US20150000334A1 - Liquefaction of Natural Gas - Google Patents

Liquefaction of Natural Gas Download PDF

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Publication number
US20150000334A1
US20150000334A1 US13/941,045 US201313941045A US2015000334A1 US 20150000334 A1 US20150000334 A1 US 20150000334A1 US 201313941045 A US201313941045 A US 201313941045A US 2015000334 A1 US2015000334 A1 US 2015000334A1
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lng
natural gas
vessel
vapour
heat exchanger
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US13/941,045
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David Edwards
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Houlder Ltd
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Houlder Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/0002Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the fluid to be liquefied
    • F25J1/0022Hydrocarbons, e.g. natural gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/006Processes or apparatus for liquefying or solidifying gases or gaseous mixtures characterised by the refrigerant fluid used
    • F25J1/007Primary atmospheric gases, mixtures thereof
    • F25J1/0072Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/0002Processes 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
    • F25J1/0203Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process using a single-component refrigerant [SCR] fluid in a closed vapor compression cycle
    • F25J1/0204Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process using a single-component refrigerant [SCR] fluid in a closed vapor compression cycle as a single flow SCR cycle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J1/00Processes or apparatus for liquefying or solidifying gases or gaseous mixtures
    • F25J1/02Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process
    • F25J1/0221Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process using the cold stored in an external cryogenic component in an open refrigeration loop
    • F25J1/0222Processes or apparatus for liquefying or solidifying gases or gaseous mixtures requiring the use of refrigeration, e.g. of helium or hydrogen ; Details and kind of the refrigeration system used; Integration with other units or processes; Controlling aspects of the process using the cold stored in an external cryogenic component in an open refrigeration loop in combination with an intermediate heat exchange fluid between the cryogenic component and the fluid to be liquefied
    • 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
    • F25J1/0234Integration with a cryogenic air separation unit
    • 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
    • F25J1/0278Unit being stationary, e.g. on floating barge or fixed platform
    • 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
    • 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
    • F17C2225/044Localisation of the filling point in the gas at several points, e.g. with a device for recondensing 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
    • 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
    • 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
    • F17C5/00Methods or apparatus for filling containers with liquefied, solidified, or compressed gases under pressures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2210/00Processes characterised by the type or other details of the feed stream
    • F25J2210/42Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2290/00Other details not covered by groups F25J2200/00 - F25J2280/00
    • F25J2290/34Details about subcooling of liquids
    • 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

Definitions

  • the present invention relates to liquefaction of natural gas vapour, particularly during the transport and storage of liquefied natural gas (LNG).
  • LNG liquefied natural gas
  • the present invention relates to the handling of boil off gas in a bunker vessel used to refuel LNG-powered vessels.
  • Liquefied natural gas is natural gas (typically methane—CH4) that has been liquefied, typically to make it more manageable during storage and/or transport. At atmospheric pressure, this means the temperature of the LNG is reduced to around ⁇ 163 degrees centigrade or below.
  • LNG carriers are vessels used to carry LNG across large distances, particularly to carry LNG from gas producing nations to gas consuming nations.
  • the journey times of such vessels are significant, measured in days, weeks and even months.
  • the LNG is stored at low temperature in order that it does not vaporise.
  • Another type of propulsion system used in LNG carriers is a dual fuel diesel electric propulsion system which can operate off either diesel or LNG itself
  • the BOG can be used as fuel for the engines to provide propulsion and electrical load. If there is insufficient engine load it is necessary to burn the excess BOG in a GCU.
  • a bunker vessel is a smaller vessel designed to carry fuel to the carrier from shore. The bunker vessel must dock with the carrier and transfer fuel from its tanks to that of the carrier.
  • the bunker vessel must cope with the fact that the process of fuel transfer is likely to involve an increased production of BOG as the LNG is transferred between the vessels. Even if this were not the case the base level production of BOG would still need to be handled. However, as both vessels are stationary during this process, the BOG created cannot be used for propulsion and must be handled in some other manner.
