US20140157824A1 - Method for improved thermal performing refrigeration cycle - Google Patents

Method for improved thermal performing refrigeration cycle Download PDF

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Publication number
US20140157824A1
US20140157824A1 US13/707,132 US201213707132A US2014157824A1 US 20140157824 A1 US20140157824 A1 US 20140157824A1 US 201213707132 A US201213707132 A US 201213707132A US 2014157824 A1 US2014157824 A1 US 2014157824A1
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stream
nitrogen
refrigeration cycle
refrigerant
expanded
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US13/707,132
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Michael A. Turney
Alain Briglia
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LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
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LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
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Priority to US13/707,132 priority Critical patent/US20140157824A1/en
Assigned to L'AIR LIQUIDE, SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE reassignment L'AIR LIQUIDE, SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BRIGLIA, ALAIN
Assigned to AIR LIQUIDE PROCESS & CONSTRUCTION, INC. reassignment AIR LIQUIDE PROCESS & CONSTRUCTION, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: TURNEY, MICHAEL A.
Assigned to L'AIR LIQUIDE, SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE reassignment L'AIR LIQUIDE, SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: AIR LIQUIDE PROCESS & CONSTRUCTION, INC.
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/0002Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the fluid to be liquefied
    • F25J1/0022Hydrocarbons, e.g. natural gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/003Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the kind of cold generation within the liquefaction unit for compensating heat leaks and liquid production
    • F25J1/0047Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the kind of cold generation within the liquefaction unit for compensating heat leaks and liquid production using an "external" refrigerant stream in a closed vapor compression cycle
    • F25J1/005Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the kind of cold generation within the liquefaction unit for compensating heat leaks and liquid production using an "external" refrigerant stream in a closed vapor compression cycle by expansion of a gaseous refrigerant stream with extraction of work
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/006Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the refrigerant fluid used
    • F25J1/007Primary atmospheric gases, mixtures thereof
    • F25J1/0072Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0203Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process using a single-component refrigerant [SCR] fluid in a closed vapor compression cycle
    • F25J1/0204Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process using a single-component refrigerant [SCR] fluid in a closed vapor compression cycle as a single flow SCR cycle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0221Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process using the cold stored in an external cryogenic component in an open refrigeration loop
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0243Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0244Operation; Control and regulation; Instrumentation
    • F25J1/0245Different modes, i.e. 'runs', of operation; Process control
    • F25J1/0249Controlling refrigerant inventory, i.e. composition or quantity
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0243Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0279Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc.
    • F25J1/0285Combination of different types of drivers mechanically coupled to the same refrigerant compressor, possibly split on multiple compressor casings
    • F25J1/0288Combination of different types of drivers mechanically coupled to the same refrigerant compressor, possibly split on multiple compressor casings using work extraction by mechanical coupling of compression and expansion of the refrigerant, so-called companders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2210/00Processes characterised by the type or other details of the feed stream
    • F25J2210/42Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2270/00Refrigeration techniques used
    • F25J2270/14External refrigeration with work-producing gas expansion loop
    • F25J2270/16External refrigeration with work-producing gas expansion loop with mutliple gas expansion loops of the same refrigerant

Definitions

  • the present invention relates to a method and device for improving the thermal performance of a nitrogen refrigeration cycle.
  • Gas liquefaction is a known process used to liquefy gases and commonly employs a nitrogen refrigeration cycle to provide the necessary refrigeration.
  • the nitrogen refrigeration cycle in its most basic terms, includes the following steps: nitrogen gas is compressed, cooled, and then expanded in a turbo booster. During this expansion, the temperature of the gas drops and the expanding gas moves the turbine, which in turn performs work on the compressor of the turbo booster. The cold gas is then used to provide the necessary cooling to liquefy the target stream.
  • FIG. 1 represents typical nitrogen refrigeration cycle 1 that is useful for providing the necessary refrigeration to liquefy the target gas.
  • Nitrogen gas 2 is partially compressed in turbo booster 10 (which is a combination of compressor 20 and turbine 30 in which the turning of turbine 30 helps to turn compressor 20 ) and then further compressed in high pressure compressor 40 and then partially cooled in a heat exchanger 50 . Cooled compressed nitrogen 41 then exits the heat exchanger 50 and is expanded in turbine 30 of the turbo booster 10 . Expanded refrigerant 32 is then used to provide refrigeration for a gas stream (not shown). During this set up, nitrogen is lost in the turbo booster 10 and high pressure compressor 40 . These losses are made up by the introduction of gaseous nitrogen from LIN tank 60 .
