Apparatus and process for the refrigeration, liquefaction and separation of gases with varying levels of purity

Information

  • Patent Grant
  • 6425263
  • Patent Number
    6,425,263
  • Date Filed
    Thursday, August 23, 2001
    22 years ago
  • Date Issued
    Tuesday, July 30, 2002
    21 years ago
Abstract
A process for the separation and liquefaction of component gasses from a pressurized mix gas stream is disclosed. The process involves cooling the pressurized mixed gas stream in a heat exchanger so as to condensing one or more of the gas components having the highest condensation point; separating the condensed components from the remaining mixed gas stream in a gas-liquid separator; cooling the separated condensed component stream by passing it through an expander; and passing the cooled component stream back through the heat exchanger such that the cooled component stream functions as the refrigerant for the heat exchanger. The cycle is then repeated for the remaining mixed gas stream so as to draw off the next component gas and further cool the remaining mixed gas stream. The process continues until all of the component gases are separated from the desired gas stream. The final gas stream is then passed through a final heat exchanger and expander. The expander decreases the pressure on the gas stream, thereby cooling the stream and causing a portion of the gas stream to liquify within a tank. The portion of the gas which is hot liquefied is passed back through each of the heat exchanges where it functions as a refrigerant.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to methods and apparatus for separating, cooling and liquefying component gases from each other in a pressurized mixed gas stream. More particularly, the invention is directed to separation techniques that utilizes some of the components of the mixed gas stream that have already been separated to cool portions of the mixed gas stream that subsequently pass through the apparatus.




2. Description of the Prior Art




Individual purified gases, such as oxygen, nitrogen, helium, propane, butane, methane, and many other hydrocarbon gases, are used extensively throughout many different industries. Such gases, however, are typically not naturally found in their isolated or purified state. Rather, each individual gas must be separated or removed from mixtures of gages For example, purified oxygen is typically obtained from the surrounding air which also includes nitrogen, carbon dioxide and many other trace elements. Similarly, hydrocarbon gases such as ethane, butane, propane, and methane are separated from natural gas which is produced from gas wells, landfills, city sewage digesters, coal mines, etc.




In addition to separating or purifying the individual gases, it is often necessary to liquify gases. For example, liquefied natural gas (LNG), which is primarily methane, is used extensively as an alternative fuel for operating automobiles and other machinery. The natural gas must be liquified or compressed since storing natural gas in an uncompressed vapor or gas state would require a storage tank of unreasonably immense proportions. Condensing or liquifying other gases is also desirable for more convenient storage and/or transportation.




The liquefaction of gases can be accomplished in a variety of different ways. The fundamental method is to compress the gas and then cool the compressed gas by passing it through a number of consecutively colder heat exchanges. A heat exchanger is simply an apparatus or process wherein the gas or fluid to be cooled is exposed to a colder environment which draws heat or energy from the gas or fluid, thereby cooling the gas. Once a gas reaches a sufficiently low temperature for a set pressure, the gas converts to a liquid.




The cold environment needed for each heat exchanger is generally produced by an independent refrigeration cycle. A refrigeration cycle, such as that used on a conventional refrigerator, utilizes a closed loop circuit having a compressor and an expansion valve. Flowing within the closed loop is a refrigerant such as Freon®. Initially, the refrigerant is compressed by the compressor which increases the temperature of the refrigerant. The compressed gas is then cooled. This is often accomplished by passing the gas through air or water cooled coils. As the compressed gas cools, it changes to a liquid. Next, the liquid passes through an expander valve which reduces the pressure on the liquid. This pressure drop produces an expansion of the liquid which may vaporize at least a portion thereof and which also significantly cools the now combined liquid and gas stream.




This cooled refrigerant stream now flows into the heat exchanger where it is exposed to the main gas stream desired to be cooled. In this environment, the refrigerant stream draws heat from the main stream, thereby simultaneously cooling the main stream and warming the refrigerant stream. As a result of the refrigerant being warmed, the remaining liquid is vaporized to a gas. This gas then returns to the compressor where the process is repeated.




By passing the main gas stream through consecutive heat exchanges having lower and lower temperatures, the main stream can eventually be cooled to a sufficiently low temperature that it converts to a liquid. The liquid is then stored in a pressurized tank.




Although the above process has been useful in obtaining liquefied gasses, it has several shortcomings. For example, as a result of the process using several discrete refrigeration cycles, each with its own compressor, the system is expensive to build, costly to run and maintain, and has an overall high complexity. A significant cost for any closed loop refrigeration system is the purchase and operation of the compressor. Not only does the compressor represent the process' largest capital expenditure, it also represents a major problem in the process system's flexibility. Once a compressor size is chosen, the process can only handle mass flow rates capable of being adequately compressed by the chosen compressor. In order to have wide flexibility in process flows, multiple compressors are then needed. These additional compressors also add to the cost and risk of equipment failure.