  • a re-liquefaction plant is impractical for a relatively small vessel such as a bunker vessel due to its large energy requirements and, as mentioned above, burning off excess BOG is both wasteful and environmentally unsound. There remains a need to find a method of handling BOG in bunker vessels that is both practical and effective.
  • a method for condensing natural gas vapour to generate liquefied natural gas (LNG), comprising:
  • liquid coolant wherein the liquid coolant has a boiling point less than that of natural gas
  • a system for condensing natural gas vapour to generate liquefied natural gas (LNG); comprising
  • a first heat exchanger arranged to cool LNG using a liquid coolant to generate sub-cooled LNG, wherein the liquid coolant has a boiling point less than that of natural gas;
  • a second heat exchanger arranged to condense natural gas vapour using the sub-cooled LNG to liquefy the natural gas vapour and thereby generate further LNG.
  • the present invention can provide an efficient method of condensing natural gas vapour to provide LNG.
  • Existing LNG is cooled at a first heat exchanger to create sub-cooled LNG that can be used to condense the natural gas vapour. This is significantly more energy efficient than provision of a plant for generating LNG directly from the natural gas vapour.
  • the use of a liquid coolant to first sub-cool existing available LNG reduces the need for energy intensive refrigeration cycles to generate a coolant to directly cool the natural gas vapour.
  • Boil-off gas is natural gas vapour that has arisen through the evaporation of an LNG source.
  • the boil-off gas is likely not to be significantly warmer than the boiling temperature of natural gas, and furthermore LNG is likely to be available for sub-cooling.
  • the natural gas vapour is boil-off gas.
  • the method may comprise receiving the LNG for cooling at the first heat exchanger from at least one LNG storage tank and returning the sub-cooled LNG to the at least one storage tank after it is used at the second heat exchanger.
  • LNG may be re-used for subsequent condensing of natural gas vapour.
  • the sub-cooled LNG is likely to have warmed somewhat, but the method is preferably arranged such that it remains in liquid form for returning to the LNG storage tank.
  • the method may further comprise delivering the further LNG to the at least one storage tank.
  • the LNG that is created through the method may subsequently be used for condensing further natural gas vapour in future cycles.
  • the system is compact and efficient in that there is no requirement for separate tanks for the coolant used at the second heat exchanger and the generated LNG.
  • the liquid coolant used at the first generator has a boiling point less than that of the natural gas vapour.
  • the natural gas vapour is preferably predominantly methane, more preferably at least 90 Mole % methane, at least 95 Mole % methane or over 97% Mole methane.
  • Methane has a boiling point at atmospheric pressure of around ⁇ 163 degrees centigrade.
  • the liquid coolant has a boiling point at atmospheric pressure of less than that of methane (i.e. less than ⁇ 163 degrees centigrade), more preferably less than ⁇ 170 degrees centigrade, and most preferably less than ⁇ 190 degrees centigrade.
  • the liquid coolant is liquid nitrogen.
  • the boiling point of nitrogen is around ⁇ 193 degrees centigrade at atmospheric pressure. References to atmospheric pressure refer to a pressure equal to the understood unit of one atmosphere, rather than to prevailing climatic conditions.
  • the system may comprise a storage facility for the liquid coolant.
  • the system may comprise at least one storage tank for storing the liquid coolant.
  • the system may additionally or alternatively comprise a generator for generating the liquid coolant.
  • the method may comprise a step of generating the liquid coolant.
  • an initial supply of liquid coolant may be provided to the storage facility from an on-shore facility while the vessel is docked, but when the vessel is at sea additional liquid coolant may be provided as needed by the generator.
  • a vessel may be provided comprising the system of the second aspect.
  • the vessel may comprise a flow boom arranged to transfer LNG to a second vessel and to receive natural gas vapour from the second vessel.
  • the method may further comprise transferring LNG from a first vessel to a second vessel, and receiving the natural gas vapour from the second vessel.
  • one or both vessels are maritime vessels.
