WO2015011742A1 - Système de compression à réfrigération utilisant deux compresseurs - Google Patents

Système de compression à réfrigération utilisant deux compresseurs Download PDF

Info

Publication number
WO2015011742A1
WO2015011742A1 PCT/JP2013/004568 JP2013004568W WO2015011742A1 WO 2015011742 A1 WO2015011742 A1 WO 2015011742A1 JP 2013004568 W JP2013004568 W JP 2013004568W WO 2015011742 A1 WO2015011742 A1 WO 2015011742A1
Authority
WO
WIPO (PCT)
Prior art keywords
compressor
outlet
refrigeration circuit
inlet
inlets
Prior art date
Application number
PCT/JP2013/004568
Other languages
English (en)
Inventor
Yoshitsugi Kikkawa
Masaaki Oishi
Toshiya MOMOSE
Hirohiko Kikuchi
Koichiro SAKAI
Original Assignee
Chiyoda Corporation
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 Chiyoda Corporation filed Critical Chiyoda Corporation
Priority to RU2016106366A priority Critical patent/RU2629101C1/ru
Priority to AP2015008918A priority patent/AP2015008918A0/xx
Priority to CA2914477A priority patent/CA2914477C/fr
Priority to PCT/JP2013/004568 priority patent/WO2015011742A1/fr
Priority to AU2013395108A priority patent/AU2013395108B2/en
Priority to US14/899,226 priority patent/US20160131422A1/en
Publication of WO2015011742A1 publication Critical patent/WO2015011742A1/fr

Links

Images

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
    • 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
    • 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
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B40/00—Subcoolers, desuperheaters or superheaters
    • F25B40/04—Desuperheaters
    • 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
    • F25J1/006—Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the refrigerant fluid used
    • F25J1/008—Hydrocarbons
    • F25J1/0087—Propane; Propylene
    • 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
    • F25J1/0243—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.
    • F25J1/0294—Multiple compressor casings/strings in parallel, e.g. split arrangement
    • 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
    • F25B1/10—Compression machines, plants or systems with non-reversible cycle with multi-stage 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
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2400/00—General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
    • F25B2400/13—Economisers
    • 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
    • F25B2400/00—General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
    • F25B2400/23—Separators