To make conventional systems cost effective to operate, such systems are typically built on a large scale. As a result, fewer facilities are built making it harder to get gas to the facility and to distribute liquified gas from the facility. By their vary nature, large facilities are required to store large quantities of liquefied gas prior to transport. Storage of LNG can be problematic in that once the LNG begins to warm from the surrounding environment, the LNG begins to vaporize within the storage tank. To prevent pressure failure of the tank, some of the pressurized gas is permitted to vent. Such venting is not only an environmental concern but is also a waste of gas.




The steps for purification or separation of the different gases from a main mixed gas are often accomplished prior to the liquefaction process and can significantly add to the expense and complexity of the process. As a result, many productive gas wells having high concentrations of undesired gases or elements are often capped rather than processed.




OBJECTS AND BRIEF SUMMARY OF THE INVENTION




Accordingly, it is an object of the present invention to provide gas processing systems which can liquify at least a portion of a mixed gas stream.




Another object of the present invention is to provide gas processing systems which simultaneously purify the liquefied gas by separating off the other mixed gases.




It is also an object of the present invention to provide the above systems that can separate off each component gas of the mixed gas in a substantially pure form for subsequent use of each of the individual gases.




Yet another object of the present invention is to provide the above system which can be operated without the required use of independently operated compressors or refrigeration systems.




Still another object of the present invention is to provide the above systems which can be effectively produced to achieve any desired flow capacity and, furthermore, can be manufactured as small mobile units that can be operated at any desired location.




To achieve the forgoing objectives, and in accordance with the invention as disclosed and broadly claimed herein, a gas processing system and method of operation is provided for separating and cooling components of a pressurized mixed gas stream for subsequent liquefaction of a final or remaining gas stream. This inventive system and process comprises passing a pressurized mixed gas stream through a series of repeated cycles until a final substantially purified gas stream for liquefying is achieved. Each cycle comprises: (1) cooling the pressurized mixed gas stream in a heat exchanger so as to condense one or more of the gas components having the highest condensation point; (2) separating the condensed components from the remaining mixed gas stream in a gas-liquid separator; (3) cooling the separated condensed component stream by passing it through an expander; and then (4) passing the cooled component stream back through the heat exchanger such that the cooled component streams function as the refrigerant for the heat exchanger. The component stream then exits the system for use depending on the type and temperature of gas.




The above cycle is then repeated for the remaining mixed gas stream so as to draw off the next component gas and further cool the remaining mixed gas stream. The process continues until all of the unwanted component gases are removed. The final gas stream, which in the case of natural gas will be substantially methane, is then passed through a final heat exchanger. The final cooled gas stream is then passed through an expander which decreases the pressure on the gas stream. As the pressure decreases, the stream is cooled causing a portion of the gas stream to liquify within a tank. The portion of the gas which is not liquified is passed back through each of the heat exchangers where it functions as a refrigerant.




Where the initial pressure of the mixed gas stream is sufficiently high, the inventive systems can be operated solely from the energy produced by dropping the pressure. As such, there is no need for independently powered compressors or refrigeration cycles. In one embodiment, however, the final expander can comprise a turbo expander which runs a turbine as the gas is expanded therethrough. The electrical or mechanical energy from the turbine can be used to input energy into the system at any desired location. For example, the turbo expander can run a compressor which is used to increase the pressure of the initial gas stream. Where there is insufficient pressure in the initial gas stream, which cannot be sufficiently increased by the turbo expander, the present invention also envisions that an independently operated compressor can be incorporated into the system.




The inventive system has a variety of benefits over conventional systems. For example, by not needing independently operated compressors or refrigeration systems, the inventive system is simpler and less expensive. Furthermore, the inventive system can be effectively constructed to fit any desired flow parameters at virtually any location. For example, one unique embodiment of the present invention is to incorporate the inventive system onto a movable platform such as a trailer. The movable unit can then be positioned at locations such as a well head, factory, refueling station, or distribution facility.




An additional benefit of the present invention is that the system and process can be used to separate off purified component gas streams while simultaneously purifying the final gas stream. For example, during the production of LNG, the system can be designed, depending on the gas composition, to condense off substantially pure propane, butane, ethane, and any other gases present for subsequent independent use in their corresponding markets. By removing all the component gases, the final methane gas is also substantially purified. Accordingly, the inventive system and process can also be used to effectively operate gas wells that have historically been caped for having too high of a concentration of undesired components.











