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WO1997033131A1 - An installation for producing liquefied natural gas - Google Patents

An installation for producing liquefied natural gas Download PDF

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Publication number
WO1997033131A1
WO1997033131A1 PCT/NO1997/000062 NO9700062W WO9733131A1 WO 1997033131 A1 WO1997033131 A1 WO 1997033131A1 NO 9700062 W NO9700062 W NO 9700062W WO 9733131 A1 WO9733131 A1 WO 9733131A1
Authority
WO
WIPO (PCT)
Prior art keywords
circuit
cooling
resp
gas turbine
installation
Prior art date
Application number
PCT/NO1997/000062
Other languages
French (fr)
Inventor
Ove Muri
Pentti Paurola
Original Assignee
Den Norske Stats Oljeselskap A/S
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 Den Norske Stats Oljeselskap A/S filed Critical Den Norske Stats Oljeselskap A/S
Priority to AU21067/97A priority Critical patent/AU717114C/en
Publication of WO1997033131A1 publication Critical patent/WO1997033131A1/en

Links

Classifications

    • 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
    • F25B1/00—Compression machines, plants or systems with non-reversible cycle
    • F25B1/04—Compression machines, plants or systems with non-reversible cycle with compressor of rotary type
    • 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
    • F25J1/0052—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 vaporising a liquid refrigerant stream
    • 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
    • F25J1/0052—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 vaporising a liquid refrigerant stream
    • F25J1/0055—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 vaporising a liquid refrigerant stream originating from an incorporated cascade
    • 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
    • F25J1/0211—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 multi-component refrigerant [MCR] fluid in a closed vapor compression cycle
    • F25J1/0214—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 multi-component refrigerant [MCR] fluid in a closed vapor compression cycle as a dual level refrigeration cascade with at least one MCR 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
    • F25J1/0211—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 multi-component refrigerant [MCR] fluid in a closed vapor compression cycle
    • F25J1/0214—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 multi-component refrigerant [MCR] fluid in a closed vapor compression cycle as a dual level refrigeration cascade with at least one MCR cycle
    • F25J1/0215—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 multi-component refrigerant [MCR] fluid in a closed vapor compression cycle as a dual level refrigeration cascade with at least one MCR cycle with one SCR cycle
    • F25J1/0216—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 multi-component refrigerant [MCR] fluid in a closed vapor compression cycle as a dual level refrigeration cascade with at least one MCR cycle with one SCR cycle using a C3 pre-cooling 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
    • F25J1/0228—Coupling of the liquefaction unit to other units or processes, so-called integrated processes
    • F25J1/0235—Heat exchange integration
    • F25J1/0237—Heat exchange integration integrating refrigeration provided for liquefaction and purification/treatment of the gas to be liquefied, e.g. heavy hydrocarbon removal from natural gas
    • F25J1/0239—Purification or treatment step being integrated between two refrigeration cycles of a refrigeration cascade, i.e. first cycle providing feed gas cooling and second cycle providing overhead gas cooling
    • 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
    • F25J1/0228—Coupling of the liquefaction unit to other units or processes, so-called integrated processes
    • F25J1/0235—Heat exchange integration
    • F25J1/0242—Waste heat recovery, e.g. from heat of compression
    • 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
    • F25J1/0244—Operation; Control and regulation; Instrumentation
    • F25J1/0245—Different modes, i.e. 'runs', of operation; Process control
    • F25J1/0247—Different modes, i.e. 'runs', of operation; Process control start-up of the process
    • 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.
    • F25J1/0285—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.
    • F25J1/029—Mechanically coupling of different refrigerant compressors in a cascade refrigeration system to a common 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.
    • F25J1/0292—Refrigerant compression by cold or cryogenic suction of the refrigerant 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
    • F25J1/02—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
    • F25J2220/62—Separating low boiling components, e.g. He, H2, N2, Air
    • 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
    • F25J2280/00—Control of the process or apparatus
    • F25J2280/10—Control for or during start-up and cooling down of the installation

