Flexible natural gas storage facility

Information

  • Patent Grant
  • 6813893
  • Patent Number
    6,813,893
  • Date Filed
    Friday, March 7, 2003
    21 years ago
  • Date Issued
    Tuesday, November 9, 2004
    20 years ago
Abstract
The Flexible Natural Gas Storage Facility stores natural gas in one or more man-made salt caverns typically located in a single salt dome or in bedded salt. The Flexible Natural Gas Storage Facility can access different sources of natural gas. A first gas source is from a natural gas pipeline(s) and a second gas source is from LNG. Depending on economic conditions, supply conditions and other factors, the Flexible Natural Gas Storage Facility can receive gas from the natural gas pipeline(s) and/or from LNG to fill the salt caverns. Of course, the LNG must be warmed before being stored in a salt cavern.
Description




BACKGROUND OF THE INVENTION




Much of the natural gas used in the United States is produced along the Gulf Coast. There is an extensive pipeline network both offshore and onshore that transports this natural gas from the wellhead to market. In other parts of the world, there is also natural gas production, but sometimes there is no pipeline network to transport the gas to market. In the industry, this sort of natural gas is often referred to as “stranded” because there is no ready market or pipeline connection. As a result, this stranded gas that is produced concurrently with crude oil is often burned at a flare. This is sometimes referred to as being “flared off.”




Different business concepts have been developed to more effectively utilize stranded gas. One such concept is construction of a petrochemical plant near the source of natural gas to use the gas as a feedstock for the plant. Several ammonia and urea plants have been constructed around the world for this purpose.




Another approach is to liquefy the natural gas at or near the source and to transport the LNG via ship to a receiving terminal. At the LNG receiving facility, the LNG is offloaded from the transport ship and stored in cryogenic tanks located onshore. At some point, the LNG is transferred from the cryogenic storage tanks to a conventional vaporizer system and gasified. The gas is then sent to market via a pipeline. At the start of this process, liquefaction may consume 9-10% of the LNG by volume. At the end of the process, the gasification may consume an additional 2-3% of the LNG by volume. To the best of Applicants knowledge, none of the existing conventional LNG facilities that use vaporizer systems thereafter store the resulting gas in salt caverns. Rather, the conventional LNG facilities with vaporizers transfer all of the resulting gas to a pipeline for transmission to market.




Currently there are more than 100 LNG transport ships in service worldwide and more are on order. LNG transport ships are specifically designed to transport the LNG as a cryogenic liquid at or below −250° F. and near or slightly above atmospheric pressure. Further, the ships run on the LNG and are counter-flooded to maintain a constant draft of about 40 feet. The LNG ships currently in service vary in size and capacity, but some hold about 3 billion cubic feet of gas (Bcf) (approx. 840,000 barrels) or more. Some of the ships of the future may have even greater capacity and as much as 5 Bcf. One of the reasons LNG is transported as a liquid is because it takes less space.




There are a number of LNG facilities around the world. In the U.S., two LNG receiving facilities are currently operational (one located in Everett, Mass. and one located south of Lake Charles, La.) and two are being refurbished (one located in Cove Point, Md. and one located at Elba Island, Ga.). Construction of additional LNG facilities in the U.S. has been announced by several different concerns.




The LNG receiving facilities in the U.S. typically include offloading pumps and equipment, cryogenic storage tanks and a conventional vaporizer system to convert the LNG into a gas. The gas may be odorized using conventional equipment before it is transmitted to market via a pipeline. LNG terminals are typically designed for peak shaving or as a base load facility. Base load LNG vaporization is the term applied to a system that requires almost constant vaporization of LNG for the basic load rather than periodic vaporization for seasonal or peak incremental requirements for a natural gas distribution system. At a typical base load LNG facility, a LNG ship will arrive every 3-5 days to offload the LNG. The LNG is pumped from the ship to the LNG storage tank(s) as a liquid (approx. −250° F.) and stored as a liquid at low-pressure (about one atmosphere). It typically may take 12 hours or more to pump the LNG from the ship to the cryogenic storage tanks onshore.




LNG transport ships may cost more than $100,000,000 to build. It is therefore expedient to offload the LNG as quickly as possible so the ship can return to sea and pick up another load. A typical U.S. LNG base load facility will have three or four cryogenic storage tanks with capacities that vary, but are in the range of 250,000-400,000 barrels each. Many of the current LNG ships have a capacity of approximately 840,000 barrels. It therefore will take several cryogenic tanks to hold the entire cargo from one LNG ship. These tanks are not available to receive LNG from another ship until they are again mostly emptied.




Conventional base load LNG terminals are continuously vaporizing the LNG from the cryogenic tanks and pumping it into a pipeline for transport to market. So, during the interval between ships (3-5 days), the facility converts the LNG to gas (referred to as regasification, gasification or vaporization) which empties the cryogenic tanks to make room for the next shipment. The LNG receiving and gasification terminal may produce in excess of a billion cubic feet of gas per day (BCFD). In summary, transport ships may arrive every few days, but vaporization of the LNG at a base load facility is generally continuous. Conventional vaporizer systems, well known to those skilled in the art, are used to warm and convert the LNG to usable gas. The LNG is warmed from approximately −250° F. in the vaporizer system and converted from liquid phase to usable gas before it can be transferred to a pipeline. Unfortunately, some of the gas is used as a heat source in the vaporization process, or if ambient temperature fluids are used, very large heat exchangers are required. There is a need for a more economical way to convert the LNG from a cold liquid to usable gas.




LNG cryogenic storage tanks are expensive to build and maintain. Further, the cryogenic tanks are on the surface and present a tempting terrorist target. There is therefore a need for a new way to receive and store LNG for both base load and peak shaving facilities. Specifically, there is a need to develop a new methodology that eliminates the need for the expensive cryogenic storage tanks. More importantly, there is a need for a more secure way to store huge amounts of flammable materials.




There are many different types of salt formations around the world. Some, but not all of these salt formations are suitable for cavern storage of hydrocarbons. For example, “domal” type salt is usually suitable for cavern storage. In the U.S., there are more than 300 known salt domes, many of which are located in offshore territorial waters. Salt domes are also known to exist in other areas of the world including Mexico, Northeast Brazil and Europe. Salt domes are solid formations of salt that may have a core temperature of 90° F. or more. A well can be drilled into the salt dome and fresh water can be injected through the well into the salt to create a cavern. Salt cavern storage of hydrocarbons is a proven technique that is well established in the oil and gas industry. Salt caverns are capable of storing large quantities of fluid. Salt caverns have high sendout capacity and most important, they are very, very secure. For example, the U.S. Strategic Petroleum Reserve now stores approximately 600,000,000 barrels of crude oil in salt caverns in Louisiana and Texas, i.e., at Bryan Mound, Tex.




When fresh water is injected into domal salt, it dissolves thus creating brine, which is returned to the surface. The more fresh water that is injected into the salt dome, the larger the cavern becomes. The tops of many salt domes are often found at depths of less than 1500 feet. A salt cavern is an elongate chamber that may be up to 1,500 feet in length and have a capacity that varies between 3-15,000,000 barrels. The largest is about 40 million barrels. Each cavern itself needs to be fully surrounded by the salt formation so nothing escapes to the surrounding strata or another cavern. Multiple caverns will typically be formed in a single salt dome. Presently, there are more than a 1,000 salt caverns being used in the U.S. and Canada to store hydrocarbons including the aforementioned crude oil stored in the Strategic Petroleum Reserve. Sixty or more of these salt caverns are being used to store natural gas.




Two different conventional techniques are used in salt cavern storage-compensated and uncompensated. In a compensated cavern, brine or water is pumped into the bottom of the salt cavern to displace the hydrocarbon or other product out of the cavern. The product floats on top of the brine. When product is injected into the cavern, the brine is forced out. Hydrocarbons do not mix with the brine making it an ideal fluid to use in a compensated salt cavern. In an uncompensated storage cavern, no displacing liquid is used. Uncompensated salt caverns are commonly used to store natural gas that has been produced from wells. High-pressure compressors are used to inject the natural gas in an uncompensated salt cavern. Some natural gas must always be left in the cavern to prevent cavern closure due to salt creep. The volume of gas that must always be left in an uncompensated cavern is sometimes referred to in the industry as a “cushion.” This gas provides a minimum storage pressure that must be maintained in the cavern. Again, to the best of Applicants knowledge, none of the present LNG receiving facilities take the LNG from the tankers, vaporize it and then store the resulting gas in salt caverns.




Uncompensated salt caverns for natural gas storage preferably operate in a temperature range of approximately +40° F. to +140° F. and pressures of 1500 to 4000 psig. If a cryogenic fluid at sub-zero temperature is pumped into a cavern, thermal fracturing of the salt may occur and degrade the integrity of the salt cavern. For this reason, LNG at very low temperatures cannot be stored in conventional salt caverns. If a fluid is pumped into a salt cavern and the fluid is above 140° F. it will encourage creep and decrease the volume of the salt cavern.




U.S. Pat. No. 5,511,905 is owned by the assignee of the present application. William M. Bishop is listed as a joint inventor on the present application and the '905 patent. This prior art patent discloses warming of LNG with brine (at approximately 90° F.) using a heat exchanger in a compensated salt cavern. This prior patent teaches storage in the dense phase in the compensated salt cavern. The '905 patent does not disclose use of an uncompensated salt cavern. The '905 patent also discloses that cold fluids may be warmed using a heat exchanger at the surface. The surface heat exchanger might be used where the cold fluids being offloaded from a tanker are to be heated for transportation through a pipeline. The brine passing through the surface heat exchanger could be pumped from a brine pond rather than the subterranean cavern.




