000. The second density sensor 4054 may be used to detect the flow rate and/or density or specific gravity of the fluid (liquid) from the separator 1000. The density sensor 4054 may be in electronic communication with the controller 4000, and the controller 4000 may be programmed or configured to open, close, or modulate the shutoff valve 4120 depending on the flow rate and/or density or specific gravity of the fluid (liquid) in the separator 1000 (detected by sensor 4052) in comparison to the flow rate and/or sand concentration of the liquid, sand, and debris output from the separator 1000. By comparing the density measured by density sensor 4052 to the density measured by density sensor 4054 an accurate estimation of sand concentration can be ascertained thereby helping to understand in real time the density of fluid flowing through the separator 1000. The determined density and flow rates of fluid flowing through the separator 1000 may be used to provide volume control of production out of the well. It can also serve as a safety device shutting in the system if gas is present.

Referring again to FIGS. 2-6, a relief valve 1070 may be provided at or near the top of the upper vessel section 1100 and may be configured to open at a predetermined pressure to allow pressurized gases to escape from the interior chamber 1010. The pressure at which the relief valve 1070 is configured to open may be selected to prevent damage to the separator 1000 and/or downstream components from excess gas pressure. For example, the relief valve 1070 may be configured to open if the gas pressure in the interior chamber 1070 exceeds the maximum operating temperature of the separator 1000, for example approximately 5,000 psi. The relief valve 1070 may be passive, e.g. having a spring that deflects at a predetermined crack pressure, or may be actively controlled by the controller 4000.

With continued reference to FIGS. 2-6, the relative vertical locations of the various ports may optimize performance of the separator 1000. For example, the inlet port 1020 may be located below the bridle ports 1040a-1040f, with the baffle 1024 directing inflow downward, so that contaminants do not flow toward and become trapped in the bridle 1300. The inlet port 1020 may also be located below the gas outlet port 1050 so that less dense gas rises above relatively more dense water, such that only the gas exits the separator 1000 via the gas outlet port 1050. Moreover, the gas outlet port 1050 may be located at the top of the main body 1100, and therefore above the intended liquid level within the separator 1000, again to prevent water from exiting through the gas outlet port 1050. The liquid, sand, and debris outlet port 1030 may be positioned as near to the base of the separator 1000 as is reasonably practical so that liquid and contaminants cannot collect below the liquid, sand, and debris outlet port 1030. The upper sensor port 1060 may be located above the uppermost bridle port 1040a and the lower sensor port 1062 may be provided below the lowermost bridle port 1040f, such that the upper and lower limit sensors 1064, 1066 may serve as failsafes in the event that the liquid level sensor 1400 fails to detect and account for the liquid level being outside the intended range.

It should be noted that an increased vertical length of the bridle 1300 may provide additional reaction time for the valve 2000 to release the liquid, sand, and debris from the main body 1010 of the separator 1000. In some embodiments, the length of the bridle 1300 and the probe length of the liquid level sensor 1400 may be selected such that the liquid level sensor 1400 has a probe length of approximately 80 inches and a targeted liquid level (e.g., a midpoint length of the bridle 1300) of approximately 55 inches.

A user interface 4002 may be communicatively coupled to the controller 4000 for outputting real time or near-real time data from the controller 4000 to a user. The user interface 4002 may take the form of a general computer, a handheld device, a siren, a light bar placed atop the separator, or any other component designed to output information to a user. The user interface 4002 may output alerts when the liquid level is outside of a desired range, a malfunction or obstruction in the valve 2000 is detected, a detected sand density of the fluid flow indicates that the volume of well production should be adjusted, or regular maintenance is needed.

In some embodiments, as shown in FIG. 8, an electronically controlled valve 4055 may be present on a gas line 4022 downstream of the gas outlet 1050 of the separator 1000. The valve 4055 on the gas line 4022 may include any desired type of valve such as, for example, a choke. The valve 4055 may be communicatively coupled to the controller 4000, which controls operation of the valve 4055 to control flow of gas through the separator 1000. The controller 4000 may communicate with one or both of the valve 4055 and the valve 2000 to control flow of fluid through the separator 1000 to maintain the desired liquid level in the separator 1000.

In some embodiments, a bypass line 4056 may be fluidly coupled to the gas outlet 1050 to bypass the electronically controlled valve 4055 on the gas line 4022. A bypass valve 4058 is disposed along the bypass line 4056, and the valve 4058 may be selectively opened to allow gas to flow around the electronically controlled valve 4055. The bypass line 4056 and the bypass valve 4058 may be smaller than the gas line 4022 and the electronically controlled valve 4055, respectively, to handle the smaller volumetric flow rates of gas exiting the separator during the initial phases of flowback operations where very little gas is present. The bypass valve 4058 may be manually operated or electronically activated. The bypass line 4056 and valve 4058 may be used to “burp” the separator 1000 during initial phases of flowback operations, for example, when extremely large volumes of liquid, sand, and debris are flowing through the separator 1000 without much gas. To maintain the liquid level in the separator 1000 in a desired range during initial phases of flowback, the electronically controlled valve 4055 on the gas line 4022 may be closed. A gas pocket eventually forms at an upper portion of the interior chamber 1100 of the separator 1000, at which point the separator 1000 would need to be “burped” to remove the gas pocket and restore the liquid level. The bypass valve 4058 may be opened and then closed again, thereby removing the gas pocket. The process may be repeated at regular intervals throughout flowback operations, these intervals getting shorter and shorter until there is a steady stream of gas flowing through the separator 1000. Once a steady stream of gas is flowing through the separator 1000, the bypass line 4056 may be closed and the electronically controlled valve 4055 operated after the initial flowback operations.

Having generally described the components of the separator 1000, detailed operation of the separator 1000 will now be described with reference to FIG. 8. Gas initially enters the separator 1000 from the wellbore W via the inlet port 1020. The inlet port 1020 may be fluidly connected to the wellbore W by piping 4100. The gas entering the separator 1000 may carry with it various contaminants, including water (in both liquid and vapor form) and sand from hydraulic fracturing (i.e. “fracking”). Additionally, the gas may carry debris, such as fragments (e.g., plug pieces) from plugs used during the fracturing process. Once inside the separator 1000, all media including gas, liquid, sand, and debris may flow through the pipe 1022 and be deflected downward by the baffle 1024, in the direction of arrow A. In an alternate embodiment, the pipe 1022 may have multiple openings, as shown in FIG. 7A.

Solid contaminants, such as sand and debris, settle in the bottom of the interior chamber 1010. Liquid, such as water, fills the interior chamber 1010 from the bottom up, establishing a liquid level L. Gas, being less dense than the liquid flows toward the top of the interior chamber 1010 in the direction of arrow B, rises above the liquid to fill the top of the interior chamber 1010. A diffuser (e.g., 1054 of FIG. 6) in the separator 1000 may assist the upward movement of gas through the interior chamber 1010. Once the liquid level L reaches the lowermost bridle port 1040f, the gas and liquid may flow freely between the interior chamber 1010 and the bridle 1300 in the direction of arrows C via the bridle ports 1040a-1040f. The liquid level L thus equalizes between the interior chamber 1010 and the bridle 1300.

The gas flows out of the separator 1000 via the gas outlet port 1050 in the direction of arrow D to piping 4022. The piping 4022 may in turn be fluidly connected to downstream components (e.g. a line heater or molecular dryer).

As the liquid level L rises from continued inflow from the wellbore, the valve 2000 may be opened to allow liquid, sand, and debris to flow out of the separator 1000 in the direction of arrow E via the outlet port 1030. In particular, the liquid, sand, and debris may flow through piping 4300 to the holding tank 3000, as shown in FIG. 8. To prevent large debris, such as plug fragments, from clogging or damaging the valve 2000, a strainer 4110 may be provided upstream of the valve 2000 to capture such debris.