Definitions

  • the present invention relates to an installation or plant for producing liquefied natural gas, comprising a precool ⁇ ing circuit and a main cooling circuit containing cooling medium for cooling the natural gas, each of the cooling circuits comprising at least one compressor for compressing the cooling medium of the circuit, and at least one gas turbine for operation of the compressors.
  • the cooling of the natural gas mainly consisting of methane gas, which is to be cooled down to liquid form, usually takes place in two cooling circuits, more specifically a precooling circuit and a main cooling circuit. Both of these circuits have separate cooling media circulating in closed systems, and which are not mixed with the feed gas, i.e. the natural gas which is to be made liquid.
  • the cooling circuits contain large compressors compressing the cooling media in the respective circuits. During the compression the medium becomes hot. It is cooled down with large quantities of water. Thereafter the medium again expands, and there is generated cold which is transferred to the feed gas.
  • the gas must be cooled to a temperature of -162 °C in order to become liquid at atmosphere pressure.
  • the precooling circuit usually contains one compressor, whereas the main cooling circuit contains two compressors. These compressors are very large and may have a size of up to 40 000 kW, or somewhat above 50 000 HP.
  • LNG installations which are built, or which are being built today, there is used either a separate driver for each compressor, or there is used a separate driver for the compressor in the precooling circuit and a common driver for the two compressors in the main cooling circuit.
  • large capacity of the compressors it is usual today to use large gas turbines as drivers. These gas turbines s are very expensive, and each single unit needs much expensive supplementary equipment. The installation therefore becomes correspondingly expensive.
  • the object of the invention is to provide an LNG installation which can be built with substantially reduced costs o in relation to the hitherto known installations, and which is also more economic in operation.
  • the solution according to the invention may be used both for larger and smaller gas turbines.
  • the invention will be further described below in connection with an exemplary embodiment with reference to the drawing the only figure of which shows a simplified flow diagram of an LNG installation according to the invention.
  • the installation shown in the drawing comprises a precooling circuit 1 and a main cooling circuit 2 for the cooling of purified natural gas (feed gas) which is supplied to the installation or plant via a pipeline 3 for treatment in the installation as further described below.
  • the gas for example may be supplied in a quantity of about 490 tons per hour.
  • the precooling circuit and the main cooling circuit are separate, closed circuits for circulation of respective cooling media.
  • the temperature (in °C) of the cooling media and the feed gas at different places in the system is indicated in the drawing in rectangle symbols, whereas the pressure (in bar a) of the cooling media and the feed gas at different places is indicated in circle symbols.
  • the precooling circuit 1 in the illustrated case is presupposed to use propane as a cooling medium, whereas the cooling medium may also consist of a mixture of different gases.
  • the circuit contains a two-step compres ⁇ sor 4 for compression of the cooling medium. From the compressor 4 a line 5 leads via a heat exchanger 6 to a plate-rib heat exchanger 7, and from this heat exchanger two lines 8, 9 lead back to the compressor 4.
  • the cooling medium is heated, and it is therefore cooled in the heat exchanger 6 by means of cooling water.
  • the medium is expanded and thereby strongly cooled.
  • the medium gives off cold in the heat exchanger and thereby absorbs heat from the feed gas which is supplied via the pipeline 3 and carried through the heat exchanger in separate channels.
  • the feed gas thereby is cooled from about +25 °C to about -35 °C.
  • the heated cooling medium is returned to the compressor 4 via the lines 8, 9 to be compressed again.
  • the main cooling circuit 2 comprises a low-pressure compressor 15 and a high-pressure compressor 16 for compression of the cooling medium.
  • the low-pressure compressor 15 has an s inlet 17 and a outlet 18, whereas the high-pressure compressor 16 has an inlet 19 and an outlet 20.
  • From the outlet 18 of the low-pressure compressor a line 21 leads via a heat exchanger 22 to the inlet 19 of the high-pressure compressor.
  • From the outlet 20 thereof a line 23 leads via a heat exchanger 24 to the plate- o rib heat exchanger 7. From this heat exchanger the circuit continues via a line 25 to a separator 26. This has two outlets from which respective lines 27, 28 lead to a main heat exchanger 29 via respective valves 30, 31.
  • From the main heat exchanger a line 32 leads back to the inlet 17 of the low-pressure compressor s 15.
  • the cooling medium in the main cooling circuit consists of an adapted mixture of gases (e.g. methane, ethane and propane) with different boiling points in order to obtain a well distri ⁇ ubbed heat transfer.
  • gases e.g. methane, ethane and propane
  • CW cooling water
  • the medium is supplied to the plate-rib heat exchanger 7 wherein it is further cooled and thereby is made partly liquid.
  • the mixture of gas and liquid is separated in the separator 26 and is carried 5 further to the main heat exchanger 29 in two flows via the lines 27, 28.
  • the cooling medium flow is carried via respective ones of the valves 30 and 31 into a second part of the heat exchanger wherein the flows expand and thereby become further 0 strongly cooled.