Definitions

  • the present invention relates to a refrigeration compression system for use in a refrigeration circuit of a liquefaction plant, and in particular to a refrigeration compression system that can be constructed as a compact unit for a given production rate.
  • Natural gas is known to be environmentally favorable as compared with other fossil fuels and nuclear fuels, but is required to be processed in an appropriate manner before it can be delivered to the final users.
  • the cost for such processing is highly important for the natural gas to be competitive with other forms of fuels.
  • natural gas is most often required to be liquefied for the convenience of storage and delivery to the final users, and the cost of liquefaction accounts for a large part of the cost of natural gas.
  • liquefaction of natural gas is usually accomplished by compressing the natural gas by using a series of compressors which are powered by gas turbine drivers, and removing heat from the compressed natural gas by using heat exchangers.
  • the cost of liquefaction can be reduced by using a refrigerant system with a higher refrigeration duty.
  • the C3 MR (propane pre-cooled mixed refrigerant process) and the optimized cascade process are the two processes that are currently most widely used. These processes use C3 refrigerant for the pre-cooling of the process flow, and it is the pre-cooling process that imposes the most critical design issue in increasing the production rate of the system.
  • the production rate of the pre-cooling process can be increased by using larger compressors that can accommodate larger inlet volumes, but there is a limit to the size of the compressors for the given driver speed.
  • a simple method to increase the compressor inlet volume is to increase the impeller diameter.
  • the required yield strength of the impeller tip would increase so sharply as the impeller diameter is increased that the difficulty and cost of manufacture become unacceptable once a certain limit is reached.
  • the inlet flow Mach number is increased, the operating range of the compressor is narrowed, and the efficiency of the compressor starts dropping sharply.
  • the problem is particularly acute because the sonic velocity in LP C3 refrigerant is very low, typically approximately 230 m/sec. As a result, the impeller size at the LP stage would be limited below 1,320 mm when the rotor speed is selected at the typically speed of 3,600 rpm.
  • the last stage of the compressor must treat a high volume flow particularly when a side-stream compressor machine is used as is often the case in large refrigeration plants. This will lead to a drop in aerodynamic performance because of the need to select a large flow coefficient impeller in order to handle the large flow rate with a limited size of the impeller.
  • the flow coefficient is one of the dimensionless quantities used by the manufacturers to show the impeller performance, and is expressed by the formula given below.
  • F Q 0 / ⁇ (pi/4)D 2 U2 ⁇
  • Q suction volume flow (m 3 /sec)
  • D impeller diameter (m)
  • U2 impeller tip speed (m/s)
  • the proven range of the flow coefficient is below 0.155.
  • a liquefaction plant typically employs a number of identical compressor trains. Therefore, designing the compressor trains in an optimum fashion is highly important in increasing the efficiency of the liquefaction plant.
  • the production rate of a C3 can be increased by using two compressors of a limited size in separate casings in a 50%-50% parallel scheme.
  • this scheme requires a large amount of piping in an exactly symmetric 3D configuration, and the necessary material and labor cost prevents it from becoming a practical solution.
  • a primary object of the present invention is to provide apparatus for compressing gaseous refrigerant for use in a refrigeration circuit of a liquefaction plant which is highly compact and can still maximize the product output rate.
  • a second object of the present invention is to provide apparatus for compressing gaseous refrigerant which can maximize the product output rate by using readily available, relatively inexpensive compressors.
  • a third object of the present invention is to provide apparatus for compressing gaseous refrigerant which can maximize the product output rate without suffering from the problem of reduced efficiency.
  • such objects can be at least partly accomplished by providing apparatus for compressing gaseous refrigerant for use in a refrigeration circuit of a liquefaction plant, the apparatus comprising: a refrigeration circuit including an inlet for refrigerant at a refrigeration pressure, a low pressure outlet for gaseous refrigerant at a low pressure, a high pressure outlet for gaseous refrigerant at a high pressure and at least one intermediate pressure outlet for gaseous refrigerant at an intermediate pressure; a first compressor received in a first casing and provided with a double suction configuration including at least two main inlets and one outlet; a second compressor received in a second casing separate from the first casing and having an at least one inlet and an outlet, the outlet of the second compressor being connected to the inlet of the refrigeration circuit; and a common power source including an output shaft for driving the first and second compressors; wherein the first and second compressors are provided with inlets and outlets that are functionally connected to the inlet and the outlets of the refrigeration circuit, and the outlets
  • the use of a double suction compressor for the first compressor allows the flow rate at the main inlets of the first compressor to be maximized without excessively increasing the flow velocity at the inlets.
  • the two main inlets of the first compressor are commonly connected in a symmetric configuration.
  • the outlets and the inlets of the first and second compressors being connected at least partly in a mutually parallel flow configuration means that the refrigerant flow that leaves the refrigeration circuit from a plurality of outlets thereof is distributed between the two compressors before joining at the inlet of the refrigeration circuit.
  • the two main inlets of the first compressor are connected to the low pressure outlet of the refrigeration circuit, the flow rate of the low pressure gaseous refrigerant to be maximized without excessively increasing the flow velocity of the low pressure gaseous refrigerant.
  • the two main inlets of the first compressor may be connected to the intermediate pressure outlet of the refrigeration circuit.
  • the first compressor is further provided with a pair of side inlets in a symmetric configuration that are connected to the intermediate pressure outlet of the refrigeration circuit.
  • the second compressor may be provided with either a straight suction configuration or a double suction configuration. If the second compressor is provided with a straight suction configuration, the outlet of the second compressor may be connected to the inlet of the refrigeration circuit via an economizer so that an economical operation of the refrigeration compression system can be achieved even when the available power of the compressor driver is not sufficient.