The valve 2000 may be opened and closed by the controller 4000 based on the liquid level L as measured by the liquid level sensor 1400. The controller 4000 may receive a signal from the liquid level sensor 1400 indicating the vertical position of the liquid level L. If the liquid level L is at or above a maximum safe liquid level L_max, the controller 4000 may transmit a signal to the valve 2000 to open the valve 2000. With the valve 2000 open, liquid, sand, and debris in the interior chamber 1010 may flow out of the outlet port 1030 in the direction of arrow E, thereby lowering the liquid level L.

The valve 2000 may remain open until the liquid level L has reached a minimum safe liquid level L_min. When the liquid level sensor 1400 detects that the liquid level L has reached the minimum safe liquid level L_min the liquid level sensor 1400 may transmit a signal to the controller 4000 which in turn may transmit a signal to the valve 2000 to close the valve 2000. With the valve 2000 closed, the liquid level L may again rise to the maximum safe liquid level L_max, at which time the controller 4000 may again open the valve 2000 based on the determination from the liquid level sensor 1400. The valve 2000 may be repeatedly opened and closed in this manner to maintain the liquid level L between the maximum safe liquid level L_max and the minimum safe liquid level L_min as gas is extracted from the wellbore. In some embodiments, the valve 4055 on the gas line 4022 may be similarly opened and closed to maintain the liquid level L between the maximum safe liquid level L_max and the minimum safe liquid level L_min as gas is extracted from the wellbore. By maintaining the liquid level L in this manner, liquid water is prohibited from flowing out of the gas outlet port 1050 and gas is prevented from flowing out of the outlet port 1030.

As shown in FIG. 8, the maximum safe liquid level L_max may correspond to the position of the uppermost bridle port 1040a, and the minimum safe liquid level L_min may correspond to the position of the lowermost bridle port 1040d. However, it is to be understood that the maximum safe liquid level L_max and the minimum safe liquid level L_min need not correspond to the positions of the bridle port third form the top 1040c and the lowermost bridle port 1040f, but could rather correspond to any locations at which liquid may be present in the bridle 1300. With continued reference to FIG. 8, the piping 4100 leading from the wellbore to the separator 1000 may include a shutoff valve 4120, which may be manually or automatically closed to halt flow into the separator 1000. In some embodiments, the shutoff valve 4120 may be controlled by the controller 4000 in response to measurements taken by the liquid level sensor 1400, the upper and lower limit sensors 1062, 1066, the density sensors 4052, 4054, or a combination of all of the sensors. The controller 4000 may receive signals from the limit sensors 1064, 1066, and based on those signals, transmit a signal to actuate the shutoff valve 4120. If, based on a signal received from the upper limit sensor 1064, the controller 4000 determines that the liquid level within the interior chamber 1010 is above a predetermined maximum, the controller 4000 may transmit a signal to close the shutoff valve 4120. By closing the shutoff valve 4120, flow into and out of the separator 1000 is halted, thereby preventing liquid from advancing downstream.

Similarly, the controller 4000 may transmit a signal to close the shutoff valve 4120 if the controller 4000 determines that the liquid level within the interior chamber 1010 is below a predetermined minimum, based on a signal received from the lower limit sensor 1066. By closing the shutoff valve 4120, flow into and out of the separator 1000 is halted, thereby preventing the separator 1000 from running dry and the pressure from getting too high in the holding tank 3000.

The controller 4000 may also transmit a signal to open, close, or modulate the shutoff valve 4120 to control the flow of fluid into the separator 1000 from the well based on a determination of the sand concentration of the fluid flowing through the separator 1000. As discussed above, the controller 4000 may determine the real time concentration of sand flowing through the separator 1000 based on measurements taken via the density sensors 4052, 4054. The controller 4000 could also be programmed to close the valve 4120 if fluid flow is detected through valve 2000 by sensor 4054 when valve 2000 is in the closed position.

In some embodiments, the controller 4000 may utilize proportional—integral— derivative (PID) logic to continuously and/or repeatedly receive measurement signals from the liquid level sensor 1400, and subsequently actuate the valve 2000 and/or the valve 4055 to maintain the desired liquid level L in the manner described herein. Similarly, the controller 4000 may utilize proportional—integral—derivative (PID) logic to continuously and/or repeatedly receive measurement signals from the upper and lower limit sensors 1064, 1066 and/or the density sensors 4052, 4054 and subsequently actuate the shutoff valve 4120 in response to fluid level in the interior chamber 1010 and/or the concentration of sand flowing through the separator 1000.

As described herein, the controller 4000 may be in communication with the liquid level sensor 1400, the valve 2000, the valve 4055, the upper and lower limit sensors 1064, 1066, the density sensors 4052, 4054, the shutoff valve 4120, and the valve position sensor 4050. The controller 4000 may include at least one processor programmed or configured to execute instructions stored on computer-readable media. The controller 400 may communicate with the liquid level sensor 1400, the valve 2000, the valve 4055, the upper and lower limit sensors 1064, 1066, the density sensors 4052, 4054, the shutoff valve 4120, and the valve position sensor 4050 by any suitable wired or wireless communication protocols and interfaces such as 4-20 milliamp HART signal, Ethernet, fiber optics, coaxial, infrared, radio frequency (RF), a universal serial bus (USB), Wi-Fi®, cellular network, and/or the like. The controller 4000 may be in communication with a user interface 4002 to provide real-time feedback to the electronic controller and/or to an operator of the liquid level L within the interior chamber 1010, and/or real-time feedback that the separator 1000 and its associated components are operating properly.

Referring now to FIGS. 13 and 14, the separator 1000 may be used as a component of a gas processing facility 5000 including the separator 1000 and a line heater and choke assembly 5100. FIG. 13 shows two separators 1000 feeding into a single line heater and choke assembly 5100, although a single separator 1000 may also be used. The two separators 1000 may be used to produce gas from two different wells simultaneously. As illustrated, the two separators 1000 may be positioned side by side and connected to the same skid 1090 of downstream equipment (e.g., a single line heater and choke assembly 5100 for both separators 1000), thereby saving space. The line heater and choke assembly 5100 includes a line heater 5200 and a choke 5300. Gas, water, and contaminants flow in the separator 1000 from the wellbore W, where the water and contaminants are separated from the gas as described herein. Gas flowing out of the separator 1000 via the gas outlet port 1050 and the piping 4022 flows into the line heater 5200. The line heater 5200 may include, for example, one or more coils disposed in a heated glycol bath. Gas from the separator 1000 flows through the coils until the gas reaches a desired temperature and/or pressure. The gas exiting the line heater 5200 then flows through the choke 5300, which drops the pressure of the gas to a desired line pressure, for example 1,400 psi.

Referring now to FIG. 15, a flow diagram of a process 6000 for gas production from a well is shown as substantially described herein. The process 6000 may be a process for producing a pressurized natural gas stream from a fluid being produced from a wellbore. The process 6000 may be fully or partially automated by the controller 4000. At step 602, the gas flow to the separator 1000 from the wellbore W may be initiated. This may be achieved, for example, by opening the shutoff valve 4120 via the controller 4000. Alternatively, the shutoff valve 4120 may be manually opened. The fluid may be directed into the separator 1000 at a pressure substantially equal to the pressure of the fluid being produced from the wellbore.

At step 604, the liquid level L within the interior chamber 1010 may be determined. In particular, the liquid level sensor 1400 may transmit a signal indicating the liquid level L to the controller 4000. The liquid level sensor 1400 may provide real-time feedback of the liquid level L to the controller 4000.

