EP2336677A1 - Refrigeration system and method - Google Patents

Refrigeration system and method Download PDF

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Publication number
EP2336677A1
EP2336677A1 EP09015486A EP09015486A EP2336677A1 EP 2336677 A1 EP2336677 A1 EP 2336677A1 EP 09015486 A EP09015486 A EP 09015486A EP 09015486 A EP09015486 A EP 09015486A EP 2336677 A1 EP2336677 A1 EP 2336677A1
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EP
European Patent Office
Prior art keywords
compressor
refrigerant fluid
compressors
turboexpander
directly connected
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP09015486A
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German (de)
French (fr)
Inventor
Hans-Gerd Kölscheid
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens AG
Original Assignee
Siemens AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens AG filed Critical Siemens AG
Priority to EP09015486A priority Critical patent/EP2336677A1/en
Priority to PCT/EP2010/069756 priority patent/WO2011073255A1/en
Publication of EP2336677A1 publication Critical patent/EP2336677A1/en
Withdrawn legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B27/00—Machines, plants or systems, using particular sources of energy
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/06—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using expanders
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/0002—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the fluid to be liquefied
    • F25J1/0022—Hydrocarbons, e.g. natural gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/003—Processes 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
    • F25J1/0047—Processes 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
    • F25J1/005—Processes 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/006—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the refrigerant fluid used
    • F25J1/007—Primary atmospheric gases, mixtures thereof
    • F25J1/0072—Nitrogen
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02—Processes 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
    • F25J1/0203—Processes 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
    • F25J1/0204—Processes 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02—Processes 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
    • F25J1/0243—Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0279—Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc.
    • F25J1/0281—Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc. characterised by the type of prime driver, e.g. hot gas expander
    • F25J1/0283—Gas turbine as the prime mechanical driver
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02—Processes 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
    • F25J1/0243—Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0279—Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc.
    • F25J1/0281—Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc. characterised by the type of prime driver, e.g. hot gas expander
    • F25J1/0284—Electrical motor as the prime mechanical driver
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02—Processes 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
    • F25J1/0243—Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0279—Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc.
    • F25J1/0285—Combination of different types of drivers mechanically coupled to the same refrigerant compressor, possibly split on multiple compressor casings
    • F25J1/0287—Combination of different types of drivers mechanically coupled to the same refrigerant compressor, possibly split on multiple compressor casings including an electrical motor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02—Processes 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
    • F25J1/0243—Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0279—Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc.
    • F25J1/0285—Combination of different types of drivers mechanically coupled to the same refrigerant compressor, possibly split on multiple compressor casings
    • F25J1/0288—Combination 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02—Processes 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
    • F25J1/0243—Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0279—Compression of refrigerant or internal recycle fluid, e.g. kind of compressor, accumulator, suction drum etc.
    • F25J1/0298—Safety aspects and control of the refrigerant compression system, e.g. anti-surge control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2220/00—Processes or apparatus involving steps for the removal of impurities
    • F25J2220/60—Separating impurities from natural gas, e.g. mercury, cyclic hydrocarbons
    • F25J2220/64—Separating heavy hydrocarbons, e.g. NGL, LPG, C4+ hydrocarbons or heavy condensates in general
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2230/00—Processes or apparatus involving steps for increasing the pressure of gaseous process streams
    • F25J2230/20—Integrated compressor and process expander; Gear box arrangement; Multiple compressors on a common shaft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25J—LIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2270/00—Refrigeration techniques used
    • F25J2270/14—External refrigeration with work-producing gas expansion loop
    • F25J2270/16—External refrigeration with work-producing gas expansion loop with mutliple gas expansion loops of the same refrigerant

Definitions

  • the present invention relates to a refrigeration system.
  • a refrigeration system may be used, for example, for liquefaction of gaseous hydrocarbon fuels, such as natural gas.
  • gaseous hydrocarbon fuels such as natural gas are liquefied to reduce their volume for easier transportation and storage.
  • the liquefaction involves a refrigeration process, wherein a refrigerant fluid, typically comprising nitrogen, is circulated in a refrigeration cycle.
  • a typical refrigeration cycle involves compressing the refrigerant in successive compressor stages, partially cooling the refrigerant at a relatively constant pressure and then expanding the refrigerant in one or more expander stages resulting in a temperature drop of the refrigerant.
  • the cooled refrigerant and the gaseous fuel are passed through a cryogenic heat exchanger, wherein the refrigerant absorbs heat from the gaseous fuel resulting in liquefaction of the gaseous fuel.
  • the refrigerant exiting the heat exchanger is passed back to the compressor stages, whereby the above cycle is repeated.
  • Some existing refrigeration systems are known to use integrally geared compressor stages for successive compression of the refrigerant, along with turboexpanders for expanding the refrigerant.