BRIEF DESCRIPTION OF THE DRAWINGS




In order that the manner in which the above-recited and other advantages and objects of the invention are obtained, a more particular description of the invention briefly described above will be rendered by reference to specific embodiments thereof which are illustrated in the appended drawings. Understanding that these drawings depict only typical embodiments of the invention and are not therefore to be considered to be limiting of its scope, the invention will be described and explained with additional specificity and detail through the use of the accompanying drawings in which:





FIG. 1

is a schematic flow diagram which illustrates one possible embodiment of the inventive gas processing system;





FIG. 2

is a schematic flow diagram of the system shown in

FIG. 1

incorporating a turbo expander operating a compressor;





FIGS. 3-6

are schematic flow diagrams of the system shown in

FIG. 2

wherein the compressor is compressing alternative gas streams;





FIG. 7

is a schematic flow diagram of an alternative configuration of the system shown in

FIG. 1

;





FIG. 8

is a schematic flow diagram of one example of one of the cycles shown in

FIG. 1

;





FIG. 9

is a perspective view of a mobile unit incorporating the system shown in

FIG. 1

;





FIG. 10

is a schematic flow diagram of the system shown in

FIG. 1

incorporating vacuum chambers; and





FIG. 11

is a schematic flow diagram of the system shown in

FIG. 1

modified to recondense vapor from a storage tank.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Depicted in

FIG. 1

is one embodiment of a gas processing system


1


incorporating features of the present invention. Although system


1


can be adapted for use with any type of mixed gas stream, the operation of system


1


will be discussed with regard to the use of natural gas. Natural gas includes methane and other higher hydrocarbons such as propane, butane, pentane, and ethane. In one embodiment, system


1


is designed to substantially remove the higher hydrocarbons from the natural gas so as to produce a liquified natural gas (LNG) which is predominately methane.




Depicted in

FIG. 1

, a pressurized initial mixed gas stream


100


is introduced into system


1


. Mixed gas stream


100


comprises a plurality of mixed component gases, such as found in most natural gas coming from a well head. As discussed below in greater detail, exiting from system


1


is a first component stream


102


, a second component stream


104


, a final liquid stream


106


, and a final gas stream


108


.




At any gas pressure, each of the component gases within mixed gas stream


100


have a different condensation point or temperature where the gas condenses to a liquid. As disclosed herein, this principle is used in the separation, cooling, and liquefaction of gas stream


100


. While the present disclosed embodiment describes a process with at least three component gases, no limitation exists as to the number of minimum or maximum components or separation steps. Mixed gas stream


100


simply needs a minimum of two gases, and no maximum limit on the number of possible s gases exists. Likewise, while typically the individual components will be sequentially and individually removed, this invention contains no such limiting requirement. It is well within the scope of this invention to separate groups of gas components together, although the discussion which follows will refer to the separation of single component streams.




Typically, gas stream


100


is delivered to gas processing system


1


at a pressure greater than 250 psia, preferably greater than 500 psia, and more preferably greater than 1000 psia. These pressures can be obtained naturally from a gas well or obtained by adding energy through the use of one or more compressors. Since a high pressure drop is helpful in the liquefaction process, initial higher pressures are typically preferred.




Some of the factors which influence the required initial pressure of gas stream


100


are the required output pressures and temperatures, the gas mixture composition, and the heat capacities of the different components. Since gas stream


100


is pressurized, it inherently contains cooling potential. With a simple expansion, the entire stream can be cooled. Additionally, once the stream's components are condensed to a liquid phase and separated, that liquid phase stream can also be expanded for cooling.




None of the Figures show, nor does this invention affect, the pretreatment steps which often would precede or accompany a process of separation and liquefaction. The pretreatment steps may be separate steps located either upstream of the cooling cycles to be discussed, or may even be found downstream of one or all of the various cooling cycles. Some of the known means taught in the art and readily available in the marketplace include sorption processes using an aqueous phase containing amines for removal of acid gases and at times mercaptan, simple processes of compression and cooling followed by a two-phase gas-liquid separation for removal of unwanted water, and sorbent beds and regenerable molecular sieves for removal of contaminants such as mercury, water, and acid gases.




Returning to

FIG. 1

, the first step of the separation, cooling, and liquefaction process comprises passing mixed gas stream


100


through one or more first heat exchanges


10


. First heat exchanger


10


lowers the temperature of mixed gas stream


100


below the condensation point of what will be called a first component. This first component is defined as the gas, or gases, having the highest condensation point. For example, in one embodiment the first component may be propane. The effective cooling of first heat exchanger


10


is selectively controlled and depends, in part, on the types of gases to be condensed.




As discussed later in greater detail, the refrigerant for first heat exchanger


10


comes from two cooling streams, a first component stream


110


and final gas stream


108


. In alternative embodiments, only one of streams


108


and


110


are necessary for cooling within first heat exchanger


10


. Mixed gas stream


100


leaves first heat exchanger


10


as mixed gas stream


114


containing the condensed first component.




It is noted that each of the different process streams undergo changes in their physical characteristics as the streams are heated, cooled, expanded, evaporated, separated, and/or otherwise manipulated within the inventive system. The fact that the name of a stream does not change, but its reference number does, simply indicates that some characteristic of the stream has changed.




