EP3433530B1 - Facility for feeding fuel gas to a member consuming gas and for liquefying said fuel gas - Google Patents

Facility for feeding fuel gas to a member consuming gas and for liquefying said fuel gas Download PDF

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Publication number
EP3433530B1
EP3433530B1 EP17716958.8A EP17716958A EP3433530B1 EP 3433530 B1 EP3433530 B1 EP 3433530B1 EP 17716958 A EP17716958 A EP 17716958A EP 3433530 B1 EP3433530 B1 EP 3433530B1
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EP
European Patent Office
Prior art keywords
path
tank
combustible gas
heat
installation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP17716958.8A
Other languages
German (de)
French (fr)
Other versions
EP3433530A1 (en
Inventor
Bruno Deletre
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Gaztransport et Technigaz SA
Original Assignee
Gaztransport et Technigaz SA
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Filing date
Publication date
Application filed by Gaztransport et Technigaz SA filed Critical Gaztransport et Technigaz SA
Priority to PL17716958T priority Critical patent/PL3433530T3/en
Publication of EP3433530A1 publication Critical patent/EP3433530A1/en
Application granted granted Critical
Publication of EP3433530B1 publication Critical patent/EP3433530B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C9/00Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure
    • F17C9/02Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure with change of state, e.g. vaporisation
    • F17C9/04Recovery of thermal energy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/0002Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the fluid to be liquefied
    • F25J1/0022Hydrocarbons, e.g. natural gas
    • F25J1/0025Boil-off gases "BOG" from storages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0228Coupling of the liquefaction unit to other units or processes, so-called integrated processes
    • F25J1/0229Integration with a unit for using hydrocarbons, e.g. consuming hydrocarbons as feed stock
    • F25J1/023Integration with a unit for using hydrocarbons, e.g. consuming hydrocarbons as feed stock for the combustion as fuels, i.e. integration with the fuel gas system
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0243Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0257Construction and layout of liquefaction equipments, e.g. valves, machines
    • F25J1/0258Construction and layout of liquefaction equipments, e.g. valves, machines vertical layout of the equipments within in the cold box
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0243Start-up or control of the process; Details of the apparatus used; Details of the refrigerant compression system used
    • F25J1/0257Construction and layout of liquefaction equipments, e.g. valves, machines
    • F25J1/0275Construction and layout of liquefaction equipments, e.g. valves, machines adapted for special use of the liquefaction unit, e.g. portable or transportable devices
    • F25J1/0277Offshore use, e.g. during shipping
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J5/00Arrangements of cold exchangers or cold accumulators in separation or liquefaction plants
    • F25J5/002Arrangements of cold exchangers or cold accumulators in separation or liquefaction plants for continuously recuperating cold, i.e. in a so-called recuperative heat exchanger
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/10Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically
    • F28D7/12Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged one within the other, e.g. concentrically the surrounding tube being closed at one end, e.g. return type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/16Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation
    • F28D7/163Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation with conduit assemblies having a particular shape, e.g. square or annular; with assemblies of conduits having different geometrical features; with multiple groups of conduits connected in series or parallel and arranged inside common casing
    • F28D7/1669Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation with conduit assemblies having a particular shape, e.g. square or annular; with assemblies of conduits having different geometrical features; with multiple groups of conduits connected in series or parallel and arranged inside common casing the conduit assemblies having an annular shape; the conduits being assembled around a central distribution tube
    • F28D7/1676Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation with conduit assemblies having a particular shape, e.g. square or annular; with assemblies of conduits having different geometrical features; with multiple groups of conduits connected in series or parallel and arranged inside common casing the conduit assemblies having an annular shape; the conduits being assembled around a central distribution tube with particular pattern of flow of the heat exchange media, e.g. change of flow direction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F27/00Control arrangements or safety devices specially adapted for heat-exchange or heat-transfer apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01Mounting arrangements
    • F17C2205/0123Mounting arrangements characterised by number of vessels
    • F17C2205/013Two or more vessels
    • F17C2205/0134Two or more vessels characterised by the presence of fluid connection between vessels
    • F17C2205/0142Two or more vessels characterised by the presence of fluid connection between vessels bundled in parallel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0352Pipes
    • F17C2205/0367Arrangements in parallel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • F17C2221/032Hydrocarbons
    • F17C2221/033Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/033Small pressure, e.g. for liquefied gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/04Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
    • F17C2223/042Localisation of the removal point
    • F17C2223/043Localisation of the removal point in the gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/04Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
    • F17C2223/042Localisation of the removal point
    • F17C2223/046Localisation of the removal point in the liquid
    • F17C2223/047Localisation of the removal point in the liquid with a dip tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2225/00Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/01Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the phase
    • F17C2225/0107Single phase
    • F17C2225/0123Single phase gaseous, e.g. CNG, GNC
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2225/00Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/01Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the phase
    • F17C2225/0146Two-phase
    • F17C2225/0153Liquefied gas, e.g. LPG, GPL
    • F17C2225/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2225/00Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/03Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the pressure level
    • F17C2225/033Small pressure, e.g. for liquefied gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2225/00Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/03Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the pressure level
    • F17C2225/035High pressure, i.e. between 10 and 80 bars
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2225/00Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/04Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by other properties of handled fluid after transfer
    • F17C2225/042Localisation of the filling point
    • F17C2225/043Localisation of the filling point in the gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/01Propulsion of the fluid
    • F17C2227/0121Propulsion of the fluid by gravity
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/01Propulsion of the fluid
    • F17C2227/0128Propulsion of the fluid with pumps or compressors
    • F17C2227/0157Compressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/03Heat exchange with the fluid
    • F17C2227/0302Heat exchange with the fluid by heating
    • F17C2227/0306Heat exchange with the fluid by heating using the same fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/03Heat exchange with the fluid
    • F17C2227/0337Heat exchange with the fluid by cooling
    • F17C2227/0339Heat exchange with the fluid by cooling using the same fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/03Heat exchange with the fluid
    • F17C2227/0367Localisation of heat exchange
    • F17C2227/0388Localisation of heat exchange separate
    • F17C2227/0393Localisation of heat exchange separate using a vaporiser
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/04Methods for emptying or filling
    • F17C2227/044Methods for emptying or filling by purging
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/03Control means
    • F17C2250/032Control means using computers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04Indicating or measuring of parameters as input values
    • F17C2250/0404Parameters indicated or measured
    • F17C2250/043Pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04Indicating or measuring of parameters as input values
    • F17C2250/0404Parameters indicated or measured
    • F17C2250/0443Flow or movement of content
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/06Controlling or regulating of parameters as output values
    • F17C2250/0605Parameters
    • F17C2250/0626Pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/06Controlling or regulating of parameters as output values
    • F17C2250/0605Parameters
    • F17C2250/0636Flow or movement of content
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/03Dealing with losses
    • F17C2260/035Dealing with losses of fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/05Improving chemical properties
    • F17C2260/056Improving fluid characteristics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2265/00Effects achieved by gas storage or gas handling
    • F17C2265/01Purifying the fluid
    • F17C2265/015Purifying the fluid by separating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2265/00Effects achieved by gas storage or gas handling
    • F17C2265/01Purifying the fluid
    • F17C2265/015Purifying the fluid by separating
    • F17C2265/017Purifying the fluid by separating different phases of a same fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2265/00Effects achieved by gas storage or gas handling
    • F17C2265/03Treating the boil-off
    • F17C2265/032Treating the boil-off by recovery
    • F17C2265/033Treating the boil-off by recovery with cooling
    • F17C2265/034Treating the boil-off by recovery with cooling with condensing the gas phase
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2265/00Effects achieved by gas storage or gas handling
    • F17C2265/06Fluid distribution
    • F17C2265/066Fluid distribution for feeding engines for propulsion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2265/00Effects achieved by gas storage or gas handling
    • F17C2265/07Generating electrical power as side effect
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0102Applications for fluid transport or storage on or in the water
    • F17C2270/0105Ships
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0102Applications for fluid transport or storage on or in the water
    • F17C2270/0105Ships
    • F17C2270/0107Wall panels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2290/00Other details not covered by groups F25J2200/00 - F25J2280/00
    • F25J2290/62Details of storing a fluid in a tank
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2265/00Safety or protection arrangements; Arrangements for preventing malfunction
    • F28F2265/26Safety or protection arrangements; Arrangements for preventing malfunction for allowing differential expansion between elements