  • the vessel comprising the system i.e. the first vessel
  • the second vessel may be an LNG fuelled vessel.
  • the second vessel may be a carrier, particularly an LNG carrier.
  • a bunker vessel is a vessel arranged to re-fuel other vessels while at sea.
  • one or both vessels are LNG powered vessels.
  • FIG. 1 is a schematic diagram showing a bunker vessel comprising a system or handling LNG;
  • FIG. 2 is a schematic diagram showing the connection between various elements of the system in more detail.
  • FIG. 3 is a schematic diagram illustrating the components of a re-condenser unit.
  • FIG. 1 a schematic diagram is provided showing the principle elements of a LNG handling system aboard a bunker vessel 1 for re-fuelling larger ships.
  • the system comprises two LNG storage tanks 10 , port and starboard manifolds 20 , a liquid nitrogen tank 30 , a gaseous nitrogen tank 40 , a liquid nitrogen generator 50 , a re-condenser unit 60 , engines 70 and a flow boom 80 .
  • FIG. 1 illustrates functional connections between the various illustrated elements of the system for the transfer of LNG (indicated as “L”, dotted lines), natural gas vapour (indicated as “V”, thick lines) and nitrogen (both liquid and gaseous indicated as “N”, thin lines).
  • the port and starboard manifolds 20 are arranged to allow transfer of LNG, natural gas vapour, and nitrogen between the bunker vessel and an on-shore facility.
  • LNG received from the port and starboard manifolds is stored in the storage tanks 10 .
  • the storage tanks are pressurised, C-class, storage tanks which may operate at up to 10 bar, but the skilled person will recognize that alternative tanks may be used.
  • the storage tanks may be any type of chamber or container suitable to act as a reservoir for LNG. Pressurised tanks, particularly pressurised “C” Type tanks, allow a wider range of operating temperature and pressure within the bunker vessel.
  • the storage tanks store LNG at around ⁇ 163 degrees centigrade.
  • Liquid nitrogen received from the manifolds 20 is stored in liquid nitrogen tank 30 .
  • Nitrogen that evaporates from liquid nitrogen tank 30 may be received in gas nitrogen tank 40 from where it is passed to the ship's systems for use in for purging of cargo/fuel lines, inerting tanks and hold spaces and so on. Alternatively or additionally, nitrogen may be vented to the atmosphere or re-used by liquid nitrogen generator 50 .
  • the liquid nitrogen tank 30 and the gas nitrogen tank 40 may be any suitable container or chamber suitable to act as a reservoir for liquid nitrogen and gaseous nitrogen respectively.
  • the liquid nitrogen generator 50 passes generated liquid nitrogen back to the liquid nitrogen tank 30 .
  • the liquid nitrogen generator 50 may be a compression cooling system, and is preferably powered by the vessel's electrical systems.
  • the liquid nitrogen generator 50 may be arranged to filter and compress atmospheric air before carbon dioxide water and residual hydrocarbons are removed in an air purification unit. The air is then passed to a cold box where it is cooled and liquefied. The liquid air is distilled then in a distillation column to yield pure nitrogen gas which is condensed in a condenser to yield pure liquid nitrogen.
  • the system comprises a flow boom 80 for transferring LNG to another vessel, such as an LNG carrier.
  • the flow boom 80 is a transfer boom in this embodiment.
  • the transfer boom 80 receives LNG from LNG storage tank 10 and may also receive natural gas vapour from the other vessel. Natural gas vapour received by the transfer boom is passed to the re-condenser unit 60 .
  • the re-condenser unit 60 also receives natural gas vapour from the LNG storage tank 10 .
  • the re-condenser unit 60 is arranged to re-liquefy the natural gas vapour to return it to an LNG state. Once re-liquefied the LNG may be passed back to the LNG storage tank 10 .
  • the re-condenser unit 60 also receives liquid nitrogen from the liquid nitrogen tank 30 and LNG from the LNG tanks 10 . These liquids are used during the processes of cooling the natural gas vapour at the re-condenser unit, as will be explained in greater detail below with reference to FIG. 3 .