It should also be recognized that the present invention is not limited by a type or sequence of heat exchange. First heat exchanger


10


simply must remove sufficient energy or heat from gas stream


100


to facilitate condensation of the first component. This heat removal can be accomplished with any conventional or newly developed heat exchanger using an individual or any combination of the first component stream


110


and final gas stream


108


. As needed, the cooling potential of the two cooling streams


108


and


110


can be varied in an almost infinite number of ways.




Mixed gas stream


114


next travels to a gas-liquid separator


14


. Such separators come in a variety of different configurations and may or may not be part of heat exchanger


10


. Separator


14


separates the condensed first component from the remaining gases. The gas phase, now at least mostly devoid of the first component, exits separator


14


as a diminished mixed gas stream


116


. The condensed first component exits separator


14


as a liquid first gas stream


118


.




Liquid first component stream


118


is next cooled by passing through an expander


12


. As used in the specification and appended claims, the term “expander” is broadly intended to include all apparatus and method steps which can be used to obtain a pressure reduction in either a liquid or gas. By way of example and not by limitation, an expander can include a plate having a hole in it or conventional valves such as the Joule-Thompson valve. Other types of expanders include vortex tubes and turbo expanders. The present invention also appreciates that there are a variety of expanders that are currently being developed or that will be developed in the future and such devices are also encompassed within the term “expander.”




Expander


12


produces a pressure drop between liquid first component stream


118


entering expander


12


and first component stream


110


exiting expander


12


. As a result of the pressure drop, first component stream


110


expands to produce and adiabatic cooling of stream


110


. Depending on the amount of the pressure drop, some or all of stream


110


can be vaporized. This vaporization is a type of evaporization in that the stream goes through a phase change from a liquid to a vapor. To some extent, the greater the pressure drop, the lower the temperature of stream


110


, and the higher the extent of cooling or vaporization.




As previously discussed, first component stream


110


is next fed into heat exchanger


10


where it functions as a refrigerant to draw heat from initial mixed gas stream


100


, thereby cooling gas stream


100


. Since first component stream


110


is functioning as a refrigerant, the amount of pressure drop at expander


12


is dependent on the amount of required cooling for heat exchanger


10


. In general, it is preferred that at least a portion of first component stream


110


remain in a liquid state as it enters first heat exchanger


10


. The liquid has a greater heat absorption potential since it will absorb energy during evaporization within first heat exchanger


10


.




First component stream


110


exits first heat exchanger


10


as first component stream


102


. Depending on the pressure and cooling potential of stream


102


, stream


102


can be looped back through the system, as discussed later, to produce further cooling. Otherwise, stream


102


can be disposed of, collected, or otherwise transported off site for use consistent with the type of gas.




The disclosed unique removal of first component stream


102


from mixed gas stream


100


produces a variety of benefits. For example, depending on the controlled temperatures of first heat exchanger


10


, stream


102


can be removed as a substantially pure discrete gas. That is, where propane is the highest hydrocarbon gas in gas stream


100


, the propane can be removed as stream


102


in a substantially pure state for subsequent use or sale. Simultaneously, by drawing off first component stream


118


, diminished mixed gas stream


116


has been refined in that it now has a higher concentration of methane.




One of the more significant advantages of the inventive separation process is that it uses a portion of the initial mixed gas stream


100


to continually function as the refrigerant for cooling initial gas stream


100


. As a result, the need for an independent cooling cycle, such as a closed refrigeration cycle found in most conventional liquefaction systems, is eliminated. In addition, where the initial pressure of mixed gas stream


100


is sufficiently high, separation and use of the first component stream as the cooling mechanism is accomplished without the addition of external energy, such as through the use of a compressor.




The above process is next repeated for mixed gas stream


116


so as to remove the next component gas. That is, diminished mixed gas stream


116


passes through one or more second heat exchanges


20


and is cooled to a temperature below the highest condensation point of the remaining gas components. As a result, a second component condenses within mixed gas stream


124


leaving second heat exchanger


20


. The refrigerant for second heat exchanger


20


is also obtained from two cooling streams, a second component stream


120


and final gas stream


108


.




The condensed second component is removed as a liquid from mixed gas stream


124


in a second gas-liquid separator


24


. The gas phase, now at least mostly devoid of the second component, exits second separator


24


as a second diminish mixed gas stream


126


. The condensed second component exists second separator


24


as a liquid second component stream


128


. In turn, second component stream


128


passes through a second expander


22


where it experiences a pressure drop. As a result of the pressure drop, second component stream


120


leaving expander


22


is cooled and, in most embodiments, at least partially vaporized. As discussed above, second component stream


120


passes through second heat exchanger


20


where it functions as a refrigerant for withdrawing heat from mixed gas stream


116


. After passing through second heat exchanger


20


, the second component stream exits as second component stream


104


. As with stream


102


, stream


104


can also be cycled back through the system for further cooling or removed for independent use.