  • the cooled-down cooling medium flows are sprayed out within the heat exchanger and cause a strong cooling of the feed gas passing the main heat exchanger in separate channels.
  • a bypass valve 33 is arranged between the 5 inlet 17 and the outlet 18 of the low-pressure compressor 15.
  • a similar bypass valve 34 is arranged between the inlet 19 and the outlet 20 of the high-pressure compressor 16. The purpose of these valves will be further described later.
  • the compressor in the precooling circuit for example may be a centrifugal compressor having a power or output of about 21 500 kW.
  • the low-pressure compressor in the main cooling circuit may be an axial compressor having a power of about 38 000 MW, whereas the high-pressure 5 compressor may be a centrifugal compressor having a power of about 27 000 kW.
  • this is cooled as mentioned in the heat exchanger 7 and is carried further therefrom via a line 35 to a condensate separator 36.
  • a condensate separator 36 In this unit there is separated o condensate which is supplied via a line 37 to a condensate storage (not shown).
  • the feed gas From the condensate separator 36 the feed gas is supplied to the main heat exchanger 29 via a line 38. Because of the strong cooling of the feed gas when this passes the main heat exchanger, it passes into liquid form, but is still s under pressure. From the main heat exchanger the feed gas is supplied via a line 39 to a nitrogen separator 40.
  • the feed gas is expanded into the nitrogen separator wherein the nitrogen (N 2 ) in the gas is separated by evaporation, at the same time as the liquid gas is additionally cooled so that it is in liquid form o at atmospheric pressure.
  • the liquid natural gas (LNG) then has a temperature of -162 °C.
  • the liquid gas is supplied to storage tanks 41, in the shown example in a quantity of about 450 tons per hour, in order thereafter to be pumped on board special tankers for transport to the topical destinations. 5
  • the above-mentioned compressors 4, 15 and 16 are connected in series and in accor ⁇ dance with the invention are arranged to be driven by a single common driver in the form of a gas turbine 42.
  • the gas turbine is shown to have two inlets 43, 44 for the supply of air and gas, respectively, in operation of the turbine, and an outlet for exhaust gas which is delivered via a unit 45 through which hot oil circulates.
  • the gas turbine suitably may be a single shaft turbine which produces power firstly at a high drive speed (RPM) , and only within a limited drive speed region. It is therefore necessary to use a starter or auxiliary engine 46 to bring the gas turbine up to the necessary drive speed before it can be loaded.
  • the gas turbine may be of the type "General Electric Frame 7", having a power of 85 000 kW and a drive speed of 3 600 ⁇ 5 % revolutions per minute.
  • an electric auxiliary engine of 8 MW having a variable drive speed from 0 to 3 600 revolutions per minute.
  • the engine or motor is used s as a helper for the gas turbine, in order in this manner to increase the power and thereby increase the production.
  • an even larger motor e.g. of 10 MW
  • an even larger motor e.g. of 10 MW
  • the entire described unit consisting of the three compressors, the gas turbine and the auxiliary engine, are fixedly interconnected, and in the illustrated example may have a total weight of about 450 tons and a total length of about 45 m.
  • the whole unit is very large and represents a substan- i5 tial part of the investment of the installation. It is therefore very important that start-up of the unit takes place in a secure manner. Relief possibilities for the equipment during start-up of the unit are absolutely necessary. If the start-up is not carried out in a proper manner, the load on the motor and the gas
  • the entire fixedly interconnected unit must be brought up to a suitable drive speed by means of the electromotor before air and gas are brought into the combustion chamber of the gas turbine and the turbine achieves the necessary power to get the
  • the resistance of the cooling circuits must be reduced to a minimum. This is done by opening the bypass valves
  • cooling circuits 35 12, 14, 33 and 34 of the compressors, and also the valves 30 and 31.
  • the motor 46 is started and sets going the gas turbine and the fixedly connected compressors until the whole unit has come up to a drive speed at which the gas turbine develops a s sufficient own power. All valves at the suction side of the compressors are closed. Thereafter the gas turbine is started. When the gas turbine yields a sufficient own power, the valves in the installation are opened, so that feed gas in a limited quantity can be carried through the plate-rib heat exchanger 7 o and the main heat exchanger 29. The gas is carried to the flare system of the installation and burnt.
  • the precooling circuit When pressurizing the installation, the precooling circuit is firstly pressurized.
  • the bypass valves 12 and 14 are closed and adjustments of other valves and equipment are carried out, so that the compressed gas is firstly cooled in the heat exchanger 6 and thereafter can expand in the heat exchanger 7 and cool the feed gas.
  • the main cooling circuit can be pressurized.
  • the bypass valves thereof are closed, and thereafter the valves 30 and 31 and other equipment are adjusted in order to achieve the correct pressure drop and expansion of the cooling medium.
  • the cooling medium is cooled in the cooling water heat exchangers 22 and 24 and is additionally cooled in the heat exchanger 7.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
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  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
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Abstract