  • the two main inlets of the first compressor may also be connected to different outlets of the refrigeration circuit. In such a case, the first compressor having a double suction configuration may be provided with either a symmetric or asymmetric configuration.
  • the refrigeration circuit typically comprises two intermediate pressure outlets for gaseous refrigerant at intermediate pressures, but may also be provided with one, three or more intermediate pressure outlets.
  • the mass flow rate of the highest pressure gaseous refrigerant can be divided between the two compressors, and the mass flow rate at the outlet of each compressor can be avoided from become excessive.
  • FIG. 1a is a schematic diagram of a first embodiment of the apparatus for compressing gaseous refrigerant according to the present invention
  • Fig. 1b is a view similar to Fig. 1a showing a modification of the first embodiment
  • Fig. 2a is a view similar to Fig. 1a showing a second embodiment of the present invention
  • Fig. 2b is a view similar to Fig. 2a showing a modification of the second embodiment
  • Figs. 3 to 20 are views similar to Fig. 1a showing other embodiments of the present invention.
  • Fig. 1a shows a first embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • This embodiment is particularly suited for use in the C3MR process.
  • C3 MR propane pre-cooled mixed refrigerant process
  • US5,832,745 for the details of the C3 MR (propane pre-cooled mixed refrigerant process), reference may be made to US5,832,745.
  • the present invention may also be used in other applications where refrigerant is cooled by using a refrigeration circuit having a plurality of outlets and a compressor system including a plurality of stages corresponding to the outlets of the refrigeration circuit.
  • This apparatus comprises a propane (C3) refrigeration circuit 1 which includes an inlet 2 and four outlets 3, 4, 5 and 6 for refrigerant at different temperatures and pressures.
  • the four outlets consist of a low pressure (LP) outlet 3 for refrigerant at -40deg. C and 112.5kPa, a medium pressure (MP) outlet 4 for refrigerant at -21deg. C and 234.5kPa, a high pressure (HP) outlet 5 for refrigerant at -6.6 deg. C and 384.8kPa, and a high high pressure (HHP) outlet 6 for refrigerant at 16.3 deg. C and 757.7kPa.
  • LP low pressure
  • MP medium pressure
  • HP high pressure
  • HP high pressure
  • This apparatus comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 is received in a single casing receiving two sets of impellers in a symmetric arrangement such that a pair of main inlets 12 and 13 are defined on either axial end of the casing, and an outlet 11 is defined in an axially middle part of the casing.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 is also received in a single casing, and includes a plurality of impeller disks arranged in series along the axial length thereof and typically supported by a common shaft.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a first inlet 22 at the other axial end thereof, and three more additional four inlets 23, 24 and 25 in axially intermediate positions thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30. It is also possible to use other drive sources such as an electric motor or electric motors, instead of the gas turbine driver.
  • the LP outlet of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10, and the outlet 11 of the first compressor 10 is connected to the high high high (HHHP) inlet 25 of the second compressor 20.
  • the MP outlet 5 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20, and the HP outlet 6 and the HHP outlet 7 of the refrigeration circuit 1 are connected to the HP and HHP inlets 23 and 24 of the second compressor 20, respectively.
  • the outlet 21 of the second compressor 20 is connected to the inlet 2 of the refrigeration circuit 1.
  • the HHHP inlet 25 may be omitted, and the outlet 11 of the first compressor 10 may be directly connected to the inlet 2 of the refrigeration circuit 1 as indicated by the dotted line in Fig. 1a. It should be noted that connecting the outlet of the first compressor 10 to an HHHP inlet of the second compressor 20, instead of the inlet 2 of the refrigeration circuit 1 is an option also in other embodiments, wherever applicable, which will be described hereinafter.
  • Fig. 1b shows a modification of the first embodiment which is similar to the first embodiment except for the provision of an economizer circuit in the outlet circuit that can be used for reducing the flow rate of the refrigerant and hence the power consumption of the gas turbine driver 30.
  • the outlet 21 of the second compressor 20 is connected to an inlet of a desuperheater 41, instead of being connected directly to the inlet 2 of the refrigeration circuit 1.
  • the outlet of the desuperheater 41 is connected to an economizer 44 via a condenser 42, an accumulator 43 and an adjustment valve 45, in that order.
  • the economizer 44 is also connected to a high high high (HHHP) inlet 25 of the second compressor 20 (or the outlet 11 of the first compressor 10), and to the inlet 2 of the refrigeration circuit 1.
  • HHHP high high high high
  • the refrigerant flow can be adjusted depending on the demand for the refrigerant.
  • This economizer circuit can also be optionally included in any of the following embodiments which will be described hereinafter, where the second compressor 20 is provided with a straight suction configuration.
  • Fig. 2a shows a second embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the second embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing, a pair of side inlets 14 and 15 and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof and a single side inlet 23 in an axially intermediate position thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20, and the MP outlet 5 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the two side inlets 14 and 15 of the first compressor 10, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the side inlet 23 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 2b shows a modification of the second embodiment which is similar to the second embodiment except for the provision of an economizer circuit in the outlet circuit that can be used for reducing the flow rate of the refrigerant and hence the power consumption of the gas turbine driver 30.
  • the outlet 21 of the second compressor 20 is connected to an inlet of a desuperheater 41, instead of being connected directly to the inlet 2 of the refrigeration circuit 1.
  • the outlet of the desuperheater 41 is connected to an economizer 44 via a condenser 42, an accumulator 43 and an adjustment valve 45, in that order.
  • the economizer 44 is also connected to a high high high (HHHP) inlet 25 of the second compressor 20 and to the inlet 2 of the refrigeration circuit 1.
  • the outlet 11 of the first compressor 10 is connected to the high high high (HHHP) inlet 25 of the second compressor 20.
  • the refrigerant flow can be adjusted depending on the demand for the refrigerant.
  • This economizer circuit can also be optionally included in any of the following embodiments which will be described hereinafter, where the second compressor 20 is provided with a straight suction configuration.