It should now be recognized that the process steps of: (1) cooling the mixed gas stream to condense at least one component; (2) separating the condensed liquid component; (3) cooling the separated liquid component by expansion; and (4) using the cooled component stream independently or in conjunction with a final gas stream to cool the incoming gas stream can be repeated as many times as necessary and desired. That is, the above process can be repeated to independently draw off as many discrete components as desired. In this fashion, discrete components gases can be drawn off independently in a substantially pure form. Alternatively, the component gases can be-drawn off in desired groups of gases.




In this example, where no further components are to be drawn off, the second diminished mixed gas stream


126


is further cooled by passing through a third heat exchanger


30


to create a final mixed gas stream


132


. The refrigerant for third heat exchanger


30


comprises final gas stream


108


. Final mixed gas stream


132


can, depending on the desired final product, be a single purified component which has the lowest condensation point of any of the components in original gas stream


100


, or be a combination of the gas components.




In one embodiment, final mixed gas stream


132


is substantially pure methane in a gas phase. To liquify gas stream


132


, gas stream


132


is passed through an expander


32


to produce a pressure drop. The pressure drop cools gas stream


132


causing at least a portion of gas stream


132


to liquify as it travels into a final gas-liquid separator


34


. The liquified gas exits separator as final liquid stream


106


while the gas or vapor within separator


34


exits as final gas stream


108


. As previously discussed, final gas stream


108


passes back through each of heat exchanges


10


,


20


and


30


where it functions as a refrigerant. Final gas stream


108


can then be recycled into the system, transported off site, or connected with municipal gas line for conventional home or business use. In one embodiment, final gas stream


108


has a pressure less than about 100 psia and more preferably less than about 50 psia.




As set forth above, the operation of liquefaction system


1


to produce a liquid final product stream


106


can be accomplished without the addition energy, such as the use of a compressor. Operation of the system in this manner, however, typically requires that the input pressure of gas stream


100


be greater than about 500 psia and preferably greater than about 1000 psia. In order to obtain a high percentage of liquid methane, it is preferred to have an input pressure of 1500 psia and more preferably greater than about 2000 psia. Where the well head pressures are insufficient, the present invention envisions that a compressor can be used to increase the pressure of initial mixed gas stream


100


.




Depicted in

FIGS. 2-7

are alternative embodiments of system


1


. The different embodiments are not intended to be limiting but rather examples intending to demonstrate the flexibility of the present invention.




Depicted in

FIG. 2

, initial gas stream


100


is initially passed through a compressor


80


to increase the pressure thereat prior to entering the system. To minimize the energy requirement of compressor


80


, expander


32


of

FIG. 1

is comprised of a turbo expander


82


. Turbo expander


82


facilitates expansion of mixed gas stream


132


while simultaneously rotating a turbine. The turbine can be used to generate mechanical or electrical energy which runs compressor


80


. Accordingly, by using compressor


80


which is run by turbo expander


82


, the initial gas pressure can be increased without the required addition of an external energy source. In alternative embodiments, additional energy sources, such as an external motor, can also be used to independently drive or assist in driving compressor


80


.




Although not required, in one embodiment compressed gas stream


100


′ leaving compressor


80


is passed through a preliminary heat exchanger


83


. Heat exchanger


83


can comprise a variety of configurations which depend on the surrounding environment. For example, heat exchanger


83


can be a conventional ambient air cooled heat exchanger or, were available, different water sources such as a river or lake can be used as the cooling element of heat exchanger


83


. The preliminary cooled gas stream


101


travels from heat exchanger


83


to first heat exchanger


10


where the process as discussed with regard to

FIG. 1

is performed.




Of course, compressor


80


can be used for compressing the gas stream at any point along the system. Furthermore, compressor


80


can be replaced with a refrigeration system which is also run by turbo expander


82


. The refrigeration system can be used for further cooling the gas stream at any point along the system.




In the embodiment depicted in

FIG. 3

, first component stream


102


and second component stream


104


are fed into compressor


80


which is again operated by turbo expander


82


. The resulting compressed gas stream


150


is fed back into initial mixed gas stream


100


, thereby recycling the various component streams for use as refrigerants. Furthermore, depending on the temperature of streams


102


and


104


, feeding compressed gas stream


150


into stream


100


can also lower the temperature of stream


100


.




In another embodiment as depicted in

FIG. 4

, compressor


80


is configured to compress final gas stream


108


leaving gas-liquid separator


34


. Compressor


80


is again driven by turbo expander


82


having final mixed gas stream


132


passing therethrough. Final gas stream


108


leaving compressor


80


is cooled by passing through an expander


84


. Cooled gas stream


108


then passes through each of heat exchanges


10


,


20


and


30


in series, as previously discuses with regard to

FIG. 1

, to facilitate the cooling of the mixed gas streams passing therethrough.