Definitions

  • the invention relates to the field of installations for processing a combustible gas, for example liquefied natural gas (LNG).
  • a combustible gas for example liquefied natural gas (LNG).
  • LNG liquefied natural gas
  • the invention relates more particularly to an installation aimed, on the one hand, at supplying combustible gas to a gas consuming member and, on the other hand, at liquefying said combustible gas.
  • Liquefied natural gas is stored in sealed and thermally insulating tanks, in a two-phase liquid / vapor equilibrium state, at cryogenic temperatures.
  • the thermal insulation barriers of liquefied natural gas storage tanks are the seat of a thermal flux tending to heat the contents of the tanks, which results in evaporation of the liquefied natural gas.
  • the gas resulting from natural evaporation is generally used to feed a gas consuming organ in order to develop it.
  • the evaporated gas is used to power the powertrain making it possible to propel the ship or the generator sets supplying the electricity necessary for the operation of the on-board equipment.
  • such a practice makes it possible to recover the gas resulting from natural evaporation in the tanks, it does not make it possible to reduce its quantity.
  • the composition of the vapor phase resulting from natural evaporation is different from that of the liquid phase and moreover tends to vary over time.
  • the vapor phase resulting from natural evaporation naturally presents a composition richer in the most volatile components, such as nitrogen for liquefied natural gas, than the liquid phase.
  • the calorific value of the gas resulting from natural evaporation like that of the liquefied gas remaining in the tank is variable over time when natural evaporation prevails.
  • the supply of a consumer organ with a combustible gas whose calorific capacity undergoes significant variations is likely to cause imperfect combustion of the gas as well as malfunctions and variable efficiency of the gas consuming member.
  • JP0960799 describes an LNG storage installation with an LNG vaporization circuit and a gas recondensation circuit from natural evaporation.
  • the vaporization of LNG in the vaporization circuit is produced by the heat supplied by the heater 24.
  • the document KR20100021774 describes an apparatus for supplying combustible gas to a high pressure gas injection engine in a ship.
  • This device comprises a liquefied gas supply line connecting a liquefied gas fuel tank to a high pressure gas injection engine, a re-liquefaction circulation line, a compression unit installed in the liquid supply line.
  • liquefied gas liquefied gas
  • a vaporized gas liquefaction unit a vaporized gas re-liquefaction unit
  • the controller regulates the adjustment pressure of the liquefied fuel tank and the quantity of liquefied gas supply according to the load variations acting on the high pressure gas injection engine.
  • An idea underlying the invention is to propose an installation aiming at supplying combustible gas to a gas consuming member and at re-liquefying said combustible gas which does not have at least some of the drawbacks of the prior art.
  • Certain aspects of the invention start from the idea of using the liquid phase of the combustible gas as a refrigerant in a heat exchanger to cool and condense the gas resulting from natural evaporation.
  • such an installation may include one or more of the following characteristics.
  • the outlet of the spraying path is arranged lower than the inlet of the spraying path.
  • both the first flow of combustible gas in the condensation path and the second flow of combustible gas in the vaporization path realize a downward movement, which promotes the exploitation of gravity to maintain the circulation of these two flows.
  • this orientation of the flows makes it possible to carry out a co-current heat exchange between the liquid phase of the combustible gas used as refrigerant and the gas resulting from natural evaporation to promote an isothermal heat exchange by phase change.
  • the vaporization path is configured to flow the second flow of combustible gas in the form of falling liquid films.
  • the vaporization path of the heat exchanger comprises a phase separation tank disposed at the bottom of the vaporization path, the phase separation tank having a bottom wall and a side wall extending upward from the bottom wall, the outlet of the spray path opening through the side wall of the phase separation tank at a position spaced above the bottom wall.
  • a purge circuit opens out through the bottom wall of the phase separation tank in order to be able to evacuate a liquid phase from the phase separation tank by gravity.
  • an evacuation of this liquid fraction is facilitated in order to avoid saturating or obstruct the spray path.
  • the vaporization path of the heat exchanger is placed in depression, that is to say at a pressure lower than the pressure prevailing in the vapor phase of the sealed and thermally insulating tank. It is thus possible to further force the vaporization of the combustible gas in the vaporization path, by the cumulative effect of the heat supply in the condensation path and of the vacuum in the vaporization path. In addition, since the vacuum moves the two-phase equilibrium temperature down in the vaporization path, it is thus possible to increase the heat flow transferred from the vapor phase in the condensation path to the gas located in the vaporization route.
  • the absolute pressure in the vaporization path is greater than 120 mbar absolute. It is indeed preferable for the pressure inside the vaporization path to be higher than the pressure corresponding to the triple point of the methane phase diagram so as to avoid solidification of the natural gas inside the vaporization path. .
  • the pressure in the vaporization path can in particular be between 500 mbar absolute and 980 mbar absolute.
  • the installation further comprises a vacuum pump or vacuum pump connected to the vaporization path to place the vaporization path of the heat exchanger at a pressure lower than the pressure prevailing in the vapor phase of the waterproof and thermally insulating tank
  • such a vacuum pump can be controlled as a function of a flow rate setpoint or a pressure setpoint.
  • a flow or pressure setpoint can be predetermined or generated by the gas consuming member.
  • connection between the outlet of the vaporization channel and the gas consuming member can be direct or indirect, depending on the requirements of the consuming member.
  • the aforementioned vacuum pump is arranged between the outlet of the vaporization path and the gas consuming member.
  • a compressor is arranged between the outlet of the vaporization path and the gas consuming member to supply a flow of gas in the vapor phase at a pressure higher than the storage pressure in the tank.
  • the heat exchanger comprises a sealed and thermally insulating envelope delimiting an interior space containing the condensation channel, the envelope being arranged above the sealed and thermally insulating tank and comprising a lower opening communicating with the interior space of the sealed and thermally insulating tank and constituting the outlet of the condensation channel.
  • Such a sealed and thermally insulating envelope can be produced in different ways, for example in one piece with a top wall of the tank or else in the form of an assembly attached to the top wall of the tank.
  • a top wall of the sealed and thermally insulating tank has an opening connected to the lower opening of the envelope, the envelope further comprising a fixing flange arranged around the lower opening of the envelope, the fixing flange being attached to the top wall of the sealed and thermally insulating tank around the opening of the top wall.
  • the heat exchanger further comprises a collecting pipe extending from the lower opening of the envelope to near a top wall of the envelope and having a lower end opening into the interior space of the tank and an upper end opening into the interior space of the casing, the collecting pipe delimiting within the interior space of the casing an interior space of the collecting pipe forming the vapor collector circuit and an outer space of the collecting pipe forming the condensation path of the heat exchanger.
  • the heat exchanger and the vapor collecting circuit can be produced in a relatively space-saving integrated form and having a relatively reduced exchange surface with the external environment, which limits the heat flows liable to increase natural evaporation.
  • the installation comprises a plurality of sealed and thermally insulating tanks comprising an interior space intended to be filled with combustible gas in a liquid-vapor two-phase equilibrium state, said vapor collector circuit being a collector circuit common connecting the inlet of the condensation channel to each of said tanks to collect the gases from evaporation in each of the tanks. It is thus possible to operate the heat exchanger jointly for a set of tanks.
  • the inlet distributor is disposed higher than the upper end of the collecting pipe.
  • the parallel tubes can extend over almost the same length as the collecting pipe.
  • the tubes parallel to the manifold have heat exchange fins arranged on the outer surface of the tubes parallel to the manifold.
  • the first flow of combustible gas cooled by the heat exchange can flow by natural convection, ie by gravity, towards the interior space of the tank, which favors the production of a suction in the vapor collector circuit, thus maintaining the first flow without additional mechanical work.
  • this method is implemented so as to vaporize all or almost all of the second flow of combustible gas in the vaporization path.
  • the content of the most volatile compounds is substantially equal to that of the liquid phase of the gas stored in the tank.
  • the concentration of the most volatile compounds in the vaporized gas flow is therefore limited and substantially constant over time.
  • the vaporization of the liquefied gas can be carried out without the aid of an external heat source, as opposed to forced vaporization installations using a heat exchange with sea water, a intermediate liquid or combustion gases from the engine or specific burners.
  • the gas present in the upper portion of the interior space of the tank thus acts as a hot source for the flow to be vaporized. Also, the installation allows both to produce a flow of vapor and to cool and condense the vapor phase resulting from natural evaporation present in the gaseous sky of the tank, so as to limit natural evaporation.
  • the invention provides a ship comprising an aforementioned installation.
  • the invention also provides a method of loading or unloading such a ship, in which combustible gas is conveyed through insulated pipes from or to a floating or terrestrial storage installation towards or from the tank. waterproof and thermally insulating of the ship.
  • the invention also provides a transfer system for a combustible gas, the system comprising the abovementioned ship, isolated pipes arranged so as to connect the tank installed in the hull of the ship to a floating storage installation or terrestrial and a pump for driving a flow of combustible gas through the insulated pipes from or to the floating or terrestrial storage installation towards or from the watertight and thermally insulating vessel of the ship.
  • combustion gas is generic in nature and is intended equally to refer to a gas consisting of a single pure body or to a gas mixture consisting of a plurality of components.
  • an installation 1 aiming, on the one hand, at supplying combustible gas to one or more gas consuming members and, on the other hand, at liquefying combustible gas is illustrated.
  • Such an installation 1 can be installed on land or on a floating structure.
  • the installation 1 can be intended for a liquefaction or regasification barge, for a liquefied natural gas transport vessel, such as an LNG carrier, or more generally for any equipped vessel. of a gas consuming organ.
  • Installation 1 illustrated on the figure 1 comprises a steam outlet line 3 which can supply directly or indirectly different types of fuel gas consuming devices not shown, namely in particular a burner, an electric generator and / or an engine for the propulsion of a ship.
  • Such a burner is integrated into an energy production installation.
  • the energy production installation may in particular include a steam production boiler.
  • the steam can be used to power steam turbines for energy production and / or to power a ship's heating network.
  • Such an electric generator comprises for example a thermal engine with mixed diesel / natural gas supply, for example of DFDE technology for “Dual Fuel Diesel Electric” in English.
  • a thermal engine with mixed diesel / natural gas supply for example of DFDE technology for “Dual Fuel Diesel Electric” in English.
  • Such an engine can burn a mixture of diesel and natural gas or use either of these two fuels.
  • the natural gas supplying such a heat engine must have a pressure of the order of a few bars to a few tens of bars, for example of around 6 to 8 bars absolute.
  • one or more compressors 4 can be provided on the steam outlet line 3.
  • Such an engine for propelling the ship is, for example, a low-speed two-stroke dual-fuel engine of “ME-GI” technology, developed by the company MAN.
  • Such an engine uses natural gas as fuel and a small amount of pilot fuel which is injected before the injection of natural gas so that it ignites.
  • natural gas must first be compressed under a high pressure of between 150 and 400 bar absolute, and more particularly between 250 and 300 bar absolute.
  • one or more compressors 4 can be provided on the steam outlet line 3.
  • the installation 1 comprises a sealed and thermally insulating tank 2.
  • the tank 2 is a membrane tank.
  • membrane tanks are described in patent applications WO14057221 , FR2691520 and FR2877638 .
  • Such membrane tanks are intended to store combustible gas at pressures substantially equal to atmospheric pressure or slightly higher.
  • the tank 2 can also be a self-supporting tank and can in particular have a parallelepiped, prismatic, spherical, cylindrical or multi-lobic shape. Certain types of tank 2 allow gas to be stored at pressures substantially higher than atmospheric pressure.
  • the tank 2 has an internal space 7 intended to be filled with combustible gas.
  • the combustible gas can in particular be a liquefied natural gas (LNG), that is to say a gaseous mixture mainly comprising methane as well as one or more other hydrocarbons, such as ethane, propane, n-butane , i-butane, n-pentane i-pentane, neopentane, and nitrogen in small proportion.
  • LNG liquefied natural gas
  • the combustible gas can also be ethane or a liquefied petroleum gas (LPG), that is to say a mixture of hydrocarbons resulting from the refining of petroleum comprising essentially propane and butane.
  • the combustible gas is stored in the internal space 7 of the tank 2 in a liquid-vapor two-phase equilibrium state.
  • the gas is therefore present in the vapor phase, in the upper part 8 of the tank 2 and in the liquid phase in the lower part 9 of the tank 2.
  • This stratification is obtained naturally due to the specific density of each phase.
  • the location of the liquid-vapor interface naturally depends on the filling level of the tank 2.
  • the equilibrium temperature of the liquefied natural gas corresponding to its two-phase liquid-vapor equilibrium state is approximately -162 ° C when it is stored at atmospheric pressure.
  • a heat exchanger 10 which jointly makes it possible to re-liquefy gas in the vapor phase originating from natural evaporation in the upper part 8 of the tank 2 while forcibly vaporizing gas in the liquid phase taken from the lower part 9 of the tank 2.
  • the vapor collector circuit 13 and the condensate return circuit 14 pass through the top wall 5 of the tank 2, but other arrangements are possible, in particular for the condensate return circuit 14, for example by crossing the wall lateral 6 in the upper portion 8 of the tank 2.
  • the steam collector circuit 13 may include several branches connected to several tanks to serve as a common collector connecting a set of tanks to the condensation path of the heat exchanger 10. Valves, not shown, can be provided on each branch to keep the possibility of isolating the tanks from each other in this case.
  • the condensate return circuit 14 could be connected to several tanks.
  • the heat exchanger 10 also has a vaporization circuit 15 which is arranged in the interior space 12, shown here in the form of a helical coil but the shape of which can vary to a large extent.
  • the vaporization circuit 15 is supplied with combustible gas in liquid phase from the lower part 9 of the tank 2 by a circulation pump 16 and an inlet pipe 17 joining the inlet of the vaporization circuit 15 by passing through seals the outer envelope 11.
  • the gas in the liquid phase circulating in the vaporization circuit 15 is vaporized and the vapor phase thus formed flows towards the outlet line 3, which is connected to the outlet of the vaporization circuit 15 by sealingly passing through the external envelope 11.
  • the outlet of the vaporization circuit 15 is preferably located lower than the inlet of the vaporization circuit 15.
  • a vacuum pump 51 can be used, for example in place of the compressor 4.
  • the vacuum pump 51 must be a cryogenic pump, that is to say a pump capable of withstanding cryogenic temperatures below -150 ° vs. It must also comply with ATEX regulations, that is to say designed to eliminate any risk of explosion.
  • a pressure drop member for example an expansion valve 45, is placed at the inlet of the vaporization circuit 15, preferably inside the external envelope 11.
  • the figure 1 shows in broken lines another possible arrangement of the vapor collecting circuit, in the form of a collecting pipe 113 concentrically disposed in the condensate return circuit 14 from the upper part 8 of the tank 2 to the top of the interior space 12.
  • the admission of gas in the vapor phase takes place from the interior of the collecting pipe 113, while the condensate return flows in the annular space around the collecting pipe 113 in the condensate return circuit 14.
  • the operation is identical.
  • FIG. 1 illustrates a heat exchanger whose vaporization path is contained and bathed in the fluid of the condensation path
  • a reverse configuration is also possible, namely a condensation path contained and bathed in the fluid of the vaporization path.
  • Other configurations are also possible, for example with a heat exchanger in which the two channels have substantially the same volume.
  • the outer casing 111 has the general shape of a cylindrical bottle with a vertical axis, turned upside down with the neck. More specifically, the main body delimiting the interior space 112 has a larger diameter than the condensate return tube 114.
  • the watertight and thermally insulating walls are here formed of two parallel layers of mutually spaced metal sheets, with a vacuum space between the two. Other forms of thermal insulation could be used.
  • the condensate return tube 114 has bellows for absorbing thermal contraction when the temperature of the outer casing 111 changes, especially when it is put into service. It is terminated at its lower end by a fixing flange 21 for fixing to the top wall of the tank 2.
  • the collecting pipe 213 is arranged concentrically in the condensate return tube 114 from the end of the condensate return tube 114 and enters the interior space 112 over a large part of its height.
  • the upper end of the collecting pipe 213 is open and opens into the upper part of the interior space 112.
  • fixing members can be provided to link the collecting pipe 213 to the external envelope 111.
  • fixing lugs 22 are here provided at the upper end of the collecting pipe 213 and attached to the vaporization circuit 115, itself fixed to the external envelope 111.
  • the finned tubes 25 each have an upper end 27 opening into the annular chamber 26 of the inlet distributor 23 through the bottom wall thereof and a lower end 28 opening into the annular chamber 29 of the outlet housing 24 to through the cover wall of it. They constitute the heat exchange walls of the heat exchanger 110, which make it possible to jointly carry out the vaporization of the liquid phase flowing downwards in the finned tubes 25 and the condensation of the gaseous phase flowing down in the interior space 112.
  • the finned tubes 25 are distributed throughout the interior space 112 all around the collecting pipe 213, as partially shown in the figure 3 , in order to maximize the exchange surface between the two flows and to homogenize the heat transfers.
  • the figure 4 shows two embodiments of the finned tubes 25.
  • the tube body 30 is surrounded by fins 31 in the form of discs extending transversely to the tube body 30 and distributed in a mutually spaced manner over the entire length of tube body 30.
  • the tube body 30 is surrounded by fins 32 in the form of rectangular or polygonal blades extending parallel to the tube body 30 over the entire length of the tube body 30 and distributed in a mutually spaced manner all around of the tube body 30.
  • the fins are eliminated, which makes it possible to reduce the lateral size of each tube and therefore to increase the number of tubes, to also obtain a high exchange surface.
  • the annular chamber 26 of the inlet distributor 23 has here a square cross section and extends in line with the fin tubes 25, therefore at the periphery of the collecting pipe 213. Furthermore, a conical wall is arranged in the center of the distributor inlet 23, with its top facing the upper end of the collecting pipe 213 to close the center of the inlet distributor 23, and thus force the vapor phase to flow laterally towards the top of the fin tubes 25 in leaving the collecting pipe 213.
  • An inlet tube 117 extends laterally from the annular chamber 26 to the outside of the outer casing 111. Sealed welds or seals, not shown, are provided around the inlet tube 117 at the level of the crossing of the outer casing 111 to maintain the sealing thereof.
  • the inlet tube 117 is connected to the circulation pump 16 by any suitable pipe, preferably provided with thermal insulation.
  • the outlet casing 24 has a hollow toroidal shape around and away from the collecting pipe 213. Its bottom wall 33 is concave in order to form a phase separation tank which makes it possible to collect by gravity the non-vaporized part of the flow of gas in liquid phase injected from the inlet tube 117.
  • a purge pipe 34 opening at the bottom of the bottom wall 33 makes it possible to evacuate this liquid fraction, for example to reinject it into the tank 2.
  • an outlet tube 103 extends laterally from the annular chamber 29 to the outside of the envelope 111. The outlet tube 103 opens into the annular chamber 29 above the concave bottom wall 33, in order to avoid collecting the liquid phase.
  • the filling level of the bottom wall 33 must be kept relatively low to avoid an overflow of the liquid phase towards the outlet tube 103. Sealed welds or seals not shown are provided around the tube. exit 103 at the crossing of the outer casing 111 to maintain the seal thereof.
  • the outlet tube 103 is connected to the fuel gas consuming members, directly or via other gas processing equipment, for example, compressor, heater, etc.
  • the latter relatively hot compared to the liquid phase located in the lower part 9 of the tank 2, enters through the collecting pipe 213 and arrives at the top of the heat exchanger 110.
  • the architecture shown here with an inlet at the top and an outlet at the bottom uses a film falling technique.
  • the operation to be obtained is that this film has lost all of the components which can vaporize during the time between its entering chamber 26 and arriving in chamber 29, subject to the low volatility bodies which it is likely to contain and which will then arrive in liquid phase on the bottom wall 33.
  • a valve 49 is preferably arranged on the purge pipe 34, to close the purge pipe 34 during normal operation of the installation and open the purge pipe 34 intermittently to evacuate the liquid fraction rich in heavy bodies.
  • the evacuation of the liquid fraction can be brought about either by injection of gas under pressure into the inlet tube 117, or by gravity under the sole effect of the hydrostatic pressure of the accumulated heavy bodies. This purge operation can thus be done even when the installation is in operation.
  • a valve 149 is used on the purge pipe 34 instead of the valve 49, in order to be able to close the purge pipe 34 if necessary and open the purge pipe 34 intermittently or continuously to evacuate the liquid fraction rich in heavy bodies .
  • the evacuation of the liquid fraction can be caused by gravity when the valve is in the open position, under the sole effect of the hydrostatic pressure of the accumulated heavy bodies. This purge operation can also be done when the installation is in operation.
  • a pump external to the tank can be used to evacuate this remaining liquid fraction, intermittently or continuously.
  • a pump external to the tank can be used to evacuate this remaining liquid fraction, intermittently or continuously.
  • One of the advantages of this architecture is that the risk of saturation of the vaporization circuit 115 by the liquid phase is relatively limited: if the heat supplied by the vapor is insufficient to vaporize the liquid, the remaining liquid phase can be evacuated as it arrives without interrupting the spraying process. This would not be the case with a boiling vessel fed from below and in which a liquid heel is brought to the boil.
  • valves 52 and 149 When the vaporization circuit 115 is placed under vacuum, a second valve 52 is added to the purge pipe 34 upstream of the valve 149 in order to create a buffer volume 53 which can take the form of a pipe or a reservoir.
  • the operation of valves 52 and 149 is alternative: we start by opening the second valve 52 to let the buffer space 53 fill with heavy bodies. Then close the second valve 52 before opening the valve 149 to empty the buffer volume by gravity before closing the valve 149.
  • the opening of the valves 52 and 149 can be caused either by gas injection or by electric control as for solenoid valves.
  • the opening frequency of valves 52 and 149 is directly linked to the composition of the LNG, so the more the LNG contains a large fraction of heavy compounds the greater the opening frequency of the valves 52 and 149.
  • the architecture of the heat exchanger 110 makes it possible to carry out a heat exchange with parallel currents or co-currents. In theory, this form of heat exchange has less efficiency than counter-current heat exchange.
  • this form of heat exchange has less efficiency than counter-current heat exchange.
  • the two fluids enter the exchanger with a given temperature difference between the two fluids. If the heat exchange is done against the current, the outlet temperature of one of the fluids tends towards the inlet temperature of the other and vice versa.
  • the two fluids tend towards a mixing temperature.
  • the proportion of sensible heat to bring this vapor to -160 ° C is approximately 130 kJ / kg while the latent heat necessary to condense it is 510kJ / kg.
  • the majority of the heat transfer isothermal. It is the same for the liquid phase in the vaporization circuit 115.
  • FIG. 6 there is a cutaway view of an LNG tanker 70 equipped with a fuel gas supply installation for gas consuming bodies and liquefaction of said fuel gas as described above.
  • the figure 6 shows a sealed and insulated tank 71 of generally prismatic shape mounted in the double hull 72 of the ship.
  • the wall of the tank 71 comprises a primary waterproof barrier intended to be in contact with the LNG contained in the tank, a secondary waterproof barrier arranged between the primary waterproof barrier and the double hull 72 of the ship, and two insulating barriers arranged respectively between the primary waterproof barrier and the secondary waterproof barrier and between the secondary waterproof barrier and the double shell 72.
  • loading / unloading lines 73 arranged on the upper deck of the ship can be connected, using appropriate connectors, to a maritime or port terminal to transfer a cargo of LNG from or to the tank 71.
  • the figure 6 represents an example of a maritime terminal comprising a loading and unloading station 75, an underwater pipe 76 and a shore installation 77.
  • the loading and unloading station 75 is a fixed offshore installation comprising a movable arm 74 and a tower 78 which supports the movable arm 74.
  • the movable arm 74 carries a bundle of insulated flexible pipes 79 which can be connected to the loading / unloading pipes 73.
  • the movable arm 74 can be adjusted to suit all sizes of LNG carriers.
  • a connection pipe, not shown, extends inside the tower 78.
  • the loading and unloading station 75 allows the loading and unloading of the LNG carrier 70 from or to the onshore installation 77.
  • This comprises liquefied gas storage tanks 80 and connecting pipes 81 connected by the subsea pipe 76 to the loading or unloading station 75.
  • the subsea pipe 76 allows the transfer of the liquefied gas between the loading or unloading station 75 and the shore installation 77 over a long distance, for example 5 km, which makes it possible to keep the LNG carrier 70 at a great distance from the coast during the loading and unloading operations.
  • pumps on board the ship 70 and / or pumps fitted to the shore installation 77 and / or pumps fitted to the loading and unloading station 75 are used.