U.S. Pat. No. 6,298,671 is owned by BP Amoco Corporation and is for a Method for Producing, Transporting, Offloading, Storing and Distributing Natural Gas to a Marketplace. The patent teaches production of natural gas from a first remotely located subterranean formation, which is a natural gas producing field. The natural gas is liquefied and shipped to another location. The LNG is re-gasified and injected into a second subterranean formation capable of storing natural gas which is a depleted or at least a partially depleted subterranean formation which has previously produced gas in sufficient quantities to justify the construction of a system of producing wells, gathering facilities and distribution pipelines for the distribution to a market of natural gas from the subterranean formation. The patent teaches injection of the re-gasified natural gas into the depleted or partially depleted natural gas field at temperatures above the hydrate formation level from 32° F. to about 80° F. and at pressures of from about 200 to about 2500 psig. This patent makes no mention of a salt cavern. This patent makes no mention of dense phase or the importance thereof. Furthermore, there are limitations on the injection and send out capacity of depleted and partially depleted gas reservoirs that are not present in salt cavern storage. In addition, temperature variances between the depleted reservoir and the injected gas create problems in the depleted reservoir itself that are not present in salt cavern storage. For all of these many reasons, salt caverns are preferred over cryogenic storage tanks or depleted gas reservoirs for use in a modern LNG facility.




Salt cavern natural gas storage is known and utilized between natural gas production facilities and natural gas markets to provide a buffer to swings in supply of natural gas and to swings in demand for natural gas. Swings in supply from gas production wells can be caused by weather phenomenon such as freezes or hurricanes or in the normal maintenance associated with natural gas production facilities. Swings in natural gas demand can be weather related such as demand for heating in cold weather or in demand for electricity generated from natural gas fueled generators. Salt cavern storage of natural gas is widely known as an excellent technology to accommodate very large demand increases in natural gas because of the ability of caverns to deliver large amounts of natural gas to pipelines on very short notice. The U.S. on average consumes about 60 billion cubic feet per day (Bcf/D) of natural gas but in peak demand periods can consume in excess of 115 Bcf/D. Natural gas storage is used to accommodate that wide variation in demand. There is over 3 trillion cubic feet (TCF) of natural gas storage capacity in the US of which about 95% is storage of natural gas in depleted reservoirs and aquifers and the remaining 5% in salt caverns. While salt caverns make up only about 5% of the storage capacity they provide more than 14% of the delivery capacity illustrating that salt caverns have much higher deliverability than other forms of storage. Salt caverns are characterized as having very high deliverability instantaneously available to be delivered to the pipeline grid.




The U.S. has the most comprehensive energy infrastructure in the world. The U.S. is the largest energy consuming nation in the world and there are projections that the demand for natural gas and the swings in that demand will increase in the future. There is an extensive pipeline network both offshore and onshore that transports this natural gas from the wellhead to market. Much of the natural gas used in the United States is produced along the Gulf Coast, where there is an abundance of natural gas pipeline distribution networks in proximity to navigable waters. An abundance of natural gas pipeline networks is sometimes referred to as the natural gas infrastructure.




Currently the U.S. consumes more natural gas than it produces. The shortfall in supply is largely made up by pipeline imports from Canada. Only about 1% of the current U.S. natural gas demand is supplied by imported LNG. However there are projections by the Energy Information Agency of the U.S. Department of Energy that in the future imported LNG could supply as much as 6% of demand. Some gas industry projections are that imported LNG could grow to supply more than 10% of demand.




Salt caverns are used to store natural gas that has been produced from wells and transported to the salt caverns via pipelines. Salt cavern storage of natural gas sourced from pipelines is well known to those skilled in the art. Generally pipelines operate at pressures lower than the maximum operating pressures of salt caverns therefore high-pressure compressors are used to boost the pressure from the pipelines and inject the natural gas in to salt caverns. Salt caverns for natural gas storage are preferably operated in a temperature range of approximately +40° F. to +140° F. and pressures from about 1500 to about 4000 psig. Salt has varying degrees of plasticity depending primarily upon temperature and pressure. The hot discharge from natural gas compressors is commonly cooled prior to injection into salt caverns to temperatures below +140° F. to reduce salt movement or “creep.” Salt caverns store natural gas at pressures exceeding the operating pressures of the pipelines to which they are connected so the general method of delivery from the caverns to the pipelines is by the positive pressure differential from the cavern to the pipelines. In periods of high natural gas demand salt cavern storage facilities are depleted rapidly and generally the storage inventories are not replenished until periods of low natural gas demand. The practice in the industry of filling a salt cavern storage facility and then redelivering the inventory to a natural gas pipeline network is called a turnaround or turn. The number of turns a facility can perform during a period of time is a measure of its utilization. In periods of continued high demand for natural gas such as in a prolonged cold wave there may be an inability to refill the salt cavern storage facility because of the general inability of the U.S. domestic production of natural gas to match the high rates of natural gas consumption. In general natural gas production from production wells is at a relatively steady rate while consumption of natural gas in the U.S. is highly variable and subject to significant peaks and valleys. Salt cavern storage facilities are recognized as an excellent way to fill the gaps in supply and demand on a quick response basis. The trend in the U.S. to build more gas fueled electrical generating facilities will exacerbate the swings in demand since a gas fueled generation plant is characterized by the ability to rapidly shift its output which could increase its fuel requirement as much as 50% in a short time period.




In the U.S. there are more than 60 salt caverns utilized for storing natural gas sourced from pipelines. To the best of the Applicant's knowledge, none of the existing salt caverns used for natural gas storage are also used for the receipt and storage of natural gas sourced from LNG.




SUMMARY OF THE INVENTION




The Bishop One-Step Process warms a cold fluid using a heat exchanger mounted onshore or a heat exchanger mounted offshore on a platform or subsea and stores the resulting DPNG in an uncompensated salt cavern. In an alternative embodiment, a conventional LNG vaporizer system can also be used to gasify a cold fluid prior to storage in an uncompensated salt cavern or transmission through a pipeline.




The term “cold fluid” as used herein means liquid natural gas (LNG), liquid petroleum gas (LPG), liquid hydrogen, liquid helium, liquid olefins, liquid propane, liquid butane, chilled compressed natural gas and other fluids that are maintained at sub-zero temperatures so they can be transported as a liquid rather than as gases. The heat exchangers of the present invention use a warm fluid to raise the temperature of the cold fluid. This warm fluid used in the heat exchangers will hereinafter be referred to as warmant. Warmant can be fresh water or seawater. Other warmants from industrial processes may be used where it is desired to cool a liquid used in such a process.




To accomplish heat exchange in a horizontal flow configuration, such as the Bishop One-Step Process, it is important that the cold fluid be at a temperature and pressure such that it is maintained in the dense or critical phase so that no phase change takes place in the cold fluid during its warming to the desired temperature. This eliminates problems associated with two-phase flow such as stratification, cavitation and vapor lock.




The dense or critical phase is defined as the state of a fluid when it is outside the two-phase envelope of the pressure-temperature phase diagram for the fluid (see FIG.


9


). In this condition, there is no distinction between liquid and gas, and density changes on warming are gradual with no change in phase. This allows the heat exchanger of the Bishop One-Step Process to reduce or avoid stratification, cavitation and vapor lock, which are problems with two-phase gas-liquid flows.




The present invention is a Flexible Natural Gas Storage Facility. The Flexible Natural Gas Storage Facility stores natural gas in one or more man-made salt caverns typically located in a single salt dome. The Flexible Natural Gas Storage Facility can access different sources of natural gas. A first gas source is from a natural gas pipeline(s) and a second gas source is from LNG. Depending on economic conditions, supply conditions and other factors, the Flexible Natural Gas Storage Facility can receive gas from the natural gas pipeline(s) and/or from LNG to fill the salt caverns. Of course, the LNG must be warmed before being stored in a salt cavern. The preferred LNG source is from a transport ship. Pipeline gas is the only source of gas for conventional natural gas storage in a salt cavern. Conventional natural gas salt cavern storage facilities therefore lack the flexibility and economic advantages of the present invention which is capable of receiving fluids from at least two different sources.











BRIEF DESCRIPTION OF DRAWINGS





FIG. 1

is a schematic view of the apparatus used in the Bishop One-Step Process including a dockside heat exchanger, salt caverns and a pipeline.





FIG. 2

is an enlarged section view of the heat exchanger of FIG.


1


. The flow arrows indicate a parallel flow path. Surface reservoirs or ponds are used to store the warmant.





FIG. 3

is a section view of the heat exchanger of

FIG. 2

except the flow arrows now indicate a counter-flow path. Surface reservoirs or ponds are used to store the warmant.





FIG. 4

is a schematic view of the apparatus used in the offshore Bishop One-Step Process including a heat exchanger mounted on the sea floor, salt caverns and a pipeline.





FIG. 5

is an enlarged section view of a portion of the equipment in

FIG. 4

showing a parallel flow heat exchanger mounted on the sea floor.





FIG. 6

is a section view of a portion of the heat exchanger along the lines


6





6


of FIG.


2


.





FIG. 7

is a section view of an alternative embodiment of the heat exchanger.





FIG. 8

is a section view of a second alternative embodiment of the heat exchanger.





FIG. 9

is a temperature-pressure phase diagram for natural gas.





FIG. 10

is a schematic view of an alternative embodiment including a vaporizer system for gasification of cold fluids with subsequent storage in salt caverns without first going to a cryogenic storage tank.





FIG. 11

is a block diagram of the Flexible Natural Gas Storage Facility including four salt caverns.











DETAILED DESCRIPTION





FIG. 1

is the schematic view of the apparatus used in the Bishop One-Step Process including a dockside heat exchanger for converting a cold fluid to a dense phase fluid for delivery to various subsurface storage facilities and/or a pipeline (

FIG. 1

is not drawn to scale.). The entire onshore facility is generally identified by the numeral


19


. Seawater


20


covers much, but not all, of the surface


22


of the earth


24


. Various types of strata and formations are formed below the surface


22


of the earth


24


. For example, a salt dome


26


is a common formation along the Gulf Coast both onshore


27


and offshore.




A well


32


extends from the surface


22


through the earth


24


and into the salt dome


26


. An uncompensated salt cavern


34


has been washed in the salt dome


26


using techniques that are well known to those skilled in the art. Another well


36


extends from the surface


22


, through the earth


24


, the salt dome


26


and into a second uncompensated salt cavern


38


. The upper surface


40


of the salt dome


26


is preferably located about 1500 feet below the surface


22


of the earth, although salt domes occurring at other depths both onshore


27


or offshore


28


may also be suitable. A typical cavern


34


may be disposed 2,500 feet below the surface


22


of the earth


24


, have an approximate height of 2,000 feet and a diameter of approximately 200 feet. The size and capacity of the cavern


34


will vary. Salt domes and salt caverns can occur completely onshore


27


, completely offshore


28


or somewhere in between. A pipeline


42


has been laid under the surface


22


of the earth


24


.