In a similar embodiment depicted in

FIG. 5

, final gas stream


108


is again compressed by compressor


80


driven by turbo expander


82


. Rather than using a single expander


84


, however, separate expanders


84




a


,


84




b


and


84




c


are coupled with heat exchanges


10


,


20


, and


30


, respectively. Final gas stream


108


is connected to each of expanders


84




a


,


84




b


and


84




c


in parallel. As a result, the cooling of final gas stream


108


by expanders


84




a


,


84




b


and


84




c


is equally effective for each of heat exchanges


10


,


20


, and


30


.




Final gas stream


108


, as previously discussed with

FIG. 1

, is typically connected to an output line for feeding residential and commercial gas needs. Connecting to such a line, however, requires that the gas have a minimal pressure which is typically greater than about 40 psia. As depicted in

FIG. 6

, where the pressure of final gas stream


108


has drop below the minimal required pressure, final gas stream


108


can be feed through compressor


80


operated by turbo expander


82


. The departing gas stream


152


would then have the required minimal pressure for connection to the output line. Depending on the quality of gas required, first component stream


102


and second component stream


104


can be feed into final gas stream


108


.




In yet another embodiment as depicted in

FIG. 7

, a pressurized mixed gas stream


200


is cooled in a first heat exchange


40


with a final gas stream


202


. Just as in

FIG. 1

, first heat exchanger


40


causes the condensation of a first component in mixed gas stream


200


. The condensed first component is separated from the remaining gases of the resulting mixed gas stream


204


in a liquid-gas separator


42


. The gas phase components exit separator


42


as a diminished mixed gas stream


206


. The condensed first component exits separator


42


as a liquid first component stream


208


. The liquid first component stream


208


is cooled by passing through a first expander


44


to produce a cooled first component stream


210


.




The difference between the present embodiment and the embodiment described in

FIG. 1

, is that instead of using first component stream


210


to cool the pressurized mixed gas stream


200


in first heat exchanger


40


, first component stream


210


is used as a refrigerant in the heat exchanger of the next separation cycle. In this specific embodiment, first component stream


210


cools diminished mixed gas stream


206


as it passes through a second heat exchanger


50


. Additional cooling can also be obtained in second heat exchanger


50


by using final gas stream


202


. First component stream


210


exits second heat exchanges


50


as first component stream


214


. The diminished mixed gas stream


206


is cooled in second heat exchanger


50


, thereby creating a mixed gas stream


216


with a condensed second component.




Next, mixed gas stream


216


follows the same process steps as described above for mixed gas stream


204


. The process continues with the separation of the condensed second component from the remaining gas phase components in a second gas-liquid separator


52


. The remaining gas phase components exit the second separation


52


as a second diminished mixed gas stream


218


. The condensed second component exits the second separator


52


as a liquid second component stream


220


. Liquid second component stream


220


passes through a second expander


54


to create a cooled second component stream


222


.




Second component stream


222


is then used to cool second diminished mixed gas stream


218


in a third heat exchanger


60


. Additional cooling can also be accomplished in third heat exchanger


60


by using final gas stream


202


. Second component stream


222


then exits third heat exchanger


60


as a second component stream


226


. Second diminished mixed gas stream


218


is cooled in third heat exchanger


60


creating a final mixed gas stream


228


. This final mixed gas stream


228


is then expanded through an expander


62


to produce a cooled, low pressure liquid and gas product. The liquid and gas produce is separated in a final gas-liquid separator


64


. The liquid exits the process as a final liquid stream


230


, and the gas phase exiting the final separator


64


as the final gas stream


202


. Final gas stream


202


travels back through heat exchanges


40


,


50


, and


60


as previously discussed.





FIG. 8

shows a more detailed flow diagram for a single process cycle of cooling a mixed gas stream to produce condensed component; separation of the condensed component from the remaining gas; expansion of liquid component, and using the cooled, expanded component for further cooling. It is to be understood that this recital of equipment and methods are not to be considered limiting, but are presented to illustrate and set forth one example.




A diminished mixed gas stream


300


exits a first gas-liquid separator


70


and is cooled by passing through a first heat exchanger


72


. A final gas stream


302


functions as the refrigerant for first heat exchanger


72


. The now cooled diminished mixed gas stream


304


is further cooled in a second heat exchanger


74


. A cooled component stream


306


functions as the refrigerant for second heat exchanger


74


. The first and second heat exchanges


72


and


74


of

FIG. 8

correspond to heat exchanger


10


of FIG.


1


. Second heat exchanger


74


cools diminished mixed gas stream


304


to below the condensation point of the stream's highest component, thereby creating a gas and liquid mixture which is separated in a second gas-liquid separator


76


. The gas phase then exits second separator


76


to enter into the next cycle. The liquid condensed component is expanded through a Joule-Thompson expansion valve


78


which not only evaporates the liquid, but further cools the stream with expansion creating the cooled component stream


306


. After component stream


306


cools the diminished mixed gas stream


304


in second heat exchanger


74


, it exits the process as a component stream


310


.