Description

Domaine techniqueTechnical area

L'invention se rapporte au domaine des installations de traitement d'un gaz combustible, par exemple du gaz naturel liquéfié (GNL).The invention relates to the field of installations for processing a combustible gas, for example liquefied natural gas (LNG).

L'invention vise plus particulièrement une installation visant, d'une part, à alimenter en gaz combustible un organe consommateur de gaz et, d'autre part, à liquéfier ledit gaz combustible.The invention relates more particularly to an installation aimed, on the one hand, at supplying combustible gas to a gas consuming member and, on the other hand, at liquefying said combustible gas.

Arrière-plan technologiqueTechnological background

Le gaz naturel liquéfié est stocké dans des cuves étanches et thermiquement isolantes, dans un état d'équilibre diphasique liquide/vapeur, à des températures cryogéniques. Les barrières d'isolation thermique des cuves de stockage de gaz naturel liquéfié sont le siège d'un flux thermique tendant à réchauffer le contenu des cuves, ce qui se traduit par une évaporation du gaz naturel liquéfié. Le gaz issu de l'évaporation naturelle est généralement utilisé pour alimenter un organe consommateur de gaz afin de le valoriser. Ainsi, sur un navire méthanier par exemple, le gaz évaporé est utilisé pour alimenter le groupe motopropulseur permettant de propulser le navire ou les groupes électrogènes fournissant l'électricité nécessaire au fonctionnement des équipements de bord. Toutefois, si une telle pratique permet de valoriser le gaz issu de l'évaporation naturelle dans les cuves, elle ne permet pas de diminuer sa quantité.Liquefied natural gas is stored in sealed and thermally insulating tanks, in a two-phase liquid / vapor equilibrium state, at cryogenic temperatures. The thermal insulation barriers of liquefied natural gas storage tanks are the seat of a thermal flux tending to heat the contents of the tanks, which results in evaporation of the liquefied natural gas. The gas resulting from natural evaporation is generally used to feed a gas consuming organ in order to develop it. Thus, on an LNG tanker for example, the evaporated gas is used to power the powertrain making it possible to propel the ship or the generator sets supplying the electricity necessary for the operation of the on-board equipment. However, if such a practice makes it possible to recover the gas resulting from natural evaporation in the tanks, it does not make it possible to reduce its quantity.

De plus, lorsque le gaz combustible est constitué d'un mélange gazeux, la composition de la phase vapeur issue de l'évaporation naturelle est différente de celle de la phase liquide et a en outre tendance à varier dans le temps. En effet, la phase vapeur issue de l'évaporation naturelle présente naturellement une composition plus riche en composants les plus volatils, tels que l'azote pour le gaz naturel liquéfié, que la phase liquide. Or, il résulte de ces variations de composition que le pouvoir calorifique du gaz issu de l'évaporation naturelle comme celui du gaz liquéfié restant dans la cuve est variable au cours du temps lorsque l'évaporation naturelle prévaut. Or, l'alimentation d'un organe consommateur avec un gaz combustible dont la capacité calorifique subit d'importantes variations est susceptible d'entraîner une combustion imparfaite du gaz ainsi que des défauts de fonctionnement et un rendement variable de l'organe consommateur de gaz.In addition, when the combustible gas consists of a gaseous mixture, the composition of the vapor phase resulting from natural evaporation is different from that of the liquid phase and moreover tends to vary over time. Indeed, the vapor phase resulting from natural evaporation naturally presents a composition richer in the most volatile components, such as nitrogen for liquefied natural gas, than the liquid phase. However, it follows from these variations in composition that the calorific value of the gas resulting from natural evaporation like that of the liquefied gas remaining in the tank is variable over time when natural evaporation prevails. However, the supply of a consumer organ with a combustible gas whose calorific capacity undergoes significant variations is likely to cause imperfect combustion of the gas as well as malfunctions and variable efficiency of the gas consuming member.

On connaît d'après US-A-2010170297 un dispositif de re-liquéfaction du gaz issu de l'évaporation naturelle dans une cuve de GNL. Ce dispositif comporte une unité d'échange de chaleur disposée au-dessus de la cuve de GNL pour condenser le gaz issu de l'évaporation naturelle par échange de chaleur avec un liquide réfrigérant secondaire tel que l'azote liquide. L'installation prévue pour produire, refroidir et liquéfier l'azote est consommatrice d'énergie.We know from US-A-2010170297 a device for re-liquefying the gas resulting from natural evaporation in an LNG tank. This device comprises a heat exchange unit arranged above the LNG tank to condense the gas resulting from natural evaporation by heat exchange with a secondary coolant such as liquid nitrogen. The installation intended to produce, cool and liquefy nitrogen consumes energy.

JP0960799 décrit une installation de stockage de GNL avec un circuit de vaporisation du GNL et un circuit de recondensation du gaz issu de l'évaporation naturelle. La vaporisation du GNL dans le circuit de vaporisation est produite par la chaleur fournie par le réchauffeur 24. JP0960799 describes an LNG storage installation with an LNG vaporization circuit and a gas recondensation circuit from natural evaporation. The vaporization of LNG in the vaporization circuit is produced by the heat supplied by the heater 24.

Le document KR20100021774 décrit un appareil pour fournir du gaz combustible à un moteur à injection de gaz à haute pression dans un navire. Cet appareil comporte une conduite d'alimentation en gaz liquéfié reliant une cuve de carburant de gaz liquéfié à un moteur à injection haute pression de gaz, une conduite de circulation de re-liquéfaction, une unité de compression installée dans la conduite d'alimentation en gaz liquéfié, une unité de liquéfaction de gaz vaporisé, une unité de re-liquéfaction de gaz vaporisé et un contrôleur. Le contrôleur régule la pression de réglage du réservoir de carburant liquéfié et la quantité d'alimentation en gaz liquéfié en fonction des variations de charge agissant sur le moteur à injection haute pression de gaz.The document KR20100021774 describes an apparatus for supplying combustible gas to a high pressure gas injection engine in a ship. This device comprises a liquefied gas supply line connecting a liquefied gas fuel tank to a high pressure gas injection engine, a re-liquefaction circulation line, a compression unit installed in the liquid supply line. liquefied gas, a vaporized gas liquefaction unit, a vaporized gas re-liquefaction unit and a controller. The controller regulates the adjustment pressure of the liquefied fuel tank and the quantity of liquefied gas supply according to the load variations acting on the high pressure gas injection engine.

Résumésummary

Une idée à la base de l'invention est de proposer une installation visant à alimenter en gaz combustible un organe consommateur de gaz et à re-liquéfier ledit gaz combustible qui ne présente pas au moins certains des inconvénients de l'art antérieur. Certains aspects de l'invention partent de l'idée d'utiliser la phase liquide du gaz combustible comme réfrigérant dans un échangeur de chaleur pour refroidir et condenser le gaz issu de l'évaporation naturelle.An idea underlying the invention is to propose an installation aiming at supplying combustible gas to a gas consuming member and at re-liquefying said combustible gas which does not have at least some of the drawbacks of the prior art. Certain aspects of the invention start from the idea of using the liquid phase of the combustible gas as a refrigerant in a heat exchanger to cool and condense the gas resulting from natural evaporation.

Selon un mode de réalisation, l'invention fournit une installation d'alimentation en gaz combustible d'un organe consommateur de gaz et de liquéfaction dudit gaz combustible, l'installation comportant :

  • une cuve étanche et thermiquement isolante comportant un espace intérieur destiné à être rempli de gaz combustible dans un état d'équilibre diphasique liquide-vapeur;
  • un échangeur de chaleur disposé à une position plus haute que la cuve étanche et thermiquement isolante, l'échangeur de chaleur comprenant une voie de vaporisation et une voie de condensation séparées de manière étanche l'une de l'autre par des parois d'échange de chaleur permettant de transférer de la chaleur entre un fluide contenu dans la voie de condensation et un fluide contenu dans la voie de vaporisation, la voie de vaporisation et la voie de condensation comportant chacune une entrée et une sortie,
  • l'entrée de la voie de condensation étant raccordée à la cuve étanche et thermiquement isolante par un circuit collecteur de vapeur comportant une admission débouchant dans une portion supérieure de l'espace intérieur de la cuve pour prélever un premier flux de gaz combustible en phase vapeur dans l'espace intérieur de la cuve, l'entrée de la voie de condensation est disposée plus haut que la sortie de la voie de condensation,
  • la sortie de la voie de condensation étant raccordée à l'espace intérieur de la cuve pour transférer par gravité une fraction liquide du premier flux de gaz combustible dans l'espace intérieur de la cuve, la fraction liquide du premier flux de gaz combustible étant obtenue par condensation dans la voie de condensation,
  • l'entrée de la voie de vaporisation étant raccordée à la cuve étanche et thermiquement isolante par un circuit d'entrée de liquide, le circuit d'entrée de liquide comportant une admission débouchant dans une portion inférieure de l'espace intérieur de la cuve pour prélever un deuxième flux de gaz combustible en phase liquide dans l'espace intérieur de la cuve et une pompe de circulation pour transférer le deuxième flux de gaz combustible en phase liquide dans la voie de vaporisation,
  • la sortie de la voie de vaporisation étant raccordée à un organe consommateur de gaz pour transférer une fraction vapeur du deuxième flux de gaz combustible vers l'organe consommateur de gaz, la fraction vapeur du deuxième flux de gaz combustible étant obtenue par vaporisation dans la voie de vaporisation.
According to one embodiment, the invention provides an installation for supplying combustible gas to a gas consuming member and to liquefaction of said combustible gas, the installation comprising:
  • a sealed and thermally insulating tank having an interior space intended to be filled with combustible gas in a two-phase liquid-vapor equilibrium state;
  • a heat exchanger disposed at a higher position than the sealed and thermally insulating tank, the heat exchanger comprising a vaporization path and a condensation path separated in a sealed manner from one another by exchange walls heat making it possible to transfer heat between a fluid contained in the condensation path and a fluid contained in the vaporization path, the vaporization path and the condensation path each comprising an inlet and an outlet,
  • the inlet of the condensation channel being connected to the sealed tank and thermally insulating by a vapor collector circuit comprising an inlet opening into an upper portion of the interior space of the tank to draw a first flow of combustible gas in vapor phase in the interior space of the tank, the inlet of the track is located higher than the outlet of the condensation channel,
  • the outlet of the condensation channel being connected to the interior space of the tank to transfer by gravity a liquid fraction of the first flow of combustible gas into the interior space of the tank, the liquid fraction of the first flow of combustible gas being obtained by condensation in the condensation channel,
  • the inlet of the vaporization path being connected to the sealed and thermally insulating tank by a liquid inlet circuit, the liquid inlet circuit comprising an inlet opening into a lower portion of the interior space of the tank for taking a second flow of combustible gas in liquid phase in the interior space of the tank and a circulation pump to transfer the second flow of combustible gas in liquid phase in the vaporization path,
  • the outlet of the vaporization path being connected to a gas consuming member for transferring a vapor fraction of the second flow of combustible gas to the gas consuming member, the vapor fraction of the second flow of combustible gas being obtained by vaporization in the path vaporization.

Selon des modes de réalisation, une telle installation peut comporter une ou plusieurs des caractéristiques suivantes.According to embodiments, such an installation may include one or more of the following characteristics.

Selon un mode de réalisation, la sortie de la voie de vaporisation est disposée plus bas que l'entrée de la voie de vaporisation. Ainsi, à la fois le premier flux de gaz combustible dans la voie de condensation et le deuxième flux de gaz combustible dans la voie de vaporisation réalisent un mouvement descendant, ce qui favorise l'exploitation de la gravité pour entretenir la circulation de ces deux flux. Par ailleurs, cette orientation des flux permet de réaliser un échange de chaleur à co-courant entre la phase liquide du gaz combustible utilisée comme réfrigérant et le gaz issu de l'évaporation naturelle pour favoriser un échange de chaleur isotherme par changement de phase. De préférence dans ce cas, la voie de vaporisation est configurée pour écouler le deuxième flux de gaz combustible sous la forme de films liquides tombant.According to one embodiment, the outlet of the spraying path is arranged lower than the inlet of the spraying path. Thus, both the first flow of combustible gas in the condensation path and the second flow of combustible gas in the vaporization path realize a downward movement, which promotes the exploitation of gravity to maintain the circulation of these two flows. . Furthermore, this orientation of the flows makes it possible to carry out a co-current heat exchange between the liquid phase of the combustible gas used as refrigerant and the gas resulting from natural evaporation to promote an isothermal heat exchange by phase change. Preferably in this case, the vaporization path is configured to flow the second flow of combustible gas in the form of falling liquid films.

Selon un mode de réalisation, la voie de vaporisation de l'échangeur de chaleur comporte un bac de séparation de phases disposé au bas de la voie de vaporisation, le bac de séparation de phases comportant une paroi de fond et une paroi latérale s'étendant vers le haut depuis la paroi de fond, la sortie de la voie de vaporisation débouchant à travers la paroi latérale du bac de séparation de phases à une position espacée au-dessus de la paroi de fond. Grâce à un tel un bac de séparation de phases, il est facile de séparer par gravité la fraction vapeur issue du deuxième flux de gaz combustible de la fraction restée liquide.According to one embodiment, the vaporization path of the heat exchanger comprises a phase separation tank disposed at the bottom of the vaporization path, the phase separation tank having a bottom wall and a side wall extending upward from the bottom wall, the outlet of the spray path opening through the side wall of the phase separation tank at a position spaced above the bottom wall. With such a phase separation tank, it is easy to separate by gravity the vapor fraction from the second flow of combustible gas from the fraction that remains liquid.

Selon un mode de réalisation, un circuit de purge débouche à travers la paroi de fond du bac de séparation de phases pour pouvoir évacuer une phase liquide du bac de séparation de phases par gravité. Ainsi, dans le cas où une fraction non vaporisée du deuxième flux subsiste, par exemple composée des espèces chimiques les moins volatiles d'un mélange (corps lourds), une évacuation de cette fraction liquide est facilitée afin d'éviter de saturer ou d'obstruer la voie de vaporisation.According to one embodiment, a purge circuit opens out through the bottom wall of the phase separation tank in order to be able to evacuate a liquid phase from the phase separation tank by gravity. Thus, in the case where an unvaporized fraction of the second stream remains, for example composed of the least volatile chemical species of a mixture (heavy bodies), an evacuation of this liquid fraction is facilitated in order to avoid saturating or obstruct the spray path.