A dock


44


has been constructed on the bottom


46


of a harbor, not shown. A cold fluid transport ship


48


is tied up at the dock


44


. The cold fluid transport ship


48


typically has a plurality of cryogenic tanks


50


that are used to store cold fluid


51


. The cold fluid is transported in the cryogenic tanks


50


as a liquid having a sub-zero temperature. Low-pressure pump systems


52


are positioned in the cryogenic tanks


50


or on the transport ship


48


to facilitate off loading of the cold fluid


51


.




After the cold fluid transport ship


48


has tied up to the dock


44


, an articulated piping system


54


on the dock


44


, which may include hoses and flexible loading arms, is connected to the low-pressure pump system


52


on the transport ship


48


. The other end of the articulated piping system


54


is connected to high-pressure pump system


56


mounted on or near the dock


44


. Various types of pumps are used in the LNG industry including vertical, multistaged deepwell turbines, multistage submersibles and multistaged horizontal.




When it is time to begin the off loading process, the low-pressure pump system


52


and the high-pressure pump system


56


transfer the cold fluid


51


from the cryogenic tanks


50


on the transport ship


48


through hoses, flexible loading arms and articulated piping


54


and additional piping


58


to the inlet


60


of a heat exchanger


62


used in the present invention. When the cold fluid


51


leaves the high-pressure pump system


56


it has been converted to a dense phase fluid


64


because of the pressure imparted by the pump. The term dense phase is discussed in greater detail below concerning FIG.


9


. The Bishop Process™ heat exchanger


62


will warm the cold fluid to approximately +40° F. or higher, depending on downstream requirements. Bishop Process is a trademark owned by Conversion Gas Imports, L.P. of Houston. Tex. This heat exchanger makes use of the dense phase state of the fluid and a high Froude number for the flow to ensure that stratification, phase change, cavitation and vapor lock do not occur in the heat exchange process, regardless of the orientation of the flow with respect to gravity. These conditions are essential to the warming operation and are discussed in detail below in connection with FIG.


9


. When the cold fluid


51


leaves the outlet


63


of the heat exchanger


62


, it is a dense phase fluid


64


. A flexible joint


65


or an expansion joint is connected to the outlet


63


of the heat exchanger


62


to accommodate expansion and contraction of the cryogenically compatible piping


61


, better seen in

FIG. 2

, inside the heat exchanger


62


(high nickel steel may be suitable for the piping


61


).




Piping


70


connects the heat exchanger


62


with a wellhead


72


, mounted on a well


36


. Additional piping


74


connects the heat exchanger


62


with another wellhead


76


, mounted on the well


32


. The high-pressure pump system


56


generates sufficient pressure to transport the dense phase fluid


64


through the flexible joint


65


, the piping


70


, through the wellhead


72


, the well


36


into the uncompensated salt cavern


38


. Likewise the pressure from the high-pressure pump system


56


will be sufficient to transport the dense phase fluid


64


through the flexible joint


65


, the piping


70


and


74


, through the wellhead


76


and the well


32


into the uncompensated salt cavern


34


. Dense phase fluid


64


therefore can be injected via the wells


32


and


36


for storage into uncompensated salt caverns


34


and


38


.




In addition, dense phase fluid


64


can be transferred from the heat exchanger


62


through piping


78


to a throttling valve


80


or regulator which connects via additional subsurface or surface piping


84


to the inlet


86


of the pipeline


42


. The dense phase fluid


64


is then transported via the pipeline


42


to market. (The pipeline


42


may also be on the surface.)




If additional pumps are needed, they may be added to the piping system at appropriate points, not shown in this schematic. The cold fluid


51


may also be delivered to the facility


19


via inland waterway, rail or truck, not shown.





FIG. 2

is enlarged section view of the Bishop Process heat exchanger


62


. (

FIG. 2

is not drawn to scale.) The heat exchanger


62


can be formed from one section or multiple sections as shown in FIG.


2


. The number of sections used in the heat exchanger


62


depends on the spatial configuration and the overall footprint of the facility


19


, the temperature of the cold fluid


51


, the temperature of the warrant


99


and other factors. The heat exchanger


62


includes a first section


100


and a second section


102


. The term “warmant” as used herein means fresh water


19


(including river water) or seawater


20


, or any other suitable fluid including that participating in a process that requires it to be cooled, i.e. a condensing process.




The first section


100


of the heat exchanger


62


includes a central cryogenically compatible pipe


61


and an outer conduit


104


. (High nickel steel pipe may be suitable in this low temperature application). The interior cryogenically compatible conduit


61


is positioned at or near the center of the outer conduit


104


by a plurality of centralizers


106


,


108


and


110


.




A warmant


99


flows through the annular area


101


of the first section


100


of heat exchanger


62


. The annular area


101


is defined by the outside diameter of the cryogenically compatible pipe


61


and the inside diameter of the outer conduit


104


.




The second section


102


of the heat exchanger


62


is likewise formed by the cryogenically compatible pipe


61


and the outer conduit


112


. The cryogenically compatible pipe


61


is positioned, more or less, in the center of the outer conduit


112


by a plurality of centralizers


114


,


116


and


118


. All of the centralizers,


106


,


108


,


110


,


114


,


116


and


118


, are formed generally the same as shown in FIG.


6


.




A first surface reservoir


120


, sometimes referred to as a pond, and a second surface reservoir


122


are formed onshore


27


near the heat exchanger


62


and are used to store warmant


99


. Piping


124


connects the first reservoir


120


with a low-pressure pump


126


. Piping


128


connects the low-pressure pump


126


with ports


130


to allow fluid communication between the reservoir


122


and the first section


100


of heat exchanger


62


. The warmant flows through the annular area


101


as indicated by the flow arrows and exits the first section


100


of the heat exchanger


62


at ports


132


as indicated by the flow arrows. Additional piping


134


connects the ports


132


with the second reservoir


122


.




Piping


136


connects the first reservoir


120


with low-pressure pump


138


. Piping


140


connects low-pressure


138


with ports


142


formed in the second section


102


of the heat exchanger


62


. The warmant is pumped from the first reservoir


120


through the pump


138


into the annular area


103


between the outside diameter of the cryogenically compatible pipe


61


and the inside diameter of the outer conduit pipe


112


. The warm ant


99


flows through the annular area


103


of the second section


102


of the heat exchanger


62


as indicated by the flow arrows and exits at the ports


144


which are connected by pipe


146


to the second reservoir


122


. The cold fluid


51


enters the inlet


60


of the heat exchanger


62


as a cold liquid and leaves the outlet


63


as a warm dense phase fluid


64


. The cryogenically compatible pipe


61


is connected to a flexible joint


65


to account for expansion and contraction of the cryogenically compatible pipe


61


. All piping downstream of flexible joint


65


is not cryogenically compatible.




In the parallel flow configuration of

FIG. 2

, the heat exchanger


62


transfers warmant


99


from the first surface reservoir


120


through the first section


100


to the second reservoir


122


. Likewise, additional warmant is transferred from the first reservoir


120


through the second section


102


of the heat exchanger


62


to the second reservoir


122


. Over time, the volume of warmant


99


and the first reservoir


120


will be diminished and the volume of warmant


99


in the second reservoir


122


will be increased. It will therefore be necessary to move to a counter-flow arrangement better seen in

FIG. 3

so that the warmant


99


can be transferred from the second reservoir


122


back to the first reservoir


120


. In an alternative arrangement, that avoids the necessity for counter-flow, the warmant


99


can be returned from the first section


100


through piping


148


, shown in phantom, to the first reservoir


120


allowing for continuous parallel flow through the first section


100


of the heat exchanger


62


. In a similar arrangement, the warmant from the second section


102


is transferred from a second reservoir


122


through piping


150


, shown in phantom, to the pump


138


. In this fashion, the warmant


99


is continually cycled in a parallel flow through the second section


102


of the heat exchanger


62


. If river water is used as the warmant


99


, the surface ponds


120


and


122


are not needed. Instead, the piping


124


connects to a river, as does the piping


136


,


134


and


146


. When river water is used as a warmant


99


it is always returned to its source and the piping is modified accordingly.




It is important to avoid freez-up of the heat exchanger


62


. Freez-up blocks the flow of warmant


94


and renders the heat exchanger


62


inoperable. It is also important to reduce or eliminate icing. Icing renders the heat exchanger


62


less efficient. It is therefore necessary to carefully design the area, generally identified by the numeral


63


where the cold fluid


51


in the pipe


61


first encounters the warmant


99


in the annular area


101


of the first section


100


of the heat exchanger


62


. Here it is necessary to prevent or reduce freezing of the warmant


99


on the pipe


61


, which could block the ports,


130


and the annular area


101


. In most cases, it is possible to choose flow rates and pipe diameter ratio such that freezing is not a problem. For example, if a dense phase natural gas expands by a factor of four in the warming process, the heat balance then indicates that the warm ant flow rate is required to be four times that of the inlet dense phase. This results in a diameter ratio of two (outer pipe/inner pipe) in order to balance friction losses in the two paths. However, the heat transfer rate is improved if the diameters are closer together. An optimum ratio is approximately 1.5. Where conditions are extreme, it is possible to prevent local freezing by increasing the thermal insulation at the wall of the cryogenically compatible pipe


61


in this region


63


. One method for doing this is to simply increase the wall thickness of the pipe


61


. This has the effect of pushing some of the warming function downstream to where the cold fluid


51


has already been warmed to some extent, and the possibility of freezing has been reduced. This may also increase the length of the heat exchanger.





FIG. 3

is an enlarged section view of the Bishop Process heat exchanger


62


in a counter-flow mode. (

FIG. 3

is not drawn to scale.) Warmant


99


is transferred from the second reservoir


122


through piping


200


, the pump


202


, piping


204


, the ports


144


into the annular area


103


of the second section


102


of the heat exchanger


62


as indicated by the flow arrows. The warmant


99


exits the annular area


103


through the ports


142


and travels through the piping


206


to the first reservoir


120


. Low-pressure pump


138


transfers warmant


99


from the second reservoir


122


through piping


150


,


206


and the ports


132


into the annular area


101


of the first section


100


of the heat exchanger


62


as indicated by the flow arrows. The warmant


99


leaves the annular area


102


of the first section


100


through the ports


130


and piping


210


to return to the first reservoir


120


. This counter-flow circuit continues until most of the warmant


99


has been transferred from the second reservoir


122


back to the first reservoir


120


.