  • Liquid nitrogen 62 is withdrawn from LIN tank 60 and vaporized in ambient vaporizer 64 .
  • ambient vaporizer 64 is supplemented with an electric heater which requires at least some utility cost or other type of vaporizer such as steam sparged water bath, natural gas fired water bath, electric, etc . . . Therefore, methods known heretofore may require additional utility cost.
  • a first portion 66 is used to provide the makeup losses for high pressure compressor 40 and turbo booster 10 by injecting first portion 66 into the warm end of heat exchanger 50 .
  • a second portion can be used as utility nitrogen for other users (e.g., instrument, purge/utility gas for both this plant or another nearby plant).
  • the present invention is directed to a device and a method that satisfies at least one of these needs.
  • Certain embodiments of the present invention relate to the use of an improved refrigeration cycle as part of a liquefaction process, in which makeup refrigerant is introduced on the cool side of the heat exchanger as opposed to the warm side of the heat exchanger.
  • the method for producing a liquefied gas stream from an inlet gas feed stream can include the steps of:
  • introducing a liquid refrigerant makeup stream into the refrigeration cycle by adding the liquid refrigerant makeup stream to the expanded refrigerant prior to heat exchange contact with the inlet gas feed stream to provide for makeup losses in the refrigeration cycle and to provide additional refrigeration to the refrigeration cycle.
  • the inlet gas feed stream to be liquefied is natural gas.
  • the refrigeration cycle is a nitrogen refrigeration cycle and the liquid refrigerant makeup stream originates from a liquid nitrogen tank containing liquid nitrogen.
  • the expanded refrigerant is nitrogen.
  • the expanded refrigerant is expanded in a device selected from the group consisting of an expansion valve, a turbo-expander, and a liquid (or dense fluid) expander.
  • the method can further includes the steps of withdrawing a utility nitrogen stream from the nitrogen vapor stream subsequent to heat exchange contact with the inlet gas feed stream, and introducing the utility nitrogen stream to a second user for use as utility nitrogen.
  • the method producing a liquefied gas stream from an inlet gas feed stream can include the steps of:
  • the nitrogen refrigeration cycle can include the steps of: expanding a nitrogen stream to a cold nitrogen vapor stream, cooling at least a portion of the inlet feed gas stream by heat exchange contact with the cold nitrogen vapor stream, compressing the cold nitrogen vapor stream to form a compressed nitrogen vapor stream, and cooling at least a portion of the compressed nitrogen vapor stream by heat exchange contact with the cold nitrogen vapor stream.
  • an apparatus for producing a liquefied gas stream from an inlet gas feed stream can include a heat exchanger, a refrigeration cycle, and a makeup liquid refrigerant tank.
  • the heat exchanger has a cold side and a warm side and is configured to receive the inlet gas feed stream and to produce the liquefied gas stream.
  • the refrigeration cycle is configured to provide refrigeration to the heat exchanger.
  • the refrigeration cycle further includes a compressor and an expander, wherein the compressor is configured to compress a refrigerant to a compression pressure, wherein the expander is configured to receive the compressed refrigerant and expand the compressed refrigerant to an expanded pressure to produce a cold refrigerant at an outlet of the expander, and wherein the outlet of the expander is in fluid communication with the cold side of the heat exchanger.
  • the makeup liquid refrigerant tank is configured to introduce a makeup liquid refrigerant with the cold refrigerant prior to heat exchange with the inlet gas feed stream.
  • the makeup liquid refrigerant tank is in fluid communication with the refrigeration cycle at a point downstream the outlet of the expander and upstream the cold side of the heat exchanger.
  • the expander is a device selected from the group consisting of an expansion valve, a turbo-expander, and a liquid/dense fluid expander.
  • the apparatus can further include a utility nitrogen withdrawal line configured to withdraw a nitrogen stream from the refrigeration cycle at a point downstream the warm side of the heat exchanger and introduce the nitrogen stream to a second user for use as utility nitrogen.
  • Certain embodiments of the present invention advantageously do not require supplemental energy for the vaporization of the make up fluid.
  • FIG. 1 shows a refrigeration cycle in accordance with the prior art.
  • FIG. 2 shows a refrigeration cycle in accordance with an embodiment of the invention.