  • the axial load or thrust on the transmission gear train lead to increased vibration of the transmission gear train, loss of power and a reduction in overall efficiency of the system.
  • the axial load or thrust increases with increase in the number of compressor stages, this leads to a limitation of the total number compressor stages, thus limiting the refrigerating capacity of the system.
  • the objective of the present invention is to minimize load on the transmission gear train for refrigeration systems involving geared compressor stages and one or more turboexpanders.
  • the underlying idea of the present invention is to compensate loads on the transmission (i.e., the gear train) of integrally geared compressor stages by directly connecting one of the compressors to the drive and directly connecting one or more other compressor to a respective turboexpander.
  • This has the advantage that power consumption of a compressor and the power output of the respective turboexpander connected thereto now compensate each other, so that the transmission has to transmit only the difference. This leads to reduced power loss and greater overall efficiency of the system.
  • the proposed system includes a plurality of compressors in addition to said first compressor, operable for compressing said refrigerant fluid in successive stages of compression, and a plurality of turboexpanders operable to expand portions of the refrigerant fluid downstream of said compressors, said system further characterized in that
  • the proposed system is further characterized in that one or more turboexpanders are operable such that the mechanical power output of each of said one or more turboexpanders balances power consumption by a respective compressor directly connected thereto. This leads to a further reduction in the power transmitted by the transmission, which reduces mechanical load on the transmission.
  • the proposed system is further characterized in that each compressor and the drive or turboexpander connected thereto are arranged on opposite sides of said transmission gear train.
  • the proposed system is further characterized in that one or more of said turboexpanders comprise inlet guide vanes, said inlet guide vanes being adjustable to regulate flow of the refrigerant fluid through a respective compressor directly connected thereto.
  • said turboexpanders comprise inlet guide vanes, said inlet guide vanes being adjustable to regulate flow of the refrigerant fluid through a respective compressor directly connected thereto.
  • said drive comprises a gas turbine.
  • a starter-helper motor is drivingly coupled to said transmission gear train. The starter-helper motor can be used to facilitate starting of the gas turbine drive and to further boost the rated power output of the gas turbine drive at higher ambient temperatures prevailing at most gas liquefaction plants.
  • the system 1 includes a plurality of compressors, in this example, a first compressor 2a and a second compressor 2b, and includes at least one turboexpander 4a.
  • the first compressor 2a is directly connected to a drive 3 by means of a first shaft 5a.
  • the second compressor 2b is directly connected to the turboexpander 4a by means of a second shaft 5b.
  • the first shaft 5a and the second shaft 5b are drivingly coupled by a transmission gear train 6.
  • the drive 3 provides power to the transmission gear train 6.
  • the drive 3 includes a gas turbine. Alternately, the drive 3 may include an electrical motor.
  • the compressors 2a and 2b compress a stream 10 of the refrigerant fluid in successive stages of compression. Downstream of the compressors 2a and 2b, a stream 10i of the refrigerant fluid is partially cooled and subsequently expanded by the turboexpander 4a, which resultantly produces a mechanical power output, which, in turn, is used to drive the second compressor 2b connected to the turboexpander 4a.
  • the proposed arrangement has the advantage that power consumption of the compressor 2b and the power output of the turboexpander 4a now compensate each other, so that the gear train 6 has to transmit only the difference. This leads to reduced power loss and greater overall efficiency of the system 1.
  • the turboexpander 4a is operated such that the mechanical power output of the turboexpander 4a balances the power consumption of the second compressor 2b, i.e. the power output of the turboexpander 4a and the power consumption of the second compressor 2b are substantially equal. Since the power transmitted by gear train 6 from the second shaft 5b is a difference of the power output of the turboexpander 4a and the power consumed by the second compressor 2b, the above arrangement leads to a significant reduction in the power transmitted by the gear train 6, which reduces mechanical load on the gear train 6. Further preferably, as shown, the first compressor 2a and the drive 3 are arranged on opposite sides of the transmission gear train 6, and the second compressor 2b and the expander 4a are arranged on opposite sides of the transmission gear train 6. The above arrangement has the advantage that the axial load or thrust on the gear train 6 by compressors 2a and 2b are respectively compensated by the drive 3 and the turboexpander 4a.
  • a starter-helper motor 9 is drivingly coupled to the gear train 6.
  • the starter-helper motor 9 can be used to facilitate starting of the gas turbine 3 and to further boost the rated power output of the gas turbine 3 at higher ambient temperatures prevailing at most gas liquefaction plants.
  • the turboexpander 4a includes adjustable inlet guide vanes 8c to control power output of the turboexpander 4a, and, in turn, the flow of refrigerant fluid through the second compressor 2b.
  • the flow of refrigerant fluid through the first compressor 2a may be controlled by adjustable inlet guide vanes 8c provided on the suction end of the compressor 2a.