In an alternative flow arrangement, the warmant


99


leaves the annular area


103


through the ports


142


and is transferred through the piping


212


, shown in phantom, back to the second reservoir


122


making a continuous loop from and to the second reservoir


122


. Likewise warmant


99


can be transferred from the first reservoir


120


through piping


214


, as shown in phantom, to the pump


138


, piping


206


through the ports


132


into the annular area


101


of the first section


100


of the heat exchanger


62


. The warmant is then returned through the ports


130


and the piping


210


to the first reservoir


120


.




The design of the heat exchanger


62


and the number of surface reservoirs is determined by a number of factors including the amount of space that is available and ambient temperatures of warmant


99


. For example, if the warmant


99


has an average temperature of more than 80° F., the heat exchanger


62


may only need one section. However, if the warmant


99


is on average less than 80° F., two or more segments may be necessary, such as the two-segment design shown in

FIGS. 2 and 3

. Surface reservoirs that are relatively shallow and have a large surface area are desirable for this purpose because they act as a solar collector raising the temperature of the warmant


99


during sunny days. This alternative arrangement constitutes a continuous counter-flow loop from and to the first reservoir


120


. In the alternative, if the river water is being used as the warmant, no reservoirs may be required. In the case of river water, it may simply be returned to the river.




EXAMPLE #1




This hypothetical example is-designed to give broad operational parameters for the Bishop One-Step Process conducted at or near dockside as shown in

FIG. 1. A

number of factors must be considered when designing the facility


19


including the type of cold fluid and warmant that will be used. Conventional instrumentation for process measurement, control and safety are included in the facility as needed including but not limited to: temperature and pressure sensors, flow measurement sensors, overpressure reliefs, regulators and valves. Various input parameters must also be considered including, pipe geometry and length, flow rates, temperatures and specific heat for both the cold fluid and the warmant. Various output parameters must also be considered including the type, size, temperature and pressure of the uncompensated salt cavern. For delivery directly to a pipeline, other output parameters must also be considered such as pipe geometry, pressure, length, flow rate and temperature. Other design parameters to prevent freez-up include temperature of the warmant at the inlet and the outlet of each section of the heat exchanger, temperature in the reservoirs, and the temperature at the initial contact area


63


. Other important design considerations include the size of the cold fluid transport ship and the time interval during which the ship must be fully offloaded and sent back to sea.




Assume that 800,000 barrels of LNG (125,000 cubic meters) are stored in the cryogenic tanks


50


on the transport ship


48


at approximately one atmosphere and a temperature of −250° F. or colder. The low-pressure pump system


52


has the following general operational parameters: approx. 22,000 gpm (5000 m3/hr) with approx. 600 horsepower to produce a pressure of approximately 60 psig (4 bars). Due to frictional losses approximately 40 psig is delivered to the intake of the high-pressure pump system


56


. The high-pressure pump system


56


will raise the pressure of the LNG typically to 1860 psig (120 bars) or more so that the cold fluid


51


will be in the dense phase after it leaves the high-pressure pump system


56


. There are approximately ten pumps in the high-pressure pump system


56


, each with a nominal pumping rate of 2,200 gpm (500 m3/hr) at a pressure increase of 1860 psig (120 bars), resulting in approximately 1900 psig (123 bars) available for injection into the uncompensated salt caverns


34


and


38


. The total required horsepower for the ten high-pressure pump system is approximately 24,000 hp. This represents the maximum power required when the uncompensated salt caverns are fully pressured, i.e. when they are full. The average fill rate may be higher than 22,000 gpm (5000 m3/hr). Assuming 13⅜″ nominal diameter pipe in the injection wells


32


and


36


, approximately four uncompensated salt caverns having a minimum total capacity of approximately 3 billion cubic feet. The volume of the LNG will generally expand by a factor 2-4 during the heat exchange process, depending on the final pressure in the uncompensated salt cavern. Larger injection wells are feasible, along with more caverns if higher flows are needed.




Pumps


124


and


138


for the warmant


99


will be high-volume, low-pressure pump system with a combined flow rate of about 44,000 gpm (10,000 m3/hr) at about 60 psig (4 bars). The flow rate of the warmant through the heat exchanger


62


will be approximately two to four times the flow rate of the LNG through the cryogenically compatible tubing


61


. The flow rate of the warmant will depend on the temperature of the warmant and the number of sections in the heat exchanger. (Each section has a separate warmant injection point.) The warmant could be treated for corrosion and fouling prevention to improve the efficiency of the heat exchanger


62


. As the dense phase fluid


64


passes through the heat exchanger


62


it warms and expands. As it expands, the velocity increases through the heat exchanger.




Assuming an LNG flow rate of 22,000 gpm the heat exchanger


62


could have a cryogenically compatible center pipe


61


with a nominal outside diameter of approximately 13 ⅜ inches and the outer conduits


104


and


112


could have a nominal outside diameter of approximately 20 inches. The overall length of the heat exchanger


62


would be long enough, given the temperature of the warmant and other factors to allow the dense phase fluid


64


to reach a temperature of about 40° F. This could result in an overall length of several thousand feet and perhaps in the neighborhood of 5,000 feet. Multiple warmant injection points and parallel flow lines can greatly reduce this length. Depending on the distance from the receiving point to the storage space, the length may not be a problem. Parallel systems may also be used depending on the size of the facility and the need for redundancy. Pipe size and length can be greatly reduced by dividing the LNG flow into separate parallel paths. Two parallel heat exchangers


62


could have a cryogenically compatible center pipe


61


with a nominal outside diameter of approximately 8 inches and the outer conduits


104


and


112


could have a nominal outside diameter of approximately 12 inches. Use of parallel heat exchangers


62


is a design choice dependent upon material availability, ease of construction, and distance to storage.




In addition, the heat exchanger


62


need not be straight. To conserve space, or for other reasons the heat exchanger


62


may adopt any path such as an S-shaped design or a corkscrew-shaped design. The heat exchanger


62


can have 90° elbows and 180° turns to accommodate various design requirements.




If the dense phase fluid


64


is to be stored in an uncompensated salt cavern


34


, one first needs to determine the minimum operational pressure of the salt cavern


34


. For example, hypothetically, if the uncompensated cavern


34


had a maximum operating pressure of about 2,500 psig, the high-pressure pump system


56


would have the ability to pump at 2,800 psig or more. Of course operating at less than maximum is also possible, provided that pressure exceeds about 1,200 psig to maintain dense phase.




If the cold fluid


51


is to be heated and transferred directly into the pipeline


42


, one first needs to determine the operational pressure of the pipeline. For example, hypothetically, if the pipeline operates at 1,000 psig, the high-pressure pump system


56


might still need to operate at pressures above 1,200 psig to maintain the dense phase of the fluid


64


depending on the temperature-pressure phase diagram. In order to reduce the pressure of the dense phase fluid


64


to pipeline operating pressures, it passes through the throttling valve


80


or regulator prior to entering the pipeline


42


. Heating might also be necessary at this point to prevent the formation of two-phase flow, i.e. to keep liquids from forming. Conversely, the heat exchanger could be lengthened to increase the temperature such that subsequent expansion and cooling does not take the fluid out of the dense phase.




After dense phase fluid


64


has been injected into the uncompensated caverns


34


and


38


, it can be stored until needed. The dense phase fluid


64


may be stored in the uncompensated salt cavern at pressures well exceeding the operational pressures of the pipeline. Therefore, all that is needed to transfer the dense phase fluid from the salt cavern


34


and


38


is to open valves, not shown, on the wellheads


72


and


76


and allow the dense phase fluid to pass through the throttling valve


80


or regulator which reduces its operational pressure to pressures compatible with the pipeline. In conclusion, the well


32


acts both to fill and empty the uncompensated salt cavern


34


as indicated by the flow arrows. Likewise, well


36


acts to both fill and empty the salt cavern


38


as indicated by the flow arrows.





FIG. 4

is a schematic view of the apparatus used in the Bishop One-Step Process when a ship is moored offshore


28


. (

FIG. 4

is not drawn to scale.) The facility


298


is located offshore


28


and the facility


299


is located onshore


27


. The offshore facility


298


may be several miles from land and is connected to the onshore facility


299


by a subsea pipeline


242


.




A subsea Bishop Process heat exchanger


220


may be located on the sea floor


222


in proximity to the platform


226


. In an alternative embodiment, not shown, the heat exchanger


220


could be mounted on the platform


226


above the surface


21


of the water


20


. In a second alternative embodiment, not shown, the heat exchanger


220


could be mounted on and between the legs


227


(Best seen in

FIG. 5

) of the platform


226


. When mounted on or between the legs


227


, all or part of the heat exchanger


220


could be below the surface


21


of the water


20


. The mooring/docking device


224


is secured to the sea floor


222


and allows cold fluid transport ships


48


to be tied up offshore


28


. Likewise a platform


226


has legs


227


, which are secured to the sea floor


222


, and provides a stable facility for equipment and operations described below.




After the cold fluid transport ship


48


has been successfully secured to the mooring/docking device


228


, articulated piping, hoses and flexible loading arms


228


are connected to the low-pressure pump system


52


located in the cryogenic tanks


50


or on board the transport ship


48


. The other end of the articulated piping


228


is connected to a high-pressure pump system


230


located on the platform


226


. Additional cryogenically compatible piping


232


connects the high-pressure pump system


230


to the inlet


234


of the subsea heat exchanger


220


.




After the cold fluid


51


passes through the high-pressure pump system


230


it is converted into a dense phase fluid


64


and then passes through the heat exchanger


220


. The fluid


64


stays in the dense phase as it passes through the heat exchanger


220


. The outlet


236


of the heat exchanger


220


is connected to a flexible joint


238


or an expansion joint. The cryogenically compatible piping


235


in the heat exchanger


220


connects to one end of the flexible joint


238


and non-cryogenically piping


240


connects to the other end of the flexible joint


238


. This allows for expansion and contraction of the cryogenically compatible piping


235


. The subsea pipeline


242


is formed from non-cryogenically compatible piping.