  • FIG. 3 shows a liquefaction process in accordance with the prior art.
  • FIG. 4 shows a liquefaction process in accordance with an embodiment of the invention.
  • Nitrogen refrigeration cycle 1 of FIG. 2 is largely similar to nitrogen refrigeration cycle 1 of FIG. 1 , with the exception of the makeup nitrogen.
  • LIN tank 60 is in fluid communication with the cold side of the heat exchanger.
  • liquid nitrogen 62 travels from LIN tank 60 and is combined with gaseous nitrogen 32 where liquid nitrogen 62 vaporizes.
  • the flow rate of liquid nitrogen 62 is about 1% of the flow rate of expanded refrigerant 32 , thereby allowing liquid nitrogen 62 to vaporize when combining with expanded refrigerant 32 before going through heat exchanger 50 .
  • a small amount of second portion 68 can be withdrawn on the warm side of heat exchanger 50 in order to provide a makeup stream for nearby utilities.
  • FIG. 3 represents another example as known in the prior art while FIG. 4 represents another embodiment of the present invention. These figures are used to show the comparative advantages of embodiments of the present invention.
  • Compressed nitrogen 42 exits high pressure compressor 40 and is split into two portions.
  • First portion 44 is compressed in first turbo-booster 15 and then further compressed in second turbo-booster 25 .
  • Fully compressed nitrogen 27 is cooled in heat exchanger 50 and then expanded in second turbo-booster 25 to provide expanded first portion 34 .
  • Expanded first portion 34 is introduced into the cool side of heat exchanger 50 where it provides refrigeration to feed gas 48 in order to produce liquid feed 52 .
  • Feed gas 48 can be any gas that is desirable to liquefy, for example, natural gas.
  • Expanded first portion 34 exits heat exchanger 50 and is recompressed in high pressure compressor 40 to start the cycle over again.
  • second portion 46 enters heat exchanger 50 and is only partially cooled before being expanded in first turbo-booster 15 to reduce both its pressure and temperature. Expanded second portion 36 is introduced to heat exchanger 50 to provide additional cooling before it combines with expanded first portion 34 on its way back to high pressure compressor 40 .
  • first turbo-booster 15 As in FIG. 1 , nitrogen is lost in first turbo-booster 15 , second turbo-booster 25 , and high pressure compressor 40 . These losses are made up by the introduction of gaseous nitrogen 66 from LIN tank 60 . Liquid nitrogen 62 is withdrawn from LIN tank 60 and vaporized in ambient vaporizer 64 . A first portion 66 is used to provide the makeup losses for high pressure compressor 40 and turbo booster 10 by injecting first portion 66 into the warm end of heat exchanger 50 . A second portion 68 can be used as utility nitrogen for other users (e.g., for makeup losses for a nearby air separation plant) or as instrument gas and/or purge gas for this plant and/or another nearby facility.
  • Nitrogen refrigeration cycle 3 of FIG. 4 is largely similar to nitrogen refrigeration cycle 3 of FIG. 3 , with the exception of the makeup nitrogen.
  • LIN tank 60 is in fluid communication with the cold side of the heat exchanger 50 .
  • liquid nitrogen 62 travels from LIN tank 60 and is combined with expanded refrigerant 34 , where it vaporizes.
  • FIG. 4 % Change Nitrogen flow leaving High 22613 20797 8% Pressure Compressor (Nm 3 /hr) Loss if First Turbo-booster 68 68 — (Nm 3 /hr) Loss in Second Turbo-booster 68 68 — (Nm 3 /hr) Loss in High Pressure 102 102 — Compressor (Nm 3 /hr) Utility Usage (kW) 1213 1112 8% Total Make-up LIN (Nm 3 /hr) 338 338 — LIN added to Recycle (Nm 3 /hr) 238 238 — LIN sent to Utilities (Nm 3 /hr) 100 100 —
  • embodiments of the present invention can achieve approximately an 8% improvement over methods and apparatus of the prior art. This is extremely beneficial as embodiments of the present invention can provide a cost savings on both the capital cost because of the reduced size of the refrigeration cycle equipment and on the energy required to run the high pressure compressor.
  • Optional or optionally means that the subsequently described event or circumstances may or may not occur.
  • the description includes instances where the event or circumstance occurs and instances where it does not occur.
  • Ranges may be expressed herein as from about one particular value, and/or to about another particular value. When such a range is expressed, it is to be understood that another embodiment is from the one particular value and/or to the other particular value, along with all combinations within said range.