  • the inlet guide vanes 8a and 8c may controlled, individually, or in combination for regulating the refrigerant flow rate through the compressors and hence, the regulating the refrigerating capacity of the system 1. This provides simplicity to the refrigeration process obviating the need for cut-off valves and complicated piping.
  • a stream 10 of the refrigerant fluid is compressed in a first stage of compression by the first compressors 2a.
  • the compressed stream 10a of the refrigerant fluid flowing out of the first compressor 2a is cooled by a first aftercooler 7a and a cooled stream 10b of the refrigerant fluid is further compressed in a second stage of compression by the second compressor 2b.
  • the compressed refrigerant fluid 10c flowing out of the second compressor 2b is optionally cooled by a second aftercooler 7b.
  • the refrigerant fluid stream 10g flowing out of the aftercooler 7b is partially cooled in a heat exchanger 11, against a low temperature, low pressure returning stream 10j of the refrigerant fluid.
  • the partially cooled refrigerant fluid stream 10i is expanded by the turboexpander 4a, resulting in a drop in temperature and pressure of the refrigerant fluid.
  • expansion of the refrigerant fluid by the turboexpander 4a produces mechanical power, which is transmitted to the second compressor 2b through the shaft 5b.
  • the refrigerant fluid stream 10j exiting the expander at low temperature and pressure is passed to the heat exchanger 11, wherein it absorbs heat from the stream 10g of refrigerant fluid downstream of the compressor stages to partially cool the refrigerant fluid prior to expansion by the turboexpander 4a.
  • a stream 13 of natural gas is passed through the heat exchanger 11, wherein it is cooled and subsequently liquefied by heat transfer to the refrigerant fluid stream 10j.
  • liquefaction may be achieved by cooling the stream 13 of natural gas over multiple stages.
  • a liquefied stream 13a of natural gas coming out of the heat exchanger 11 is passed into a separator 12.
  • the liquefied stream 13a is expanded by a throttle valve 14, wherein the liquefied gas is flashed to a lower pressure.
  • the flashed vapors 13e from the expansion are separated and are generally collected for re-liquefaction.
  • the present invention may also be used for refrigeration systems having more than two compressors, and multiple turboexpanders, for increased refrigerating capacity.
  • the first compressor stage may be directly connected to the drive by a shaft, and each of the other compressors directly connected to a respective turboexpander via separate shafts, the shafts being drivingly coupled by a transmission gear train.
  • FIG 2 illustrates an example of a refrigeration system 1 having three compressors 2a, 2b and 2c and two expanders 4a and 4b.
  • the arrangement of the compressors 2a and 2b with respect to the drive 3 and the first turboexpander 4a are similar to that of the earlier mentioned embodiment ( FIG 1 ).
  • a third compressor 2c is directly connected to a second turboexpander 4b by a third shaft 5c.
  • the shafts 5a, 5b and 5c are drivingly coupled by the gear train 6.
  • the power consumptions by the compressors 2b and 2c and the power outputs of the turboexpanders 4a and 4b respectively compensate each other, leading to reduced load on the gear train 6.
  • each of the turboexpanders 4a and 4b is operated such that their mechanical power output balance (i.e., are substantially equal to) the power consumption of the respective compressors 2b and 2c, thereby significantly reducing the power to be transmitted by the gear train 6.
  • each of the compressors and the corresponding turboexpander/drive are arranged on opposite sides of the transmission gear train 6 for compensation of axial load or thrusts on the gear train 6.
  • refrigerant fluid flow and hence the refrigerating capacity of the system 1 may be regulated by controlling, individually or in combination, adjustable inlet guide vanes 8a, 8b and 8c provided respectively on the inlets of the turboexpanders 4a and 4b and the compressor 2a.
  • a stream 10 of the refrigerant fluid is compressed in a first stage of compression by the first compressors 2a.
  • the compressed stream 10a of the refrigerant fluid flowing out of the first compressor 2a is cooled by a first aftercooler 7a and a cooled stream 10b of the refrigerant fluid is further compressed in a second stage of compression by the second compressor 2b.
  • the compressed refrigerant fluid 10c flowing out of the second compressor 2b is optionally cooled by a second aftercooler 7b.
  • the refrigerant fluid stream 10d flowing out of the aftercooler 7b is further compressed in a third stage of compression by the third compressor 2c.
  • the compressed refrigerant fluid 10e flowing out of the third compressor 2c is optionally cooled by a third aftercooler 7c.
  • the refrigerant fluid stream 10f flowing out of the third aftercooler 7c is divided into two stream portions 10g and 10h and passed into the heat exchanger 11.
  • the first divided stream 10g is partially cooled in the heat exchanger 11 against a low temperature, low pressure returning stream 10n of the refrigerant fluid.