The process 6000 may further include controlling the liquid level L in the separator 1000 between two predetermined set points (e.g., L_max and L_min) by regulating the flow of the liquid, sand, and other solid debris out of a lower portion of the separator 1000. For example, at step 606, the electronically controlled valve 2000 may be opened or closed, or modulated, in response to the determination of the liquid level L. In particular, the controller 4000 may transmit a signal to open the valve 2000 if the liquid level L is at or above the maximum safe liquid level L_max, and the controller 4000 may transmit a signal to close the valve 2000 if the liquid level L is at or below the minimum safe liquid level L_min. Modulation of the valve 2000 also allows accumulated sand and debris to exit the separator 1000, such that manual cleaning is not required. The process 6000 may further include directing the gas (substantially cleaned of liquid, sand, and debris) out of the separator 1000 at a pressure substantially equal to the pressure of the wellbore.

At step 608, the liquid level L within the internal chamber 1010 of the separator 1000 may be verified or confirmed to be within a proper range utilizing the upper limit sensor 1064 and/or the lower limit sensor 1066 in case of a malfunction of the liquid level sensor 1400. In particular, the upper limit sensor 1064 and/or the lower limit sensor 1066 may transmit a signal to the controller 4000 indicative of the presence of liquid at the upper sensor port 1060 and the lower sensor port 1062.

At step 610, the shutoff valve 4120 may be closed in response to determining that the liquid level L in the interior chamber 1010 is outside of the proper range. In particular, the controller 4000 may transmit a signal to close the shutoff valve 4120 if the liquid level L is above the upper limit sensor 1064 or if the liquid level L is below the lower limit sensor 1066. Steps 604, 606, 608, and 610 may be repeated periodically, continuously, and/or at predetermined time intervals during the service life of the well.

In some embodiments, the controller 4000 may require a “handshake” verification between the liquid level sensor 1400 and the upper and lower limit sensors 1064, 1066 to actuate the valve 2000. That is, the controller 4000 may require that the liquid level determined by the liquid lever sensor 1400 matches the liquid level determined by the upper and/or lower limit sensors 1064, 1066 prior to actuating the valve 2000. The controller 4000 may use this “handshake” to diagnose a fault in the liquid level sensor 1400, the upper limit sensor 1064, and/or the lower limit sensor 1066. The controller 4000 may use this manner of fault detection to ensure that the separator 1000 is operating properly and may provide feedback to an operator that the separator 1000 is (or is not) operating properly. With this precision control, electronic, real-time feedback provided to the operator to ensure that the separator 1000 is operating properly, and redundant protections to ensure that the separator 1000 does not overflow or empty, it is virtually impossible for gas to be lost to tanks on location.

The system and process of the present disclosure can allow for higher gas and liquid flow rates than the existing sand separator and GPU legacy configuration. Because fluid separation is occurring downstream of the pressure cut in the GPU within the legacy configuration, and the associated gas expansion and system velocities increase, turbulence in the GPU is amplified. As such, the legacy system can be limited to a maximum of 60 barrels/hour. The separator 1000 of the present disclosure allows for liquid separation to occur at significantly higher pressures than in the existing system, which means that the liquid separation of the present disclosure occurs at lower fluid velocity and, consequently, less turbulent flow. For example, the separator 1000 may allow for liquid handling capacities in excess of 200 barrels/hour using a separator 1000 with a working volume of only 8 barrels. This advantage may eliminate the need to employ third party flowback services, which require process flowrates on the order of 120 barrels/hour. Additionally, manpower is greatly reduced utilizing the technology described as almost all aspects of the operation are automated. The operation can be considered “eFlowback”.

Due to the safety concerns associated with gas production, any of the components of the separator 1000 described herein may be provided in duplicate and/or may include redundant systems in order to ensure safe operation of the separator 1000. Additionally, two separators 1000, 1001 may be built onto one skid and used in series, the first acting as a primary separator and the second as a polishing or back up vessel in the event fluid is carried over from the primary vessel. This arrangement is illustrated in FIG. 21. This configuration is particularly advantageous in systems that use a molecular dryer, as it is critical that free liquid should never make contact with the molecular dryer and molecular sieve, desiccant or other material it contains. Alternatively, in operations where some free liquid carryover is not problematic the separator 1000 can be used in parallel, for example as shown in FIG. 17 where the separator 1000 is working in tandem with conventional production equipment shown in FIG. 1. In this example, the skid may have two separators 1000 in parallel that can be used to flowback two wells, as shown in FIG. 17A. Ultimately, in this configuration, the system can serve in two unique applications.

Having generally described the separator 1000 and its operation, various applications in which the separator 1000 may be used will now be described with reference to FIGS. 17-21. However, as those of ordinary skill in the art will appreciate, the separator 1000 may also be used in conjunction with a conventional GPU 20 (as shown in FIG. 1). FIG. 17 illustrates a gas production facility 700 including the separator 1000 being used to perform a flowback operation for a well. The well is designated in FIG. 17 by a tree 702, which is located at the wellhead. The tree 702 may be a standard Christmas tree 702 located above a well and comprising multiple valves and bores through which fluid may be directed from the well. The tree 702 is configured to output fluid produced from a wellbore. The fluid produced from the wellbore may include gas, liquid, sand, and debris.

During flowback operations, liquid, sand, and debris may make up a significant proportion of the fluid being produced from the wellbore. Flowback operations may last for 5 days, 1 week, 2 weeks, or up to a month or more. Permanent production equipment that is used to process gas output from the well is not designed to handle the large amounts of liquid, sand, and debris that is removed from the well during flowback operations. The separator 1000 described at length above may be used to clean the liquid, sand, and debris from the well fluid during flowback operations so that the same gas processing equipment (e.g., gas processing unit 704) may be used to process the gas during flowback operations and during the longer production phase after flowback operations. The gas processing unit 704 may include at least a choke for reducing a pressure of the gas or fluid flowing therethrough. The illustrated arrangement of the separator 1000 and gas processing unit 704 used to provide flowback operations has a much smaller footprint than conventional third-party flowback spreads.

The separator 1000 may be connected to the tree 702 and gas production unit 704 via a series of flow paths, each flow path taking the form of rigid or flexible piping. The gas production facility 700 may include, for example, a first flow path 706 connecting a first outlet 708 of the tree 702 to the inlet 1020 of the separator 1000. The inlet 1020 delivers the fluid into the separator 1000 at a first pressure. The fluid may comprise liquid, gas, sand, and debris. As illustrated and described in detail above, the separator 1000 includes the inlet 1020 and a gas outlet 1050 through which gas (separated from the liquid, sand, and debris) is delivered from the separator 1000. The gas production facility 700 may also include a second flow path 710 connecting a second outlet 712 of the tree 702 to the gas production unit 704. Fluid may flow from the well directly to the gas production unit 704 via the second flow path 710 when a valve at the second outlet 712 is open. The gas production facility 700 may further include a third flow path 714 connecting the gas outlet 1050 of the separator to the gas production unit 704 or, more particularly, to the second flow path 710 leading to the gas production unit 704. As illustrated, a valve 716 may be disposed along the third flow path 714 for selectively opening and closing the third flow path 714. As illustrated in FIGS. 17 and 17A, a by-pass valving system (e.g., including an electronically controlled valve 4055, bypass line 4056, bypass valve 4058, and/or gas measurement device 1057 as discussed with reference to FIG. 8) may be disposed along the third flow path 714 in addition to the valve 716. The by-pass valving system may enable the control of gas flowing from the separator 1000 throughout flowback operations (e.g., when it may be desirable to “burp” the vessel of the separator 1000) and after flowback operations when a substantially flow of gas has been established. In some embodiments, the valve 716 may not be present such that the by-pass valving system provides all control of flow through the third flow path 714.

During flowback operations, a valve at the second outlet 712 of the tree 702 may be closed while a valve at the first outlet 708 of the tree 702 may be opened. That way, fluid containing large amounts of liquid, sand, and debris is directed to the separator 1000 through the first flow path 706. The separator 1000 may remove the liquid, sand, and debris through the outlet 1030 by controlling the valve 2000 according to the method described above. The gas separated from the liquid, sand, and debris is delivered out of the separator 1000 through the outlet 1050 and through the third flow path 714 and the second flow path 710 to the gas production unit 704 (e.g., following arrows 718). The liquid, sand, and debris separated from the gas may pass through a junk catcher or other type of filter 4110 so as not to clog the valve 2000. Downstream of the valve 2000, the liquid, sand, and debris may be manifolded to an outlet of the gas production unit 704 through which liquid, sand, and/or debris may also be directed out of the gas production unit 704.