An installation for producing liquefied natural gas comprises a precooling circuit (1) and a main cooling circuit (2) containing cooling medium for cooling the natural gas, each of the cooling circuits (1, 2) comprising at least one compressor (4 resp. 15, 16) for compressing the cooling medium of the circuit. The compressors (4, 15, 16) in the precooling circuit (1) and the main cooling circuit (2) are mechanically interconnected and are arranged to be driven by a single common gas turbine (42). This is preferably a single shaft turbine having an essentially fixed drive speed during operation, an auxiliary engine (44) being arranged for start-up of the gas turbine (42) and the compressors (4, 15, 16), and for possibly assisting the gas turbine during operation.

Description

An installation for producing liquefied natural σas
The present invention relates to an installation or plant for producing liquefied natural gas, comprising a precool¬ ing circuit and a main cooling circuit containing cooling medium for cooling the natural gas, each of the cooling circuits comprising at least one compressor for compressing the cooling medium of the circuit, and at least one gas turbine for operation of the compressors.
Installations for the production of liquefied natural gas or NG are extremely capital demanding. Thus, a larger LNG installation will require investments of the order of 1,5 billion US dollars. In addition to the installation cost there come field development, pipeline for landing when it is the question of an offshore field, and dedicated ships for transport of the LNG product. It is therefore very essential to reduce the costs in this connection.
In an LNG installation 30 - 40 % of the building costs lies in the cooling plant proper. The cooling of the natural gas, mainly consisting of methane gas, which is to be cooled down to liquid form, usually takes place in two cooling circuits, more specifically a precooling circuit and a main cooling circuit. Both of these circuits have separate cooling media circulating in closed systems, and which are not mixed with the feed gas, i.e. the natural gas which is to be made liquid. The cooling circuits contain large compressors compressing the cooling media in the respective circuits. During the compression the medium becomes hot. It is cooled down with large quantities of water. Thereafter the medium again expands, and there is generated cold which is transferred to the feed gas. The gas must be cooled to a temperature of -162 °C in order to become liquid at atmosphere pressure.
The precooling circuit usually contains one compressor, whereas the main cooling circuit contains two compressors. These compressors are very large and may have a size of up to 40 000 kW, or somewhat above 50 000 HP. In LNG installations which are built, or which are being built today, there is used either a separate driver for each compressor, or there is used a separate driver for the compressor in the precooling circuit and a common driver for the two compressors in the main cooling circuit. Because of the large capacity of the compressors, it is usual today to use large gas turbines as drivers. These gas turbines s are very expensive, and each single unit needs much expensive supplementary equipment. The installation therefore becomes correspondingly expensive.
The object of the invention is to provide an LNG installation which can be built with substantially reduced costs o in relation to the hitherto known installations, and which is also more economic in operation.
The above-mentioned object is achieved with an instal¬ lation of the introductorily stated type which, according to the invention, is characterized in that the compressors in the s precooling circuit and the main cooling circuit are mechanically interconnected and are arranged to be driven by a single common gas turbine.
By means of the above-mentioned solution, which uses only one driver or gas turbine for all the three compressors, o there is achieved a number of substantial advantages, such as
fewer equipment units, also with respect to supplementary equipment, fewer pipeline systems, 5 a smaller area for the process plant and conse¬ quently shorter pipe connections, lower cost per unit of power, i.e. a higher efficiency and consequently smaller C02 effluence, a higher service factor (hours of operation per o year) , smaller investments and lower running expenses. As a driver in a representative installation according to the invention, which may for example have a capacity of 4 - 5 GSmVyear, there may suitably be used a gas turbine of the type 5 "General Electric Frame 7" as a common driver, instead of three "Frame 5" gas turbines. Because of the above-mentioned advantages this results in a cost saving of the order of 40 million US dollars. The solution according to the invention may be used both for larger and smaller gas turbines. The invention will be further described below in connection with an exemplary embodiment with reference to the drawing the only figure of which shows a simplified flow diagram of an LNG installation according to the invention. The installation shown in the drawing comprises a precooling circuit 1 and a main cooling circuit 2 for the cooling of purified natural gas (feed gas) which is supplied to the installation or plant via a pipeline 3 for treatment in the installation as further described below. The gas for example may be supplied in a quantity of about 490 tons per hour. As appears, the precooling circuit and the main cooling circuit are separate, closed circuits for circulation of respective cooling media. The temperature (in °C) of the cooling media and the feed gas at different places in the system is indicated in the drawing in rectangle symbols, whereas the pressure (in bar a) of the cooling media and the feed gas at different places is indicated in circle symbols.