  • the engines 70 of the bunker vessel use the stored LNG as a fuel source.
  • natural gas vapour is used for combustion in the engines.
  • the natural gas vapour used for this purpose may be boil-off gas (BOG) spontaneously occurring in the LNG storage tanks 10 , or may be deliberately vaporised LNG from the LNG storage tanks.
  • LNG from the storage tank may be vaporised by a forcing vaporizer, for example.
  • FIG. 2 shows in more detail the connections between various elements of the system of FIG. 1 .
  • FIG. 2 illustrates the LNG storage tanks 10 and the port and starboard manifolds 20 .
  • a variety of valves are provided to control the flows and pressures of gas and liquid in the system.
  • FIG. 2 also illustrates various connection points to other elements of the system.
  • connection points 201 are provided for LNG returning from the re-condenser unit 60
  • connection points 202 are provided for natural gas vapour passed to the re-condensing unit 60 .
  • connection point 210 for passing LNG to the re-condensing unit 60 for use during a re-liquefaction process implemented by the re-condensing unit 60 and a connection point 214 for receiving LNG from the re-condensing unit that has been used for this purpose.
  • LNG that is extracted from the LNG storage tanks 10 but is not ultimately used in the engine 70 or the re-condensing unit 60 may be returned to the LNG storage tanks via connection points 215 .
  • Connection point 203 is shown for passing LNG to the transfer boom 80 , while connection point 204 receives natural gas vapour from the transfer boom 80 .
  • LG can be transferred to another vessel, while excess boil-off as from the vessel can be retrieved for handling on the bunker vessel.
  • Connection point 205 is provided for passing gas vapour to the engines 70 .
  • connection point 206 for transferring natural gas vapour to a gas combustion unit (GCU). In an emergency situation, this GCU may be used to burn and thus dispose of natural gas vapour that is not otherwise handled by the system.
  • GCU gas combustion unit
  • this GCU may be used to burn and thus dispose of natural gas vapour that is not otherwise handled by the system.
  • vent 208 to vent natural gas vapour to the atmosphere where this is appropriate.
  • Connection point 207 is provided for the receipt of nitrogen vapour for purging of lines, and inerting spaces as required. Excess vapour would be vented via the GCU. The vapour may be received from the gas nitrogen tank 40 which receives boil-off from the liquid nitrogen tank 30 . Connection point 210 is for supply of liquid nitrogen via the manifolds 20 from shore for charging the liquid nitrogen storage tank 30 .
  • Each LNG storage tank is provided with a discharge pump 11 for pumping LNG to the transfer boom 80 and a LNG fuel pump 12 for pumping LNG to the engines 70 .
  • Various connections allow the LNG pumped by either the discharge pump 11 or the LNG fuel pump 12 to be re-directed as appropriate.
  • Each LNG storage tank 10 also comprises a first LNG inlet 13 and a second LNG inlet 14 .
  • LNG can be received at the LNG storage tanks 10 from the re-condenser unit 60 via connection points 201 and from the port and starboard manifolds 20 .
  • the LNG storage tanks also comprise a gas dome 15 above the storage tanks, where boil off gas (BOG) from the stored LNG is collected.
  • the LNG storage tanks 10 comprise a gas outlet 17 for passing this natural gas vapour to other elements of the system.
  • the LNG storage tanks 10 also comprise a return spray header 16 .
  • the spray header returns a proportion of the LNG extracted from the LNG storage tank 10 as a spray applied to the surface of the stored LNG in the tank. This helps to maintain uniform temperature within the stored LNG and thereby reduces the rate of generation of boil off gas.
  • the port and starboard manifolds 20 comprise a first LNG interface 21 .
  • a second LNG interface 22 a natural gas vapour interface 23 and a nitrogen interface 24 .
  • LNG may be provided to the LNG storage tanks 10 via the LNG interfaces 21 , 22 while natural gas vapour may be returned to shore via the gas vapour interface 23 .