After flowback operations are completed or once a gas volume suitable for permanent equipment is reached (e.g., once the well is producing largely gas), the valve at the second outlet 712 of the tree 702 may be opened and the valve at the first outlet 708 closed, thereby allowing the fluid to flow from the well directly to the gas production unit 704 instead of the separator 1000. Thus, the separator 1000 may alone or in combination with a conventional system as shown in FIG. 1 replace a conventional flowback spread for removing large amounts of liquid, sand, and debris.

Referring to FIGS. 18-21, the separator 1000 according to the present disclosure may be used not only for gas production to a pipeline, but to generate other products or energy using substantially less equipment on location and at lower cost than conventional methods. This is because the disclosed separator 1000 is able to output a highly pressurized and substantially clean gas stream. Removing all free liquid from the gas stream at approximately wellhead pressure (prior to any pressure cut) enables new and improved uses of wellhead energy. For example, the wellhead energy may be used for one or more of power generation, as subsequently hydrogen, oxygen, a naturally formed compressed natural gas (CNG) production, and liquefied natural gas (LNG) production, and other useful products

FIG. 18 illustrates a system 800 that may utilize the pressurized gas stream to simultaneously power one or more processes in addition to, or in lieu of, supplying gas to a pipeline 810. Each of the components illustrated in FIG. 18 may be an individual piece of mobile equipment brought to a well location. The separator 1000, as illustrated, may generally include the inlet 1020, the liquid, sand, and debris outlet 1030, and the gas outlet 1050. The separator 1000 may include the same components and operate as described above with reference to any of FIGS. 2-12 and 16. The inlet 1020 may deliver fluid being produced from a wellbore into the separator 1000 at a first pressure, and the fluid may comprise liquid, gas, sand, and debris. The gas outlet 1050 is configured for delivering gas separated from the liquid, sand, and debris out of the separator 1000 at a second pressure. The second pressure may be substantially equivalent to the first pressure in some embodiments. In other embodiments, the second pressure may be different than the first pressure. The outlet 1050 may be connected to a particulate filter 802, which may be connected to a molecular dryer 804. As such, the outlet 1050 is connected to the molecular dryer 804. The outlet 1050 may also or alternatively connected to a gas processing unit 704.

The molecular dryer 804 is a molecular vapor dryer, which removes water vapor from the gas stream. As those of ordinary skill in the art will appreciate, the molecular dryer 804 may be a molecular sieve, a membrane, or any other device or process capable of removing all or most of the water vapor from the gas stream output from the outlet 1050, such that the remaining gas stream could meet the parts per million (PPM) requirements needed for powering certain downstream equipment. As illustrated, the molecular dryer 804 has at least one outlet through which the gas substantially removed of water vapor is directed out of the molecular dryer 804. As those of ordinary skill in the art will appreciate, the molecular dryer could be any device that removes water vapor from gas.

After passing through the molecular dryer 804, the gas stream may be split and/or directed downstream to perform one or more processes. In the illustrated embodiment, the gas stream is split after the molecular dryer 804. The different portions of the gas stream are then delivered to a CNG filling station 806, delivered to a pipeline 810, liquefied to produce LNG 818, used to generated electricity 812, and the power would then be used to generate hydrogen 814. As those of ordinary skill in the art will appreciate, CNG filling station 806 may be stationary storage tanks or trucks. The stream of gas directed into the CNG filling station is compressed natural gas, which the industry defines as CNG. Because the CNG produced through this process does not use external or human-made compression, it will be referred to herein as “naturally compressed natural gas.” Although all these processes are illustrated in FIG. 18, it should be understood that fewer or more processes may be performed using the pressurized gas stream output from the molecular dryer 804. The one or more gas streams may be output from the molecular dryer 804 at a third pressure, which may be substantially the same or different than one or both of the first and second pressures described above.

As illustrated, the CNG filling station 806 may be connected to an outlet of the molecular dryer 804 such that a first gas stream output from the molecular dryer may be directed to the CNG filling station 806. In some embodiments, a pressure control valve 820 is disposed between the CNG filling station and the molecular dryer for reducing or otherwise controlling the pressure of the gas being directed out of the molecular dryer from the third pressure to a lower pressure. For example, the third pressure may be approximately 5,000 psi, while the fourth pressure may be approximately 3,600 psi. That way, the gas stream is brought down to a desired pressure needed for filling CNG tanks. In other embodiments, the pressure control valve 820 may not be present.

Modern CNG is typically compressed from pipeline pressure as low as 50 psi up to pressures of approximately 5,000 psi. By precisely removing all free liquid from the well at wellbore pressures via the separator 1000 and molecular dryer 804, CNG may be generated with no compression. There is significant reduction of capital, operating costs and emissions associated with eliminating the compression element of producing CNG and allowing the wellbore pressure to provide the pressure necessary to fill tanks or high-pressure pipelines.

As illustrated in FIG. 18, the system 800 may comprise a turbo expander 808 connected to an outlet of the molecular dryer 804. An exemplary turbo expander converts changes in pressure into rotational/mechanical energy that can be used for compression, power generation and the like. (As used herein, a “turbo expander” is defined as a device that creates mechanical energy from a pressure differential). It may also produce cooling via the Jules Thompson Effect. It may include and be coupled with or connected to a gas compressor, an electric generator or any other device, system or process requiring the mechanical energy and/or rotational energy it produces. As those of ordinary skill in the art will appreciate, wherever it is disclosed to use a turbo expander, a piston expander, reciprocating expander, centrifugal compressor or a positive displacement expander may be used in its place. An exemplary combination turbo expander compressor might include a Compander™ brand turbo expander/compressor. The turbo expander 808 may be powered by the gas directed out of the molecular dryer and used to generate electricity (812) and subsequently hydrogen (814) through electrolysis. The turbo expander 808 may include an inlet for receiving the pressurized clean gas flow from the molecular dryer 804 and one or more outlets through which gas is output from the turbo expander at a lower pressure. In some embodiments, the system 800 may include a pressure control valve 822 disposed between the outlet of the molecular dryer 804 and the turbo expander 808 for reducing a pressure of the gas being directed out of the molecular dryer from one pressure to a lower pressure. For example, the pressure control valve 822 may reduce the pressure from approximately 5,000 psi to approximately 2,500 psi or the technical limits of existing turbo expander technology. Existing Utica wells can generate the equivalent of over 10,000 horsepower of energy. This may bring the gas stream down to a desired pressure so that the gas stream is output from the turbo expander at an appropriate pipeline pressure (e.g., 1,000 psi). It should be noted that the pressures listed here are merely examples and other embodiments may include the gas stream at different pressures.

The turbo expander 808 may function as a generator, converting the pressure drop of the gas moving through the turbo expander 808 into electricity (812). The pressurized gas flow is able to be used in a turbo expander due to the fact that all liquid has been removed from the gas stream (e.g., via the separator 1000 and the molecular dryer 804) without a significant pressure drop. In some embodiments, the generated electricity (812) may be used to power on-site equipment or distributed to the local power grid. In some embodiments, the electricity may be used to generate emissions free hydrogen through electrolysis (814). Using the separator 1000, the molecular dryer 804, and the turbo expander 808, the system 800 may be able to generate electricity at the well with zero emissions.