The subsea pipeline


242


connects to a wellhead


76


, which connects to the well


32


and the uncompensated salt cavern


34


. Again, by opening valves, not shown, on the wellhead


76


, dense phase fluid


64


can be transported from the subsea pipeline


242


through the well


32


and injected in the uncompensated salt cavern


34


for storage.




In addition, the dense phase fluid


64


can be transported through the subsea pipeline


242


to a throttling valve


80


or regulator which reduces the pressure and allows the dense phase fluid


64


to pass through the piping


84


into the inlet


86


of the pipeline


42


for transport to market.




After a sufficient amount of dense phase fluid


64


has been stored in the salt cavern


34


, the valves, not shown, on the wellhead


76


can be shut off. This isolates the dense phase fluid


64


under pressure in the uncompensated salt cavern


34


. In order to transfer the dense phase fluid


64


from the uncompensated salt cavern


34


to the pipeline


42


, other valves, not shown, are opened on the wellhead


76


allowing the dense phase fluid which is under pressure in the uncompensated salt cavern


34


to move through the throttling valve


80


or regulator and the pipe


84


to the pipeline


42


.




Because the pressure in the uncompensated salt cavern


34


is higher than the pressure in the pipeline


42


, all that is necessary to get the dense phase fluid to market is to open one or more valves, not shown, on the wellhead


76


which allows the dense phase fluid


64


to pass through the throttling valve


80


. The well


32


is used to inject and remove dense phase fluid


64


from the uncompensated salt cavern


34


as shown by the flow arrows.





FIG. 5

is an enlargement of the offshore facility


298


and subsea Bishop Process heat exchanger


220


of FIG.


4


. (

FIG. 5

is not drawn to scale.) The subsea heat exchanger


220


includes a first section


250


and a second section


252


. The cryogenically compatible piping


235


is positioned in the middle of the outer conduits


254


and


256


by a plurality of centralizers


258


,


260


,


262


and


264


. These centralizers used in the subsea heat exchanger


220


are identical to the centralizers used in the surface mounted heat exchanger


62


as better-seen in FIG.


6


. Some slippage must be allowed between the centralizers and the outer conduits


254


and


256


to allow for expansion and contraction.




Cold fluids


51


leave the cryogenic storage tanks


50


on the cold fluid transport ship


48


and are pumped by the low-pressure pump


52


through the articulated piping


228


to the high-pressure pump system


230


located on the platform


226


. The cold fluid


51


then passes through piping


232


to the inlet


234


of the subsea heat exchanger


220


. The piping


228


,


232


and


235


must be cryogenically compatible with the cold fluid


51


.




The offshore heat exchanger


220


uses seawater


20


as a warmant


99


. The warmant enters piping


246


on the platform


226


and passes through the low-pressure warmant pump


244


. The warmant pump


244


may also be submersible. Piping


248


connects the low-pressure warmant pump


244


to the inlet ports


266


on the first section


250


of the heat exchanger


220


. The warmant


99


passes through the annular area


268


between the outside diameter of the cryogenically compatible pipe


235


and the inside diameter of the pipe


254


. The warmant


99


then exits the outlet ports


270


as indicated by the flow arrows. A submersible low-pressure pump


272


pumps additional warmant


99


into the second section


252


of the heat exchanger


220


. In the alternative, the pump


272


could also be located on the platform


226


. The warmant passes through the inlet ports


274


into the annular area


276


as indicated by the flow arrows. The annular area


276


is between the outside diameter of the cryogenically compatible pipe


235


and the interior diameter of the outer conduit


256


. The warmant


99


exits the second section


252


through the outlet ports


278


as indicated by the flow arrows.




The cold fluid


51


enters the heat exchanger at the inlet


234


as a dense phase fluid


64


as it leaves the outlet


236


of the heat exchanger


220


as a dense phase fluid. The cryogenically compatible pipe


235


is connected to non-cryogenically compatible pipe


240


by a flexible joint


238


or an expansion joint. This allows the remainder of the subsea pipeline


242


to be constructed from typical carbon steels that are less expensive than cryogenically compatible steels. The heat exchanger


220


must be designed to avoid freez-up and to reduce or avoid icing within the heat exchanger


62


. Similar design considerations, previously discussed that apply to the heat exchanger


62


also apply to the heat exchanger


220


.




EXAMPLE #2




This hypothetical example is-designed to give broad operational parameters for the Bishop One-Step Process conducted offshore as shown in

FIGS. 4 and 5

. A number of factors must be considered when designing the facilities


298


and


299


including the type of cold fluid and the temperature of the warmant that will be used. Conventional instrumentation for process measurement, control and safety are included in the facility as needed including but not limited to: temperature and pressure sensors, flow measurement sensors, overpressure reliefs, regulators and valves. Various input parameters must also be considered including, pipe geometry and length, flow rates, temperatures and specific heat for both the cold fluid and the warmant. Various output parameters must also be considered including the type, size, temperature and pressure of the uncompensated salt cavern. For delivery directly to a pipeline, other output parameters must also be considered such as pipe geometry, pressure, length, flow rate and temperature. Other design parameters to prevent freez-up include temperature of the warmant at the inlet and the outlet of each section of the heat exchanger, and the temperature at the initial contact area


235


. Other important design considerations include the size of the cold fluid transport ship and the time interval during which the ship must be fully offloaded and sent back to sea.




Assume that 800,000 barrels of LNG (125,000 cubic meters) are stored in the cryogenic tanks


50


on the transport ship


48


at approximately one atmosphere and a temperature of −250° F. or colder. The cold fluid transport ship


48


is moored to a dolphin


224


or some other suitable mooring/docking apparatus such as a single point mooring/docking or multiple anchored mooring/docking lines. LNG flows from the ship


48


through the low-pressure pump system


52


, through hoses, flexible loading arms and/or articulated piping


228


to the high-pressure pump system


230


on the platform


226


. The dense phase fluid


64


leaves the outlet of the high-pressure pump system


230


and enters the heat exchanger


220


. The heat exchanger


220


is shown on the sea floor


222


, but it could be located elsewhere as previously discussed. Also the heat exchanger


222


can assume various shapes as previously discussed in Example 1.




Ambient heated vaporizers are known in conventional LNG facilities (See pg. 69 of the Operating Section Report of the AGA LNG Information Book, 1981). According to the aforementioned Operating Section Report, “Most base load (ambient heated) vaporizers use sea or river water as the heat source.” These are sometimes called open rack vaporizers. On information and belief, conventional open rack vaporizers generally operate at pressures in the neighborhood of 1,000-1,200 psig. These open rack vaporizers are different than the heat exchangers


62


and


220


used in the Bishop One-Step Process.




Comparison of heat exchangers used in the invention with conventional open rack vaporizers.




First, the heat exchangers in the Bishop One-Step Process easily accommodate higher pressures suitable for injection into uncompensated salt caverns. Typically, conventional vaporizer systems are not designed for operational pressures in excess of 1,200 psig.




Second, the sendout capacity of each conventional open rack vaporizer is substantially less than the sendout capacity of the heat exchangers used in the Bishop One-Step Process. On information and belief, several open rack vaporizers must be used in a bank to achieve the desired sendout capacity that can be achieved by one Bishop One-Step Process heat exchanger.




Third, the conventional open rack vaporizer is also believed to be more prone to ice formation and freezing problems that the heat exchangers in the Bishop One-Step Process. Vaporizers that avoid this problem sometimes use water-glycol mixtures, which introduce an environmental hazard.




Fourth, the heat exchanger used in the Bishop One-Step Process provides a needed path to the uncompensated salt cavern or pipeline, in addition to heating the fluid. The length of the exchanger can be varied by using alternate designs as needed.




Fifth, the heat exchanger used in the Bishop One-Step Process is easily flushed for cleaning, as with a biocide. There is little chance of clogging when doing this.




Sixth, the construction of the heat exchanger used in the Bishop One-Step Process is extremely simple from widely available materials, and can be done on site.




Seventh, the heat exchanger used in the Bishop One-Step Process can accommodate a wide range of cold fluids with no change in design—LNG, ethylene, propane, etc.




Eighth, the heat exchanger used offshore in the Bishop One-Step Process uses little space, (because it can be on the sea floor) which is highly advantageous on platforms. The weight contribution is also almost negligible.




Ninth and dependent on all of the above features, the heat exchanger used in the Bishop One-Step Process is extremely low cost both in capital and operations.




Recognizing some of these performance problems with open rack vaporizers, Osake Gas has developed a new vaporizer called the SUPERORV, which uses seawater as the warmant. Drawings of the SUPERORV and conventional open rack vaporizers are shown on the Osaka Gas web site (www.osakagas.co.jp). The distinctions listed above between the heat exchanger used in the Bishop One-Step Process are likewise believed to be applicable to the SUPERORV.





FIG. 6

is a section view of the first section of the heat exchanger along the line


6





6


of FIG.


2


. (

FIG. 6

is not drawn to scale.) The coaxial heat exchanger


62


includes a center pipe


61


formed of material suitable for low temperature and high-pressure service, while the outer conduit


104


may be a material not suited for this service. This allows the outer conduit


104


to be formed from plastic, fiberglass or some other material that may be highly corrosion or fouling resistant, as it needs to be in order to transport the warmant


99


such as fresh water


19


or sea water


20


. The annular area


101


between the outside diameter of the central pipe


61


and the inside diameter of the outer conduit


104


may need to be treated chemically periodically for fouling. The center pipe


61


will typically have corrosion resistant properties.