  • Fig. 3 shows a third embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the parts corresponding to those of the previous embodiment without necessarily repeating the description of such parts.
  • the apparatus of the third embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing, a pair of side inlets 14 and 15 and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof and typically supported by a common shaft.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof, and a single side inlet 23 in an axially intermediate position thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the two side inlets 14 and 15 of the first compressor 10.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the side inlet 23 of the second compressor 20.
  • the outlet 21 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 4 shows a fourth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • Fig. 4 and other drawings showing different embodiments of the present invention which are to be described hereinafter, the parts corresponding to those of the preceding embodiments are denoted with like numerals without necessarily repeating the description of such parts.
  • the apparatus of the fourth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing, a pair of side inlets 14 and 15 and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing, a pair of side inlets 24 and 25 and an outlet 21 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the two side inlets 14 and 15 of the first compressor 10.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the main inlets 22 and 23 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the side inlets 24 and 25 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 5 shows a fifth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the fifth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing, a pair of side inlets 14 and 15 and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing, a pair of side inlets 24 and 25 and an outlet 21 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the main inlets 22 and 23 of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the side inlets 24 and 25 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the two side inlets 14 and 15 of the first compressor 10.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 6 shows a sixth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the sixth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing, a pair of side inlets 14 and 15 and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing, a pair of side inlets 24 and 25 and an outlet 21 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the main inlets 22 and 23 of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the two side inlets 14 and 15 of the first compressor 10, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the side inlets 24 and 25 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 7 shows a seventh embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the seventh embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing, a pair of side inlets 14 and 15, and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof and a single side inlet 23 in an axially intermediate position thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20, and the HP outlet 4 of the refrigeration circuit 1 is connected to the two side inlets 14 and 15 of the first compressor 10, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the side inlet 23 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 8 shows an eighth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the eighth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing, a pair of side inlets 14 and 15 and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof and a single side inlet 23 in an axially intermediate position thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the side inlet 23 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the two side inlets 14 and 15 of the first compressor 10.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 9 shows a ninth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the ninth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof, and a pair of side inlets 23 and 24 in axially intermediate positions thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20, and the MP outlet 5 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the one of the side inlets 23 (lower pressure side) of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the other side inlet 24 (higher pressure side) of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 10 shows a tenth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the tenth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing, preferably all in a symmetric arrangement.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof and a pair of side inlets 23 and 24 in axially intermediate positions thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20, and the MP outlet 5 of the refrigeration circuit 1 is connected to one of the side inlets 23 (lower pressure side) of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the two main inlets 12 and 13 of the first compressor 10, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the other side inlet 24 (higher pressure side) of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 11 shows an eleventh embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the eleventh embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof and a single side inlet 23 in an axially intermediate position thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to one of the main inlets 12 of the first compressor 10, and the MP outlet 4 of the refrigeration circuit 1 is connected to the other main inlet 13 of the first compressor 10.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the side inlet 23 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 12 shows a twelfth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the twelfth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing, a pair of side inlets 24 and 25 and an outlet 21 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the second compressor 20 are preferably symmetric to each other.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to one of the two main inlets 12 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the other main inlet 13 of the first compressor.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the main inlets 22 and 23 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the two side inlets 24 and 25 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 13 shows a thirteenth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the thirteenth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing and an outlet 21 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to one of the two main inlets 12 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the other main inlet 12 of the first compressor 10.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to one of the two main inlets 22 of the first compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the other main inlet 23 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 14 shows a fourteenth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the fourteenth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof and a single side inlet 23 in an axially intermediate position thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20, and the MP outlet 4 of the refrigeration circuit 1 is connected to one of the main inlets 12 of the first compressor 10.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the other main inlet 13 of the first compressor 10, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the side inlet 23 of the second compressor 20.