As illustrated, the system 800 may include a gas pipeline 810 connected to the outlet of the turbo expander 808. In other embodiments, the system 800 may include a gas pipeline 810 connected to an outlet of the molecular dryer 804. The gas pipeline 810 may deliver natural gas to a natural gas pipeline. As will be understood by one of skill in the art, the gas pipeline 810 may deliver natural gas at a pipeline pressure (e.g., 1,000 psi) that is lower than the pressure at which gas is output from the molecular dryer 804 (e.g., 5,000 psi). As such, the pressure of the gas is reduced prior to supplying the gas to the pipeline 810. This pipeline pressure may be a pressure at which the natural gas grid supplies gas to communities. In FIG. 18, for example, the turbo expander 808 is connected between the gas pipeline 810 and the molecular dryer 804 for reducing the pressure of the gas being directed through the turbo expander 808 to a lower pressure that is substantially equal to the desired pipeline pressure and generating electricity and subsequently hydrogen in the process. The pressure control valve 822 may also reduce the pressure exiting the molecular dryer. In some embodiments, although not explicitly depicted, the turbo expander may be omitted, replaced with a JT (Joule Thomson) valve or the pipeline 810 may not be connected to the turbo expander 808. In such instances, a pressure control valve 822 may be connected between the gas pipeline 810 and the molecular dryer 804, and the pressure control valve 822 may reduce the pressure of gas being directed out of the molecular dryer 804 to a pressure that is substantially equal to the desired pipeline pressure.

The disclosed system 800 may provide gas to the pipeline 810 with reduced or no emissions. Because of the use of the disclosed separator 1000 in combination with the molecular dryer 804, the gas being provided to the pipeline 810 and/or other downstream components of the system 800 is substantially free of water vapor and contaminants. When the pressure of the gas is reduced, by a pressure control valve 822, JT valve, turbo expander 808, or all three, there is no possibility of water vapor in the gas stream freezing and damaging equipment. Therefore, no burners or other heat sources are needed to prevent water from freezing in the gas stream. As such, the pressure reduction needed to bring the gas stream to pipeline pressure can be accomplished without the emissions released by conventional burners.

The separator 1000, molecular dryer 804, and turbo expander 808 may also enable the generation of LNG 818 without electricity or outside energy. LNG 818 is natural gas that has been cryogenically cooled to −260° F. to liquify LNG 818 and is typically stored at 5 PSIG or less. As illustrated, the system 800 may include a cold box 816 connected to the turbo expander 808. In other embodiments, although not explicitly depicted, the system 800 may include a cold box 816 connected to an outlet of the molecular dryer 804. (The cold box 816 is configured to capture the cold gas exiting the turbo expander 808 (or molecular dryer 804) so as to produce LNG 818 at lower pressure than the incoming gas. As used herein “cold box” is defined as one or more components of a heat exchange equipment, valves, controllers, heat retention and all other associated devices and processes to support the liquification process) In the embodiment of FIG. 18, the turbo expander 808 may produce supercooled gas in additional to electricity 812 and subsequently hydrogen 814. The turbo expander 808 may be connected to refrigeration compression. The cold box 816 may be connected to refrigerated fluid or gas outlet to receive the cooling fluid 824 for cryogenically cooling the gas exiting the turbo expander 808 (or molecular dryer 804).

The disclosed system 800, in which pressurized gas is provided via the separator 1000 and molecular dryer 804, may aid in lowering the capital and operating expense of a liquefaction facility for generating LNG, since no outside electricity or energy is needed to reduce the gas pressure or operate the cold box 816. The disclosed system 800 may further reduce the environmental and emissions footprint needed for producing LNG. Depending on gas composition, additional gas conditioning downstream of the molecular dryer maybe be required for LNG production, such as carbon dioxide and heavy hydrocarbon (e.g., Butane, Pentane, etc.) removal. Accordingly, the embodiments shown in FIGS. 18-21 optionally include a conditioner 805 immediately downstream of the molecular dryer 804.

FIG. 19 depicts another system 900 that may utilize the pressurized gas stream to simultaneously power one or more processes in addition to, or in lieu of, supplying gas to a pipeline 810. The system 900 shown in FIG. 19 is similar to the system 800 shown in FIG. 18, except that the pressure control valves 820 and 822 have been replaced with another turbo expander 826. This second turbo expander 826 is disposed between the outlet of the molecular dryer 804 and the turbo expander 808. The turbo expander 826 may reduce the pressure of the gas being directed out of the molecular dryer 804, and the turbo expander 808 may then reduce the pressure of the gas being directed out of the turbo expander 826. In general, any pressure drop that is needed to provide gas to a downstream process may be accomplished using a turbo expander 808, 826 as illustrated. This may help to further conserve energy by converting all pressure drops into work to generate electricity 812, 828, hydrogen via hydrolysis 814, 830, and/or cooling fluid 824, 832 to supply a cold box 816. Any desired number of turbo expanders may be connected in series between the molecular dryer 804 and the downstream component(s) needing a reduced pressure flow of gas.

As shown in FIG. 19, the system 900 may include a compressed natural gas filling station 806 connected to an outlet of the closest turbo expander 826 to the molecular dryer 804. The turbo expander 826 connected between the compressed natural gas filling station 806 and the molecular dryer 804 may reduce the pressure of gas being directed out of the molecular dryer to a lower pressure that can be used to fill CNG tanks (806). The CNG filling station 806 may need gas provided at a pressure higher than some other downstream processes (e.g., LNG generation or supplying the pipeline), which is why it receives gas output after the first pressure drop via turbo expander 826.

FIG. 20 depicts yet another system 2001 that may utilize the pressurized gas stream to simultaneously power one or more processes in addition to, or in lieu of, supplying gas to a pipeline 810. The system 2001 shown in FIG. 20 is similar to the system 800 shown in FIG. 19, except that an auxiliary chiller 852 is connected to the cold box 816 to further chill hydrogen 848 and/or oxygen 850 being produced through the electrolysis process 846 to produce liquid hydrogen (H₂) and liquid oxygen (O₂). As those of ordinary skill in the art will appreciate, because oxygen liquifies at a higher temperature than hydrogen, each would need its own unique flow path from the auxiliary chiller 852 or alternatively separate heat exchange/auxiliary chilling devices. Power 842 output from the turbo expanders 808 and 826 through the power generation and cooling steps 840 is used to separate hydrogen 848 from oxygen 850 in an electrolysis process 846. The hydrogen 848 and oxygen 850 are then fed into the cold box 816 (which is made cold as noted above with reference to FIGS. 18 and 19 through the cooling fluid exiting the turbo expanders 808 and 826 as the gas passes through these devices). The cold box 816 can produce LNG 818 as described in FIGS. 18 and 19 and also liquid oxygen 854 and liquid hydrogen 856 through the aid of auxiliary chiller 852, which could be powered by a turbo expander via electricity or mechanically through compression. The auxiliary chiller 852 further cools these gases to the point that they undergo a phase change and become liquid. The liquid oxygen 854 is cooled to approximately −297° F. and the liquid hydrogen 856 is cooled to approximately −423° F. The oxygen 850 is stored at approximately 350 psi or lower as it passes through the auxiliary chiller 852 and the hydrogen 848 is stored at approximately 45 psi as it passes through the auxiliary chiller 852.

FIG. 20 illustrates that another turbo expander 834 can be connected downstream of turbo expander 808 to generate additional power and cooling by harvesting the energy generated by further reducing the gas pressure to get it to a pressure which would allow it to be transported by gas pipeline 810. In the embodiments shown in, and described in reference to, FIGS. 18-21, a compressor may optionally be connected to, and powered by, the turbo expanders within the system, either through direct connection compression or power by the electricity generated within the process. These compressors can be utilized for facilitating the compression of hydrogen, oxygen, natural gas, refrigerant gases or other gases into a truck, a separate pipeline, the cold box or for blending with natural gas in pipeline 810.