The precooling circuit 1 in the illustrated case is presupposed to use propane as a cooling medium, whereas the cooling medium may also consist of a mixture of different gases. In the shown embodiment the circuit contains a two-step compres¬ sor 4 for compression of the cooling medium. From the compressor 4 a line 5 leads via a heat exchanger 6 to a plate-rib heat exchanger 7, and from this heat exchanger two lines 8, 9 lead back to the compressor 4.
During the compression in the compressor 4 the cooling medium is heated, and it is therefore cooled in the heat exchanger 6 by means of cooling water. In the heat exchanger 7 the medium is expanded and thereby strongly cooled. The medium gives off cold in the heat exchanger and thereby absorbs heat from the feed gas which is supplied via the pipeline 3 and carried through the heat exchanger in separate channels. The feed gas thereby is cooled from about +25 °C to about -35 °C. The heated cooling medium is returned to the compressor 4 via the lines 8, 9 to be compressed again.
As appears from the drawing, at the inlets 10, 11 of the compressor 4 between the lines 8 and 9, there is arranged a bypass valve 12, and between the inlet 10 and the outlet 13 of the compressor there is similarly arranged a bypass valve 14. The purpose of these valves will be further described later.
The main cooling circuit 2 comprises a low-pressure compressor 15 and a high-pressure compressor 16 for compression of the cooling medium. The low-pressure compressor 15 has an s inlet 17 and a outlet 18, whereas the high-pressure compressor 16 has an inlet 19 and an outlet 20. From the outlet 18 of the low-pressure compressor a line 21 leads via a heat exchanger 22 to the inlet 19 of the high-pressure compressor. From the outlet 20 thereof a line 23 leads via a heat exchanger 24 to the plate- o rib heat exchanger 7. From this heat exchanger the circuit continues via a line 25 to a separator 26. This has two outlets from which respective lines 27, 28 lead to a main heat exchanger 29 via respective valves 30, 31. From the main heat exchanger a line 32 leads back to the inlet 17 of the low-pressure compressor s 15.
The cooling medium in the main cooling circuit consists of an adapted mixture of gases (e.g. methane, ethane and propane) with different boiling points in order to obtain a well distri¬ buted heat transfer. After a first compression in the low- o pressure compressor 15, the heated medium is cooled in the heat exchanger 22 by means of cooling water (CW). Thereafter the medium is supplied to the plate-rib heat exchanger 7 wherein it is further cooled and thereby is made partly liquid. The mixture of gas and liquid is separated in the separator 26 and is carried 5 further to the main heat exchanger 29 in two flows via the lines 27, 28. After partly cooling in a first part of the main heat exchanger 29 the cooling medium flow is carried via respective ones of the valves 30 and 31 into a second part of the heat exchanger wherein the flows expand and thereby become further 0 strongly cooled. The cooled-down cooling medium flows are sprayed out within the heat exchanger and cause a strong cooling of the feed gas passing the main heat exchanger in separate channels.
In a manner similar to that of the compressor 4 in the precooling circuit, a bypass valve 33 is arranged between the 5 inlet 17 and the outlet 18 of the low-pressure compressor 15. A similar bypass valve 34 is arranged between the inlet 19 and the outlet 20 of the high-pressure compressor 16. The purpose of these valves will be further described later.
In the illustrated installation the compressor in the precooling circuit for example may be a centrifugal compressor having a power or output of about 21 500 kW. The low-pressure compressor in the main cooling circuit may be an axial compressor having a power of about 38 000 MW, whereas the high-pressure 5 compressor may be a centrifugal compressor having a power of about 27 000 kW.