  • the stream 10g exits the heat exchanger as a partially cooled refrigerant stream 10i, which is expanded by the turboexpander 4a to result in a drop in temperature and pressure of the refrigerant.
  • embodiments of the present invention may also include refrigeration systems having more than three compressors and more than two turboexpanders, as may be necessary, for example, for providing a required refrigerating capacity. It is therefore contemplated that all such embodiments are within the scope of the present invention as defined by the below-mentioned patent claims.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Separation By Low-Temperature Treatments (AREA)

Abstract

A refrigeration system (1) for circulating a refrigerant fluid (10) comprises a first compressor (2a) and a second compressor (2b) operable to compress said refrigerant fluid (10) in separate stages of compression and at least one turboexpander (4a) operable to expand at least a portion (10i) of the refrigerant fluid downstream of said compressors (2a,2b). In accordance with the present invention, a drive (3) is directly connected to the first compressor (2a) by a first shaft (5a), the turboexpander (4a) is directly connected to the second compressor (2b) by a second shaft (5b) and is operable to drive the second compressor (2b) by a mechanical power output resultant from said expansion and the first shaft (5a) is drivingly coupled to the second shaft (5b) by a transmission gear train (6).

Description

  • The present invention relates to a refrigeration system. Such a system may be used, for example, for liquefaction of gaseous hydrocarbon fuels, such as natural gas.
  • Generally, gaseous hydrocarbon fuels, such as natural gas are liquefied to reduce their volume for easier transportation and storage. The liquefaction involves a refrigeration process, wherein a refrigerant fluid, typically comprising nitrogen, is circulated in a refrigeration cycle. A typical refrigeration cycle involves compressing the refrigerant in successive compressor stages, partially cooling the refrigerant at a relatively constant pressure and then expanding the refrigerant in one or more expander stages resulting in a temperature drop of the refrigerant. The cooled refrigerant and the gaseous fuel are passed through a cryogenic heat exchanger, wherein the refrigerant absorbs heat from the gaseous fuel resulting in liquefaction of the gaseous fuel. The refrigerant exiting the heat exchanger is passed back to the compressor stages, whereby the above cycle is repeated.
  • Some existing refrigeration systems are known to use integrally geared compressor stages for successive compression of the refrigerant, along with turboexpanders for expanding the refrigerant. However, in such systems, the axial load or thrust on the transmission gear train lead to increased vibration of the transmission gear train, loss of power and a reduction in overall efficiency of the system. Further, since the axial load or thrust increases with increase in the number of compressor stages, this leads to a limitation of the total number compressor stages, thus limiting the refrigerating capacity of the system.
  • The objective of the present invention is to minimize load on the transmission gear train for refrigeration systems involving geared compressor stages and one or more turboexpanders.
  • The above object is achieved by the system according to claim 1 and the method according to claim 9.
  • The underlying idea of the present invention is to compensate loads on the transmission (i.e., the gear train) of integrally geared compressor stages by directly connecting one of the compressors to the drive and directly connecting one or more other compressor to a respective turboexpander. This has the advantage that power consumption of a compressor and the power output of the respective turboexpander connected thereto now compensate each other, so that the transmission has to transmit only the difference. This leads to reduced power loss and greater overall efficiency of the system.
  • In one example embodiment, the proposed system includes a plurality of compressors in addition to said first compressor, operable for compressing said refrigerant fluid in successive stages of compression, and a plurality of turboexpanders operable to expand portions of the refrigerant fluid downstream of said compressors, said system further
    characterized in that
    • each of said plurality of turboexpanders is directly connected to one of the compressors of said plurality of compressors by a respective shaft, each of said plurality of turboexpanders operable to drive the respective compressor directly connected thereto by a mechanical power output resultant of said expansions, and
    • said shafts are drivingly coupled by the transmission gear train. Thus any number of compressor trains can be used for increase in the refrigerating capacity of the system, without a substantial increase in load on the transmission, due to the power compensation as mentioned above.
  • In an advantageous embodiment, the proposed system is further characterized in that one or more turboexpanders are operable such that the mechanical power output of each of said one or more turboexpanders balances power consumption by a respective compressor directly connected thereto. This leads to a further reduction in the power transmitted by the transmission, which reduces mechanical load on the transmission.
  • In a preferred embodiment, to further compensate axial load or thrust on the transmission, the proposed system is further characterized in that each compressor and the drive or turboexpander connected thereto are arranged on opposite sides of said transmission gear train.
  • In a preferred embodiment, the proposed system is further characterized in that one or more of said turboexpanders comprise inlet guide vanes, said inlet guide vanes being adjustable to regulate flow of the refrigerant fluid through a respective compressor directly connected thereto. This provides simplicity to the refrigeration process wherein the refrigerating capacity of the system can be regulated by adjusting the inlet guide vanes, obviating the need for cut-off valves and complicated piping.