The embodiment in FIG. 20 further proposes to harvest additional energy from the high-pressure liquid exiting from the bottom of the separator 1000. First, the liquid, sand and debris existing the separator 1000 through outlet port 1030 must have the solids material removed from it. This is done by passing the fluid mixture through a mechanism for removing solids 860. As those of ordinary skill in the art will recognize the mechanism for removing solids from the liquid may include a strainer or junk catcher or similar device. Once the sand and other solid debris is removed the resultant high-pressure liquid can be passed through hydroelectric turbine 870, which in turn can generate electricity 812 for local power consumption (e.g., in powering the various equipment used in the above mentioned processes) and/or for delivery to the power grid. As will be appreciated by those of ordinary skill in the art multiple hydroelectric turbines 870 may be connected in series to harvest as much energy as possible from the high-pressure liquid.

The embodiment of FIG. 20 may further comprise a compressor 880 fluidly connected to the electrolysis device 846 into which the hydrogen 848 may be fed to allow the hydrogen to be compressed and subsequently delivered to customers, for example, via a truck 882 or the gas pipeline 810. Alternatively, the hydrogen 848 can be delivered via a dedicated hydrogen pipeline 890. As those of ordinary skill in the art will appreciate compressed hydrogen can be blended with natural gas as burned for power generation as newer gas turbine engines are capable of burning a blend of hydrogen and natural gas. In one exemplary embodiment, the fuel for such a turbine contains 15% hydrogen. Similarly, the truck 882 can transport the hydrogen gas for subsequent blending or other use at a remote location.

FIG. 21 illustrates the system 2001 of FIG. 20 having two separators 1000 and 1001 coupled in series to provide the pressurized gas flow to the molecular dryer 804 and other downstream components, as referenced above.

The systems 800, 900 and 2001 of FIGS. 18-21, are merely examples of different arrangements of processes that may be combined to utilize the pressurized gas output from separator 1000. Other arrangements may be possible in other embodiments. Since free and abundant energy is available through the pressurized flow of gas from the separator 1000, there is no need to design the entire system around one product (e.g., CNG, LNG, electricity, or hydrogen). Since CNG and LNG can be produced without compression, all the waste energy from the pressure drops through the system can be harnessed to generate electricity and/or to make hydrogen.

FIG. 22 depicts yet another system 2200 that may utilize a pressurized gas stream to simultaneously power one or more processes in addition to, or in lieu of, supplying gas to a pipeline 2212. FIGS. 23 and 24 depict more detailed embodiments of the system 2200 depicted schematically in FIG. 22.

The system 2200 illustrated in FIG. 22 may be used within the system(s) illustrated in FIGS. 20 and 21. For example, the system 2200 (or one or more components thereof) may be used in place of the cold box 816, turbo expander 834, and/or turbo expander 808 illustrated in FIGS. 20 and 21. FIG. 22 depicts a conditioner 2202 located upstream of the other components of the system 2200. The term “conditioner” 2202 may refer to any number of pieces of equipment used to condition a pressurized gas stream (such as the filter 802, molecular dryer 804, and/or conditioner 805 in FIGS. 20 and 21). Any desired number and arrangement of equipment may be located within or upstream of the conditioner 2202 in FIG. 22, as long as the conditioner 2202 outputs a pressurized gas flow. The pressurized gas flow may be at a pressure approximately equal to a pressure at which gas is produced from a wellbore. The pressurized gas flow may be at least 1,500 psig. The pressurized gas flow may be substantially removed of water vapor. The pressurized gas flow may be a stream of gas that was produced from a wellbore and separated from liquid, sand, and debris at a pressure substantially equal to wellbore pressure (e.g., via the separator 1000 described above), thereby harnessing the energy from the wellbore. In other embodiments, the pressurized gas flow may be any other type of high pressure gas feed, such as a transmission pipeline gas feed. In such instances, components of the system 2200 may be located at or proximate a pressure letdown station where the transmission pipeline gas is throttled from a higher pressure to a lower pressure for sending to a distribution pipeline (e.g., the pipeline 2212).

The system 2200 of FIG. 22 includes a heat exchanger 2204, which may also be referred to as a “cold box”. The heat exchanger 2204 may include a number of passages therein through which the pressurized gas stream output and other gas/vapor streams flow. The heat exchanger may enable cooling/heating of certain streams flowing therethrough. The heat exchanger 2204 may include a first inlet 2205 fluidly connected to the conditioner 2202 and configured to receive a first pressurized gas stream. The heat exchanger 2204 may also include a first outlet 2207 connected to the first inlet 2205. The heat exchanger 2204 may cool the first pressurized gas stream moving through the heat exchanger from the first inlet 2205 to the first outlet 2207. As such, the first outlet 2207 may output a chilled gas stream produced by the heat exchanger 2204 cooling the first pressurized gas stream.

The system 2200 also includes a turbo expander 2206 coupled to the first outlet 2207 of the heat exchanger 2204. The turbo expander 2206 may be referred to as an “LNG turbo expander”, as it is used to produce LNG 2208. The turbo expander 2206 is connected to the first outlet 2207 of the heat exchanger 2204 for receiving the chilled gas stream produced by the heat exchanger 2204 and then producing a partially liquified gas stream. The partially liquified gas stream may comprise LNG 2208 and (non-liquified) vapors. During operation, the turbo expander 2206 reduces the pressure of the cryogenically cooled gas (e.g., expanding the chilled gas stream output from the outlet 2207 of the heat exchanger 2204), thereby cooling the gas further and partially condensing it into LNG 2208. The turbo expander 2206 may chill the cold, high-pressure gas stream down to a point where approximately 38% of the gas stream is liquified. In some embodiments, the turbo expander 2206 may reduce the pressure of the chilled gas stream to 10 psig or less, more particularly 7.5 psig or less, or more particularly approximately 5 psig.

As the turbo expander 2206 only partially liquifies the gas stream, the system 2200 may further include at least one separator 2214 connected to the turbo expander 2206. The partially liquified gas stream is fed into the separator(s) 2214 and the separator(s) 2214 separate the vapors from the LNG 2208. Thus, the system allows for production and isolation of LNG 2208, which can be stored in tanks for transportation away from the wellsite or used as fuel on location. The separator(s) 2214 may include one or more vessels for separating cryogenically cooled vapors from LNG at various pressures.

The vapors removed from the LNG via the separator(s) 2214 may be directed into the heat exchanger 2204 for use as additional cooling fluid. To that end, the heat exchanger 2204 may include at least one vapor inlet (e.g., 2215) connected to the separator(s) 2214 for receiving vapors removed by the separator(s) 2214. The heat exchanger 2204 may then cool the first pressurized gas stream via heat transfer between the first pressurized gas stream and the vapors. In particular, the first pressurized gas stream entering via inlet 2205 and exiting via outlet 2207 is cooled, while the pre-chilled vapors entering via inlet(s) 2215 are heated in the heat exchanger 2204.

The heat exchanger 2204 may also include at least one vapor outlet (e.g., 2217) used to output the vapors from the heat exchanger 2204. The system 2200 may include a vapor recovery unit (VRU) designed to use a majority or all of the vapors output from the separators 2214 so that the vapors do not have to be burned. The VRU, for example, may include a compressor used to raise the pressure of the cryogenically cooled vapors to a pressure greater than or equal to pipeline pressure. The VRU essentially boosts the leftover vapors to pipeline pressure so as to avoid releasing emissions by flaring the vapors. As illustrated, the system 2200 may include at least one compressor 2216 connected between the at least one vapor outlet 2217 of the heat exchanger 2204 and the pipeline 2212. The at least one compressor 2216 may compress the vapors output from the heat exchanger to a pressure suitable for the pipeline 2212 and output a compressed gas toward the pipeline 2212 at a pipeline-suitable pressure.