Selon un mode de réalisation, la voie de vaporisation de l'échangeur de chaleur est placée en dépression, c'est-à-dire à une pression inférieure à la pression régnant dans la phase vapeur de la cuve étanche et thermiquement isolante. Il est ainsi possible de forcer davantage la vaporisation du gaz combustible dans la voie de vaporisation, par l'effet cumulé de l'apport de chaleur dans la voie de condensation et de la dépression dans la voie de vaporisation. De plus, étant donné que la dépression déplace la température d'équilibre diphasique vers le bas dans la voie de vaporisation, il est ainsi possible d'augmenter le flux de chaleur transféré depuis la phase vapeur dans la voie de condensation vers le gaz situé dans la voie de vaporisation.According to one embodiment, the vaporization path of the heat exchanger is placed in depression, that is to say at a pressure lower than the pressure prevailing in the vapor phase of the sealed and thermally insulating tank. It is thus possible to further force the vaporization of the combustible gas in the vaporization path, by the cumulative effect of the heat supply in the condensation path and of the vacuum in the vaporization path. In addition, since the vacuum moves the two-phase equilibrium temperature down in the vaporization path, it is thus possible to increase the heat flow transferred from the vapor phase in the condensation path to the gas located in the vaporization route.

De préférence dans ce cas, la pression absolue dans la voie de vaporisation est supérieure à 120 mbars absolue. Il est en effet préférable que la pression à l'intérieur de la voie de vaporisation soit supérieure à la pression correspondant au point triple du diagramme de phase du méthane de sorte à éviter une solidification du gaz naturel à l'intérieur de la voie de vaporisation. La pression dans la voie de vaporisation peut notamment être comprise entre 500 mbars absolue et 980 mbars absolue.Preferably in this case, the absolute pressure in the vaporization path is greater than 120 mbar absolute. It is indeed preferable for the pressure inside the vaporization path to be higher than the pressure corresponding to the triple point of the methane phase diagram so as to avoid solidification of the natural gas inside the vaporization path. . The pressure in the vaporization path can in particular be between 500 mbar absolute and 980 mbar absolute.

Selon l'invention, l'installation comporte en outre une pompe à vide ou pompe à dépression reliée à la voie de vaporisation pour placer la voie de vaporisation de l'échangeur de chaleur à une pression inférieure à la pression régnant dans la phase vapeur de la cuve étanche et thermiquement isolanteAccording to the invention, the installation further comprises a vacuum pump or vacuum pump connected to the vaporization path to place the vaporization path of the heat exchanger at a pressure lower than the pressure prevailing in the vapor phase of the waterproof and thermally insulating tank

Selon des modes de réalisation, une telle pompe à vide peut être commandée en fonction d'une consigne de débit ou d'une consigne de pression. Une telle consigne de débit ou de pression peut être prédéterminée ou générée par l'organe consommateur de gaz.According to embodiments, such a vacuum pump can be controlled as a function of a flow rate setpoint or a pressure setpoint. Such a flow or pressure setpoint can be predetermined or generated by the gas consuming member.

Selon des modes de réalisation correspondants, l'installation peut présenter une ou plusieurs des caractéristiques suivantes :

  • l'installation comporte un capteur de mesure de débit apte à délivrer un signal représentatif du débit du flux de vapeur aspiré à travers l'admission et refoulé vers l'organe consommateur de gaz et un dispositif de commande apte à commander la pompe à vide en fonction du signal représentatif du débit du flux de vapeur et d'une consigne de débit générée par l'organe consommateur de gaz.
  • l'installation comporte un capteur de pression apte à délivrer un signal représentatif de la pression régnant dans la voie de vaporisation et un dispositif de commande apte à commander la pompe à vide en fonction du signal représentatif de la pression et d'une consigne de pression.
According to corresponding embodiments, the installation can have one or more of the following characteristics:
  • the installation includes a flow measurement sensor capable of delivering a signal representative of the flow rate of the vapor flow drawn through the inlet and discharged towards the gas consuming member and a control device capable of controlling the vacuum pump in function of the signal representative of the flow rate of the vapor flow and of a flow rate setpoint generated by the gas consuming member.
  • the installation comprises a pressure sensor capable of delivering a signal representative of the pressure prevailing in the vaporization path and a control device capable of controlling the vacuum pump as a function of the signal representative of the pressure and of a pressure setpoint .

La liaison entre la sortie de la voie de vaporisation et l'organe consommateur de gaz peut être directe ou indirecte, selon les exigences de l'organe consommateur. Selon un mode de réalisation, la pompe à vide précitée est agencée entre la sortie de la voie de vaporisation et l'organe consommateur de gaz. Selon un autre mode de réalisation, un compresseur est agencé entre la sortie de la voie de vaporisation et l'organe consommateur de gaz pour fournir un flux de gaz en phase vapeur à une pression supérieure à la pression de stockage dans la cuve.The connection between the outlet of the vaporization channel and the gas consuming member can be direct or indirect, depending on the requirements of the consuming member. According to one embodiment, the aforementioned vacuum pump is arranged between the outlet of the vaporization path and the gas consuming member. According to another embodiment, a compressor is arranged between the outlet of the vaporization path and the gas consuming member to supply a flow of gas in the vapor phase at a pressure higher than the storage pressure in the tank.

Selon un mode de réalisation, l'échangeur de chaleur comporte une enveloppe étanche et thermiquement isolante délimitant un espace intérieur contenant la voie de condensation, l'enveloppe étant agencée au-dessus de la cuve étanche et thermiquement isolante et comportant une ouverture inférieure communiquant avec l'espace intérieur de la cuve étanche et thermiquement isolante et constituant la sortie de la voie de condensation.According to one embodiment, the heat exchanger comprises a sealed and thermally insulating envelope delimiting an interior space containing the condensation channel, the envelope being arranged above the sealed and thermally insulating tank and comprising a lower opening communicating with the interior space of the sealed and thermally insulating tank and constituting the outlet of the condensation channel.

Une telle enveloppe étanche et thermiquement isolante peut être réalisée de différentes manières, par exemple d'un seul tenant avec une paroi de sommet de la cuve ou bien sous la forme d'un ensemble rapporté à la paroi de sommet de la cuve.Such a sealed and thermally insulating envelope can be produced in different ways, for example in one piece with a top wall of the tank or else in the form of an assembly attached to the top wall of the tank.

Selon un mode de réalisation, une paroi de sommet de la cuve étanche et thermiquement isolante présente une ouverture reliée à l'ouverture inférieure de l'enveloppe, l'enveloppe comportant en outre une bride de fixation agencée autour de l'ouverture inférieure de l'enveloppe, la bride de fixation étant attachée à la paroi de sommet de la cuve étanche et thermiquement isolante autour de l'ouverture de la paroi de sommet.According to one embodiment, a top wall of the sealed and thermally insulating tank has an opening connected to the lower opening of the envelope, the envelope further comprising a fixing flange arranged around the lower opening of the envelope, the fixing flange being attached to the top wall of the sealed and thermally insulating tank around the opening of the top wall.

De préférence dans ce cas, l'échangeur de chaleur comporte en outre un canalisation collectrice s'étendant depuis l'ouverture inférieure de l'enveloppe jusqu'à proximité d'une paroi de sommet de l'enveloppe et présentant une extrémité inférieure débouchant dans l'espace intérieur de la cuve et une extrémité supérieure débouchant dans l'espace intérieur de l'enveloppe, la canalisation collectrice délimitant au sein de l'espace intérieur de l'enveloppe un espace intérieur de la canalisation collectrice formant le circuit collecteur de vapeur et un espace extérieur de la canalisation collectrice formant la voie de condensation de l'échangeur de chaleur.Preferably in this case, the heat exchanger further comprises a collecting pipe extending from the lower opening of the envelope to near a top wall of the envelope and having a lower end opening into the interior space of the tank and an upper end opening into the interior space of the casing, the collecting pipe delimiting within the interior space of the casing an interior space of the collecting pipe forming the vapor collector circuit and an outer space of the collecting pipe forming the condensation path of the heat exchanger.

Grâce à ces caractéristiques, l'échangeur de chaleur et le circuit collecteur de vapeur peuvent être réalisés sous une forme intégrée relativement peu encombrante et présentant une surface d'échange relativement réduite avec l'environnement extérieur, ce qui limite les flux thermiques susceptibles d'augmenter l'évaporation naturelle.Thanks to these characteristics, the heat exchanger and the vapor collecting circuit can be produced in a relatively space-saving integrated form and having a relatively reduced exchange surface with the external environment, which limits the heat flows liable to increase natural evaporation.

Selon un autre mode de réalisation, l'installation comporte une pluralité de cuves étanches et thermiquement isolantes comportant un espace intérieur destiné à être rempli du gaz combustible dans un état d'équilibre diphasique liquide-vapeur, ledit circuit collecteur de vapeur étant un circuit collecteur commun raccordant l'entrée de la voie de condensation à chacune desdites cuves pour collecter les gaz issus de l'évaporation dans chacune des cuves. Il est ainsi possible d'exploiter l'échangeur de chaleur conjointement pour un ensemble de cuves.According to another embodiment, the installation comprises a plurality of sealed and thermally insulating tanks comprising an interior space intended to be filled with combustible gas in a liquid-vapor two-phase equilibrium state, said vapor collector circuit being a collector circuit common connecting the inlet of the condensation channel to each of said tanks to collect the gases from evaporation in each of the tanks. It is thus possible to operate the heat exchanger jointly for a set of tanks.

Selon un mode de réalisation correspondant, l'échangeur de chaleur comporte :

  • une pluralité de tubes parallèles à la canalisation collectrice disposés dans l'espace extérieur de la canalisation collectrice autour de la canalisation collectrice, les tubes parallèles constituant lesdites parois d'échange de chaleur de l'échangeur de chaleur,
  • un distributeur d'entrée disposé dans l'espace intérieur de l'enveloppe, le distributeur d'entrée s'étendant à la périphérie de la canalisation collectrice et présentant une paroi de fond à travers laquelle débouche une extrémité supérieure de chacun des tubes parallèles,
  • un tube d'entrée constituant l'entrée de la voie de vaporisation et s'étendant à travers l'enveloppe entre l'extérieur de l'enveloppe et le distributeur d'entrée,
  • un carter de sortie disposé dans l'espace extérieur de la canalisation collectrice autour de la canalisation collectrice plus bas que la chambre d'entrée et présentant une paroi de sommet à travers laquelle débouche une extrémité inférieure de chacun des tubes parallèles, et
  • un tube de sortie constituant la sortie de la voie de vaporisation et s'étendant à travers l'enveloppe entre le carter de sortie et l'extérieur de l'enveloppe.
According to a corresponding embodiment, the heat exchanger comprises:
  • a plurality of tubes parallel to the collecting pipe arranged in the external space of the collecting pipe around the collecting pipe, the parallel tubes constituting said heat exchange walls of the heat exchanger,
  • an inlet distributor arranged in the interior space of the envelope, the inlet distributor extending at the periphery of the collecting pipe and having a bottom wall through which opens an upper end of each of the parallel tubes,
  • an inlet tube constituting the inlet of the vaporization path and extending through the enclosure between the exterior of the enclosure and the inlet distributor,
  • an outlet casing disposed in the external space of the collecting pipe around the collecting pipe lower than the inlet chamber and having a top wall through which opens a lower end of each of the parallel tubes, and
  • an outlet tube constituting the outlet of the vaporization path and extending through the envelope between the outlet casing and the exterior of the envelope.

Afin de maximiser le rendement de l'échangeur de chaleur, il est en effet souhaitable de réaliser le contact thermique entre la voie de vaporisation et la voie de condensation sur la plus grande hauteur possible de l'enveloppe externe. Avantageusement, le distributeur d'entrée est disposé plus haut que l'extrémité supérieure de la canalisation collectrice. Ainsi les tubes parallèles peuvent s'étendre sur quasiment la même longueur que la canalisation collectrice.In order to maximize the efficiency of the heat exchanger, it is indeed desirable to make thermal contact between the vaporization path and the condensation path over the greatest possible height of the external envelope. Advantageously, the inlet distributor is disposed higher than the upper end of the collecting pipe. Thus the parallel tubes can extend over almost the same length as the collecting pipe.

Selon un mode de réalisation, les tubes parallèles à la canalisation collectrice présentent des ailettes d'échange de chaleur disposées sur la surface extérieure des tubes parallèles à la canalisation collectrice.According to one embodiment, the tubes parallel to the manifold have heat exchange fins arranged on the outer surface of the tubes parallel to the manifold.

Selon un mode de réalisation, l'invention fournit aussi un procédé d'alimentation en gaz combustible d'un organe consommateur de gaz et de liquéfaction dudit gaz combustible, à l'aide d'une installation précitée, comportant :

  • admettre un premier flux de gaz combustible en phase vapeur à l'entrée de la voie de condensation depuis la portion supérieure de l'espace intérieur de la cuve étanche et thermiquement isolante à travers le circuit collecteur de vapeur,
  • transférer un deuxième flux de gaz combustible en phase liquide depuis la portion inférieure de l'espace intérieur de la cuve jusqu'à l'entrée de la voie de vaporisation à l'aide de la pompe de circulation,
  • réaliser un échange de chaleur entre le premier flux de gaz combustible dans la voie de condensation et le deuxième flux de gaz combustible dans la voie de vaporisation, de manière à vaporiser au moins une fraction du deuxième flux de gaz combustible, initialement en phase liquide, dans la voie de vaporisation en condensant au moins une fraction du premier flux de gaz combustible, initialement en phase vapeur, dans la voie de condensation,
  • transférer par gravité la fraction liquide du premier flux de gaz combustible depuis la sortie de la voie de condensation jusqu'à l'espace intérieur de la cuve, et
  • transférer la fraction vapeur du deuxième flux de gaz combustible depuis la sortie de la voie de vaporisation vers l'organe consommateur de gaz.
According to one embodiment, the invention also provides a method for supplying combustible gas to a gas consuming member and for liquefying said combustible gas, using a said installation, comprising:
  • admit a first flow of combustible gas in the vapor phase at the entry of the condensation channel from the upper portion of the interior space of the sealed and thermally insulating tank through the vapor collecting circuit,
  • transfer a second flow of combustible gas in liquid phase from the portion lower of the interior space of the tank up to the entry of the vaporization path using the circulation pump,
  • performing a heat exchange between the first flow of combustible gas in the condensation path and the second flow of combustible gas in the vaporization path, so as to vaporize at least a fraction of the second flow of combustible gas, initially in the liquid phase, in the vaporization path by condensing at least a fraction of the first flow of combustible gas, initially in the vapor phase, in the condensation path,
  • gravity transfer the liquid fraction of the first flow of combustible gas from the outlet of the condensation channel to the interior of the tank, and
  • transfer the vapor fraction of the second flow of combustible gas from the outlet of the vaporization path to the gas consuming member.

Grâce à l'orientation descendante de la voie de condensation, le premier flux de gaz combustible refroidi par l'échange de chaleur peut s'écouler par convection naturelle, i.e. par gravité, vers l'espace intérieur de la cuve, ce qui favorise la production d'une aspiration dans le circuit collecteur de vapeur, pour ainsi entretenir le premier flux sans travail mécanique supplémentaire.Thanks to the downward orientation of the condensation channel, the first flow of combustible gas cooled by the heat exchange can flow by natural convection, ie by gravity, towards the interior space of the tank, which favors the production of a suction in the vapor collector circuit, thus maintaining the first flow without additional mechanical work.

De préférence, ce procédé est mis en oeuvre de manière à vaporiser la totalité ou quasi-totalité du deuxième flux de gaz combustible dans la voie de vaporisation. Ainsi, en produisant la phase vapeur par vaporisation forcée d'un flux de liquide prélevé dans la portion inférieure de la cuve, la teneur en composés les plus volatils est sensiblement égale à celle de la phase liquide du gaz stocké dans la cuve. La concentration en composés les plus volatils du flux de gaz vaporisé est donc limitée et sensiblement constante dans le temps.Preferably, this method is implemented so as to vaporize all or almost all of the second flow of combustible gas in the vaporization path. Thus, by producing the vapor phase by forced vaporization of a flow of liquid taken from the lower portion of the tank, the content of the most volatile compounds is substantially equal to that of the liquid phase of the gas stored in the tank. The concentration of the most volatile compounds in the vaporized gas flow is therefore limited and substantially constant over time.