  • Liquid nitrogen may also be provided to the liquid nitrogen tank 30 via the nitrogen interface 24 .
  • FIG. 2 also illustrates a forcing vaporiser 211 on the line between the LNG storage tanks and connection point 205 to the engines 70 .
  • This is used to vaporise LNG to produce natural gas vapour which can be combusted by the engines 70 to generate power for the bunker vessel's propulsion and electrical systems.
  • the system further comprises a compressor 212 for compressing gas passed through the vaporiser 211 before it reaches the engines 70 .
  • a further compressor 213 may also be provided for natural gas vapour being returned to the port and starboard manifolds 20 .
  • FIG. 3 illustrates the re-condensing unit 60 in more detail.
  • various functionally equivalent connections portions are shown in FIG. 3 using the same reference numerals as used in FIG. 2 .
  • FIG. 3 shows connection points 202 for providing natural gas vapour, particularly BOG, to the re-condensing unit 60 .
  • connection points 201 for receiving the re-liquefied LNG from the re-condensing unit 60 and returning this to the LNG storage tanks 10 are also shown.
  • FIG. 3 also illustrates liquid nitrogen tank 30 and gaseous nitrogen tank 40 .
  • the liquid nitrogen tank 30 is filled from the port and starboard manifolds via connection point 209 (also shown in FIG. 2 ) and may also be filled from bunker vessel's liquid nitrogen generator 50 via connection point 301 .
  • Nitrogen which evaporates from the liquid nitrogen tank 30 may be passed to the gaseous nitrogen tank 40 , from where it may be vented via connection point 302 or passed to consumers via connection point 303 .
  • Consumers in this case may include systems aboard the vessel; for example, nitrogen vapour may be used for purging of cargo/fuel lines, inerting tanks and hold spaces and so on.
  • the re-condensing unit 60 comprises a first heat exchanger 62 , a second heat exchanger 64 and a compressor 66 .
  • the first heat exchanger 62 is an LNG sub-cooler and is coupled to the liquid nitrogen tank 30 and to LNG outlets of the LNG tanks 10 .
  • LNG from the LNG tanks 10 is cooled using liquid nitrogen from the liquid nitrogen tank 30 to below its temperature in the LNG tanks 10 .
  • the LNG cooled in this manner is referred to as “sub-cooled”.
  • the second heat exchanger 64 is coupled to the first heat exchanger 62 so as to receive the sub-cooled LNG therefrom.
  • the second heat exchanger 64 is also arranged to receive natural gas vapour.
  • the natural gas vapour may originate either at the LNG tanks 10 or be received from another vessel via the transfer boom 80 .
  • the natural gas vapour is BOG that has occurred by evaporation of LNG.
  • the second heat exchanger 64 is a condenser arranged to cool the natural gas vapour using the sub-cooled LNG received from the first heat exchanger such that it is liquefied.
  • the second heat exchanger thus generates LNG which is returned to the LNG tanks 10 . Furthermore, once it has passed through the second heat exchanger, the sub-cooled LNG is returned to the LNG tanks 10 .
  • the re-condensing unit also comprises a compressor 66 .
  • the compressor 66 is used to compress natural gas vapour prior to its injection into the second heat exchanger 64 . This is found to increase the efficiency of heat exchange at the second heat exchanger 64 .
  • the bunker vessel comprising the system illustrated in FIG. 1 is docked with another vessel which it is to re-fuel.
  • this other ship is an LNG fuelled vessel.
  • the transfer boom 80 is used to transfer LNG from the LNG tanks 10 to the LNG carrier.
  • natural gas vapour is displaced from the tanks aboard the LNG carrier, and boil-off gas is also generated from the LNG tanks 10 on the bunker vessel and at other points in the system.
  • This natural gas vapour is directed towards the re-condensing unit, where it first encounters 60 the compressor 66 .