The above described systems depicted in

FIGS. 1-8

and variations thereon, can be used in a variety of different environments and configurations to perform different functions. For example, as discussed above, one of the basic operations of the inventive system is in the production of liquified natural gas (LNG). LNG is becoming increasing more important as an alternative fuel for running automobiles and other types of motorized equipment or machines. To produce the required need for LNG, the inventive system can be selectively designed and manufactured to accommodate small, medium, and large capacities.




For example, one preferred application for the inventive system is in the liquefaction of natural gas received from conventional transport pipelines. Inlet natural gas streams typically have pipeline pressures from between about 500 psi to about 900 psi and the product liquid natural gas streams may have flow volumes between about 1,000 gallons/day to about 10,000 gallons/day. The inventive system can also be used in peak demand storage. In this embodiment, pipeline gas at between about 500 psi to about 900 psi is liquefied and put in large tanks for use at peak demand times. The product liquid natural gas stream volumes, however, are very large, typically ranging from about 70,000 gallons/day to about 100,000 gallons/day. Similar to peak demand storage is export storage. In export storage, large quantities of LNG are produced and stored prior to over seas shipping. In this embodiment even larger volumes of liquid natural gas is produced, typically between about 1 million gallons/day to about 3 million gallons/day.




Whereas most natural gas processing facilities are only economical, due to their design parameters, for manufacturing on a large scale, the inventive system is easily and effectively manufactured on a small scale. This is because the inventive system is a relatively simple continuous flow process which requires minimal, and often no, external energy sources such as independently operated refrigeration systems or compressors. Rather, the inventive system can often be run solely on the well head or gas line pressure. As a result, the inventive system can be manufactured to produce LNG at small factories, refueling stations, distribution points, and other desired locations. The inventive systems can also be designed to produce on demand so that large storage tanks are not required.




A further benefit of the self powered property of the system is that it is well suited for operation in remote locations. For example, the system can be positioned at individual well heads for processing the gas. This is beneficial in that the system can use the high well head pressure, often above 2,000 psi, to facility operation of the system. Simultaneously, the system can remove undesired impurities from the natural gas as discrete components while dropping the pressure of the resulting purified gas, typically below 1,000 psi, for feeding into a conventional transport pipeline. In one embodiment, rather than having final mixed stream


132


in

FIG. 1

pass through expander


33


for liquefaction, final mixed stream


132


can be fed directly into a transport pipeline. Alternatively, final gas stream


108


can be connected to the transport pipeline.




As depicted in

FIG. 9

, the present invention also envisions a mobile unit


95


which can be easily transported to different locations for use as required. Mobile unit


95


includes system


1


being mounted on a movable trailer


96


having wheels


97


. Alternatively unit


95


may not have wheels, but is just movable or transportable. Mobile unit


95


can be used at virtually any location. For example, mobile unit


95


can be positioned in a gas field for direct coupling with a gas well


98


.




An additional benefit of producing small facilities, such as mobile unit


95


, is the ability to better insulate the system. For example, depicted in

FIG. 10

, each heat exchanger


10


,


20


, and


30


is enclosed in a single vacuum chamber identified by dashed line


322


. Alternatively, a vacuum chamber identified by dashed line


324


can also enclose expanders


12


and


22


along with gas-liquid separators


14


and


24


. In alternative embodiments, vacuum chambers can be designed to enclose any desired elements. The incorporation of such vacuum chambers is practically impossible in large systems but produces substantial savings in the inventive small systems.




An additional use for the inventive system is in gas purification. For example, many productive gas wells are found that have high concentrations of unwanted gases such as nitrogen. Rather than transporting the gas to a large processing plant for cleaning, it is often more economical to simply cap the well. By using the present invention, however, small mobile systems can be positioned directly at the well head. By then adjusting the system to accommodate the specific gas, the various condensation cycles can be used to draw off the unwanted gas or gasses which are then vented or otherwise disposed. The remaining purified gasses can then be transported for use. Of course, in the alternative, the desired gases can be selectively drawn off in various condensations cycles while the final remaining gas is left as the unwanted product. In yet another alternative use, the inventive system can be used in capturing vapor loss in large storage facilities or tanks. That is, LNG is often stored in large tanks for use at peak demand or for overseas shipping on tankers. As the LNG warms within the stored tanks, a portion of the gas vaporizes. To prevent failure of the tank, the gas must slowly be vented so as not to exceed critical pressure limits of the storage tank. Venting the natural gas to the atmosphere, however, raises some safety and environmental concerns. Furthermore, it results in a loss of gas.