Abstract

An improved refrigeration cycle is provided. The cycle provides for improved thermal performance by incorporating a refrigerant makeup tank that introduces liquid refrigerant with expanded refrigerant upstream of the heat exchanger, thereby providing a savings in either electricity costs or refrigerant.

Description

    TECHNICAL FIELD OF THE INVENTION
  • The present invention relates to a method and device for improving the thermal performance of a nitrogen refrigeration cycle.
  • BACKGROUND OF THE INVENTION
  • Gas liquefaction is a known process used to liquefy gases and commonly employs a nitrogen refrigeration cycle to provide the necessary refrigeration. The nitrogen refrigeration cycle, in its most basic terms, includes the following steps: nitrogen gas is compressed, cooled, and then expanded in a turbo booster. During this expansion, the temperature of the gas drops and the expanding gas moves the turbine, which in turn performs work on the compressor of the turbo booster. The cold gas is then used to provide the necessary cooling to liquefy the target stream.
  • One problem with refrigeration cycles is that there are refrigerant losses. The mechanical equipment used in the process contains seals, which have gas losses to the atmosphere that must be made up. Although mechanical designs are available which recover a portion of these seal gas losses back to a low pressure stream within the refrigeration cycle, this does not completely eliminate the losses and can incur additional capital cost. One solution to this problem is shown in FIG. 1.
  • FIG. 1 represents typical nitrogen refrigeration cycle 1 that is useful for providing the necessary refrigeration to liquefy the target gas. Nitrogen gas 2 is partially compressed in turbo booster 10 (which is a combination of compressor 20 and turbine 30 in which the turning of turbine 30 helps to turn compressor 20) and then further compressed in high pressure compressor 40 and then partially cooled in a heat exchanger 50. Cooled compressed nitrogen 41 then exits the heat exchanger 50 and is expanded in turbine 30 of the turbo booster 10. Expanded refrigerant 32 is then used to provide refrigeration for a gas stream (not shown). During this set up, nitrogen is lost in the turbo booster 10 and high pressure compressor 40. These losses are made up by the introduction of gaseous nitrogen from LIN tank 60. Liquid nitrogen 62 is withdrawn from LIN tank 60 and vaporized in ambient vaporizer 64. Often, particularly in cold environments, ambient vaporizer 64 is supplemented with an electric heater which requires at least some utility cost or other type of vaporizer such as steam sparged water bath, natural gas fired water bath, electric, etc . . . Therefore, methods known heretofore may require additional utility cost. A first portion 66 is used to provide the makeup losses for high pressure compressor 40 and turbo booster 10 by injecting first portion 66 into the warm end of heat exchanger 50. A second portion can be used as utility nitrogen for other users (e.g., instrument, purge/utility gas for both this plant or another nearby plant).
  • However, there is a need for an improved refrigeration cycle that requires less power and/or makeup fluid.
  • SUMMARY OF THE INVENTION
  • The present invention is directed to a device and a method that satisfies at least one of these needs. Certain embodiments of the present invention relate to the use of an improved refrigeration cycle as part of a liquefaction process, in which makeup refrigerant is introduced on the cool side of the heat exchanger as opposed to the warm side of the heat exchanger.
  • In one embodiment, the method for producing a liquefied gas stream from an inlet gas feed stream can include the steps of:
  • cooling at least a portion of the inlet gas feed stream by heat exchange contact with an expanded refrigerant to produce the liquefied gas stream, wherein the expanded refrigerant is circulated in a refrigeration cycle; and
  • introducing a liquid refrigerant makeup stream into the refrigeration cycle by adding the liquid refrigerant makeup stream to the expanded refrigerant prior to heat exchange contact with the inlet gas feed stream to provide for makeup losses in the refrigeration cycle and to provide additional refrigeration to the refrigeration cycle.
  • In another embodiment, the inlet gas feed stream to be liquefied is natural gas. In another embodiment, the refrigeration cycle is a nitrogen refrigeration cycle and the liquid refrigerant makeup stream originates from a liquid nitrogen tank containing liquid nitrogen. In another embodiment, the expanded refrigerant is nitrogen. In another embodiment, the expanded refrigerant is expanded in a device selected from the group consisting of an expansion valve, a turbo-expander, and a liquid (or dense fluid) expander. In another embodiment, the method can further includes the steps of withdrawing a utility nitrogen stream from the nitrogen vapor stream subsequent to heat exchange contact with the inlet gas feed stream, and introducing the utility nitrogen stream to a second user for use as utility nitrogen.