As regards the feed gas, this is cooled as mentioned in the heat exchanger 7 and is carried further therefrom via a line 35 to a condensate separator 36. In this unit there is separated o condensate which is supplied via a line 37 to a condensate storage (not shown). From the condensate separator 36 the feed gas is supplied to the main heat exchanger 29 via a line 38. Because of the strong cooling of the feed gas when this passes the main heat exchanger, it passes into liquid form, but is still s under pressure. From the main heat exchanger the feed gas is supplied via a line 39 to a nitrogen separator 40. The feed gas is expanded into the nitrogen separator wherein the nitrogen (N2) in the gas is separated by evaporation, at the same time as the liquid gas is additionally cooled so that it is in liquid form o at atmospheric pressure. The liquid natural gas (LNG) then has a temperature of -162 °C. The liquid gas is supplied to storage tanks 41, in the shown example in a quantity of about 450 tons per hour, in order thereafter to be pumped on board special tankers for transport to the topical destinations. 5 As appears from the drawing, the above-mentioned compressors 4, 15 and 16 are connected in series and in accor¬ dance with the invention are arranged to be driven by a single common driver in the form of a gas turbine 42. The gas turbine is shown to have two inlets 43, 44 for the supply of air and gas, respectively, in operation of the turbine, and an outlet for exhaust gas which is delivered via a unit 45 through which hot oil circulates.
The gas turbine suitably may be a single shaft turbine which produces power firstly at a high drive speed (RPM) , and only within a limited drive speed region. It is therefore necessary to use a starter or auxiliary engine 46 to bring the gas turbine up to the necessary drive speed before it can be loaded. In the illustrated example the gas turbine may be of the type "General Electric Frame 7", having a power of 85 000 kW and a drive speed of 3 600 ± 5 % revolutions per minute. In the illustrated example there is used an electric auxiliary engine of 8 MW having a variable drive speed from 0 to 3 600 revolutions per minute. During normal operation the engine or motor is used s as a helper for the gas turbine, in order in this manner to increase the power and thereby increase the production. There may suitably be used an even larger motor (e.g. of 10 MW) to have an extra power on hot days when the gas turbine gives a reduced output. ιo The entire described unit consisting of the three compressors, the gas turbine and the auxiliary engine, are fixedly interconnected, and in the illustrated example may have a total weight of about 450 tons and a total length of about 45 m. Thus, the whole unit is very large and represents a substan- i5 tial part of the investment of the installation. It is therefore very important that start-up of the unit takes place in a secure manner. Relief possibilities for the equipment during start-up of the unit are absolutely necessary. If the start-up is not carried out in a proper manner, the load on the motor and the gas
20 turbine may be too large and result in that the entire unit stops during the start-up sequence. This may result in that the motor runs warm, and that damages may be caused on both the motor and the gas turbine.
Start-up of the unit, and the necessary preparations in
25 this connection, will be described below.
The entire fixedly interconnected unit must be brought up to a suitable drive speed by means of the electromotor before air and gas are brought into the combustion chamber of the gas turbine and the turbine achieves the necessary power to get the
30 process started. During the start-up proper therefore all resistance must be reduced to a minimum.
Thus, in order to be able to start up the large equipment unit, the resistance of the cooling circuits must be reduced to a minimum. This is done by opening the bypass valves
35 12, 14, 33 and 34 of the compressors, and also the valves 30 and 31. One must also take care that other valves (not shown) in the cooling circuits are positioned so as to give the least possible resistance in both circuits. Further, cooling water must be supplied to the heat exchangers 6, 22, 24 having water as a cooling medium.
The motor 46 is started and sets going the gas turbine and the fixedly connected compressors until the whole unit has come up to a drive speed at which the gas turbine develops a s sufficient own power. All valves at the suction side of the compressors are closed. Thereafter the gas turbine is started. When the gas turbine yields a sufficient own power, the valves in the installation are opened, so that feed gas in a limited quantity can be carried through the plate-rib heat exchanger 7 o and the main heat exchanger 29. The gas is carried to the flare system of the installation and burnt.
When pressurizing the installation, the precooling circuit is firstly pressurized. The bypass valves 12 and 14 are closed and adjustments of other valves and equipment are carried out, so that the compressed gas is firstly cooled in the heat exchanger 6 and thereafter can expand in the heat exchanger 7 and cool the feed gas.
When the precooling circuit has been made operative, the main cooling circuit can be pressurized. The bypass valves thereof are closed, and thereafter the valves 30 and 31 and other equipment are adjusted in order to achieve the correct pressure drop and expansion of the cooling medium. The cooling medium is cooled in the cooling water heat exchangers 22 and 24 and is additionally cooled in the heat exchanger 7. When both cooling circuits are operative, the burning of the feed gas via the flare is discontinued, and the feed gas is made liquid. The installation therewith is in operation.