  • the compressor 66 acts to increase the pressure within the natural gas vapour by compressing the vapour, and the compressed vapour is then passed to the second heat exchanger 64 .
  • the second heat exchanger 64 transfers heat between sub-cooled LNG and the compressed vapour, thereby cooling the compressed vapour until it condenses (i.e. liquefies), and creating LNG.
  • This LNG is then passed to the LNG storage tanks 10 .
  • the sub-cooled LNG used in the second heat exchanger 64 is also passed to the LNG storage tanks 10 after passing through the second heat exchanger 64 .
  • the sub-cooled LNG is generated by cooling using liquid nitrogen at the first heat exchanger 62 .
  • the preferred embodiment is designed for use upon a bunker vessel used to refuel another ship.
  • a bunker vessel used to refuel another ship.
  • variations may be proposed for alternative types of marine vessels, and indeed to shore-based transport and storage.

Abstract

A method and apparatus for liquefying natural gas vapour is provided. Firstly, liquid natural gas is sub-cooled at a first heat exchanger using a liquid coolant such as liquid nitrogen. The sub-cooled liquid natural gas is then used to condense the natural gas vapour at a second heat exchanger.

Description

    FIELD OF THE INVENTION
  • The present invention relates to liquefaction of natural gas vapour, particularly during the transport and storage of liquefied natural gas (LNG). In particular, but not exclusively, the present invention relates to the handling of boil off gas in a bunker vessel used to refuel LNG-powered vessels.
  • BACKGROUND TO THE INVENTION
  • Liquefied natural gas (LNG) is natural gas (typically methane—CH4) that has been liquefied, typically to make it more manageable during storage and/or transport. At atmospheric pressure, this means the temperature of the LNG is reduced to around −163 degrees centigrade or below.
  • LNG carriers are vessels used to carry LNG across large distances, particularly to carry LNG from gas producing nations to gas consuming nations. The journey times of such vessels are significant, measured in days, weeks and even months. During such time, the LNG is stored at low temperature in order that it does not vaporise.
  • Notwithstanding the efforts made to maintain this low temperature, there is in practice some evaporation of LNG during the vessel's journey. This evaporation creates boil-off gas (BOG) which must be handled by the vessel in some way. Indeed, this has been a factor in the continuing use of steam-turbine propulsion on LNG carriers. Carriers that use such a propulsion system are able to use BOG to drive turbines for propulsion and electricity generation.
  • However, steam turbine propulsion is a relatively inefficient means to drive a large ship. As a result, a move towards slow speed diesel engine powered vessels has been apparent. The diesel engine in such a ship is unable to handle BOG and instead an independent LNG re-liquefaction plant is provided on the vessel. Typically nitrogen vapour is compressed and expanded in a “compander” in such a way as to lower its temperature so that it can be used as a coolant during the re-liquefaction process. The re-liquefaction plant is typically powered by the electricity generated on-board and has significant requirements in this regard, with ratings of 5 MW or above not uncommon. Furthermore, as well as high power requirements, the re-liquefaction plant is typically unable to handle high boil-off rates. Excess BOG that the LNG re-liquefaction plant is unable to handle is burnt in a gas combustion unit (GCU) and thereby wasted.
  • Another type of propulsion system used in LNG carriers is a dual fuel diesel electric propulsion system which can operate off either diesel or LNG itself In such a vessel, the BOG can be used as fuel for the engines to provide propulsion and electrical load. If there is insufficient engine load it is necessary to burn the excess BOG in a GCU.
  • There has been an increasing drive towards the use of LNG as a primary fuel in vessels of all types, driven at least partially by the relative cost of LNG in comparison to other fuels. As mentioned above, while this offers a potential method for handling BOG needed to provide propulsion and/or electricity, there remains the issue of handling such BOG when the required load does not match the BOG present.