  • In another embodiment, the method producing a liquefied gas stream from an inlet gas feed stream can include the steps of:
  • cooling at least a portion of the inlet gas feed stream by heat exchange contact with a nitrogen refrigeration cycle to produce the liquefied gas stream; and
  • adding a liquid refrigerant makeup stream into the expanded refrigerant prior to heat exchange contact with the inlet gas feed stream to provide for makeup losses in the nitrogen refrigeration cycle and to provide additional refrigeration to the nitrogen refrigeration cycle. In one embodiment, the nitrogen refrigeration cycle can include the steps of: expanding a nitrogen stream to a cold nitrogen vapor stream, cooling at least a portion of the inlet feed gas stream by heat exchange contact with the cold nitrogen vapor stream, compressing the cold nitrogen vapor stream to form a compressed nitrogen vapor stream, and cooling at least a portion of the compressed nitrogen vapor stream by heat exchange contact with the cold nitrogen vapor stream.
  • In another aspect of the invention, an apparatus for producing a liquefied gas stream from an inlet gas feed stream is provided. In one embodiment, the apparatus can include a heat exchanger, a refrigeration cycle, and a makeup liquid refrigerant tank. In one embodiment, the heat exchanger has a cold side and a warm side and is configured to receive the inlet gas feed stream and to produce the liquefied gas stream. In one embodiment, the refrigeration cycle is configured to provide refrigeration to the heat exchanger. Preferably, the refrigeration cycle further includes a compressor and an expander, wherein the compressor is configured to compress a refrigerant to a compression pressure, wherein the expander is configured to receive the compressed refrigerant and expand the compressed refrigerant to an expanded pressure to produce a cold refrigerant at an outlet of the expander, and wherein the outlet of the expander is in fluid communication with the cold side of the heat exchanger. In one embodiment, the makeup liquid refrigerant tank is configured to introduce a makeup liquid refrigerant with the cold refrigerant prior to heat exchange with the inlet gas feed stream.
  • In another embodiment, the makeup liquid refrigerant tank is in fluid communication with the refrigeration cycle at a point downstream the outlet of the expander and upstream the cold side of the heat exchanger. In another embodiment, the expander is a device selected from the group consisting of an expansion valve, a turbo-expander, and a liquid/dense fluid expander. In an additional embodiment, the apparatus can further include a utility nitrogen withdrawal line configured to withdraw a nitrogen stream from the refrigeration cycle at a point downstream the warm side of the heat exchanger and introduce the nitrogen stream to a second user for use as utility nitrogen.
  • Certain embodiments of the present invention advantageously do not require supplemental energy for the vaporization of the make up fluid.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • These and other features, aspects, and advantages of the present invention will become better understood with regard to the following description, claims, and accompanying drawings. It is to be noted, however, that the drawings illustrate only several embodiments of the invention and are therefore not to be considered limiting of the invention's scope as it can admit to other equally effective embodiments.
  • FIG. 1 shows a refrigeration cycle in accordance with the prior art.
  • FIG. 2 shows a refrigeration cycle in accordance with an embodiment of the invention.
  • FIG. 3 shows a liquefaction process in accordance with the prior art.
  • FIG. 4 shows a liquefaction process in accordance with an embodiment of the invention.
  • DETAILED DESCRIPTION
  • While the invention will be described in connection with several embodiments, it will be understood that it is not intended to limit the invention to those embodiments. On the contrary, it is intended to cover all the alternatives, modifications and equivalence as may be included within the spirit and scope of the invention defined by the appended claims.
  • Now turning to FIG. 2. Nitrogen refrigeration cycle 1 of FIG. 2 is largely similar to nitrogen refrigeration cycle 1 of FIG. 1, with the exception of the makeup nitrogen. In FIG. 2, LIN tank 60 is in fluid communication with the cold side of the heat exchanger. As such, liquid nitrogen 62 travels from LIN tank 60 and is combined with gaseous nitrogen 32 where liquid nitrogen 62 vaporizes. In one embodiment, the flow rate of liquid nitrogen 62 is about 1% of the flow rate of expanded refrigerant 32, thereby allowing liquid nitrogen 62 to vaporize when combining with expanded refrigerant 32 before going through heat exchanger 50. A small amount of second portion 68 can be withdrawn on the warm side of heat exchanger 50 in order to provide a makeup stream for nearby utilities. By combining liquid nitrogen 62 on the cold side of heat exchanger 50, additional refrigeration is provided to nitrogen refrigeration cycle 1, whereas the prior art loses this refrigeration in ambient vaporizer 64, which often must be supplemented with electric power (utility cost) in the form of an electric trim heater.