En outre, grâce à une telle installation, la vaporisation du gaz liquéfié peut être réalisée sans l'aide d'une source de chaleur extérieure, par opposition aux installations de vaporisation forcée utilisant un échange de chaleur avec de l'eau de mer, un liquide intermédiaire ou des gaz de combustion issus de la motorisation ou de brûleurs spécifiques.In addition, thanks to such an installation, the vaporization of the liquefied gas can be carried out without the aid of an external heat source, as opposed to forced vaporization installations using a heat exchange with sea water, a intermediate liquid or combustion gases from the engine or specific burners.

Le gaz présent dans la portion supérieure de l'espace intérieur de la cuve joue ainsi le rôle de source chaude pour le flux à vaporiser. Aussi, l'installation permet à la fois de produire un flux de vapeur et de refroidir et de condenser la phase vapeur issue de l'évaporation naturelle présente dans le ciel gazeux de la cuve, de sorte à limiter l'évaporation naturelle.The gas present in the upper portion of the interior space of the tank thus acts as a hot source for the flow to be vaporized. Also, the installation allows both to produce a flow of vapor and to cool and condense the vapor phase resulting from natural evaporation present in the gaseous sky of the tank, so as to limit natural evaporation.

Selon un mode de réalisation, l'invention fournit un navire comportant une installation précitée.According to one embodiment, the invention provides a ship comprising an aforementioned installation.

Selon un mode de réalisation, l'invention fournit aussi un procédé de chargement ou déchargement d'un tel navire, dans lequel on achemine du gaz combustible à travers des canalisations isolées depuis ou vers une installation de stockage flottante ou terrestre vers ou depuis la cuve étanche et thermiquement isolante du navire.According to one embodiment, the invention also provides a method of loading or unloading such a ship, in which combustible gas is conveyed through insulated pipes from or to a floating or terrestrial storage installation towards or from the tank. waterproof and thermally insulating of the ship.

Selon un mode de réalisation, l'invention fournit aussi un système de transfert pour un gaz combustible, le système comportant le navire précité, des canalisations isolées agencées de manière à relier la cuve installée dans la coque du navire à une installation de stockage flottante ou terrestre et une pompe pour entrainer un flux de gaz combustible à travers les canalisations isolées depuis ou vers l'installation de stockage flottante ou terrestre vers ou depuis la cuve étanche et thermiquement isolante du navire.According to one embodiment, the invention also provides a transfer system for a combustible gas, the system comprising the abovementioned ship, isolated pipes arranged so as to connect the tank installed in the hull of the ship to a floating storage installation or terrestrial and a pump for driving a flow of combustible gas through the insulated pipes from or to the floating or terrestrial storage installation towards or from the watertight and thermally insulating vessel of the ship.

Brève description des figuresBrief description of the figures

L'invention sera mieux comprise, et d'autres buts, détails, caractéristiques et avantages de celle-ci apparaîtront plus clairement au cours de la description suivante de plusieurs modes de réalisation particuliers de l'invention, donnés uniquement à titre illustratif et non limitatif, en référence aux dessins annexés.

  • La figure 1 est une illustration schématique d'une installation d'alimentation en gaz combustible d'organes consommateurs de gaz et de liquéfaction dudit gaz combustible, utile à la compréhension de l'invention mais n'en faisant pas partie
  • La figure 2 est une demi-vue en perspective et en coupe longitudinale d'un échangeur de chaleur utilisable dans installation de la figure 1.
  • La figure 3 est une vue en coupe transversale de l'échangeur de chaleur de la figure 2 selon la ligne III-III.
  • La figure 4 est une vue agrandie d'un tube d'échange de chaleur de l'échangeur de chaleur de la figure 2.
  • La figure 5 est une vue analogue à la figure 1 montrant un mode de réalisation selon l'invention de l'installation d'alimentation en gaz combustible d'organes consommateurs de gaz et de liquéfaction dudit gaz combustible.
  • La figure 6 est une représentation schématique écorchée d'une cuve de navire méthanier comportant une telle installation et d'un terminal de chargement/déchargement de cette cuve.
The invention will be better understood, and other objects, details, characteristics and advantages thereof will appear more clearly during the following description of several particular embodiments of the invention, given solely by way of illustration and without limitation. , with reference to the accompanying drawings.
  • The figure 1 is a schematic illustration of an installation for supplying combustible gas to gas consuming organs and for liquefying said combustible gas, useful for understanding the invention but not forming part of it
  • The figure 2 is a half view in perspective and in longitudinal section of a heat exchanger usable in installation of the figure 1 .
  • The figure 3 is a cross-sectional view of the heat exchanger of the figure 2 along line III-III.
  • The figure 4 is an enlarged view of a heat exchanger tube of the heat exchanger of the figure 2 .
  • The figure 5 is a view analogous to the figure 1 showing an embodiment according to the invention of the installation for supplying combustible gas to organs consuming gas and for liquefying said combustible gas.
  • The figure 6 is a cutaway schematic representation of an LNG tank vessel comprising such an installation and of a loading / unloading terminal of this tank.

Description détaillée de modes de réalisationDetailed description of embodiments

Dans la description et les revendications, le terme « gaz combustible » présente un caractère générique et vise indifféremment un gaz constitué d'un seul corps pur ou un mélange gazeux constitué d'une pluralité de composants.In the description and the claims, the term “combustible gas” is generic in nature and is intended equally to refer to a gas consisting of a single pure body or to a gas mixture consisting of a plurality of components.

Sur la figure 1, une installation 1 visant, d'une part, à alimenter en gaz combustible un ou plusieurs organes consommateurs de gaz et, d'autre part, à liquéfier du gaz combustible est illustrée. Une telle installation 1 peut être installée à terre ou sur un ouvrage flottant. Dans le cas d'un ouvrage flottant, l'installation 1 peut être destinée à une barge de liquéfaction ou de regazéification, à un navire de transport de gaz naturel liquéfié, tel qu'un méthanier, ou plus généralement être destinée à tout navire équipé d'un organe consommateur de gaz.On the figure 1 , an installation 1 aiming, on the one hand, at supplying combustible gas to one or more gas consuming members and, on the other hand, at liquefying combustible gas is illustrated. Such an installation 1 can be installed on land or on a floating structure. In the case of a floating structure, the installation 1 can be intended for a liquefaction or regasification barge, for a liquefied natural gas transport vessel, such as an LNG carrier, or more generally for any equipped vessel. of a gas consuming organ.

L'installation 1 illustrée sur la figure 1 comporte une ligne de sortie de vapeur 3 qui peut alimenter directement ou indirectement différents types d'organes consommateur de gaz combustible non représentés, à savoir notamment un bruleur, un générateur électrique et/ou un moteur pour la propulsion d'un navire.Installation 1 illustrated on the figure 1 comprises a steam outlet line 3 which can supply directly or indirectly different types of fuel gas consuming devices not shown, namely in particular a burner, an electric generator and / or an engine for the propulsion of a ship.

Un tel bruleur est intégré à une installation de production d'énergie. L'installation de production d'énergie peut notamment comporter une chaudière de production de vapeur. La vapeur peut être destinée à alimenter des turbines à vapeur pour la production d'énergie et/ou à alimenter un réseau de chauffage du navire.Such a burner is integrated into an energy production installation. The energy production installation may in particular include a steam production boiler. The steam can be used to power steam turbines for energy production and / or to power a ship's heating network.

Un tel générateur électrique comporte par exemple un moteur thermique à alimentation mixte diesel/gaz naturel, par exemple de technologie DFDE pour « Dual Fuel Diesel Electric » en langue anglaise. Un tel moteur thermique peut brûler un mélange de diesel et de gaz naturel ou utiliser l'un ou l'autre de ces deux combustibles. Le gaz naturel alimentant un tel moteur thermique doit présenter une pression de l'ordre de quelques bars à quelques dizaines de bars, par exemple de l'ordre de 6 à 8 bars absolus. Pour cela, un ou plusieurs compresseurs 4 peuvent être prévus sur la ligne de sortie de vapeur 3.Such an electric generator comprises for example a thermal engine with mixed diesel / natural gas supply, for example of DFDE technology for “Dual Fuel Diesel Electric” in English. Such an engine can burn a mixture of diesel and natural gas or use either of these two fuels. The natural gas supplying such a heat engine must have a pressure of the order of a few bars to a few tens of bars, for example of around 6 to 8 bars absolute. For this, one or more compressors 4 can be provided on the steam outlet line 3.

Un tel moteur pour la propulsion du navire est, par exemple, un moteur basse vitesse deux temps bi-carburant de technologie « ME-GI », développé par la société MAN. Un tel moteur utilise du gaz naturel comme combustible et une petite quantité de carburant pilote qui est injectée avant l'injection du gaz naturel afin qu'il s'enflamme. Pour alimenter un tel moteur, le gaz naturel doit préalablement être comprimé sous une haute pression comprise entre 150 et 400 bars absolus, et plus particulièrement entre 250 et 300 bars absolus. Pour cela, un ou plusieurs compresseurs 4 peuvent être prévus sur la ligne de sortie de vapeur 3.Such an engine for propelling the ship is, for example, a low-speed two-stroke dual-fuel engine of “ME-GI” technology, developed by the company MAN. Such an engine uses natural gas as fuel and a small amount of pilot fuel which is injected before the injection of natural gas so that it ignites. To supply such an engine, natural gas must first be compressed under a high pressure of between 150 and 400 bar absolute, and more particularly between 250 and 300 bar absolute. For this, one or more compressors 4 can be provided on the steam outlet line 3.

L'installation 1 comporte une cuve 2 étanche et thermiquement isolante. Selon un mode de réalisation, la cuve 2 est une cuve à membranes. A titre d'exemple, de telles cuves à membranes sont décrites dans les demandes de brevet WO14057221 , FR2691520 et FR2877638 . De telles cuves à membranes sont destinées à stocker du gaz combustible à des pressions sensiblement égales à la pression atmosphérique ou légèrement supérieures. Selon d'autres modes de réalisation alternatifs, la cuve 2 peut également être une cuve autoporteuse et peut notamment présenter une forme parallélépipédique, prismatique, sphérique, cylindrique ou multi-lobique. Certains types de cuve 2 permettent un stockage du gaz à des pressions sensiblement supérieures à la pression atmosphérique.The installation 1 comprises a sealed and thermally insulating tank 2. According to one embodiment, the tank 2 is a membrane tank. By way of example, such membrane tanks are described in patent applications WO14057221 , FR2691520 and FR2877638 . Such membrane tanks are intended to store combustible gas at pressures substantially equal to atmospheric pressure or slightly higher. According to other alternative embodiments, the tank 2 can also be a self-supporting tank and can in particular have a parallelepiped, prismatic, spherical, cylindrical or multi-lobic shape. Certain types of tank 2 allow gas to be stored at pressures substantially higher than atmospheric pressure.

La cuve 2 comporte un espace interne 7 destiné à être rempli de gaz combustible. Le gaz combustible peut notamment être un gaz naturel liquéfié (GNL), c'est-à-dire un mélange gazeux comportant majoritairement du méthane ainsi qu'un ou plusieurs autres hydrocarbures, tels que l'éthane, le propane, le n-butane, le i-butane, le n-pentane le i-pentane, le néopentane, et de l'azote en faible proportion. Le gaz combustible peut également être de l'éthane ou un gaz de pétrole liquéfié (GPL), c'est-à-dire un mélange d'hydrocarbures issu du raffinage du pétrole comportant essentiellement du propane et du butane.The tank 2 has an internal space 7 intended to be filled with combustible gas. The combustible gas can in particular be a liquefied natural gas (LNG), that is to say a gaseous mixture mainly comprising methane as well as one or more other hydrocarbons, such as ethane, propane, n-butane , i-butane, n-pentane i-pentane, neopentane, and nitrogen in small proportion. The combustible gas can also be ethane or a liquefied petroleum gas (LPG), that is to say a mixture of hydrocarbons resulting from the refining of petroleum comprising essentially propane and butane.

Le gaz combustible est stocké dans l'espace interne 7 de la cuve 2 dans un état d'équilibre diphasique liquide-vapeur. Le gaz est donc présent en phase vapeur, dans la partie supérieure 8 de la cuve 2 et en phase liquide dans la partie inférieure 9 de la cuve 2. Cette stratification est obtenue naturellement du fait de la densité spécifique de chaque phase. La localisation de l'interface liquide-vapeur dépend naturellement du niveau de remplissage de la cuve 2. La température d'équilibre du gaz naturel liquéfié correspondant à son état d'équilibre diphasique liquide-vapeur est d'environ -162°C lorsqu'il est stocké à pression atmosphérique.The combustible gas is stored in the internal space 7 of the tank 2 in a liquid-vapor two-phase equilibrium state. The gas is therefore present in the vapor phase, in the upper part 8 of the tank 2 and in the liquid phase in the lower part 9 of the tank 2. This stratification is obtained naturally due to the specific density of each phase. The location of the liquid-vapor interface naturally depends on the filling level of the tank 2. The equilibrium temperature of the liquefied natural gas corresponding to its two-phase liquid-vapor equilibrium state is approximately -162 ° C when it is stored at atmospheric pressure.

Au-dessus de la paroi de sommet 5 de la cuve 2, on a représenté un échangeur de chaleur 10 qui permet conjointement de re-liquéfier du gaz en phase vapeur provenant d'évaporation naturelle dans la partie supérieure 8 de la cuve 2 tout en vaporisant de manière forcée du gaz en phase liquide prélevé dans la partie inférieure 9 de la cuve 2.Above the top wall 5 of the tank 2, there is shown a heat exchanger 10 which jointly makes it possible to re-liquefy gas in the vapor phase originating from natural evaporation in the upper part 8 of the tank 2 while forcibly vaporizing gas in the liquid phase taken from the lower part 9 of the tank 2.

Pour cela, l'échangeur de chaleur 10 présente une enveloppe externe 11 étanche au gaz, de préférence thermiquement isolante pour limiter le flux thermique entrant depuis l'environnement, qui est disposée au-dessus de la paroi de sommet 5 de la cuve 2, et dont l'espace intérieur 12 est en communication avec la partie supérieure 8 de la cuve 2 par au moins deux liaisons :

  • un circuit collecteur de vapeur 13 qui débouche au niveau du sommet de l'espace intérieur 12, pour amener de la vapeur du gaz combustible en haut de l'espace intérieur 12,
  • un circuit de retour de condensat 14 qui débouche en bas de l'espace intérieur 12, pour collecter par gravité le gaz combustible condensé dans l'espace intérieur 12 et le ramener vers l'intérieur de la cuve 2.
For this, the heat exchanger 10 has an external gas-tight casing 11, preferably thermally insulating to limit the heat flow entering from the environment, which is arranged above the top wall 5 of the tank 2, and whose interior space 12 is in communication with the upper part 8 of the tank 2 by at least two connections:
  • a vapor collector circuit 13 which opens at the top of the interior space 12, for bringing fuel gas vapor to the top of the interior space 12,
  • a condensate return circuit 14 which opens at the bottom of the interior space 12, for collecting by gravity the combustible gas condensed in the interior space 12 and bringing it towards the interior of the tank 2.

Sur la figure 1, le circuit collecteur de vapeur 13 et le circuit de retour de condensat 14 traversent la paroi de sommet 5 de la cuve 2, mais d'autres agencements sont possibles, notamment pour le circuit de retour de condensat 14, par exemple en traversant la paroi latérale 6 dans la portion supérieure 8 de la cuve 2.On the figure 1 , the vapor collector circuit 13 and the condensate return circuit 14 pass through the top wall 5 of the tank 2, but other arrangements are possible, in particular for the condensate return circuit 14, for example by crossing the wall lateral 6 in the upper portion 8 of the tank 2.