  • the outlet 11 of the first compressor and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 15 shows a fifteenth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the fifteenth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing, a pair of side inlets 24 and 25, and an outlet 21 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the second compressor 20 are preferably symmetric to each other.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to the two main inlets 22 and 23 of the second compressor 20, and the MP outlet 5 of the refrigeration circuit 1 is connected to one of the main inlet 12 of the first compressor.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the other main inlet 13 of the first compressor 10, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the two side inlets 24 and 25 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 16 shows a sixteenth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the sixteenth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof and a single side inlet 23 in an axially intermediate position thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to one of the main inlets 12 of the first compressor 10, and the MP outlet 4 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the side inlet 23 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the other main inlet 13 of the first compressor 10.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 17 shows a seventeenth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the seventeenth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing, a pair of side inlets 24 and 25 and an outlet 21 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the second compressor 20 are preferably symmetric to each other.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to one of the two main inlets 12 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to the main inlets 22 and 23 of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the two side inlets 24 and 25 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the other main inlet 13 of the first compressor 10.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 18 shows an eighteenth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the eighteenth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing and an outlet 21 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to one of the two main inlets 12 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to one of the two main inlets 22 of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the other main inlet 23 of the second compressor 20, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the other main inlet 12 of the first compressor 10.
  • the outlet 11 of the first compressor 10 is connected to the inlet 2 of the refrigeration circuit 1.
  • the outlet 21 of the second compressor 120 is connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 19 shows a nineteenth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the nineteenth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 having a straight suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 includes a plurality of impeller disks arranged in series along the axial length thereof.
  • the casing of the second compressor 20 defines an outlet 21 at an axial end thereof, a main inlet 22 at the other axial end thereof and a single side inlet 23 in an axially intermediate position thereof.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to one of the main inlets 12 of the first compressor 10, and the MP outlet 4 of the refrigeration circuit 1 is connected to the main inlet 22 of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the other main inlet 13 of the first compressor 10, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the side inlet 23 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • Fig. 20 shows a twentieth embodiment of the apparatus for compressing gaseous refrigerant according to the present invention.
  • the apparatus of the twentieth embodiment comprises a first compressor 10 having a double suction configuration and a second compressor 20 also having a double suction configuration.
  • the first compressor 10 includes a pair of main inlets 12 and 13 defined on either axial end of the casing and an outlet 11 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the second compressor 20 also includes a pair of main inlets 22 and 23 defined on either axial end of the casing and an outlet 21 defined in an axially middle part of the casing.
  • the two parts of the dual suction configuration of the first compressor 10 may be either symmetric or asymmetric depending on different design considerations.
  • Each set of impellers may include any number of impeller disks which are typically supported by a common shaft.
  • the two compressors 10 and 20 are driven by an output shaft 31 of a common gas turbine driver 30.
  • the LP outlet 6 of the refrigeration circuit 1 is connected to one of the two main inlets 12 of the first compressor 10, and the MP outlet 5 of the refrigeration circuit 1 is connected to one of the two main inlets 22 of the second compressor 20.
  • the HP outlet 4 of the refrigeration circuit 1 is connected to the other main inlet 12 of the first compressor 10, and the HHP outlet 3 of the refrigeration circuit 1 is connected to the other main inlet 23 of the second compressor 20.
  • the outlet 11 of the first compressor 10 and the outlet 21 of the second compressor 20 are both connected to the inlet 2 of the refrigeration circuit 1.
  • the refrigeration circuit 1 included four outlets LP, MP, HP and HHP which are denoted with numerals 6, 5, 4, 3 and 2, respectively.
  • the refrigeration circuit 1 included four outlets LP, MP, HP and HHP which are denoted with numerals 6, 5, 4, 3 and 2, respectively.
  • notations A, D and S to denote “asymmetric double suction configuration " , “symmetric double suction configuration " and “straight suction configuration” in combination with the associated outlets 6, 5, 4, 3 and 2 of the refrigeration circuit 1
  • each of the illustrated embodiments can be designated by the following notations. These notations are helpful in sorting out different combinations of the compressors and the connections between the compressors and the refrigeration circuit. Also, by using these notations, it is also possible to consider different other combinations of the compressors and the connections between the compressors and the refrigeration circuit. Such other combinations which are not covered by the foregoing embodiments are also part of the present invention.