  • EXAMPLES
  • FIG. 3 represents another example as known in the prior art while FIG. 4 represents another embodiment of the present invention. These figures are used to show the comparative advantages of embodiments of the present invention.
  • Now turning to FIG. 3. Compressed nitrogen 42 exits high pressure compressor 40 and is split into two portions. First portion 44 is compressed in first turbo-booster 15 and then further compressed in second turbo-booster 25. Fully compressed nitrogen 27 is cooled in heat exchanger 50 and then expanded in second turbo-booster 25 to provide expanded first portion 34. Expanded first portion 34 is introduced into the cool side of heat exchanger 50 where it provides refrigeration to feed gas 48 in order to produce liquid feed 52. Feed gas 48 can be any gas that is desirable to liquefy, for example, natural gas. Expanded first portion 34 exits heat exchanger 50 and is recompressed in high pressure compressor 40 to start the cycle over again. During the same cycle, second portion 46 enters heat exchanger 50 and is only partially cooled before being expanded in first turbo-booster 15 to reduce both its pressure and temperature. Expanded second portion 36 is introduced to heat exchanger 50 to provide additional cooling before it combines with expanded first portion 34 on its way back to high pressure compressor 40.
  • As in FIG. 1, nitrogen is lost in first turbo-booster 15, second turbo-booster 25, and high pressure compressor 40. These losses are made up by the introduction of gaseous nitrogen 66 from LIN tank 60. Liquid nitrogen 62 is withdrawn from LIN tank 60 and vaporized in ambient vaporizer 64. A first portion 66 is used to provide the makeup losses for high pressure compressor 40 and turbo booster 10 by injecting first portion 66 into the warm end of heat exchanger 50. A second portion 68 can be used as utility nitrogen for other users (e.g., for makeup losses for a nearby air separation plant) or as instrument gas and/or purge gas for this plant and/or another nearby facility.
  • Now turning to FIG. 4. Nitrogen refrigeration cycle 3 of FIG. 4 is largely similar to nitrogen refrigeration cycle 3 of FIG. 3, with the exception of the makeup nitrogen. In FIG. 4, LIN tank 60 is in fluid communication with the cold side of the heat exchanger 50. As such, liquid nitrogen 62 travels from LIN tank 60 and is combined with expanded refrigerant 34, where it vaporizes.
  • Simulations were run for the processes shown in FIG. 3 and FIG. 4 for liquefying a natural gas stream having a flow rate of 3,265 Nm3/hr. The results can be found in Table I below:
  • TABLE I
    Simulation Results
    FIG. 3 FIG. 4 % Change
    Nitrogen flow leaving High 22613 20797 8%
    Pressure Compressor (Nm3/hr)
    Loss if First Turbo-booster 68 68
    (Nm3/hr)
    Loss in Second Turbo-booster 68 68
    (Nm3/hr)
    Loss in High Pressure 102 102
    Compressor (Nm3/hr)
    Utility Usage (kW) 1213 1112 8%
    Total Make-up LIN (Nm3/hr) 338 338
    LIN added to Recycle (Nm3/hr) 238 238
    LIN sent to Utilities (Nm3/hr) 100 100
  • As is clearly shown in Table I, embodiments of the present invention can achieve approximately an 8% improvement over methods and apparatus of the prior art. This is extremely beneficial as embodiments of the present invention can provide a cost savings on both the capital cost because of the reduced size of the refrigeration cycle equipment and on the energy required to run the high pressure compressor.
  • While the invention has been described in conjunction with specific embodiments thereof, it is evident that many alternatives, modifications, and variations will be apparent to those skilled in the art in light of the foregoing description. Accordingly, it is intended to embrace all such alternatives, modifications, and variations as fall within the spirit and broad scope of the appended claims. The present invention may suitably comprise, consist or consist essentially of the elements disclosed and may be practiced in the absence of an element not disclosed. Furthermore, language referring to order, such as first and second, should be understood in an exemplary sense and not in a limiting sense. For example, it can be recognized by those skilled in the art that certain steps or devices can be combined into a single step/device.