Claims

P a t e n t C l a i m s
1. An installation for producing liquefied natural gas, comprising a precooling circuit ( 1 ) and a main cooling circuit
(2) containing cooling medium for cooling the natural gas, each of the cooling circuits (1, 2) comprising at least one compressor (4 resp. 15, 16) for compressing the cooling medium of the circuit, and at least one gas turbine (42) for operation of the compressors, CHARACTERIZED IN that the compressors (4, 15, 16) in the precooling circuit (1) and the main cooling circuit (2) are mechanically interconnected and are arranged to be driven by a single common gas turbine (42) .
2. An installation according to claim 1, CHARACTERIZED IN that the gas turbine (42) is a single shaft turbine having an essentially fixed drive speed during operation, an auxiliary engine (49) being arranged for start-up of the gas turbine (42) and the compressors (4, 15, 16), and for possibly assisting the gas turbine during operation.
3. An installation according to claim 1 or 2, CHARAC¬
TERIZED IN that the precooling circuit (1) contains a two-step compressor (4) and the main cooling circuit (2) contains a low- pressure compressor (15) and a high-pressure compressor (16).
4. An installation according to anyone of the claims 1- 3, CHARACTERIZED IN that, between the inlets (11 resp. 17 resp. 19) and outlets (13 resp. 18 resp. 20) of each compressor (4 resp. 15 resp. 16), there are connected bypass valves (12, 14 resp. 33 resp. 34) which are arranged to be opened during start¬ up of the installation, to relieve the auxiliary engine (46) and the gas turbine (42) during the start-up.
PCT/NO1997/000062 1996-03-06 1997-03-03 An installation for producing liquefied natural gas WO1997033131A1 (en)

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NO960911A NO300293B1 (en) 1996-03-06 1996-03-06 Plant for the production of liquefied natural gas

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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999030094A1 (en) * 1997-12-11 1999-06-17 Bhp Petroleum Pty. Ltd. Liquefaction process and apparatus
WO2000029797A1 (en) * 1998-11-18 2000-05-25 Shell Internationale Research Maatschappij B.V. Plant for liquefying natural gas
EP1031803A2 (en) * 1999-02-26 2000-08-30 Compressor Controls Corporation Method and apparatus for maximizing the productivity of a natural gas liquids production plant
WO2001040725A1 (en) * 1999-12-01 2001-06-07 Shell Internationale Research Maatschappij B.V. Offshore plant for liquefying natural gas
US6446465B1 (en) * 1997-12-11 2002-09-10 Bhp Petroleum Pty, Ltd. Liquefaction process and apparatus
US6647744B2 (en) 2002-01-30 2003-11-18 Exxonmobil Upstream Research Company Processes and systems for liquefying natural gas
US6658892B2 (en) 2002-01-30 2003-12-09 Exxonmobil Upstream Research Company Processes and systems for liquefying natural gas
WO2004031668A1 (en) * 2002-09-30 2004-04-15 Bp Corporation North America Inc. A reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines
WO2004031669A1 (en) * 2002-09-30 2004-04-15 Bp Corporation North America Inc. Reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process
US7069733B2 (en) 2003-07-30 2006-07-04 Air Products And Chemicals, Inc. Utilization of bogdown of single-shaft gas turbines to minimize relief flows in baseload LNG plants
EP1790926A1 (en) * 2005-11-24 2007-05-30 Shell Internationale Researchmaatschappij B.V. Method and apparatus for cooling a stream, in particular a hydrocarbon stream such as natural gas
WO2008015224A2 (en) * 2006-08-02 2008-02-07 Shell Internationale Research Maatschappij B.V. Method and apparatus for liquefying a hydrocarbon stream
WO2008033033A2 (en) 2006-09-12 2008-03-20 Aker Engineering & Technology As Method and system for start and operation of an electrically driven load
US7691028B2 (en) * 2006-05-02 2010-04-06 Conocophillips Company Mechanical soft-start system for rotating industrial equipment
WO2010054434A1 (en) * 2008-11-17 2010-05-20 Woodside Energy Limited Power matched mixed refrigerant compression circuit
US20100147024A1 (en) * 2008-12-12 2010-06-17 Air Products And Chemicals, Inc. Alternative pre-cooling arrangement
EP2426452A1 (en) 2010-09-06 2012-03-07 Shell Internationale Research Maatschappij B.V. Method and apparatus for cooling a gaseous hydrocarbon stream
US20120067080A1 (en) * 2008-09-19 2012-03-22 Woodside Energy Limited Mixed Refrigerant Compression Circuit
US8591199B2 (en) 2007-01-11 2013-11-26 Conocophillips Company Multi-stage compressor/driver system and method of operation