Landscapes

  • 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)

Abstract

Appareil destiné à comprimer un fluide frigorigène gazeux à utiliser dans un circuit de réfrigération d'une usine de liquéfaction (1) comprenant un circuit de réfrigération (1) et deux compresseurs (10, 20) qui sont fonctionnellement reliés au circuit de réfrigération. L'un des compresseurs est pourvu d'une configuration à double aspiration, et les orifices de sortie et les orifices d'entrée des premier et second compresseurs sont reliés au moins en partie selon une configuration d'écoulement mutuellement parallèle de sorte que l'écoulement de fluide frigorigène qui quitte le circuit de réfrigération depuis une pluralité d'orifices de sortie de celui-ci soit réparti entre les deux compresseurs avant de se rejoindre au niveau de l'orifice d'entrée du circuit de réfrigération.
PCT/JP2013/004568 2013-07-26 2013-07-26 Système de compression à réfrigération utilisant deux compresseurs WO2015011742A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
RU2016106366A RU2629101C1 (ru) 2013-07-26 2013-07-26 Холодильная компрессионная система, использующая два компрессора
AP2015008918A AP2015008918A0 (en) 2013-07-26 2013-07-26 Refrigeration compression system using two compressors
CA2914477A CA2914477C (fr) 2013-07-26 2013-07-26 Systeme de compression a refrigeration utilisant deux compresseurs
PCT/JP2013/004568 WO2015011742A1 (fr) 2013-07-26 2013-07-26 Système de compression à réfrigération utilisant deux compresseurs
AU2013395108A AU2013395108B2 (en) 2013-07-26 2013-07-26 Refrigeration compression system using two compressors
US14/899,226 US20160131422A1 (en) 2013-07-26 2013-07-26 Refrigeration compression system using two compressors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2013/004568 WO2015011742A1 (fr) 2013-07-26 2013-07-26 Système de compression à réfrigération utilisant deux compresseurs