The turbo expander 2206 may be coupled to the at least one compressor 2216, as illustrated, to supply power 2218 generated by the turbo expander 2206 to the at least one compressor 2216. The power generated by the turbo expander 2206 may be supplied to the compressor(s) 2216 for operating the compressor(s) 2216. As an example, the turbo expander 2206 may be mechanically coupled to the compressor(s) 2216, e.g., via one or more shafts and/or a set of gears. Thus, the turbo expander 2206 may supply mechanical power to drive the compressor(s) 2216. In another example, the turbo expander 2206 may be electrically coupled to the compressor(s) 2216 via a generator driven by the shaft of the turbo expander 2206, which produces electricity, and one or more motors that use the generated electricity to turn the compressor(s) 2206. The turbo expander 2206 may generate electricity via mechanisms discussed at length above with reference to FIGS. 18-21. In yet another example, the turbo expander 2206 may be mechanically coupled to the compressor(s) 2216 and also coupled to a generator, so that any additional power produced by the turbo expander 2206 over what is needed to drive the compressor(s) 2216 may be converted to electricity (which may be used to power other processes on location, supplied to a grid, etc.).

As illustrated in FIGS. 22-24, an initial gas stream 2302 (e.g., gas stream output from the conditioner 2202 of FIG. 22) may be split into a first pressurized gas stream 2306 and a second pressurized gas stream 2308. The system 2200 may include a feed splitter 2304 upstream of the heat exchanger 2204 for splitting the initial gas stream 2302 into these two component streams. The feed splitter 2304 may take any desired form apparent to a person of ordinary skill in the art. For example, the feed splitter 2304 may be a simple T-shaped or Y-shaped joint and/or may include one or more valves for controlling a relative amount of the first and second pressurized gas streams.

The first pressurized gas stream 2306 may be fed to the first inlet 2205 of the heat exchanger 2204, while the second pressurized gas stream 2308 may be fed to a second turbo expander 2210. The second turbo expander 2210 may be referred to as a “gas line turbo expander” as it is used to provide gas to the pipeline 2212. The second turbo expander 2210 may be connected between the feed splitter 2304 and a second inlet 2220 of the heat exchanger 2204. The second turbo expander 2210 receives the second pressurized gas stream 2308 and outputs an expanded gas stream to the second inlet 2220. In particular, the second turbo expander 2210 reduces a pressure of the second pressurized gas stream 2308 to produce an expanded gas stream provided to the heat exchanger 2204. A second outlet 2221 of the heat exchanger 2204 corresponds to the second inlet 2220, and the pipeline 2212 may be connected to the second outlet 2221 of the heat exchanger 2204.

In operation, the heat exchanger 2204 cools the first pressurized gas stream 2306 moving therethrough via heat transfer between the first pressurized gas stream 2306 and the expanded gas stream (output from the turbo expander 2210) in the heat exchanger 2204. This simultaneously heats the expanded gas stream in the heat exchanger 2204. As such, the heat exchanger 2204 produces a heated gas stream by heating the expanded gas stream, and the heated gas stream is output from the heat exchanger 2204 via the second outlet 2221 toward the pipeline 2212. The heated gas stream produced by the heat exchanger 2204 may be output toward the pipeline 2212 at a pressure and temperature suitable for the pipeline 2212. Providing heat exchange between the expanded gas stream and the first pressurized gas stream allows the expanded gas stream to be heated up to a pipeline-suitable temperature and the first pressurized gas flow to be pre-chilled before it is partially liquified.

As illustrated in FIG. 22, the second turbo expander 2210 may be coupled to the at least one compressor 2216 to supply power 2218 generated by the second turbo expander 2210 to the at least one compressor 2216. The power generated by the second turbo expander 2210 may be supplied to the compressor(s) 2216 for operating the compressor(s) 2216. The at least one compressor 2216 may thus be coupled to one or both of the turbo expander 2206 and the second turbo expander 2210. One or both of the turbo expander 2206 and the second turbo expander 2210 may supply power to the at least one compressor 2216. Similar to the coupling between the turbo expander 2206 and the compressor(s) 2216 described above, the second turbo expander 2210 may be mechanically or electrically coupled to the compressor(s) 2216 so as to provide mechanical power or electricity for driving the compressor(s) 2216.

As illustrated in FIGS. 22-24, the systems 2200, 2300, and 2400 each include the heat exchanger 2204 with paths therethrough for the LNG feed (e.g., first pressurized gas stream), the pipeline feed (e.g., expanded gas stream), and the chilled vapor feed(s). However, in other embodiments, only some of these components may be present. For example, the system may not include the pipeline feed and may instead simply involve the heat exchanger 2204 transferring heat between the first pressurized gas stream and the chilled vapor feed(s). In another example, the system may not include the chilled vapor feed(s) and may instead simply involve the heat exchanger 2204 transferring heat between the first pressurized gas stream and the pipeline feed. The compressor(s) 2216 and line running from the compressor(s) 2216 to the pipeline 2212 may not be present in some embodiments.

In FIGS. 22-24, the first pressurized gas stream 2306 (used to produce LNG 2208) is being cooled down in the heat exchanger 2204 while all other feeds (e.g., chilled vapor feeds, expanded gas stream) through the heat exchanger 2204 are being heated. Heat exchange between the chilled vapors/expanded gas stream and the pressurized gas stream 2306 allow the yield of LNG 2208 to be maximized. For example, the heat exchange may contribute to up to 38% liquefaction of the pressurized gas stream using only energy harnessed from the well. The systems in FIGS. 22-24 provide multiple benefits over existing systems used to produce LNG. LNG is often produced by chilling a gas stream at near-constant pressure, which requires external power to compress one or more circulating refrigerants. The disclosed system, however, enables the generation of LNG 2208 by using only the pressure energy available in the feed. The disclosed system uses a self-refrigeration process to produce LNG 2208 as a byproduct. Additionally, the process does not generate emissions, since the low pressure vapors separated from the feed are not flared. Instead, they are compressed to pipeline pressure, transported to the pipeline, and therefore not wasted.

FIG. 23 illustrates an example system 2300, which is a more detailed version of the system 2200 in FIG. 22. In FIG. 23, the system 2300 operates via a single-stage compression process. As such, the system 2300 has only one separator 2214 and one compressor 2216. The system 2300 may include a cooler 2310 connected between the compressor 2216 and the pipeline 2212. The cooler 2310 may cool the compressed gas output from the compressor 2216 to a pipeline-suitable temperature. The system 2300 may include a pipeline gas mixer 2312 at the intersection of the flow path from the second outlet 2221 of the heat exchanger 2204 and the flow path from the compressor 2216. The pipeline gas mixer 2312 mixes and directs both flows of pipeline-suitable gas to the pipeline 2212. The pipeline gas mixer 2312 may be a simple pipe tee or may include one or more valves.

FIG. 24 illustrates another example system 2400, which is a more detailed version of the system 2200 in FIG. 22. In FIG. 24, the system 2400 operates via a multi-stage compression assembly. The multi-stage compression assembly includes multiple compressors 2216A, 2216B, 2216C, and 2216D connected in series. Similarly, the system 2400 includes a multi-stage separation assembly including multiple separators 2214A, 2214B, and 2214C connected in series. Successive pressure cuts and the multiple separators 2214 on the partially liquified gas stream reduce the amount of power required for operating the VRU.

As illustrated in FIG. 24, the system 2400 may include four stages of compression for recovering vapors into the pipeline 2212. However, any desired number (e.g., 1, 2, 3, 5, 6, 7, 8, or more) stages of compression may be used in other embodiments. The heat exchanger 2204 may include multiple vapor inlets 2215A, 2215B, and 2215C, and each vapor inlet 2215 is connected to one of the multiple separators 2214. The heat exchanger 2204 may similarly include multiple vapor outlets 2217A, 2217B, and 2217C, and each vapor outlet 2217 is connected between a corresponding one of the multiple vapor inlets 2215 and a corresponding one of the multiple compressors 2216. For example, vapors flow from the last separator 2214A in the series of multiple separators 2214, through the vapor inlet 2215A and vapor outlet 2217A to the first compressor 2216A in the series of multiple compressors 2216.