  • In an exemplary embodiment, said drive comprises a gas turbine. In a further embodiment, a starter-helper motor is drivingly coupled to said transmission gear train. The starter-helper motor can be used to facilitate starting of the gas turbine drive and to further boost the rated power output of the gas turbine drive at higher ambient temperatures prevailing at most gas liquefaction plants.
  • The present invention is further described hereinafter with reference to illustrated embodiments shown in the accompanying drawings, in which:
    • FIG 1 is a block diagram of a refrigeration system involving two compressors and an expander, according to one embodiment of the present invention, and
    • FIG 2 is a block diagram of a refrigeration system involving three compressors and two expanders, according to another embodiment of the present invention.
  • Embodiments of the present invention provide a refrigeration system involving integrally geared compressors with expander stages used for circulating a refrigerant fluid, wherein the system has an arrangement that results in reduced power transmission and compensation of axial load or thrusts on the gear train. Embodiments of the present invention illustrated below deal with a refrigeration system used in liquefaction of a gaseous hydrocarbon, more particularly, to liquefaction of natural gas. However, it is to be understood that the underlying inventive principle may used for any other application.
  • Referring now to FIG 1 is illustrated a refrigeration system 1 for circulating a refrigerant fluid, typically comprising nitrogen, in accordance with one embodiment of the present invention. The system 1 includes a plurality of compressors, in this example, a first compressor 2a and a second compressor 2b, and includes at least one turboexpander 4a. The first compressor 2a is directly connected to a drive 3 by means of a first shaft 5a. The second compressor 2b is directly connected to the turboexpander 4a by means of a second shaft 5b. The first shaft 5a and the second shaft 5b are drivingly coupled by a transmission gear train 6. The drive 3 provides power to the transmission gear train 6. In the illustrated embodiment, the drive 3 includes a gas turbine. Alternately, the drive 3 may include an electrical motor. The compressors 2a and 2b compress a stream 10 of the refrigerant fluid in successive stages of compression. Downstream of the compressors 2a and 2b, a stream 10i of the refrigerant fluid is partially cooled and subsequently expanded by the turboexpander 4a, which resultantly produces a mechanical power output, which, in turn, is used to drive the second compressor 2b connected to the turboexpander 4a. The proposed arrangement has the advantage that power consumption of the compressor 2b and the power output of the turboexpander 4a now compensate each other, so that the gear train 6 has to transmit only the difference. This leads to reduced power loss and greater overall efficiency of the system 1.
  • In a preferred embodiment, the turboexpander 4a is operated such that the mechanical power output of the turboexpander 4a balances the power consumption of the second compressor 2b, i.e. the power output of the turboexpander 4a and the power consumption of the second compressor 2b are substantially equal. Since the power transmitted by gear train 6 from the second shaft 5b is a difference of the power output of the turboexpander 4a and the power consumed by the second compressor 2b, the above arrangement leads to a significant reduction in the power transmitted by the gear train 6, which reduces mechanical load on the gear train 6. Further preferably, as shown, the first compressor 2a and the drive 3 are arranged on opposite sides of the transmission gear train 6, and the second compressor 2b and the expander 4a are arranged on opposite sides of the transmission gear train 6. The above arrangement has the advantage that the axial load or thrust on the gear train 6 by compressors 2a and 2b are respectively compensated by the drive 3 and the turboexpander 4a.
  • In the illustrated embodiment, a starter-helper motor 9 is drivingly coupled to the gear train 6. Advantageously, the starter-helper motor 9 can be used to facilitate starting of the gas turbine 3 and to further boost the rated power output of the gas turbine 3 at higher ambient temperatures prevailing at most gas liquefaction plants.
  • In an advantageous embodiment of the present invention, the turboexpander 4a includes adjustable inlet guide vanes 8c to control power output of the turboexpander 4a, and, in turn, the flow of refrigerant fluid through the second compressor 2b. Also, the flow of refrigerant fluid through the first compressor 2a may be controlled by adjustable inlet guide vanes 8c provided on the suction end of the compressor 2a. Advantageously, the inlet guide vanes 8a and 8c may controlled, individually, or in combination for regulating the refrigerant flow rate through the compressors and hence, the regulating the refrigerating capacity of the system 1. This provides simplicity to the refrigeration process obviating the need for cut-off valves and complicated piping.