Publications (1)

Publication Number Publication Date
WO2015011742A1 true WO2015011742A1 (fr) 2015-01-29

Family

ID=52392829

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2013/004568 WO2015011742A1 (fr) 2013-07-26 2013-07-26 Système de compression à réfrigération utilisant deux compresseurs

Country Status (6)

Country Link
US (1) US20160131422A1 (fr)
AP (1) AP2015008918A0 (fr)
AU (1) AU2013395108B2 (fr)
CA (1) CA2914477C (fr)
RU (1) RU2629101C1 (fr)
WO (1) WO2015011742A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2013204886B2 (en) * 2013-04-12 2015-04-16 Woodside Energy Technologies Pty Ltd Compressor System and Method for Compressing
IT201600080745A1 (it) * 2016-08-01 2018-02-01 Nuovo Pignone Tecnologie Srl Compressore di refrigerante diviso per la liquefazione di gas naturale

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10544986B2 (en) * 2017-03-29 2020-01-28 Air Products And Chemicals, Inc. Parallel compression in LNG plants using a double flow compressor

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003515720A (ja) * 1999-12-01 2003-05-07 シエル・インターナシヨネイル・リサーチ・マーチヤツピイ・ベー・ウイ 天然ガスの液化プラント
WO2005028975A2 (fr) * 2003-09-23 2005-03-31 Statoil Asa Procede de liquefaction de gaz naturel
US20070204649A1 (en) * 2006-03-06 2007-09-06 Sander Kaart Refrigerant circuit
WO2008095713A2 (fr) * 2007-02-08 2008-08-14 Linde Aktiengesellschaft Procédé de liquéfaction d'un flux riche en hydrocarbures
JP2009138996A (ja) * 2007-12-05 2009-06-25 Hitachi Ltd 冷凍サイクルシステム、天然ガス液化設備、ヒートポンプシステム、及び冷凍サイクルシステムの改造方法
US20110259045A1 (en) * 2008-11-17 2011-10-27 Woodside Energy Limited Power Matched Mixed Refrigerant Compression Circuit

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4929149A (en) * 1985-01-08 1990-05-29 Superstream, Inc. Gas blower
SU1368587A1 (ru) * 1985-12-03 1988-01-23 Московский энергетический институт Способ работы криогенной установки
RU2238486C2 (ru) * 2001-11-05 2004-10-20 Закрытое акционерное общество "РУСХОЛ" Холодильная система
US20090282862A1 (en) * 2006-09-22 2009-11-19 Francois Chantant Method and apparatus for producing a cooled hydrocarbon stream
WO2009071538A2 (fr) * 2007-12-04 2009-06-11 Shell Internationale Research Maatschappij B.V. Procédé et appareil permettant de refroidir et/ou de liquéfier un flux d'hydrocarbure
CA2795970C (fr) * 2010-05-21 2016-11-29 Exxonmobil Upstream Research Company Appareil compresseur dynamique, parallele et procedes associes