The center pipe


61


will be equipped with conventional centralizers


108


to keep it centered in the outer conduit


104


. This serves two functions. Centralizing allows the warming to be uniform and thus minimize the occurrence of cold spots and stresses. Perhaps more importantly, the supported, centralized position allows the inner pipe


61


to expand and contract with large changes in temperature. The centralizer


108


has a hub


107


that surrounds the pipe


61


and a plurality of legs


109


that contact the inside surface of the outer conduit


104


. The legs


109


are not permanently attached to the outer conduit


104


and permit independent movement of the inner pipe


61


and the outer conduit


104


. This freedom of movement is important in the operation of the invention. To further permit expansion and contraction in the surface mounted heat exchanger


62


of

FIG. 1

, the outlet


63


is connected to a flexible joint


65


which also connects to non-cryogenically compatible piping


70


. Likewise in subsea heat exchanger


220


of

FIGS. 4 and 5

, the outlet


236


is connected to a flexible joint


238


which also connects to non-cryogenically compatible piping


240


. All of the centralizers that are used in this invention should allow movement (expansion, contraction and elongation) of the cryogenically compatible inner pipe independent of the outer conduit without causing significant abrasion and unnecessary wear on either. The cold fluid


51


passing through the cryogenically compatible piping is-crosshatched in

FIGS. 6

,


7


and


8


for clarity.





FIG. 7

is a section view of an alternative embodiment of the heat exchanger used in the Bishop One-Step Process. In the alternative embodiment of

FIG. 7

, a central cryogenically compatible pipe


300


is centered inside of an intermediate cryogenically compatible pipe


302


by centralizers


304


. The intermediate pipe


302


is centered inside the outer conduit


104


by centralizers


305


. The centralizer


305


has a centralizer hub


302


, which is held in place by a plurality of legs


306


. An annular area


308


is defined between the outside diameter of the intermediate pipe


302


and the inside diameter of the outer conduit


104


. Warmant


99


passes through the annular area


308


. The legs


306


are not permanently attached to the inside of the outer conduit


104


to allow the cryogenically compatible pipes to expand and contract independent of the outer conduit


104


. Warmant


99


also passes through the central pipe


300


. The cold fluid


51


passes through the annular area


309


between the outside diameter of the central pipe


300


and the inside diameter of the centralizer hub


302


. The cold fluid


51


in the annular area


309


is crosshatched in

FIG. 7

for clarity. The alternative design of

FIG. 7

has a greater heat exchange area and therefore the length of a heat exchanger using the alternative design of

FIG. 7

may be shorter than the design in FIG.


6


. In those circumstances where a relatively short heat exchanger may be preferable, the alternative design of

FIG. 7

may be more suitable than the design of FIG.


6


. In some circumstances, it may be necessary to develop even a shorter heat exchanger.





FIG. 8

is a section view of a second alternative embodiment of the heat exchanger used in the Bishop One-Step Process. Interior cryogenically compatible pipes


320


,


322


,


324


and


326


are held in a bundle and are centered inside the outer conduit


104


by a plurality of centralizers


327


. The centralizers


327


have centralizer hubs


328


. The interior pipes


320


,


322


,


324


and


326


are crosshatched to indicate that they carry the cold fluid


51


. The centralizer hub


328


is positioned in the middle of the outer conduit


104


by legs


330


, which are not permanently attached to the outer conduit


104


. Warmant


99


passes through the annular area


334


. The alternative embodiment of

FIG. 8

should allow for even a shorter length heat exchanger than the design show in FIG.


7


. When space is at a premium, alternative designs such as FIG.


7


and

FIG. 8

may be suitable and other designs may also be utilized that increase the area of heat interface.





FIG. 9

is a temperature-pressure phase diagram for natural gas. Natural gas is a mixture of low molecular weight hydrocarbons. Its composition is approximately 85% methane, 10% ethane, and the balance being made up primarily of propane, butane and nitrogen. In flow situations where conditions are such that gas and liquid phases may coexist, pump, piping and heat transfer problems, discussed below, may be severe. This is especially true where the flow departs from the vertical. In downward vertical flow such as shown in U.S. Pat. No. 5,511,905, the liquid velocity must only exceed the rise velocity of any created gas phase in order to maintain uninterrupted flow. In cases approaching horizontal flow with a two-phase fluid, the gas can stratify, preventing the heat exchange, and in extreme cases causing vapor lock. Cavitation can also be a problem.




In the present invention, these problems are avoided by insuring that the cold fluid


51


is converted by the high-pressure pump system


56


or


230


into a dense phase fluid


64


and that it is maintained in the dense phase while a) it passes through the heat exchanger


62


or


220


and b) when it is stored in an uncompensated salt cavern. The dense phase exists when the temperature and pressure are high enough such that separate phases cannot exist. In a pure substance, for which this invention also applies, this is known at the critical point. In a mixture, such as natural gas, the dense phase exists over a wide range of conditions. In

FIG. 9

, the dense phase will exist as long as the fluid conditions of temperature and pressure lie outside the two-phase envelope (crosshatched in the drawing). This invention makes use of the dense phase characteristic so there is no change in phase with increase in temperature or pressure when starting from a point on the phase diagram above the cricondenbar


350


or to the right of the cricondentherm


352


. This allows a gradual increase in temperature with a corresponding gradual decrease in density as the fluid is warmed and expanded in the heat exchanger


62


or


220


. The result is a flow process where density stratification effects become insignificant. Operational pressures for the cold fluid


51


should therefore place the fluid


64


in the dense phase in the heat exchangers


62


or


220


and downstream piping and storage. In the case of some natural gas compositions, dense phase maintenance will require pressures different from the approximately 1,200 psig shown in the example in FIG.


9


.




The effect of confining the fluid to the dense phase is illustrated by an analysis of the densimetric Froude Number F that defines flow regimes for layered or stratified flows:






F
=


V
(

gD



Δ





γ

γ


)


-

(

1
2

)













Here V is fluid velocity, g is acceleration due to gravity, D is the pipe diameter and γ is the fluid density and Δγ is the change in fluid density. If F is large, the terms involving stratification in the governing equation of fluid motion dropout of the equation. As a practical example, two-phase flows in enclosed systems generally lose all stratification when the Froude Number rises to a range of from 1 to 2. In the present invention, the value of the Froude Number ranges in the hundreds, which assures complete mixing of any density variations. These high values are assured by the fact that in dense phase flow, the term Δγ/γ in the equation above is small.




Measurement of the Froude Number occurs downstream of the high-pressure pump systems


56


and


230


and in the heat exchangers


62


and


220


. In other words, the Froude Number, using the Bishop One-Step Process should be high enough to prevent stratification in the piping downstream of the high-pressure pump systems


56


and


230


and in the heat exchangers


62


and


220


. Typically Froude Numbers exceeding 10 will prevent stratification. Note that conventional heat exchangers do not usually operate at pressures and temperatures high enough to produce a dense phase, and phase change problems may be avoided by other means.




In summary, using the present invention, the cold fluid


51


is kept in the dense phase by pressure as it leaves the high-pressure pump system


56


or


230


and thereafter as it passes through the heat exchangers


62


or


220


and while it is stored in uncompensated salt cavern.





FIG. 10

is a schematic diagram of an alternative embodiment of the present invention. The onshore facility


310


uses a conventional vaporizer system


260


to warm the cold fluid


51


prior to storage or transport.




Conventional LNG facilities offload LNG and store it onshore in cryogenic storage tanks as a liquid. In a conventional facility, the LNG is then run through a conventional vaporizer system to warm the liquid and convert it into a gas. The gas is odorized and transferred to a pipeline that transmits the gas to market. A simplified flow diagram of a conventional LNG vaporizer system is shown in FIG. 4.1 of the Operating Section Report of the AGA LNG Information Book, 1981, which is incorporated herein by reference. As discussed on page 64 of this document, various types of vaporizers are known including heated vaporizers, integral heated vaporizers, and remoted heated vaporizers, ambient vaporizers and process vaporizers. Any of these known vaporizers could be used in the vaporizer system


260


of

FIG. 10

, provided they have the capacity to quickly offload the ship


48


, and providing that they can withstand the pressures necessary for downstream injection into an uncompensated salt cavern.




In the alternative embodiment shown in

FIG. 10

, cold fluid


51


is offloaded from the transport ship


48


by the low-pressure pump system


52


located in the cryogenic storage tanks


50


or on the vessel


48


. The cold fluid


51


passes through articulated piping


54


to another high-pressure pump system


56


located on or near the dock


44


. The fluid


59


then passes through additional piping


58


to the inlet


262


of the conventional vaporizer


260


. The fluid


59


passes from the inlet


261


through the vaporizer


260


to the outlet


264


. Unlike Examples 1 and 2, it is not necessary in this alternative embodiment to have the fluid in the dense phase while it goes through the vaporizer nor are high Froude numbers required. Though not required, use of the dense phase is also acceptable. Therefore the fluid in this alternative embodiment has been assigned a different numeral, i.e.


59


. The fluid


59


passes through the non-cryogenic piping


70


and the wellhead


72


through the well


36


to the uncompensated salt cavern


38


. Likewise, the fluid


59


can pass through the non-cryogenic piping


74


, the wellhead


76


, the well


32


, to the uncompensated salt cavern


34


. When the uncompensated salt caverns


34


and


38


are full, valves, not shown, on the wellheads


76


and


72


can be shut off to store the gas in the uncompensated salt caverns


34


and


38


.




Typically, the fluid


59


will be stored at a pressure exceeding pipeline pressures. Therefore, all that is necessary to transfer the fluid


59


from the uncompensated salt caverns


34


and


38


is to open valves, not shown, on the wellhead


76


and


72


allowing the gas


320


to pass through the piping


78


and the throttling valve


80


or a regulator, the piping


84


to the inlet


86


of the pipeline


42


. Some additional heating may be necessary to the gas prior to entering the pipeline. Therefore, the wells


32


and


36


are used for injecting fluid


59


into the uncompensated salt caverns


34


and


38


and the wells are also used as an outlet for the stored fluid


59


when it is transferred to the pipeline


42


. The flow arrows in the drawing therefore go in both directions indicating the dual features of the wells


32


and


36


.




EXAMPLE #3




This hypothetical example is merely designed to give broad operational parameters for an alternative embodiment including a vaporizer system for warming of cold fluids with subsequent storage in uncompensated salt caverns and/or transportation through a pipeline, as shown in FIG.


10


. Unlike conventional LNG facilities, no cryogenic tanks are used in the on-shore facility


310


of FIG.