  • The singular forms “a”, “an”, and “the” include plural referents, unless the context clearly dictates otherwise.
  • Optional or optionally means that the subsequently described event or circumstances may or may not occur. The description includes instances where the event or circumstance occurs and instances where it does not occur.
  • Ranges may be expressed herein as from about one particular value, and/or to about another particular value. When such a range is expressed, it is to be understood that another embodiment is from the one particular value and/or to the other particular value, along with all combinations within said range.

Claims (9)

We claim:
1. A method for producing a liquefied gas stream from an inlet gas feed stream, the method comprising the steps of:
cooling at least a portion of the inlet gas feed stream by heat exchange contact with an expanded refrigerant to produce the liquefied gas stream, wherein the expanded refrigerant is circulated in a refrigeration cycle; and
introducing a liquid refrigerant makeup stream into the refrigeration cycle by adding the liquid refrigerant makeup stream to the expanded refrigerant prior to heat exchange contact with the inlet gas feed stream to provide for makeup losses in the refrigeration cycle and to provide additional refrigeration to the refrigeration cycle.
2. The method as claimed in claim 1, wherein the inlet gas feed stream is natural gas.
3. The method as claimed in claim 1, wherein the refrigeration cycle is a nitrogen refrigeration cycle and the liquid refrigerant makeup stream originates from a liquid nitrogen tank.
4. The method as claimed in claim 1, wherein the expanded refrigerant is nitrogen.
5. The method as claimed in claim 1, wherein the expanded refrigerant is expanded in a device selected from the group consisting of an expansion valve, a turbo-expander, and a liquid expander.
6. The method as claimed in claim 1, further comprising the steps of withdrawing a utility nitrogen stream from the expanded refrigerant subsequent to heat exchange contact with the inlet gas feed stream; and introducing the utility nitrogen stream to a second user for use as utility nitrogen.
7. A method for producing a liquefied gas stream from an inlet gas feed stream, the method comprising the steps of:
cooling at least a portion of the inlet gas feed stream by heat exchange contact with a nitrogen refrigeration cycle to produce the liquefied gas stream; and
adding a liquid refrigerant makeup stream into the expanded refrigerant prior to heat exchange contact with the inlet gas feed stream to provide for makeup losses in the nitrogen refrigeration cycle and to provide additional refrigeration to the nitrogen refrigeration cycle,
wherein the nitrogen refrigeration cycle comprises the steps of:
expanding a nitrogen stream to a nitrogen vapor stream;
cooling at least a portion of the inlet feed gas stream by heat exchange contact with the nitrogen vapor stream;
compressing the nitrogen vapor stream to form a compressed nitrogen vapor stream; and
cooling at least a portion of the compressed nitrogen vapor stream by heat exchange contact with the nitrogen vapor stream.
8. The method as claimed in claim 7, wherein the expanded refrigerant is expanded in a device selected from the group consisting of an expansion valve, a turbo-expander, and a liquid expander.
9. The method as claimed in claim 7, further comprising the steps of withdrawing a utility nitrogen stream from the nitrogen vapor stream subsequent to heat exchange contact with the inlet gas feed stream; and introducing the utility nitrogen stream to a second user for use as utility nitrogen.
US13/707,132 2012-12-06 2012-12-06 Method for improved thermal performing refrigeration cycle Abandoned US20140157824A1 (en)

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WO2017103536A1 (en) * 2015-12-17 2017-06-22 Engie Hybrid method for liquefying a fuel gas and facility for implementing same
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US20180038643A1 (en) * 2016-08-05 2018-02-08 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Method for the integration of liquefied natural gas and syngas production
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Publication number Priority date Publication date Assignee Title
FR3027376A1 (en) * 2014-10-15 2016-04-22 Cryostar Sas REFRIGERATION DEVICE, FOR EXAMPLE FOR A SYSTEM FOR PRODUCING LIQUEFIED GAS, COMPRISING AT LEAST ONE ROTATING MACHINE WITH A GAS SEAL
WO2017103536A1 (en) * 2015-12-17 2017-06-22 Engie Hybrid method for liquefying a fuel gas and facility for implementing same
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WO2021063429A1 (en) * 2019-10-04 2021-04-08 GasNet, s.r.o. Natural gas processing plant

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