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003515720A (ja) * 1999-12-01 2003-05-07 シエル・インターナシヨネイル・リサーチ・マーチヤツピイ・ベー・ウイ 天然ガスの液化プラント
WO2005028975A2 (fr) * 2003-09-23 2005-03-31 Statoil Asa Procede de liquefaction de gaz naturel
US20070204649A1 (en) * 2006-03-06 2007-09-06 Sander Kaart Refrigerant circuit
WO2008095713A2 (fr) * 2007-02-08 2008-08-14 Linde Aktiengesellschaft Procédé de liquéfaction d'un flux riche en hydrocarbures
JP2009138996A (ja) * 2007-12-05 2009-06-25 Hitachi Ltd 冷凍サイクルシステム、天然ガス液化設備、ヒートポンプシステム、及び冷凍サイクルシステムの改造方法
US20110259045A1 (en) * 2008-11-17 2011-10-27 Woodside Energy Limited Power Matched Mixed Refrigerant Compression Circuit

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2013204886B2 (en) * 2013-04-12 2015-04-16 Woodside Energy Technologies Pty Ltd Compressor System and Method for Compressing
IT201600080745A1 (it) * 2016-08-01 2018-02-01 Nuovo Pignone Tecnologie Srl Compressore di refrigerante diviso per la liquefazione di gas naturale
WO2018024576A1 (fr) * 2016-08-01 2018-02-08 Nuovo Pignone Tecnologie Srl Compresseur double de fluide frigorigène pour la liquéfaction de gaz naturel
KR20190033608A (ko) * 2016-08-01 2019-03-29 누보 피그노네 테크놀로지 에스알엘 천연가스의 액화를 위한 분리형 냉매 압축기
KR102300875B1 (ko) * 2016-08-01 2021-09-14 누보 피그노네 테크놀로지 에스알엘 천연가스의 액화를 위한 분리형 냉매 압축기
US11268753B2 (en) 2016-08-01 2022-03-08 Nuovo Pignone Technologie Srl Split refrigerant compressor for the liquefaction of natural gas

Also Published As

Publication number Publication date
AU2013395108B2 (en) 2018-08-02
CA2914477A1 (fr) 2015-01-29
AP2015008918A0 (en) 2015-12-31
US20160131422A1 (en) 2016-05-12
RU2629101C1 (ru) 2017-08-24
CA2914477C (fr) 2019-03-19
AU2013395108A1 (en) 2016-01-07

Similar Documents

Publication Publication Date Title
EP1697689B1 (fr) Systeme de compression a plusieurs flux d'arrivee
JP2015137651A (ja) 空気圧縮のためのシステムおよび方法
AU2011256697B2 (en) Parallel dynamic compressor apparatus and methods related thereto
US9746234B2 (en) Mixed refrigerant compression circuit
CN105408713B (zh) 用于液体天然气生产的系统和集成方法
US9109603B2 (en) Multi-stage centrifugal compressors
EP2981777B1 (fr) Compresseurs à engrenage construit d'une seule pièce pour le pré-refroidissement dans des applications lng
EP3351882B1 (fr) Train de compression comprenant un compresseur centrifuge et installation gnl
US10215190B2 (en) Refrigerant compressing process with cooled motor
US11686316B2 (en) Integrally geared compressor having a combination of centrifugal and positive displacement compression stages
TW201331463A (zh) 一種壓縮機佈置
AU2013395108B2 (en) Refrigeration compression system using two compressors
US20140086733A1 (en) Compressing system
JP2019536969A (ja) 一体型ギヤ付ターボ圧縮機を含む天然ガス液化システム
AU2013204886B2 (en) Compressor System and Method for Compressing
CN109790843B (zh) 用于天然气的液化的分离式制冷剂压缩机

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 13890071

Country of ref document: EP

Kind code of ref document: A1

ENP Entry into the national phase

Ref document number: 2914477

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 14899226

Country of ref document: US

ENP Entry into the national phase

Ref document number: 2013395108

Country of ref document: AU

Date of ref document: 20130726

Kind code of ref document: A

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2016106366

Country of ref document: RU

Kind code of ref document: A

122 Ep: pct application non-entry in european phase

Ref document number: 13890071

Country of ref document: EP

Kind code of ref document: A1