10


. (The ship


48


, as previously mentioned, does contain cryogenic tanks


50


.) A conventionally designed vaporizer system


260


is used in this alternative embodiment instead of the coaxial heat exchangers


62


and


220


, discussed in the previous examples. (Conventional vaporizer systems typically operate in the range of 1,000-1,200 psig.) The conventionally designed vaporizer system


260


will need to be modified to accept the higher pressures associated with uncompensated salt caverns (typically in the range of 1,500-2,500 psig). A number of factors must be considered when designing the facility


310


including the type of cold fluid and warmant that will be used. Conventional instrumentation for process measurement, control and safety are included in the facility as needed including but not limited to: temperature and pressure sensors, flow measurement sensors, overpressure reliefs, regulators and valves. Various input parameters must also be considered including, pipe geometry and length, flow rates, temperatures and specific heat for both the cold fluid and the warmant. Various output parameters must also be considered including the type, size, temperature and pressure of the uncompensated salt caverns. For delivery directly to a pipeline, other output parameters must also be considered such as pipe geometry, pressure, length, flow rate and temperature. Other important design considerations include the size of the cold fluid transport ship and the time interval during which the ship must be fully offloaded and sent back to sea.




A plurality of vaporizer systems


260


might be required to reach desired flow rates. The vaporizer systems used in this alternative embodiment must be designed to withstand operational pressures in the range of 1,500 to 2,500 psig to withstand the higher pressures necessary for subsurface injection.




Conventional vaporizer systems are designed to function with stratification. Unlike Examples 1 and 2, it is not necessary in this alternative embodiment to have the fluid in the dense phase while it goes through the vaporizer nor are high Froude numbers required. Though not required, use of the dense phase is also acceptable.




Referring to

FIG. 10

, LNG is pumped from the ship


48


using the low-pressure pump system


52


, through the hoses or flexible loading arms


54


to the high-pressure pump system


56


. The fluid


59


passes through the vaporizer system


260


where it is warmed. The fluid


59


then is injected into uncompensated salt caverns. Because the offload rate from the ship


48


and the storage pressures are similar, pump and flow rate characteristics described in Example 1 are applicable to Example 3. To Applicants knowledge, there is presently no conventional LNG facility using conventional vaporizers that subsequently injects gas into an uncompensated salt cavern.





FIG. 11

is a block diagram of the Flexible Natural Gas Storage Facility with four salt caverns. The drawing is not to scale. The Flexible Natural Gas Storage Facility can have a single large cavern or several separate caverns. The four caverns in

FIG. 11

are merely for illustrative purposes.




The Flexible Natural Gas Storage Facility is generally identified by the numeral


400


. The Flexible Natural Gas Storage Facility


400


can receive fluid from a pipeline(s) natural gas source


412


and/or a LNG source


414


. This gives the Facility


400


flexibility and economic advantages over conventional natural gas salt cavern storage facilities—that receive gas solely from pipelines. The LNG source can be a cold fluid transport ship


48


, not shown and/or a conventional LNG receiving terminal with surface mounted tanks. As previously discussed, the surface mounted tanks are not preferred, but as an add-on to an existing terminal may be advantageous.




The pipeline natural gas source


412


may be one or several pipelines that deliver natural gas


402


, sometimes referred to as a first fluid. The pipeline natural gas source


412


is connected via piping


416


to a conventional natural gas compressor


418


. The natural gas


402


flows from the pipeline natural gas source


412


to the compressor


418


where the natural gas is compressed to salt cavern pressure. The compression process also raises the temperature of the natural gas to about 200° F. The compressor


418


is connected via piping


420


to a conventional heat exchanger


422


. The natural gas


402


flows from the compressor to the heat exchanger


422


where it is cooled to temperatures compatible with the salt cavern as previously explained. It is preferable, though not required, to raise the pressure of the gas from the pipeline source to dense phase levels for storage in a salt cavern. However, on some days during high drawdown, the cavern pressure may fall below dense phase levels.




The cooled, compressed natural gas


402


flows via piping


424


to the inlet


426


of the manifold


428


. The manifold is connected to additional piping


430


,


432


and


434


to allow distribution of natural gas to various components in the Facility


400


. The piping


434


connects the inlet and the manifold to pipeline


436


. The piping


430


connects the inlet and the manifold to the pipeline


438


. A second manifold


440


connects to the first pipeline


436


, the second pipeline


438


and the piping


430


,


432


and


434


. A well


442


connects first salt cavern


444


with the Facility


400


. Fluid may flow from the Facility


400


into the cavern


444


or fluid may flow from the cavern


444


to another cavern or a pipeline as indicated by the bi-directional flow arrows. A second well


446


connects second salt cavern


448


with the Facility


400


. Fluid may flow from the Facility


400


into the cavern


448


or fluid may flow from the cavern


448


to another cavern or a pipeline as indicated by the bi-directional flow arrows. A third well


450


connects third salt cavern


452


with the Facility


400


. Fluid may flow from the Facility


400


into the cavern


452


or fluid may flow from the cavern


452


to another cavern or a pipeline as indicated by the bi-directional flow arrows. A fourth well


454


connects fourth salt cavern


456


with the Facility


400


. Fluid may flow from the Facility


400


into the cavern


456


or fluid may flow from the cavern


456


to another cavern or a pipeline as indicated by the bi-directional flow arrows. The Facility


400


contains at least one salt cavern, but will typically contain two to five individual caverns. Four salt caverns are shown here solely for illustrative purposes.




Each of these salt caverns,


444


,


448


,


452


and


456


are in fluid communication with the other caverns in this Facility and the pipelines


436


and


438


. This fluid communication is achieved through the first manifold


428


, the second manifold


440


, the piping


430


,


432


and


434


and the wells


442


,


446


,


450


and


454


. Various valves and other control mechanisms, not shown allow operators to control the flow of fluids in the Facility


400


.




The LNG source


414


is connected via piping


470


to a high pressure cryogenic LNG pump


56


. The LNG source


414


is sometimes simply referred to as “a source of second fluid.” The LNG itself is sometimes simply referred to as “the second fluid.” The pump


56


raises the pressure of the LNG to dense phase as previously discussed concerning FIG.


9


. Piping


472


connects the pump


56


to the LNG heat exchanger


473


. The heat exchanger


473


could be the Bishop Process Heat Exchanger


62


if the LNG source was on shore as shown in

FIG. 1

or the heat exchanger


473


could be the Bishop Process Heat Exchanger


220


if the LNG source was offshore as shown in FIG.


4


. The heat exchanger


473


warms the second fluid to temperatures that are compatible with a salt cavern, as previously explained. Piping


474


connects the heat exchanger


473


with an optional booster compressor


476


. Piping


478


connects the optional booster compressor


476


with the inlet


426


. In this manner, the LNG source


414


is in fluid communication with the pipelines


436


and


438


and the salt caverns


444


,


448


,


452


and


456


. Likewise the pipeline natural gas source is in fluid communication with the pipelines


436


and


438


and the salt caverns


444


,


448


,


452


and


456


. The pipelines


436


and


438


connect the Facility


400


with a market for natural gas, not shown.




A vaporizer


260


that has been modified to work at dense phase pressures (typically 1,000 psi and above) is connected to the LNG pump


56


via piping


479


. Dense phase LNG from the pump


56


is heated in the vaporizer


260


, as previously explained, to temperatures compatible with a salt cavern. Piping


480


connects the vaporizer


269


with an optional booster compressor


482


. Piping


484


connects the optional booster compressor


482


with the inlet


426


. In this manner, the LNG source


414


is in fluid communication with the salt caverns and the pipelines


436


and


438


.




Many pipelines in the U.S. regulate the Btu content of the natural gas that is delivered to customers. This enables users of natural gas to plan and operate their facilities with predictable results. For example, some pipelines set 1050 Btu per standard cubic foot as a standard for delivered gas. If a bakery sets burners in bread baking ovens for the pipeline standard and the delivered gas actually has a Btu content of 1100 Btu per standard cubic foot, then the top of the bread might burn. This has been a challenge for LNG that is delivered from different parts of the world. For example, Algeria is known to have rich gas that may hit 1200 Btu per standard cubic foot. Other parts of the world, such as Trinidad have lean gas that may dip to 1140 Btus per standard cubic foot. In order to deliver gas to a pipeline standard, LNG importers have sometimes had to adjust their Btu content. This may require pumping air to pipeline pressure in order to reduce the Btu content of the gas. The cost for pumping the air increases operating expenses.




The Flexible Natural Gas Storage Facility


400


provides an easy and cost effective solution to Btu variances. One solution is to commingle rich gas and lean gas in the same salt cavern to achieve the Btu level required by the pipeline. Another solution is to put rich gas in a first salt cavern and lean gas in a second salt cavern. When it is time to deliver gas to a pipeline, some rich gas can be blended with some lean gas in a manifold or other piping system prior the delivery to the pipeline to achieve the Btu level required by the pipeline.




Because the Flexible Natural Gas Storage Facility


400


has access to multiple sources of natural gas, it has economic advantages over both conventional single source salt cavern storage facilities and conventional LNG receiving terminals. In the past 20 years, some conventional LNG receiving terminals in the U.S. have ceased operations due to low demand. This represents a large capital investment that is not being utilized. The Flexible Natural Gas Storage Facility


400


overcomes this market risk because it has access to multiple sources of natural gas. In periods where there is little or no LNG being imported into the U.S., the Facility


400


would still have economic value and activity because it could receive natural gas from a pipeline source and function as a natural gas storage facility. In periods where there are large amounts of LNG being imported into the U.S., the Facility


400


would have economic value and activity because it could be used primarily for receiving, storing and distributing natural gas from a LNG source. To applicant's knowledge, there is no multi-source natural gas salt cavern storage facility like the Flexible Natural Gas Storage Facility


400


.




EXAMPLE 4




This hypothetical example is designed to give broad operational parameters for the Flexible Natural Gas Storage Facility


400


as shown in FIG.


11


.