Comme esquissé au chiffre 50, le circuit collecteur de vapeur 13 peut comporter plusieurs branches reliées à plusieurs cuves pour servir de collecteur commun reliant un ensemble de cuves à la voie de condensation de l'échangeur de chaleur 10. Des vannes, non représentées, peuvent être prévues sur chaque branche pour conserver la possibilité d'isoler les cuves entre elles dans ce cas.As sketched in figure 50, the steam collector circuit 13 may include several branches connected to several tanks to serve as a common collector connecting a set of tanks to the condensation path of the heat exchanger 10. Valves, not shown, can be provided on each branch to keep the possibility of isolating the tanks from each other in this case.

De la même manière, le circuit de retour de condensat 14 pourrait être relié à plusieurs cuves.In the same way, the condensate return circuit 14 could be connected to several tanks.

Pour prélever de la chaleur dans l'espace intérieur 12, l'échangeur de chaleur 10 présente aussi un circuit de vaporisation 15 qui est agencé dans l'espace intérieur 12, représenté ici sous la forme d'un serpentin hélicoïdal mais dont la forme peut varier dans une large mesure. Le circuit de vaporisation 15 est alimenté en gaz combustible en phase liquide à partir de la partie inférieure 9 de la cuve 2 par une pompe de circulation 16 et un tuyau d'entrée 17 rejoignant l'entrée du circuit de vaporisation 15 en traversant de manière étanche l'enveloppe externe 11. En prélevant la chaleur latente du gaz combustible en phase vapeur se trouvant dans l'espace intérieur 12, le gaz en phase liquide circulant dans le circuit de vaporisation 15 se vaporise et la phase vapeur ainsi formée s'écoule vers la ligne de sortie 3, qui est raccordée à la sortie du circuit de vaporisation 15 en traversant de manière étanche l'enveloppe externe 11. Pour cela, la sortie du circuit de vaporisation 15 est de préférence située plus bas que l'entrée du circuit de vaporisation 15. Ainsi, à la fois le flux de gaz en cours de vaporisation dans le circuit de vaporisation 15 et le flux de gaz en cours de condensation dans l'espace intérieur 12 ont un mouvement descendant, l'un sous l'effet de la pompe de circulation, l'autre uniquement sous l'effet de la gravité et de la différence de densité entre les phases liquide et vapeur.To extract heat from the interior space 12, the heat exchanger 10 also has a vaporization circuit 15 which is arranged in the interior space 12, shown here in the form of a helical coil but the shape of which can vary to a large extent. The vaporization circuit 15 is supplied with combustible gas in liquid phase from the lower part 9 of the tank 2 by a circulation pump 16 and an inlet pipe 17 joining the inlet of the vaporization circuit 15 by passing through seals the outer envelope 11. By removing the latent heat from the combustible gas in the vapor phase located in the interior space 12, the gas in the liquid phase circulating in the vaporization circuit 15 is vaporized and the vapor phase thus formed flows towards the outlet line 3, which is connected to the outlet of the vaporization circuit 15 by sealingly passing through the external envelope 11. For this, the outlet of the vaporization circuit 15 is preferably located lower than the inlet of the vaporization circuit 15. Thus, both the flow of gas being vaporized in the vaporization circuit 15 and the flow of gas being condensed in the interior space 12 have a downward movement nt, one under the effect of the circulation pump, the other only under the effect of gravity and the difference in density between the liquid and vapor phases.

Etant donné que la phase liquide est beaucoup plus dense que la phase vapeur, la consommation de vapeur par condensation crée un effet d'aspiration permanent dans le circuit collecteur de vapeur 13, comme représenté par la flèche 19. Il n'est donc généralement pas nécessaire de disposer une pompe de circulation dans le circuit collecteur de vapeur 13.Since the liquid phase is much denser than the vapor phase, the consumption of vapor by condensation creates a permanent suction effect in the vapor collector circuit 13, as shown by the arrow 19. It is therefore generally not necessary to have a circulation pump in the steam collector circuit 13.

Afin de forcer davantage la vaporisation du gaz combustible en phase liquide circulant dans le circuit de vaporisation 15, il est possible de placer ce dernier sous dépression. Pour cela, comme représenté sur la figure 5, une pompe à vide 51 peut être employée, par exemple à la place du compresseur 4. La pompe à vide 51 doit être une pompe cryogénique, c'est-à-dire une pompe apte à supporter des températures cryogéniques inférieures à -150 °C. Elle doit en outre être conforme à la réglementation ATEX, c'est-à-dire conçue afin d'écarter tout risque d'explosion. En outre, un organe de perte de charge, par exemple une vanne d'expansion 45, est placé à l'entrée du circuit de vaporisation 15, de préférence à l'intérieur de l'enveloppe externe 11.In order to further force the vaporization of the combustible gas in the liquid phase circulating in the vaporization circuit 15, it is possible to place the latter under vacuum. For this, as shown in the figure 5 , a vacuum pump 51 can be used, for example in place of the compressor 4. The vacuum pump 51 must be a cryogenic pump, that is to say a pump capable of withstanding cryogenic temperatures below -150 ° vs. It must also comply with ATEX regulations, that is to say designed to eliminate any risk of explosion. In addition, a pressure drop member, for example an expansion valve 45, is placed at the inlet of the vaporization circuit 15, preferably inside the external envelope 11.

La figure 1 représente en trait interrompu une autre disposition possible du circuit collecteur de vapeur, sous la forme d'une canalisation collectrice 113 disposée de manière concentrique dans le circuit de retour de condensat 14 depuis la partie supérieure 8 de la cuve 2 jusqu'au sommet de l'espace intérieur 12. Dans ce cas l'admission de gaz en phase vapeur a lieu par l'intérieur de la canalisation collectrice 113, tandis que le retour de condensat s'écoule dans l'espace annulaire autour de la canalisation collectrice 113 dans le circuit de retour de condensat 14. Pour le reste, le fonctionnement est identique.The figure 1 shows in broken lines another possible arrangement of the vapor collecting circuit, in the form of a collecting pipe 113 concentrically disposed in the condensate return circuit 14 from the upper part 8 of the tank 2 to the top of the interior space 12. In this case the admission of gas in the vapor phase takes place from the interior of the collecting pipe 113, while the condensate return flows in the annular space around the collecting pipe 113 in the condensate return circuit 14. For the rest, the operation is identical.

Bien que la figure 1 illustre un échangeur de chaleur dont la voie de vaporisation est contenue et baignée dans le fluide de la voie de condensation, une configuration inverse est aussi possible, à savoir une voie de condensation contenue et baignée dans le fluide de la voie de vaporisation. D'autres configurations sont encore possible, par exemple avec un échangeur de chaleur dans lequel les deux voies ont sensiblement le même volume.Although the figure 1 illustrates a heat exchanger whose vaporization path is contained and bathed in the fluid of the condensation path, a reverse configuration is also possible, namely a condensation path contained and bathed in the fluid of the vaporization path. Other configurations are also possible, for example with a heat exchanger in which the two channels have substantially the same volume.

En référence aux figures 2 à 4, on va maintenant décrite un autre mode de réalisation de l'échangeur de chaleur. Les éléments analogues ou identiques à ceux de la figure 1 portent le même chiffre de référence augmenté de 100.With reference to figures 2 to 4 , we will now describe another embodiment of the heat exchanger. Elements analogous or identical to those of the figure 1 carry the same reference figure increased by 100.

Sur la figure 2, l'enveloppe externe 111 présente la forme générale d'une bouteille cylindrique d'axe vertical, retournée avec le goulot vers le bas. Plus précisément, le corps principal délimitant l'espace intérieur 112 présente un plus grand diamètre que le tube de retour de condensat 114.On the figure 2 , the outer casing 111 has the general shape of a cylindrical bottle with a vertical axis, turned upside down with the neck. More specifically, the main body delimiting the interior space 112 has a larger diameter than the condensate return tube 114.

Les parois étanches et thermiquement isolantes sont ici formées de deux couches parallèles de tôles métalliques mutuellement espacées, avec un espace mis sous vide entre les deux. D'autres formes d'isolation thermique pourraient être utilisées.The watertight and thermally insulating walls are here formed of two parallel layers of mutually spaced metal sheets, with a vacuum space between the two. Other forms of thermal insulation could be used.

Le tube de retour de condensat 114 présente des soufflets pour absorber la contraction thermique lors des changements de température de l'enveloppe externe 111, notamment au moment de sa mise en service. Il est terminé à son extrémité inférieure par une bride de fixation 21 pour la fixation sur la paroi de sommet de la cuve 2.The condensate return tube 114 has bellows for absorbing thermal contraction when the temperature of the outer casing 111 changes, especially when it is put into service. It is terminated at its lower end by a fixing flange 21 for fixing to the top wall of the tank 2.

La canalisation collectrice 213 est disposée de manière concentrique dans le tube de retour de condensat 114 depuis l'extrémité du tube de retour de condensat 114 et pénètre dans l'espace intérieur 112 sur une grande partie de sa hauteur. L'extrémité supérieure de la canalisation collectrice 213 est ouverte et débouche dans la partie supérieure de l'espace intérieur 112. Pour garantir la tenue mécanique de la canalisation collectrice 213 dans cette position, des organes de fixation peuvent être prévus pour lier la canalisation collectrice 213 à l'enveloppe externe 111. Par exemple, des pattes de fixations 22 sont ici prévues à l'extrémité supérieure de la canalisation collectrice 213 et attachées au circuit de vaporisation 115, lui-même fixé à l'enveloppe externe 111.The collecting pipe 213 is arranged concentrically in the condensate return tube 114 from the end of the condensate return tube 114 and enters the interior space 112 over a large part of its height. The upper end of the collecting pipe 213 is open and opens into the upper part of the interior space 112. To guarantee the holding mechanical of the collecting pipe 213 in this position, fixing members can be provided to link the collecting pipe 213 to the external envelope 111. For example, fixing lugs 22 are here provided at the upper end of the collecting pipe 213 and attached to the vaporization circuit 115, itself fixed to the external envelope 111.

Le circuit de vaporisation 115 va maintenant être décrit plus en détails. Il comporte essentiellement :

  • un distributeur d'entrée 23 de forme annulaire ou torique disposé au sommet de l'espace intérieur 112,
  • un carter de sortie 24 également de forme annulaire ou torique disposé au bas de l'espace intérieur 112 autour de la canalisation collectrice 213, et
  • un grand nombre de tubes à ailettes 25 s'étendant parallèlement à la canalisation collectrice 213, de préférence verticalement, entre le distributeur d'entrée 23 et le carter de sortie 24.
The vaporization circuit 115 will now be described in more detail. It essentially comprises:
  • an annular or toroidal inlet distributor 23 disposed at the top of the interior space 112,
  • an outlet casing 24 also of annular or toroidal shape disposed at the bottom of the interior space 112 around the collecting pipe 213, and
  • a large number of finned tubes 25 extending parallel to the collecting pipe 213, preferably vertically, between the inlet distributor 23 and the outlet housing 24.

Les tubes à ailettes 25 ont chacun une extrémité supérieure 27 débouchant dans la chambre annulaire 26 du distributeur d'entrée 23 à travers la paroi de fond de celui-ci et une extrémité inférieure 28 débouchant dans la chambre annulaire 29 du carter de sortie 24 à travers la paroi de couverture de celui-ci. Ils constituent les parois d'échange de chaleur de l'échangeur de chaleur 110, qui permettent de réaliser conjointement la vaporisation de la phase liquide s'écoulant vers le bas dans les tubes à ailettes 25 et la condensation de la phase gazeuse s'écoulant vers le bas dans l'espace intérieur 112.The finned tubes 25 each have an upper end 27 opening into the annular chamber 26 of the inlet distributor 23 through the bottom wall thereof and a lower end 28 opening into the annular chamber 29 of the outlet housing 24 to through the cover wall of it. They constitute the heat exchange walls of the heat exchanger 110, which make it possible to jointly carry out the vaporization of the liquid phase flowing downwards in the finned tubes 25 and the condensation of the gaseous phase flowing down in the interior space 112.

Les tubes à ailettes 25 sont distribués dans tout l'espace intérieur 112 tout autour de la canalisation collectrice 213, comme partiellement représenté sur la figure 3, afin de maximiser la surface d'échange entre les deux flux et d'homogénéiser les transferts de chaleur.The finned tubes 25 are distributed throughout the interior space 112 all around the collecting pipe 213, as partially shown in the figure 3 , in order to maximize the exchange surface between the two flows and to homogenize the heat transfers.

La figure 4 représente deux modes de réalisation des tubes à ailettes 25. Sur la vue de droite, le corps de tube 30 est entouré d'ailettes 31 en forme de disques s'étendant transversalement au corps de tube 30 et distribuées de manière mutuellement espacée sur toute la longueur du corps de tube 30.The figure 4 shows two embodiments of the finned tubes 25. In the right view, the tube body 30 is surrounded by fins 31 in the form of discs extending transversely to the tube body 30 and distributed in a mutually spaced manner over the entire length of tube body 30.

Sur la vue de gauche, le corps de tube 30 est entouré d'ailettes 32 en forme de lames rectangulaires ou polygonales s'étendant parallèlement au corps de tube 30 sur toute la longueur du corps de tube 30 et distribuées de manière mutuellement espacée tout autour du corps de tube 30.In the left view, the tube body 30 is surrounded by fins 32 in the form of rectangular or polygonal blades extending parallel to the tube body 30 over the entire length of the tube body 30 and distributed in a mutually spaced manner all around of the tube body 30.

Dans une variante non représentée, les ailettes sont supprimées, ce qui permet de diminuer l'encombrement latéral de chaque tube et donc d'augmenter le nombre de tubes, pour obtenir également une surface d'échange élevée.In a variant not shown, the fins are eliminated, which makes it possible to reduce the lateral size of each tube and therefore to increase the number of tubes, to also obtain a high exchange surface.

La chambre annulaire 26 du distributeur d'entrée 23 présente ici une section transversale carrée et s'étend au droit des tubes à ailettes 25, donc à la périphérie de la canalisation collectrice 213. Par ailleurs, une paroi conique est disposée au centre du distributeur d'entrée 23, avec son sommet tourné vers l'extrémité supérieure de la canalisation collectrice 213 pour obturer le centre du distributeur d'entrée 23, et ainsi forcer la phase vapeur à s'écouler latéralement vers le sommet des tubes à ailettes 25 en sortant la canalisation collectrice 213.The annular chamber 26 of the inlet distributor 23 has here a square cross section and extends in line with the fin tubes 25, therefore at the periphery of the collecting pipe 213. Furthermore, a conical wall is arranged in the center of the distributor inlet 23, with its top facing the upper end of the collecting pipe 213 to close the center of the inlet distributor 23, and thus force the vapor phase to flow laterally towards the top of the fin tubes 25 in leaving the collecting pipe 213.

Un tube d'entrée 117 s'étend latéralement depuis la chambre annulaire 26 jusqu'à l'extérieur de l'enveloppe externe 111. Des soudures étanches ou des joints d'étanchéité non représentés sont prévus autour du tube d'entrée 117 au niveau de la traversée de l'enveloppe externe 111 pour conserver l'étanchéité de celle-ci. Le tube d'entrée 117 est relié à la pompe de circulation 16 par toute canalisation adaptée, de préférence munie d'une isolation thermique.An inlet tube 117 extends laterally from the annular chamber 26 to the outside of the outer casing 111. Sealed welds or seals, not shown, are provided around the inlet tube 117 at the level of the crossing of the outer casing 111 to maintain the sealing thereof. The inlet tube 117 is connected to the circulation pump 16 by any suitable pipe, preferably provided with thermal insulation.