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR768875A (en) * 1933-02-20 1934-08-14 Brown Wind heater or similar heat exchange device in which at least one of the agents used is a gas
GB1072048A (en) * 1963-12-07 1967-06-14 Dowty Technical Dev Ltd Refrigeration systems
US3817046A (en) * 1970-11-28 1974-06-18 Chinzoda Chem Eng & Constructi Absorption-multicomponent cascade refrigeration for multi-level cooling of gas mixtures
EP0142899A2 (en) * 1983-11-18 1985-05-29 Shell Internationale Researchmaatschappij B.V. A method for liquefying a gas, in particular a natural gas
WO1995018345A1 (en) * 1993-12-30 1995-07-06 Institut Français Du Petrole Method and apparatus for liquefying natural gas

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR768875A (en) * 1933-02-20 1934-08-14 Brown Wind heater or similar heat exchange device in which at least one of the agents used is a gas
GB1072048A (en) * 1963-12-07 1967-06-14 Dowty Technical Dev Ltd Refrigeration systems
US3817046A (en) * 1970-11-28 1974-06-18 Chinzoda Chem Eng & Constructi Absorption-multicomponent cascade refrigeration for multi-level cooling of gas mixtures
EP0142899A2 (en) * 1983-11-18 1985-05-29 Shell Internationale Researchmaatschappij B.V. A method for liquefying a gas, in particular a natural gas
US4566885A (en) * 1983-11-18 1986-01-28 Shell Oil Company Gas liquefaction process
WO1995018345A1 (en) * 1993-12-30 1995-07-06 Institut Français Du Petrole Method and apparatus for liquefying natural gas

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
DERWENT'S ABSTRACT, No. 46190C/26, week 8026; & SU,A,697 783 (SOYUZTURBOGAZ), 25 November 1979. *
DERWENT'S ABSTRACT, No. 60058D/33, week 8133; & SU,A,783 536 (AIR GAS COOL TURBIN), 30 November 1980. *

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US6446465B1 (en) * 1997-12-11 2002-09-10 Bhp Petroleum Pty, Ltd. Liquefaction process and apparatus
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US6389844B1 (en) 1998-11-18 2002-05-21 Shell Oil Company Plant for liquefying natural gas
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WO2001040725A1 (en) * 1999-12-01 2001-06-07 Shell Internationale Research Maatschappij B.V. Offshore plant for liquefying natural gas
US6658891B2 (en) 1999-12-01 2003-12-09 Shell Research Limited Offshore plant for liquefying natural gas
AP1430A (en) * 1999-12-01 2005-06-13 Shell Int Research Offshore plant for liquefying natural gas.
US6658892B2 (en) 2002-01-30 2003-12-09 Exxonmobil Upstream Research Company Processes and systems for liquefying natural gas
US6647744B2 (en) 2002-01-30 2003-11-18 Exxonmobil Upstream Research Company Processes and systems for liquefying natural gas
US7243510B2 (en) 2002-09-30 2007-07-17 Bp Corporation North America Inc. Reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process
WO2004031669A1 (en) * 2002-09-30 2004-04-15 Bp Corporation North America Inc. Reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process
US7131272B2 (en) 2002-09-30 2006-11-07 Bp Corporation North America Inc. Reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines
WO2004031668A1 (en) * 2002-09-30 2004-04-15 Bp Corporation North America Inc. A reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines
US7069733B2 (en) 2003-07-30 2006-07-04 Air Products And Chemicals, Inc. Utilization of bogdown of single-shaft gas turbines to minimize relief flows in baseload LNG plants
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US8181481B2 (en) 2005-11-24 2012-05-22 Shell Oil Company Method and apparatus for cooling a stream, in particular a hydrocarbon stream such as natural gas
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US9746234B2 (en) 2008-09-19 2017-08-29 Woodside Energy Ltd Mixed refrigerant compression circuit
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US20100147024A1 (en) * 2008-12-12 2010-06-17 Air Products And Chemicals, Inc. Alternative pre-cooling arrangement
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AU717114C (en) 2005-09-01
AU717114B2 (en) 2000-03-16
AU2106797A (en) 1997-09-22
NO960911D0 (en) 1996-03-06
MY117996A (en) 2004-08-30
NO960911A (en) 1997-05-05
NO300293B1 (en) 1997-05-05
ID16118A (en) 1997-09-04

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