The system 2400 may include at least one interstage vapor mixer 2402 connected between one of the multiple vapor outlets 2217 and the corresponding one of the multiple compressors 2216 for mixing vapors output from the vapor outlet 2217 with compressed vapors output from an adjacent compressor 2216. For example, vapors flow from the separator 2214B through the vapor inlet 2215B and vapor outlet 2217B to the interstage vapor 2402A, which mixes the vapors with the vapors compressed by the first compressor 2216A. The interstage vapor mixer 2402A then directs the combined flow of vapors to the second compressor 2216B providing the second stage of compression. Each interstage vapor mixer 2402 may be a simple pipe tee or may include one or more valves. As illustrated, a cooler (e.g., 2310A, 2310B, 2310C, and 2310D) may be connected downstream of each compressor (e.g., 2216A, 2216B, 2216C, and 2216D) to reduce the temperature for mixing with the next stage of vapors and/or for bringing the output vapors to a pipeline-suitable temperature.

The presence and/or number of compressors 2216, the number of separators 2214, the presence of a pipeline feed/second turbo expander 2210/second pressurized gas stream 2308, and the relative amount of the initial pressurized gas stream 2302 split off for LNG production compared to pipeline production may all be selected to optimize the efficiency of the system. The system disclosed with reference to FIGS. 22-24 may be a closed system that uses power harnessed from a well to both produce LNG 2208 and supply gas to a pipeline 2212 without generating emissions or requiring an outside power source.

While various embodiments of a separator, gas processing facility, method, and system were provided in the foregoing description, those skilled in the art may make modifications and alterations to these aspects without departing from the scope and spirit of the invention. For example, it is to be understood that this disclosure contemplates that, to the extent possible, one or more features of any aspect can be combined with one or more features of any other aspect. As another non-limiting specific example, because natural gas is often odorless, as those of ordinary skill in the art will appreciate it is customary to add an odorant, such as ethyl mercaptan, so that a gas leak can be detected anywhere the gas is being processed or consumed. Therefore, such an odorant can be added to any of the gas products produced in accordance with the present invention. Accordingly, the foregoing description is intended to be illustrative rather than restrictive. The invention described hereinabove is defined by the appended claims, and all changes to the invention that fall within the meaning and the range of equivalency of the claims are to be embraced within their scope.

Claims

1. A system, comprising: a heat exchanger comprising: a first inlet for receiving a first pressurized gas stream; anda first outlet for outputting a chilled gas stream produced by the heat exchanger cooling the first pressurized gas stream;a turbo expander connected to the first outlet of the heat exchanger for receiving the chilled gas stream from the heat exchanger and producing a partially liquified gas stream, the partially liquified gas stream comprising vapors and LNG; andat least one separator connected to the turbo expander, wherein the partially liquified gas stream is fed into the at least one separator, and the at least one separator separates the vapors from the LNG.

2. The system of claim 1, wherein the heat exchanger further comprises: at least one vapor inlet in the heat exchanger connected to the at least one separator for receiving vapors from the at least one separator.

3. The system of claim 2, further comprising: at least one vapor outlet for outputting the vapors from the heat exchanger; andat least one compressor connected between the at least one vapor outlet of the heat exchanger and a pipeline for compressing the vapors output from the heat exchanger to a pressure suitable for the pipeline.

4. The system of claim 3, wherein the turbo expander is coupled to the at least one compressor, wherein the turbo expander supplies power to the at least one compressor.

5. The system of claim 3, further comprising a cooler connected between the at least one compressor and the pipeline.

6. The system of claim 3, wherein: the at least one compressor is a multi-stage compression assembly comprising multiple compressors connected in series; andthe at least one separator is a multi-stage separation assembly comprising multiple separators connected in series.

7. The system of claim 6, wherein: the at least one vapor inlet comprises multiple vapor inlets each connected to one of the multiple separators;the at least one vapor outlet comprises multiple vapor outlets each connected between a corresponding one of the multiple vapor inlets and a corresponding one of the multiple compressors; andat least one interstage vapor mixer is connected between one of the multiple vapor outlets and the corresponding one of the multiple compressors for mixing vapors output from the one of the multiple vapor outlets with compressed vapors output from an adjacent compressor.

8. The system of claim 1, further comprising: a feed splitter upstream of the heat exchanger for splitting an initial gas stream into the first pressurized gas stream and a second pressurized gas stream;a second turbo expander connected between the feed splitter and a second inlet of the heat exchanger, wherein the second turbo expander receives the second pressurized gas stream and outputs an expanded gas stream to the second inlet; anda pipeline connected to a second outlet of the heat exchanger, the second outlet outputting a heated gas stream produced by the heat exchanger heating the expanded gas stream.

9. The system of claim 8, further comprising at least one compressor connected between the heat exchanger and the pipeline for providing compressed gas to the pipeline, wherein the heat exchanger further comprises: at least one vapor inlet for receiving vapors from the at least one separator; andat least one vapor outlet for outputting the vapors from the heat exchanger, wherein the at least one compressor is connected to the at least one vapor outlet.

10. The system of claim 9, wherein the at least one compressor is coupled to one or both of the turbo expander and the second turbo expander, wherein one or both of the turbo expander and the second turbo expander supplies power to the at least one compressor.

11. A method, comprising: receiving a first pressurized gas stream into a heat exchanger;cooling the first pressurized gas stream via the heat exchanger to produce a chilled gas stream output from the heat exchanger;expanding the chilled gas stream via a turbo expander connected to the first outlet to produce a partially liquified gas stream comprising vapors and LNG; andseparating the vapors from the LNG via a separator connected to the turbo expander.

12. The method of claim 11, further comprising: receiving the vapors from the at least one separator into at least one vapor inlet of the heat exchanger; andcooling the first pressurized gas stream via heat transfer between the first pressurized gas stream and the vapors in the heat exchanger.

13. The method of claim 12, further comprising: outputting the vapors from the heat exchanger via at least one vapor outlet of the heat exchanger; andcompressing the vapors output from the heat exchanger via at least one compressor to output a compressed gas toward a pipeline at a pressure suitable for the pipeline.

14. The method of claim 13, further comprising supplying power generated by the turbo expander to the at least one compressor for operating the at least one compressor.

15. The method of claim 13, further comprising cooling the compressed gas output from the at least one compressor via a cooler connected between the at least one compressor and the pipeline.

16. The method of claim 13, wherein: the at least one compressor is a multi-stage compression assembly comprising multiple compressors connected in series; andthe at least one separator is a multi-stage separation assembly comprising multiple separators connected in series.

17. The method of claim 16, wherein: the at least one vapor inlet comprises multiple vapor inlets each connected to one of the multiple separators;the at least one vapor outlet comprises multiple vapor outlets each connected between a corresponding one of the multiple vapor inlets and a corresponding one of the multiple compressors; andthe method further comprises mixing vapors output from the one of the multiple vapor outlets with compressed vapors output from a compressor adjacent the corresponding one of the multiple compressors.

18. The method of claim 11, further comprising: splitting an initial gas stream into the first pressurized gas stream and a second pressurized gas stream;reducing a pressure of the second pressurized gas stream via a second turbo expander to produce an expanded gas stream provided to the heat exchanger;cooling the first pressurized gas stream via heat transfer between the first pressurized gas stream and the expanded gas stream in the heat exchanger; andoutputting a heated gas stream produced by the heat exchanger heating the expanded gas stream toward a pipeline at a pressure suitable for the pipeline.

19. The method of claim 18, further comprising: receiving vapors from the at least one separator into the heat exchanger;outputting the vapors from the heat exchanger after the vapors are heated; andcompressing the vapors output from the heat exchanger via at least one compressor to output a compressed gas toward the pipeline at the pressure suitable for the pipeline.

20. The system of claim 19, further comprising: supplying power generated by one or both of the turbo expander and the second turbo expander to the at least one compressor for operating the at least one compressor.