Le carter de sortie 24 présente une forme torique creuse autour de la canalisation collectrice 213 et à distance de celle-ci. Sa paroi de fond 33 est concave afin de former un bac de séparation de phases qui permet de collecter par gravité la partie non vaporisée du flux de gaz en phase liquide injecté depuis le tube d'entrée 117. Un tuyau de purge 34 débouchant au bas de paroi de fond 33 permet d'évacuer cette fraction liquide, par exemple pour la réinjecter dans la cuve 2. Par ailleurs, un tube de sortie 103 s'étend latéralement depuis la chambre annulaire 29 jusqu'à l'extérieur de l'enveloppe externe 111. Le tube de sortie 103 débouche dans la chambre annulaire 29 au-dessus de la paroi de fond 33 concave, afin d'éviter de collecter la phase liquide. En pratique, le niveau de remplissage de la paroi de fond 33 doit être maintenu relativement bas pour éviter un débordement de la phase liquide vers le tube de sortie 103. Des soudures étanches ou des joints d'étanchéité non représentés sont prévus autour du tube de sortie 103 au niveau de la traversée de l'enveloppe externe 111 pour conserver l'étanchéité de celle-ci. Le tube de sortie 103 est relié aux organes de consommateur de gaz combustible, directement ou via d'autres équipements de traitement du gaz, par exemple, compresseur, réchauffeur, etc.The outlet casing 24 has a hollow toroidal shape around and away from the collecting pipe 213. Its bottom wall 33 is concave in order to form a phase separation tank which makes it possible to collect by gravity the non-vaporized part of the flow of gas in liquid phase injected from the inlet tube 117. A purge pipe 34 opening at the bottom of the bottom wall 33 makes it possible to evacuate this liquid fraction, for example to reinject it into the tank 2. Furthermore, an outlet tube 103 extends laterally from the annular chamber 29 to the outside of the envelope 111. The outlet tube 103 opens into the annular chamber 29 above the concave bottom wall 33, in order to avoid collecting the liquid phase. In practice, the filling level of the bottom wall 33 must be kept relatively low to avoid an overflow of the liquid phase towards the outlet tube 103. Sealed welds or seals not shown are provided around the tube. exit 103 at the crossing of the outer casing 111 to maintain the seal thereof. The outlet tube 103 is connected to the fuel gas consuming members, directly or via other gas processing equipment, for example, compressor, heater, etc.

En fonctionnement, le fait que la phase vapeur collectée dans la partie supérieure 8 de la cuve 2 soit canalisée en haut de l'échangeur de chaleur 110 par la canalisation collectrice 213, assure d'une part que l'échangeur de chaleur 110 travaille sur sensiblement toute sa hauteur et d'autre part qu'un mouvement de convection/pompage par condensation est assuré sur la phase vapeur. Cette dernière, relativement chaude par rapport à la phase liquide se trouvant dans la partie inférieure 9 de la cuve 2, rentre par la canalisation collectrice 213 et arrive au sommet de l'échangeur de chaleur 110. Elle rentre alors en contact avec les surfaces d'échange de chaleur du circuit de vaporisation, à savoir les tubes 25, se refroidit, ce qui crée un premier effet d'aspiration par contraction thermique de la vapeur, puis change d'état en cédant sa chaleur latente de vaporisation pour former des gouttelettes qui descendent alors par gravité jusqu'à la paroi de fond 35 concave de l'enveloppe externe 111, ce qui crée un second effet d'aspiration. Il est ainsi possible de se passer d'organes de pompage actifs pour entrainer la circulation de la phase vapeur.In operation, the fact that the vapor phase collected in the upper part 8 of the tank 2 is channeled at the top of the heat exchanger 110 by the collecting pipe 213, ensures on the one hand that the heat exchanger 110 works on substantially its entire height and on the other hand that a convection / pumping by condensation movement is ensured on the vapor phase. The latter, relatively hot compared to the liquid phase located in the lower part 9 of the tank 2, enters through the collecting pipe 213 and arrives at the top of the heat exchanger 110. It then comes into contact with the surfaces d heat exchange of the vaporization circuit, namely the tubes 25, cools, which creates a first suction effect by thermal contraction of the vapor, then changes state by yielding its latent heat of vaporization to form droplets which then descend by gravity to the concave bottom wall 35 of the outer casing 111, which creates a second suction effect. It is thus possible to do without active pumping members to cause the circulation of the vapor phase.

Dans le circuit de vaporisation 115, l'architecture représentée ici avec une entrée en haut et une sortie en bas utilise une technique de film tombant le fonctionnement à obtenir est que ce film ait perdu tous les composants pouvant vaporiser durant le laps de temps entre son entrée dans la chambre 26 et son arrivée dans la chambre 29, sous réserve des corps peu volatils qu'il est susceptible de contenir et qui arriveront alors en phase liquide sur la paroi de fond 33.In the vaporization circuit 115, the architecture shown here with an inlet at the top and an outlet at the bottom uses a film falling technique. The operation to be obtained is that this film has lost all of the components which can vaporize during the time between its entering chamber 26 and arriving in chamber 29, subject to the low volatility bodies which it is likely to contain and which will then arrive in liquid phase on the bottom wall 33.

Un clapet 49 est agencé de préférence sur le tuyau de purge 34, pour fermer le tuyau de purge 34 pendant le fonctionnement normal de l'installation et ouvrir le tuyau de purge 34 de façon intermittente pour évacuer la fraction liquide riche en corps lourds. L'évacuation de la fraction liquide peut être provoquée soit par injection de gaz sous pression dans le tube d'entrée 117, soit par gravité sous le seul effet de la pression hydrostatique des corps lourds accumulés. Cette opération de purge peut ainsi se faire même lorsque l'installation est en fonctionnement.A valve 49 is preferably arranged on the purge pipe 34, to close the purge pipe 34 during normal operation of the installation and open the purge pipe 34 intermittently to evacuate the liquid fraction rich in heavy bodies. The evacuation of the liquid fraction can be brought about either by injection of gas under pressure into the inlet tube 117, or by gravity under the sole effect of the hydrostatic pressure of the accumulated heavy bodies. This purge operation can thus be done even when the installation is in operation.

Alternativement, une vanne 149 est employée sur le tuyau de purge 34 au lieu du clapet 49, pour pouvoir fermer le tuyau de purge 34 si nécessaire et ouvrir le tuyau de purge 34 de façon intermittente ou continue pour évacuer la fraction liquide riche en corps lourds. L'évacuation de la fraction liquide peut être provoquée par gravité lorsque la vanne est en position ouverte, sous le seul effet de la pression hydrostatique des corps lourds accumulés. Cette opération de purge peut aussi se faire lorsque l'installation est en fonctionnement.Alternatively, a valve 149 is used on the purge pipe 34 instead of the valve 49, in order to be able to close the purge pipe 34 if necessary and open the purge pipe 34 intermittently or continuously to evacuate the liquid fraction rich in heavy bodies . The evacuation of the liquid fraction can be caused by gravity when the valve is in the open position, under the sole effect of the hydrostatic pressure of the accumulated heavy bodies. This purge operation can also be done when the installation is in operation.

Alternativement, une pompe extérieure à la cuve, non représentée, peut être utilisée pour évacuer cette fraction liquide restante, de manière intermittente ou continue. L'un des avantages de cette architecture est que le risque de saturation du circuit de vaporisation 115 par la phase liquide est relativement limité: si la chaleur amenée par la vapeur est insuffisante à assurer la vaporisation du liquide, la phase liquide restante peut être évacuée à mesure qu'elle arrive sans interrompre le procédé de vaporisation. Ceci ne serait pas le cas avec un récipient bouilleur alimenté par le bas et dans lequel un talon liquide est mis en ébullition.Alternatively, a pump external to the tank, not shown, can be used to evacuate this remaining liquid fraction, intermittently or continuously. One of the advantages of this architecture is that the risk of saturation of the vaporization circuit 115 by the liquid phase is relatively limited: if the heat supplied by the vapor is insufficient to vaporize the liquid, the remaining liquid phase can be evacuated as it arrives without interrupting the spraying process. This would not be the case with a boiling vessel fed from below and in which a liquid heel is brought to the boil.

Comme à la figure 5, il est possible de forcer davantage la vaporisation du gaz combustible en phase liquide arrivant dans le circuit de vaporisation 115 en plaçant ce dernier sous dépression. Le dispositif de purge et son fonctionnement seront modifiés dans ce cas.As in the figure 5 , it is possible to further force the vaporization of the combustible gas in the liquid phase arriving in the vaporization circuit 115 by placing the latter under vacuum. The purge device and its operation will be modified in this case.

Lorsque le circuit de vaporisation 115 est placé en dépression, on ajoute une seconde vanne 52 sur le tuyau de purge 34 en amont de la vanne 149 afin de créer un volume tampon 53 pouvant prendre la forme d'un tuyau ou d'un réservoir. Le fonctionnement des vannes 52 et 149 est alternatif : on commence par ouvrir la seconde vanne 52 pour laisser l'espace tampon 53 se remplir des corps lourds. Puis on referme la seconde vanne 52 avant d'ouvrir la vanne 149 pour vidanger le volume tampon par gravité avant de refermer la vanne 149. L'ouverture des vannes 52 et 149 peut être provoquée soit par injection de gaz soit par pilotage électrique comme pour des électro-vannes.
La fréquence d'ouverture des vannes 52 et 149 est directement liée à la composition du GNL, ainsi plus le GNL comporte une fraction importante de composés lourds plus la fréquence d'ouverture des vannes 52 et 149 est importante.
When the vaporization circuit 115 is placed under vacuum, a second valve 52 is added to the purge pipe 34 upstream of the valve 149 in order to create a buffer volume 53 which can take the form of a pipe or a reservoir. The operation of valves 52 and 149 is alternative: we start by opening the second valve 52 to let the buffer space 53 fill with heavy bodies. Then close the second valve 52 before opening the valve 149 to empty the buffer volume by gravity before closing the valve 149. The opening of the valves 52 and 149 can be caused either by gas injection or by electric control as for solenoid valves.
The opening frequency of valves 52 and 149 is directly linked to the composition of the LNG, so the more the LNG contains a large fraction of heavy compounds the greater the opening frequency of the valves 52 and 149.

L'architecture de l'échangeur de chaleur 110 permet de réaliser un échange de chaleur à courants parallèles ou co-courants. En théorie, cette forme d'échange thermique présente une efficacité moindre que l'échange thermique à contre-courant. En effet, dans un échangeur de chaleur bi-fluide, les deux fluides rentrent dans l'échangeur avec un écart de température donné entre les deux fluides. Si l'échange thermique est fait à contre-courant, la température de sortie d'un des fluides tend vers la température d'entrée de l'autre et réciproquement. En revanche, dans un échangeur à co-courant, les deux fluides tendent vers une température de mélange.The architecture of the heat exchanger 110 makes it possible to carry out a heat exchange with parallel currents or co-currents. In theory, this form of heat exchange has less efficiency than counter-current heat exchange. In fact, in a bi-fluid heat exchanger, the two fluids enter the exchanger with a given temperature difference between the two fluids. If the heat exchange is done against the current, the outlet temperature of one of the fluids tends towards the inlet temperature of the other and vice versa. On the other hand, in a co-current exchanger, the two fluids tend towards a mixing temperature.

Ces considérations ne sont pas un obstacle au bon fonctionnement de l'échangeur de chaleur 110 qui est utilisé comme un évapo-condenseur. En effet, la part de chaleur sensible dans les échanges thermiques en cause est minoritaire, et la majorité du transfert thermique est réalisée de manière isotherme par changement de phase.These considerations are not an obstacle to the proper functioning of the heat exchanger 110 which is used as an evapo-condenser. In fact, the share of sensible heat in the heat exchanges in question is a minority, and the majority of the heat transfer is carried out isothermally by phase change.

A titre d'illustration, si la phase vapeur du gaz combustible rentre à -100°C dans la canalisation collectrice 213, la part de chaleur sensible pour faire passer cette vapeur à -160°C est d'environ 130kJ/kg alors que la chaleur latente nécessaire à la condenser est de 510kJ/kg. Ainsi, la majorité du transfert thermique est isotherme. Il en est de même pour la phase liquide dans le circuit de vaporisation 115.By way of illustration, if the vapor phase of the combustible gas returns to -100 ° C in the collecting pipe 213, the proportion of sensible heat to bring this vapor to -160 ° C is approximately 130 kJ / kg while the latent heat necessary to condense it is 510kJ / kg. Thus, the majority of the heat transfer is isothermal. It is the same for the liquid phase in the vaporization circuit 115.

En référence à la figure 6, on observe une vue écorchée d'un navire méthanier 70 équipée d'une installation d'alimentation en gaz combustible d'organes consommateurs de gaz et de liquéfaction dudit gaz combustible telle que décrite ci-dessus. La figure 6 montre une cuve étanche et isolée 71 de forme générale prismatique montée dans la double coque 72 du navire. La paroi de la cuve 71 comporte une barrière étanche primaire destinée à être en contact avec le GNL contenu dans la cuve, une barrière étanche secondaire agencée entre la barrière étanche primaire et la double coque 72 du navire, et deux barrières isolante agencées respectivement entre la barrière étanche primaire et la barrière étanche secondaire et entre la barrière étanche secondaire et la double coque 72.With reference to the figure 6 , there is a cutaway view of an LNG tanker 70 equipped with a fuel gas supply installation for gas consuming bodies and liquefaction of said fuel gas as described above. The figure 6 shows a sealed and insulated tank 71 of generally prismatic shape mounted in the double hull 72 of the ship. The wall of the tank 71 comprises a primary waterproof barrier intended to be in contact with the LNG contained in the tank, a secondary waterproof barrier arranged between the primary waterproof barrier and the double hull 72 of the ship, and two insulating barriers arranged respectively between the primary waterproof barrier and the secondary waterproof barrier and between the secondary waterproof barrier and the double shell 72.

De manière connue en soi, des canalisations de chargement/déchargement 73 disposées sur le pont supérieur du navire peuvent être raccordées, au moyen de connecteurs appropriées, à un terminal maritime ou portuaire pour transférer une cargaison de GNL depuis ou vers la cuve 71.In a manner known per se, loading / unloading lines 73 arranged on the upper deck of the ship can be connected, using appropriate connectors, to a maritime or port terminal to transfer a cargo of LNG from or to the tank 71.

La figure 6 représente un exemple de terminal maritime comportant un poste de chargement et de déchargement 75, une conduite sous-marine 76 et une installation à terre 77. Le poste de chargement et de déchargement 75 est une installation fixe off-shore comportant un bras mobile 74 et une tour 78 qui supporte le bras mobile 74. Le bras mobile 74 porte un faisceau de tuyaux flexibles isolés 79 pouvant se connecter aux canalisations de chargement/déchargement 73. Le bras mobile 74 orientable s'adapte à tous les gabarits de méthaniers. Une conduite de liaison non représentée s'étend à l'intérieur de la tour 78. Le poste de chargement et de déchargement 75 permet le chargement et le déchargement du méthanier 70 depuis ou vers l'installation à terre 77. Celle-ci comporte des cuves de stockage de gaz liquéfié 80 et des conduites de liaison 81 reliées par la conduite sous-marine 76 au poste de chargement ou de déchargement 75. La conduite sous-marine 76 permet le transfert du gaz liquéfié entre le poste de chargement ou de déchargement 75 et l'installation à terre 77 sur une grande distance, par exemple 5 km, ce qui permet de garder le navire méthanier 70 à grande distance de la côte pendant les opérations de chargement et de déchargement.The figure 6 represents an example of a maritime terminal comprising a loading and unloading station 75, an underwater pipe 76 and a shore installation 77. The loading and unloading station 75 is a fixed offshore installation comprising a movable arm 74 and a tower 78 which supports the movable arm 74. The movable arm 74 carries a bundle of insulated flexible pipes 79 which can be connected to the loading / unloading pipes 73. The movable arm 74 can be adjusted to suit all sizes of LNG carriers. A connection pipe, not shown, extends inside the tower 78. The loading and unloading station 75 allows the loading and unloading of the LNG carrier 70 from or to the onshore installation 77. This comprises liquefied gas storage tanks 80 and connecting pipes 81 connected by the subsea pipe 76 to the loading or unloading station 75. The subsea pipe 76 allows the transfer of the liquefied gas between the loading or unloading station 75 and the shore installation 77 over a long distance, for example 5 km, which makes it possible to keep the LNG carrier 70 at a great distance from the coast during the loading and unloading operations.