  • Referring to FIG 1, in operation, a stream 10 of the refrigerant fluid is compressed in a first stage of compression by the first compressors 2a. Optionally, the compressed stream 10a of the refrigerant fluid flowing out of the first compressor 2a is cooled by a first aftercooler 7a and a cooled stream 10b of the refrigerant fluid is further compressed in a second stage of compression by the second compressor 2b. The compressed refrigerant fluid 10c flowing out of the second compressor 2b is optionally cooled by a second aftercooler 7b. The refrigerant fluid stream 10g flowing out of the aftercooler 7b is partially cooled in a heat exchanger 11, against a low temperature, low pressure returning stream 10j of the refrigerant fluid. The partially cooled refrigerant fluid stream 10i is expanded by the turboexpander 4a, resulting in a drop in temperature and pressure of the refrigerant fluid. As mentioned earlier, expansion of the refrigerant fluid by the turboexpander 4a produces mechanical power, which is transmitted to the second compressor 2b through the shaft 5b. The refrigerant fluid stream 10j exiting the expander at low temperature and pressure is passed to the heat exchanger 11, wherein it absorbs heat from the stream 10g of refrigerant fluid downstream of the compressor stages to partially cool the refrigerant fluid prior to expansion by the turboexpander 4a. For liquefaction of natural gas, a stream 13 of natural gas is passed through the heat exchanger 11, wherein it is cooled and subsequently liquefied by heat transfer to the refrigerant fluid stream 10j. Although not explicitly shown, liquefaction may be achieved by cooling the stream 13 of natural gas over multiple stages. In this example, a liquefied stream 13a of natural gas coming out of the heat exchanger 11 is passed into a separator 12. Herein, the liquefied stream 13a is expanded by a throttle valve 14, wherein the liquefied gas is flashed to a lower pressure. The flashed vapors 13e from the expansion are separated and are generally collected for re-liquefaction. After expansion, a portion liquefied gas 13d containing hydrocarbons of higher molecular weight than methane may be separated from the liquefied natural gas, to produce a pipeline gas predominantly comprising methane. A stream 13b of liquefied natural gas after expansion through the throttle valve 14 is passed again to the heat exchanger 11 for a further stage of cooling via heat transfer to the refrigerant stream 10j, whereby a stream 13c of further cooled liquefied natural exits the heat exchanger 11, which may be subsequently passed to a storage tank (not shown). The refrigerant stream 10 exiting the heat exchanger 11 re-enters the first stage compressor 2a and the above cycle is repeated.
  • The present invention may also be used for refrigeration systems having more than two compressors, and multiple turboexpanders, for increased refrigerating capacity. In such a case, the first compressor stage may be directly connected to the drive by a shaft, and each of the other compressors directly connected to a respective turboexpander via separate shafts, the shafts being drivingly coupled by a transmission gear train. FIG 2 illustrates an example of a refrigeration system 1 having three compressors 2a, 2b and 2c and two expanders 4a and 4b. The arrangement of the compressors 2a and 2b with respect to the drive 3 and the first turboexpander 4a are similar to that of the earlier mentioned embodiment (FIG 1). Additionally herein (FIG 2), a third compressor 2c is directly connected to a second turboexpander 4b by a third shaft 5c. The shafts 5a, 5b and 5c are drivingly coupled by the gear train 6. Herein the power consumptions by the compressors 2b and 2c and the power outputs of the turboexpanders 4a and 4b respectively compensate each other, leading to reduced load on the gear train 6. Further in a preferred embodiment, each of the turboexpanders 4a and 4b is operated such that their mechanical power output balance (i.e., are substantially equal to) the power consumption of the respective compressors 2b and 2c, thereby significantly reducing the power to be transmitted by the gear train 6. Further preferably, as shown, each of the compressors and the corresponding turboexpander/drive are arranged on opposite sides of the transmission gear train 6 for compensation of axial load or thrusts on the gear train 6. Further, similar to the earlier illustrated embodiment, refrigerant fluid flow and hence the refrigerating capacity of the system 1 may be regulated by controlling, individually or in combination, adjustable inlet guide vanes 8a, 8b and 8c provided respectively on the inlets of the turboexpanders 4a and 4b and the compressor 2a.
  • In operation of the system 1 of FIG 2, a stream 10 of the refrigerant fluid is compressed in a first stage of compression by the first compressors 2a. Optionally, the compressed stream 10a of the refrigerant fluid flowing out of the first compressor 2a is cooled by a first aftercooler 7a and a cooled stream 10b of the refrigerant fluid is further compressed in a second stage of compression by the second compressor 2b. The compressed refrigerant fluid 10c flowing out of the second compressor 2b is optionally cooled by a second aftercooler 7b. The refrigerant fluid stream 10d flowing out of the aftercooler 7b is further compressed in a third stage of compression by the third compressor 2c. The compressed refrigerant fluid 10e flowing out of the third compressor 2c is optionally cooled by a third aftercooler 7c. The refrigerant fluid stream 10f flowing out of the third aftercooler 7c is divided into two stream portions 10g and 10h and passed into the heat exchanger 11. The first divided stream 10g is partially cooled in the heat exchanger 11 against a low temperature, low pressure returning stream 10n of the refrigerant fluid. The stream 10g exits the heat exchanger as a partially cooled refrigerant stream 10i, which is expanded by the turboexpander 4a to result in a drop in temperature and pressure of the refrigerant. The second divided stream 10h is further cooled in the heat exchanger 11 against the low temperature, low pressure returning stream 10n of the refrigerant fluid. The stream 10h exits the heat exchanger as a further cooled refrigerant stream 10k, which is expanded by the turboexpander 4b to result in a further drop in temperature and pressure of the refrigerant. The refrigerant streams 10j and 101 exiting the turboexpanders 4a and 4b respectively are then merged into a low temperature, low pressure refrigerant stream in the heat exchanger 11, which is further used to for liquefaction of a stream 13 of natural gas described above.