When the LNG source for the Flexible Natural Gas Storage Facility


400


is a cold fluid transport ship


48


offloading at a dock with a land based Bishop Process Heat Exchanger, then previous Example 1 is relevant. When the LNG source for the Flexible Natural Gas Storage Facility


400


is a cold fluid transport ship


48


moored to an offshore facility with an offshore Bishop Process Heat Exchanger, then previous Example 2 is relevant. In a typical situation, the high pressure LNG pump raises the pressure of the LNG to cavern pressure. The Bishop Process Heat Exchanger then warms the fluid to a temperature that is compatible with the salt cavern, typically about 40° F. The optional booster compressor may be necessary to replace pressure lost due to pipeline friction or pressure drops due to distance or pipeline sizing between the LNG pumps and the caverns. When a vaporizer is used with a LNG source, instead of a Bishop Process Heat Exchanger, then previous Example


3


is relevant. The high pressure LNG pump raises the LNG to cavern pressure. The vaporizer then heats the fluid to a temperature that is compatible with the salt cavern, typically to about 40° F. The optional booster compressor may be necessary to replace pressure lost due to friction, pipeline sizes, or distance from the vaporizers and the caverns.




Although not preferred, the Facility


400


could receive LNG from surface mounted tanks of a conventional LNG receiving terminal such as that currently in operation south of Lake Charles, La.




When receiving natural gas from a pipeline natural gas source, the Facility


400


compresses gas from the pipeline to cavern pressure and raises the temperature of the gas to about 200° F. The gas is then cooled in a conventional heat exchanger to about 140° F. or less and is injected into a salt cavern. In this example the gas from the pipeline natural gas source is raised to dense phase pressures, but this is not essential to the invention. All that's essential is that the gas be raised to sufficient pressure to be injected into the salt cavern. The facility


400


, for example would have connections to one or more pipeline sources of natural gas. The facility


400


would have valving, piping, control, and measurement capability to both receive gas from the pipelines and deliver gas to the pipelines. This capability is sometimes called a bi-directional capability.




The Gas Compressor


418


could be a positive displacement or a centrifugal type compressor and would have sufficient capacity and horsepower to raise the pressure received from the Pipeline Natural Gas Source


412


from about 1000 psi to the pressure necessary to inject into the caverns


444


,


448


,


452


,


456


or about 2000 psi. The cavern injection pressures are determined by the design of the caverns but the volume of injection or rate at which gas can be injected into the caverns are determined by the compressor design and horsepower. For this example it is assumed that the cavern injection design rate is 300 million cubic feet of gas injected per day up to the maximum operating pressures of the caverns. This injection rate would require about 25,000 horsepower of compression.




The compressed gas discharged from the compressor would be at 2,000 psi and about 200 Degrees F. and piped to the Conventional Heat Exchanger


422


for cooling before injection into the caverns. For this example the Conventional Heat Exchanger


422


would be a fin-fan type and designed to cool the compressor discharge from about 200 Degrees F. to under 120 Degrees F. for injection into the caverns. No further processing would occur with the gas prior to cavern injection. Controls and valving would direct the gas into the appropriate cavern(s). If blending of the pipeline natural gas sourced gas was to be done in the cavern with gas from the second source for BTU control it would be so directed into the cavern(s) designated and operated for in-cavern blending.




Discharge from the caverns to the Pipeline(s)


436


,


438


would be by positive pressure differential as described in examples 1, 2, and 3. unless blending of the gas discharged from the caverns would be done at discharge instead of in the caverns. In that case, the well discharges would be controlled from the appropriate caverns so as to proportion the flow to achieve the BTU content desired in the blended stream. For example, if the desired flow to the pipelines was 600 million cubic feet per day of natural gas that could not exceed 1050 BTUs per cubic foot. If cavern


444


had gas stored in that contained 1100 BTUs per cubic foot and cavern


448


had gas stored in it that contained 1000 BTUs per cubic foot the discharge from each of the caverns could be controlled at 300 million cubic feet per day, blended in the manifold


430


,


428


,


434


and discharged to the pipelines


436


,


438


as 600 million cubic feet per day of 1050 BTU per cubic foot natural gas.




When discharging from the cavern(s)


444


,


448


,


452


,


456


,each cavern could discharge to the manifold in excess of 500 million cubic feet per day using positive pressure differential to the pipeline(s)


438


,


436


, as described earlier. This enables the facility


400


to flow to the pipeline(s) as much as 2 billion cubic feet per day if necessary. There are no LNG liquid tank based receiving and storage facilities in the U.S. that have the capability to deliver natural gas to the pipeline system at rates as high as 2 billion cubic feet per day. This assumes that the pipeline(s) are capable of receiving gas at these high volumes. Between the wells and the pipeline(s) would be valves and controls to control pressure, volumes, and flow rates as necessary and well known to those schooled in the art of salt cavern natural gas storage.




In addition, dehydration equipment may be used to reduce or remove moisture in the gas that may be picked up in the cavern(s) also well known to those schooled in the art of salt cavern natural gas storage.




Thus, the Flexible Natural Gas Storage Facility would have the capability to receive either fluid and from storage discharge the combined fluids to the pipeline(s) at rates significantly higher than a conventional LNG liquid tank based receiving and storage terminal.



Claims
  • 1. A flexible natural gas storage facility comprising:at least one man-made salt cavern; a pipeline source of a first fluid; at least one high pressure compressor to compress the first fluid; at lease one heat exchanger to cool the first fluid from the compressor to a temperature that is compatible with the salt cavern, before the first fluid is placed in the salt cavern for storage; a source of a second fluid; at least one high pressure cryogenic pump to raise the pressure of the second fluid to dense phase; at least one Bishop Process heat exchanger to heat the second fluid to a temperature that is compatible with the salt cavern, before the second fluid is placed in the salt cavern for storage; and at least one high pressure vaporizer to heat the second fluid from the high pressure LNG pump to a temperature that is compatible with the salt cavern, before the second fluid is placed in the salt cavern for storage.
  • 2. The apparatus of claim 1 further including at least one booster compressor to compress the second fluid from the vaporizer, before the second fluid is placed in the salt cavern for storage.
  • 3. A flexible natural gas storage facility comprising:at least one manmade salt cavern; a pipeline source of a first fluid; at least one high pressure compressor to compress the first fluid; at least one heat exchanger to cool the first fluid from the compressor to a temperature that is compatible with the salt cavern, before the first fluid is placed in the salt cavern for storage; a source of a second fluid; at least one high pressure cryogenic pump to raise the pressure of the second fluid to dense phase; at least one high pressure vaporizer to heat the second fluid to a temperature that is compatible with the salt cavern, before the second fluid is placed in the salt cavern for storage; and at least one Bishop Process heat exchanger to heat the second fluid from the LNG pump to a temperature that is compatible with the salt cavern, before the second fluid is placed in the salt cavern for storage.
  • 4. The apparatus of claim 3 further including at least one booster compressor to compress the second fluid from the Bishop Process heat exchanger, before the second fluid is placed in the salt cavern for storage.
  • 5. The apparatus of claim 4 further including at least one booster compressor to compress the second fluid from the vaporizer, before the second fluid is placed in the salt cavern for storage.
  • 6. A method of storing natural gas comprising:compressing a first fluid from a pipeline source of natural gas; cooling the compressed first fluid to a temperature that is compatible with a salt cavern; injecting the cooled, compressed first fluid into a first salt cavern; pressurizing a second fluid from a LNG source to the dense phase; heating the second fluid in a Bishop Process heat exchanger to a temperature that is compatible with a second salt cavern; injecting the second fluid into the second salt cavern; blending portions of the first fluid from the first salt cavern with portions of the second fluid from the second salt cavern in a third salt cavern to adjust the Btu content of the blended fluids in the third salt cavern; and releasing the blended fluid from the third salt cavern into a pipeline for transport to market.
  • 7. The method of claim 6 further including vaporizing the pressurized LNG to raise the temperature to a temperature that is compatible with the salt cavern.
  • 8. A method of storing natural gas comprising:compressing a first fluid from a pipeline and raising the pressure to dense phase; cooling the first fluid to a temperature that is compatible with a salt cavern; injecting the first fluid into a first salt cavern; pressurizing a second fluid to the dense phase; heating the second fluid in a Bishop Process heat exchanger to a temperature that is compatible with a second salt cavern; injecting the second fluid into the second salt cavern; blending a portion of the first fluid from the first salt cavern with a portion of the second fluid from the second salt cavern in a third salt cavern to adjust the Btu content of the blended fluids in the third salt cavern; and releasing the blended fluid from the third salt cavern into a pipeline for transport to market.
  • 9. The method of claim 8 further including vaporizing the second fluid to raise the temperature to a temperature that is compatible with the salt cavern.
  • 10. A method of storing natural gas comprising:compressing a first fluid from a pipeline source of natural gas; cooling the compressed first fluid to a temperature that is compatible with a first salt cavern; injecting the cooled, compressed first fluid into the first salt cavern; pressurizing a second fluid to the dense phase; vaporizing the second fluid to raise the temperature to a temperature that is compatible with a second salt cavern; injecting the second fluid into the salt cavern; blending the cooled, compressed first fluid from the first salt cavern with the second fluid from the second salt cavern in a third salt cavern to adjust the Btu content of the blended fluids in the third salt cavern; and releasing the blended fluid from the third salt cavern into a pipeline for transport to market.
  • 11. A method of storing natural gas comprising:compressing a first fluid from a pipeline and raising the pressure to dense phase; cooling the first fluid to a temperature that is compatible with a first salt cavern; injecting the cooled, first fluid into the first salt cavern; pressurizing a second fluid to the dense phase; vaporizing the second fluid to raise the temperature that is compatible with a second salt cavern; injecting the second fluid into a second salt cavern; blending a portion of the first fluid from the first salt cavern with a portion of the second fluid from the second salt cavern to adjust the Btu content of the blended fluids in a third salt cavern; and releasing the blended fluid from the third salt cavern into a pipeline for transport to market.
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation-in-part of application Ser. No. 10/246,954 filed on Sep. 18, 2002 which claims priority of U.S. provisional patent application No. 60/342,157 filed Dec. 19, 2001.

US Referenced Citations (8)
Number Name Date Kind
3724229 Seliber Apr 1973 A
4858640 Kaufmann Aug 1989 A
5052856 Tek Oct 1991 A
5129759 Bishop Jul 1992 A
5511905 Bishop et al. Apr 1996 A
5669734 Becnel, Jr. et al. Sep 1997 A
6298671 Kennelley et al. Oct 2001 B1
6374844 Hall Apr 2002 B1
Provisional Applications (1)
Number Date Country
60/342157 Dec 2001 US
Continuation in Parts (1)
Number Date Country
Parent 10/246954 Sep 2002 US
Child 10/384156 US