Depicted in

FIG. 11

is a large storage tank


312


holding LNG


314


. When pressure within tank


312


exceeds a desired limit, a vaporized gas stream


316


leaves tank


312


and is compressed by compressor


80


. In one embodiment, it is envisioned that the process can be run by the pressure build-up within tank


312


. In this embodiment, it may be possible to use turbo expander


82


with the returning gas to run compressor


80


. In alternative embodiments, an outside generator or other electrical source is used to run compressor


80


. Compressed gas stream


318


exits compressor


80


and returns to heat exchanger


10


where the cooling process begins substantially as described with regard to FIG.


1


. One of the differences, however, is that the component gas streams


102


and


104


are simply returned to tank


312


.



Claims
  • 1. A process for producing a purified methane stream comprising separating and cooling a pressurized feed mixed gas stream containing a methane component and one or more hydrocarbon components heavier that methane, wherein the latent energy of each individual, separated component is captured by the process to further cool the pressurized mixed gas stream, the process comprising the steps of:(a) cooling the mixed gas stream in a feed cooling heat exchange zone; (b) further cooling, condensing, and purifying the cooled mixed gas stream of step (a) to produce a cold methane vapor product and a hydrocarbon liquid enriched in one or more hydrocarbons heavier than methane; (c) separating the cold methane vapor product from the hydrocarbon liquid; and (d) vaporizing at least a portion of the hydrocarbon liquid of step (b) in the feed cooling heat exchange zone to provide by indirect heat exchange at least a portion of the refrigeration required to cool the mixed gas stream in the feed cooling heat exchange zone m step (a), and withdrawing a vaporized hydrocarbon product from the feed cooling heat exchange zone.
  • 2. A process as described in claim 1 which further comprises cooling and condensing the cold methane vapor product of step (c) to yield a high purity liquid methane product.
  • 3. A process as described in claim 1 wherein at least a portion of the refrigeration required to cool the feed gas in the feed cooling heat exchange zone, and to cool, condense, and rectify the cooled feed gas is provided by a closed loop refrigeration system.
  • 4. A process as described in claim 3 wherein the closed loop refrigeration system is operated using a compressor, the compressor, being at least partially energized by a turbo expander.
  • 5. A process as described in claim 1, further comprising the steps of expanding the vaporized hydrocarbon product from step (d) to create a liquid phase and a gas phase; and(a) separating the liquid phase from the gas phase.
  • 6. A process as described in claim 5, wherein the steps of expanding the vaporized hydrocarbon product from the feed cooling heat exchange zone comprises passing the hydrocarbon product, through a turbo expander.
  • 7. A process as described in claim 6, further comprising the steps of passing the feed mixed gas stream containing a methane component and one or more hydrocarbon components heavier than methane through a compressor prior to cooling the feed mixed gas stream in the feed cooling heat exchange zone, the compressor being at least partially energized by the turbo expander.
  • 8. A process as described in claim 7, further comprising the steps of:(a) passing the vaporized hydrocarbon product through a compressor, the compressor being at least partially energized by the turbo expander; and (b) feeding the compressed hydrocarbon product back into the mixed gas stream.
  • 9. A process as described in claim 1, wherein the feed mixed gas stream containing a methane component and one or more hydrocarbon components has been pre-treated to remove impurities from the feed mixed gas stream.
  • 10. A process as described in claim 9, wherein the impurity removed comprises unwanted water.
  • 11. A process for producing a purified liquid methane stream comprising separating one or more components from natural gas, comprising:(a) feeding a pressurized natural gas stream containing a methane and one or more hydrocarbons heavier than methane to heat exchanger, the heat exchanger cooling the natural gas stream so as to condense a heavier first component thereof and leaving a vaporized enriched methane component; (b) separating the condensed first component from the vaporized component rich in methane, thereby creating a first component stream in a liquid state; (c) passing the first component stream through an expander so as to cool the first component stream; (d) using the expanded first component stream to cool the natural gas stream in the heat exchanger or step (a); and (e) cooling and condensing the vaporized component stream enriched in methane to yield a liquid stream enriched in methane.
  • 12. A process as described in claim 1 wherein the condensing of the vaporized stream enriched in methane is carried out by applying closed loop refrigeration at least in part powered by energy created by a turbo expander used in this process.
RELATED APPLICATION

This application is a continuation application of United States application S/N 09/212,490 filed Dec. 16, 1992, and which claims priority to provisional application S/N 60/069,698, filed Dec. 16, 1997, now U.S. Pat. No. 6,105,390.

CONTRACTUAL ORIGIN OF THE INVENTION

This invention was made with United States Government support under Contract No. DE-AC07-94ID13223, now Contract No. DE-AC07-99ID13727 awarded by the United States Department of Energy. The United States Government has certain rights in the invention.

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Number Date Country
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Provisional Applications (1)
Number Date Country
60/069698 Dec 1997 US
Continuations (1)
Number Date Country
Parent 09/212490 Dec 1992 US
Child 09/643420 US