  • Although the invention has been described with reference to specific embodiments, this description is not meant to be construed in a limiting sense. Various modifications of the disclosed embodiments, as well as alternate embodiments of the invention, will become apparent to persons skilled in the art upon reference to the description of the invention. For example, it may be appreciated by one skilled in the art that embodiments of the present invention may also include refrigeration systems having more than three compressors and more than two turboexpanders, as may be necessary, for example, for providing a required refrigerating capacity. It is therefore contemplated that all such embodiments are within the scope of the present invention as defined by the below-mentioned patent claims.

Claims (15)

  1. A refrigeration system (1) for circulating a refrigerant fluid (10), comprising a first compressor (2a) and a second compressor (2b) operable to compress said refrigerant fluid (10) in separate stages of compression and at least one turboexpander (4a) operable to expand at least a portion (10i) of the refrigerant fluid downstream of said compressors (2a,2b), the system (1) characterized in that
    - a drive (3) is directly connected to the first compressor (2a) by a first shaft (5a),
    - the turboexpander (4a) is directly connected to the second compressor (2b) by a second shaft (5b) and is operable to drive the second compressor (2b) by a mechanical power output resultant from said expansion, and
    - the first shaft (5a) is drivingly coupled to the second shaft (5b) by a transmission gear train (6).
  2. The system (1) according any of the preceding claims, comprising a plurality of compressors (2b,2c) in addition to said first compressor (2a), operable for compressing said refrigerant fluid (10) in separate stages of compression, and a plurality of turboexpanders (4a,4b) operable to expand portions (10i, 10k) of the refrigerant fluid downstream of said compressors (2a,2b,2c), said system (1) further characterized in that
    - each of said plurality of turboexpanders (4a,4b) is directly connected to one of the compressors (2b,2c) of said plurality of compressors (2b,2c) by a respective shaft (5b, 5c), each of said plurality of turboexpanders (4a,4b) operable to drive the respective compressor (2b,2c) directly connected thereto by a mechanical power output resultant of said expansions, and
    - said shafts (5a,5b,5c) are drivingly coupled by the transmission gear train (6).
  3. The system (1) according to any of the preceding claims, further characterized in that one or more turboexpanders (4a,4b) are operable such that the mechanical power output of each of said one or more turboexpanders (4a,4b) balances power consumption by a respective compressor (2b,2c) directly connected thereto.
  4. The system (1) according to any of the preceding claims, further characterized in that each compressor (2a,2b,2c) and the drive (3) or turboexpander (4a,4b) connected thereto are arranged on opposite sides of said transmission gear train (6).
  5. The system (1) according to any of the preceding claims, further characterized in that one or more of said turboexpanders (4a,4b) comprise inlet guide vanes (8a,8b), said inlet guide vanes (8a) being adjustable to regulate flow of the refrigerant fluid through a respective compressor (2b,2c) directly connected thereto.
  6. The system (1) according to any of the preceding claims, wherein said drive (3) comprises a gas turbine.
  7. The system (1) according to claim 6, further comprising a starter-helper motor (9) drivingly coupled to said transmission gear train (6).
  8. The system (1) according to any of the preceding claims, further comprising a heat exchanger (11) for engaging heat transfer between a portion (10j) of the refrigerant fluid expanded by said at least one turboexpander (4a) and at least a portion (10g) of the refrigerant fluid compressed by said compressors, to partially cool said portion (10g) of the refrigerant fluid compressed by said compressors prior to expansion by said at least one turboexpander (4a).
  9. A refrigeration method involving circulation a refrigerant fluid (10), comprising operating a first compressor (2a) and a second compressor (2b) to compress said refrigerant fluid (10) in separate stages of compression and operating at least one turboexpander (4a) to expand at least a portion (10i) of the refrigerant fluid downstream of said compressors (2a,2b), said method characterized by
    - driving the first compressor (2a) by a drive (3) directly connected the first compressor (2a) by a first shaft (5a), and
    - driving the second compressor (2b) by a mechanical power output from the turboexpander (4a) resulting from said expansion, wherein the turboexpander (4a) is directly connected to the second compressor (2b) by a second shaft (5b), the second shaft (5b) being drivingly coupled to the first shaft (5a) by a transmission gear train (6).