Pour engendrer la pression nécessaire au transfert du gaz liquéfié, on met en œuvre des pompes embarquées dans le navire 70 et/ou des pompes équipant l'installation à terre 77 et/ou des pompes équipant le poste de chargement et de déchargement 75.To generate the pressure necessary for the transfer of the liquefied gas, pumps on board the ship 70 and / or pumps fitted to the shore installation 77 and / or pumps fitted to the loading and unloading station 75 are used.

Bien que l'invention ait été décrite en liaison avec plusieurs modes de réalisation particuliers, il est bien évident qu'elle n'y est nullement limitée et qu'elle comprend tous les équivalents techniques des moyens décrits ainsi que leurs combinaisons si celles-ci entrent dans le cadre de l'invention tel que défini par les revendications.Although the invention has been described in connection with several particular embodiments, it is obvious that it is in no way limited thereto and that it includes all the technical equivalents of the means described as well as their combinations if these fall within the scope of the invention as defined by the claims.

L'usage du verbe « comporter », « comprendre » ou « inclure » et de ses formes conjuguées n'exclut pas la présence d'autres éléments ou d'autres étapes que ceux énoncés dans une revendication.The use of the verb "to include", "to understand" or "to include" and of its conjugated forms does not exclude the presence of elements or other stages than those stated in a claim.

Dans les revendications, tout signe de référence entre parenthèses ne saurait être interprété comme une limitation de la revendication.In the claims, any reference sign in parentheses cannot be interpreted as a limitation of the claim.

Claims (17)

  1. An installation for feeding a gas-consuming member with combustible gas and for liquefying said combustible gas, the installation (1) including:
    - a leaktight heat-insulating tank (2) including an inner space (7) intended to be filled with combustible gas in a liquid-vapor two-phase state of equilibrium;
    - a heat exchanger (10, 110) placed in a higher position than the leaktight heat-insulating tank, the heat exchanger comprising a first path (15, 115) and a condensation path (12, 112) separated from each other in a leaktight manner by heat-exchange walls allowing heat to be transferred between a fluid contained in the condensation path and a fluid contained in the first path, the first path and the condensation path each including an inlet and an outlet,
    - the inlet of the condensation path being connected to the leaktight and heat-insulating tank by a vapor-collecting circuit (13, 113, 213) including an admission emerging in an upper portion (8) of the inner space of the tank to withdraw a first stream (19) of vapor-phase combustible gas in the inner space of the tank; the inlet of the condensation path is placed higher than the outlet of the condensation path,
    - the outlet of the condensation path (14, 114) being connected to the inner space of the tank to transfer by gravity a liquid fraction of the first stream of combustible gas in the inner space of the tank, the liquid fraction of the first stream of combustible gas being obtained by condensation in the condensation path,
    - the inlet of the first path (15, 115) being connected to the leaktight heat-insulating tank by a liquid inlet circuit (17, 117), the liquid inlet circuit including an admission emerging in a lower portion (9) of the inner space of the tank to withdraw a second stream of liquid-phase combustible gas in the inner space of the tank and a circulation pump (16) to transfer the second stream of liquid-phase combustible gas into the first path,
    characterized in that the first path is a vaporization path, the installation further comprising a vacuum pump (51) connected to the vaporization path (15, 115) to place the vaporization path of the heat exchanger at a pressure below the pressure prevailing in the vapor phase of the leaktight heat-insulating tank,
    and in that the outlet of the vaporization path (3, 103) is connected to a gas-consuming member to transfer a vapor fraction of the second stream of combustible gas to the gas-consuming member, the vapor fraction of the second stream of combustible gas being obtained during functioning, by vaporization of the combustible gas in the vaporization path placed at a pressure below the pressure prevailing in the vapor phase of the leaktight heat-insulating tank.
  2. The installation as claimed in claim 1, in which the vacuum pump (51) is arranged between the outlet of the vaporization path and the gas-consuming member.
  3. The installation as claimed in claim 1, in which the outlet of the the vaporization path (15, 115) is placed lower than the inlet of the vaporization path.
  4. The installation as claimed in claim 3, in which the vaporization path of the heat exchanger includes a phase separation tank (33) located at the bottom of the vaporization path, the phase separation tank including a base wall and a side wall extending upward from the base wall, the vaporization path outlet (103) emerging through the side wall of the phase separation tank at a position spaced above the base wall.
  5. The installation as claimed in claim 4, also including a purge circuit (34) emerging through the base wall of the phase separation tank to be able to evacuate a liquid phase from the phase separation tank by gravity.
  6. The installation as claimed in any one of claims 1 to 5, also including a compressor (4) arranged between the outlet of the vaporization path and the gas-consuming member.
  7. The installation as claimed in any one of claims 1 to 6, in which the heat exchanger includes a leaktight heat-insulating envelope (11, 111) delimiting an inner space (12, 112) containing the condensation path, the envelope being arranged above the leaktight heat-insulating tank and including a lower aperture (14, 114) communicating with the inner space of the leaktight heat-insulating tank and constituting the outlet of the condensation path.
  8. The installation as claimed in claim 7, in which a top wall (5) of the leaktight heat-insulating tank has an aperture connected to the lower aperture of the envelope, the envelope also including a fastening clip (21) arranged around the lower aperture of the envelope, the fastening clip being attached to the top wall of the leaktight heat-insulating tank around the aperture of the top wall.
  9. The installation as claimed in claim 8, in which the heat exchanger also includes a collecting pipe (113, 213) extending from the lower aperture of the envelope to a position close to a top wall of the envelope (11, 111) and having a lower extremity emerging in the inner space of the tank and an upper extremity emerging in the inner space (12, 112) of the envelope, the collecting pipe delimiting within the inner space of the envelope an inner space of the collecting pipe forming the vapor-collecting circuit and an outer space of the collecting pipe forming the condensation path of the heat exchanger.
  10. The installation as claimed in claim 9, in which the heat exchanger includes:
    a plurality of tubes (55) parallel to the collecting pipe arranged in the outer space of the collecting pipe around the collecting pipe, the parallel tubes constituting said heat-exchange walls of the heat exchanger,
    an inlet distributor (23) arranged in the inner space of the envelope, the inlet distributor extending to the periphery of the collecting pipe and having a base wall through which emerges an upper extremity of each of the parallel tubes,
    an inlet tube (117) constituting the inlet of the vaporization path and extending through the envelope between the exterior of the envelope and the inlet distributor,
    an outlet case (24) arranged in the outer space of the collecting pipe around the collecting pipe lower than the inlet chamber and having a top wall through which emerges a lower extremity of each of the parallel tubes, and
    an outlet tube (103) constituting the outlet of the vaporization path and extending through the envelope between the outlet case and the exterior of the envelope.
  11. The installation as claimed in claim 10, in which the inlet distributor (23) is arranged higher than the upper extremity of the collecting pipe (213).
  12. The installation as claimed in claim 11, in which the tubes (25) parallel to the collecting pipe have heat-exchange vanes (31, 32) arranged on the outer surface of the tubes parallel to the collecting pipe (213).
  13. The installation as claimed in any one of claims 1 to 12, also including a plurality of leaktight heat-insulating tanks including an inner space intended to be filled with the combustible gas in a liquid-vapor two-phase state of equilibrium, said vapor-collecting circuit (13) being a common collecting circuit connecting the inlet of the condensation path to each of said tanks to collect the gases derived from evaporation in each of the tanks.
  14. A process for feeding a gas-consuming member with combustible gas and for liquefying said combustible gas by means of an installation as claimed in any one of claims 1 to 12, including:
    - introducing a first stream of vapor-phase combustible gas (19) into the inlet of the condensation path (12, 112) from the upper portion (8) of the inner space of the leaktight heat-insulating tank through the vapor-collecting circuit,
    characterized in that he method further comprises:
    - transferring a second stream of liquid-phase combustible gas from the lower portion of the inner space of the tank to the inlet of the vaporization path (15, 115) by means of the circulation pump (16),
    - placing the vaporization path of the heat exchanger at a pressure below the pressure prevailing in the vapor phase of the leaktight heat-insulating tank,
    - exchanging heat between the first stream of combustible gas in the condensation path and the second stream of combustible gas in the vaporization path, so as to vaporize at least a fraction of the second stream of combustible gas in the vaporization path placed at a pressure below the pressure prevailing in the vapor phase of the leaktight heat-insulating tank while condensing at least a fraction of the first stream of combustible gas in the condensation path,
    - transferring by gravity the liquid fraction of the first stream of combustible gas from the outlet of the condensation path (14, 114) to the inner space of the tank, and
    - transferring the vapor fraction of the second stream of combustible gas from the outlet of the vaporization path to the gas-consuming member.
  15. A ship (70) including an installation (1) as claimed in any one of claims 1 to 12.
  16. A process for loading or emptying a ship (70) as claimed in claim 15, in which combustible gas is conveyed through insulated pipelines (73, 79, 76, 81) from or to a floating or land-based storage installation (77) to or from the ship's leaktight heat-insulated tank (71).
  17. A system for transferring a combustible gas, the system including a ship (70) as claimed in claim 15, insulated pipelines (73, 79, 76, 81) arranged so as to connect the tank (71) installed in the ship's hull to a floating or land-based storage installation (77), and a pump for entraining combustible gas through the insulated pipelines from or to the floating or land-based storage installation to or from the ship's leaktight heat-insulated tank (71).
EP17716958.8A 2016-03-22 2017-03-21 Facility for feeding fuel gas to a member consuming gas and for liquefying said fuel gas Active EP3433530B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL17716958T PL3433530T3 (en) 2016-03-22 2017-03-21 Facility for feeding fuel gas to a member consuming gas and for liquefying said fuel gas

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1652456A FR3049331B1 (en) 2016-03-22 2016-03-22 FUEL GAS SUPPLY INSTALLATION OF A GAS CONSUMER ORGAN AND LIQUEFACTION OF SUCH FUEL GAS
PCT/FR2017/050657 WO2017162977A1 (en) 2016-03-22 2017-03-21 Facility for feeding fuel gas to a member consuming gas and for liquefying said fuel gas

Publications (2)

Publication Number Publication Date
EP3433530A1 EP3433530A1 (en) 2019-01-30
EP3433530B1 true EP3433530B1 (en) 2020-04-22

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EP17716958.8A Active EP3433530B1 (en) 2016-03-22 2017-03-21 Facility for feeding fuel gas to a member consuming gas and for liquefying said fuel gas

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EP (1) EP3433530B1 (en)
JP (1) JP6942143B2 (en)
KR (1) KR102302436B1 (en)
CN (1) CN109154421B (en)
ES (1) ES2802601T3 (en)
FR (1) FR3049331B1 (en)
PL (1) PL3433530T3 (en)
SG (1) SG11201808311PA (en)
WO (1) WO2017162977A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201719399D0 (en) 2017-11-22 2018-01-03 Bennamann Services Ltd Liquid methane storage and fuel delivery system
KR102450533B1 (en) * 2018-01-25 2022-10-05 한국조선해양 주식회사 Volatile organic compounds treatment system and ship having the same
FR3093785B1 (en) * 2019-03-15 2021-06-04 Gaztransport Et Technigaz Pressure control system in a liquefied natural gas tank.
FR3108167B1 (en) * 2020-03-11 2022-02-11 Gaztransport Et Technigaz System for processing natural gas from a tank of a floating structure configured to supply natural gas as fuel to a natural gas-consuming device
FR3114797B1 (en) * 2020-10-02 2023-03-03 Gaztransport Et Technigaz Gas supply system for appliances using high and low pressure gas
JP2023545979A (en) * 2020-10-02 2023-11-01 ギャズトランスポルト エ テクニギャズ Gas supply systems for high-pressure and low-pressure gas consumers
FR3119420B1 (en) * 2021-01-29 2023-01-13 Safran SET FOR TURBOMACHINE
WO2023107062A2 (en) * 2021-12-06 2023-06-15 Aygaz Dogal Gaz Toptan Satis A.S. A double-tank mobile lng filling station and a filling method thereof
FR3130928A1 (en) * 2021-12-22 2023-06-23 Faurecia Systemes D'echappement Hydrogen storage and supply device and corresponding assembly

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5481303A (en) * 1977-12-12 1979-06-28 Chiyoda Chem Eng & Constr Co Ltd Heating of liquefied petroleum gas and equipment for the same
FR2691520B1 (en) 1992-05-20 1994-09-02 Technigaz Ste Nle Prefabricated structure for forming watertight and thermally insulating walls for containment of a fluid at very low temperature.
JP3591927B2 (en) * 1995-08-25 2004-11-24 株式会社神戸製鋼所 Cryogenic liquid with multiple components and boil-off gas treatment device
CN1194188C (en) * 1995-10-11 2005-03-23 卡古拉因贝斯特株式会社 Liquefied petroleum gas heat exchanging system
JP2912862B2 (en) * 1995-10-11 1999-06-28 カグラインベスト株式会社 Liquefied gas outflow prevention valve
BRPI0515295B1 (en) * 2004-09-14 2019-04-24 Exxonmobil Upstream Research Company METHOD AND SYSTEM FOR LIQUID NATURAL GAS PROCESSING
FR2877638B1 (en) 2004-11-10 2007-01-19 Gaz Transp Et Technigaz Soc Pa THERMALLY INSULATED AND THERMALLY INSULATED TANK WITH COMPRESSION-RESISTANT CALORIFIC ELEMENTS
CN200999962Y (en) * 2007-01-04 2008-01-02 刘凤国 Device for vaporizing liquid gas raffinate
JP5148319B2 (en) 2008-02-27 2013-02-20 三菱重工業株式会社 Liquefied gas reliquefaction apparatus, liquefied gas storage equipment and liquefied gas carrier equipped with the same, and liquefied gas reliquefaction method
JP2010043708A (en) * 2008-08-13 2010-02-25 Mitsubishi Heavy Ind Ltd Regional energy supply system
KR101009920B1 (en) * 2008-08-18 2011-01-20 에스티엑스조선해양 주식회사 Apparatus and method for supplying fuel gas in ships, floating vessels or floating facilities
FR2993643B1 (en) * 2012-07-17 2014-08-22 Saipem Sa NATURAL GAS LIQUEFACTION PROCESS WITH PHASE CHANGE
FR2996520B1 (en) * 2012-10-09 2014-10-24 Gaztransp Et Technigaz SEALED AND THERMALLY INSULATING TANK COMPRISING A METALIC MEMBRANE WOUNDED ACCORDING TO ORTHOGONAL PLATES
CN103994325B (en) * 2014-05-05 2016-06-01 中国寰球工程公司 Gas-liquid shunts the energy-saving low-temperature liquid ethylene gasifying process system of recovery mutually

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
FR3049331B1 (en) 2018-09-14
PL3433530T3 (en) 2020-10-19
JP2019512651A (en) 2019-05-16
CN109154421A (en) 2019-01-04
WO2017162977A1 (en) 2017-09-28
CN109154421B (en) 2020-12-04
SG11201808311PA (en) 2018-10-30
ES2802601T3 (en) 2021-01-20
KR20180133859A (en) 2018-12-17
FR3049331A1 (en) 2017-09-29
JP6942143B2 (en) 2021-09-29
EP3433530A1 (en) 2019-01-30
KR102302436B1 (en) 2021-09-16

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