  10. The method according to claim 9, comprising operating a plurality of compressors (2b,2c) in addition to said first compressor (2a) for compressing said refrigerant fluid (10) in separate stages of compression, and operating a plurality of turboexpanders (4a,4b) to expand portions (10i, 10k) of the refrigerant fluid downstream of said compressors (2a,2b,2c), said method further characterized by
    - driving each of said plurality of compressors (2b,2c) by a mechanical power output of a respective turboexpander (4a,4b) directly connected thereto by a respective shaft (5b,5c), the mechanical power output of said turboexpanders (4a,4b) resultant from said expansions, wherein said shafts (5a,5b,5c) are drivingly coupled by the transmission gear train (6).
  11. The method according to any of claims 9 and 10, further characterized by operating one or more turboexpanders (4a,4b) such that the mechanical power output of each of said one or more turboexpanders (4a,4b) balances power consumption by a respective compressor (2b,2c) directly connected thereto.
  12. The method according to any of claims 9 to 11, wherein each compressor (2a,2b,2c) and the drive (3) or turboexpander (4a,4b) connected thereto are arranged on opposite sides of said transmission gear train (6).
  13. The method according to any of claims 9 to 12, further characterized by regulating flow through one or more compressors (2b,2c) by adjusting inlet guide vanes (8a,8b) of a respective turboexpander (4a,4b) directly connected thereto.
  14. The method according to any of claims 9 to 13, comprising operating a gas turbine as said drive (3).
  15. The method according to claim 14, further comprising operating a starter-helper motor (9) drivingly coupled to said transmission gear train (6).
EP09015486A 2009-12-15 2009-12-15 Refrigeration system and method Withdrawn EP2336677A1 (en)

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FR2977015A1 (en) * 2011-06-24 2012-12-28 Saipem Sa METHOD FOR LIQUEFACTING NATURAL GAS WITH TRIPLE FIRM CIRCUIT OF REFRIGERATING GAS
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ITFI20130076A1 (en) * 2013-04-04 2014-10-05 Nuovo Pignone Srl "INTEGRALLY-GEARED COMPRESSORS FOR PRECOOLING IN LNG APPLICATIONS"
US20160177955A1 (en) * 2013-08-07 2016-06-23 Hanwha Techwin Co., Ltd. Compression system
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WO2022221154A1 (en) * 2021-04-15 2022-10-20 Praxair Technology, Inc. System and method to produce liquefied natural gas using two distinct refrigeration cycles with an integral gear machine
WO2022221160A1 (en) * 2021-04-15 2022-10-20 Praxair Technology, Inc. System and method to produce liquefied natural gas using two distinct refrigeration cycles with an integral gear machine
WO2023063993A1 (en) * 2021-10-13 2023-04-20 Praxair Technology, Inc. System and method to produce liquefied natural gas
WO2023063992A1 (en) * 2021-10-13 2023-04-20 Praxair Technology, Inc. System and method to produce liquefied natural gas
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JP5705375B2 (en) * 2012-04-13 2015-04-22 大陽日酸株式会社 Cooling device for high temperature superconducting equipment and method for operating the same
WO2013154185A1 (en) * 2012-04-13 2013-10-17 大陽日酸株式会社 Cooling device for high temperature superconducting apparatus and operation method therefor
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WO2021254597A1 (en) * 2020-06-16 2021-12-23 Wärtsilä Finland Oy A system for producing liquefied product gas and method of operating the same
WO2022221154A1 (en) * 2021-04-15 2022-10-20 Praxair Technology, Inc. System and method to produce liquefied natural gas using two distinct refrigeration cycles with an integral gear machine
WO2022221160A1 (en) * 2021-04-15 2022-10-20 Praxair Technology, Inc. System and method to produce liquefied natural gas using two distinct refrigeration cycles with an integral gear machine
WO2023063993A1 (en) * 2021-10-13 2023-04-20 Praxair Technology, Inc. System and method to produce liquefied natural gas
WO2023063992A1 (en) * 2021-10-13 2023-04-20 Praxair Technology, Inc. System and method to produce liquefied natural gas
WO2023063991A1 (en) * 2021-10-13 2023-04-20 Praxair Technology, Inc. System and method to produce liquefied natural gas
WO2023069139A1 (en) * 2021-10-21 2023-04-27 Praxair Technology, Inc. System and method to produce liquefied natural gas
US12123646B2 (en) 2022-04-08 2024-10-22 Praxair Technology, Inc. System and method to produce liquefied natural gas using a three pinion integral gear machine

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