  • Simply burning the BOG in a GCU is both wasteful and polluting. Nor can the BOG simply be vented to the atmosphere, for similar reasons. Indeed, environmental regulations in many territories prohibit the handling of BOG in this way within close proximity to shore. Furthermore, using LNG as a primary fuel source creates its own challenges. For example, in many circumstances it may be desirable to re-fuel an LNG fuelled vessel using a bunker vessel. A bunker vessel is a smaller vessel designed to carry fuel to the carrier from shore. The bunker vessel must dock with the carrier and transfer fuel from its tanks to that of the carrier.
  • As well as having to handle BOG during general operation, the bunker vessel must cope with the fact that the process of fuel transfer is likely to involve an increased production of BOG as the LNG is transferred between the vessels. Even if this were not the case the base level production of BOG would still need to be handled. However, as both vessels are stationary during this process, the BOG created cannot be used for propulsion and must be handled in some other manner.
  • A re-liquefaction plant is impractical for a relatively small vessel such as a bunker vessel due to its large energy requirements and, as mentioned above, burning off excess BOG is both wasteful and environmentally unsound. There remains a need to find a method of handling BOG in bunker vessels that is both practical and effective.
  • SUMMARY OF THE INVENTION
  • According to a first aspect of the present invention there is provided a method for condensing natural gas vapour to generate liquefied natural gas (LNG), comprising:
  • providing a liquid coolant, wherein the liquid coolant has a boiling point less than that of natural gas;
  • cooling LNG at a first heat exchanger using the liquid coolant to generate sub-cooled LNG; and
  • condensing natural gas vapour at a second heat exchanger using the sub-cooled LNG to liquefy the natural gas vapour and thereby generate further LNG.
  • According to a second aspect of the present invention, there is provided a system for condensing natural gas vapour to generate liquefied natural gas (LNG); comprising
  • a first heat exchanger arranged to cool LNG using a liquid coolant to generate sub-cooled LNG, wherein the liquid coolant has a boiling point less than that of natural gas; and
  • a second heat exchanger arranged to condense natural gas vapour using the sub-cooled LNG to liquefy the natural gas vapour and thereby generate further LNG.
  • The present invention can provide an efficient method of condensing natural gas vapour to provide LNG. Existing LNG is cooled at a first heat exchanger to create sub-cooled LNG that can be used to condense the natural gas vapour. This is significantly more energy efficient than provision of a plant for generating LNG directly from the natural gas vapour. The use of a liquid coolant to first sub-cool existing available LNG reduces the need for energy intensive refrigeration cycles to generate a coolant to directly cool the natural gas vapour.
  • The present invention finds particular utility in circumstances in which boil-off gas is present. Boil-off gas is natural gas vapour that has arisen through the evaporation of an LNG source. In such circumstances, the boil-off gas is likely not to be significantly warmer than the boiling temperature of natural gas, and furthermore LNG is likely to be available for sub-cooling. Thus, in a preferred embodiment, the natural gas vapour is boil-off gas.
  • The method may comprise receiving the LNG for cooling at the first heat exchanger from at least one LNG storage tank and returning the sub-cooled LNG to the at least one storage tank after it is used at the second heat exchanger. In this manner, LNG may be re-used for subsequent condensing of natural gas vapour. After use at the second heat exchanger the sub-cooled LNG is likely to have warmed somewhat, but the method is preferably arranged such that it remains in liquid form for returning to the LNG storage tank.
  • Preferably, the method may further comprise delivering the further LNG to the at least one storage tank. Accordingly, the LNG that is created through the method may subsequently be used for condensing further natural gas vapour in future cycles. Furthermore, the system is compact and efficient in that there is no requirement for separate tanks for the coolant used at the second heat exchanger and the generated LNG.
  • As mentioned above, the liquid coolant used at the first generator has a boiling point less than that of the natural gas vapour. The natural gas vapour is preferably predominantly methane, more preferably at least 90 Mole % methane, at least 95 Mole % methane or over 97% Mole methane. Methane has a boiling point at atmospheric pressure of around −163 degrees centigrade. Preferably, the liquid coolant has a boiling point at atmospheric pressure of less than that of methane (i.e. less than −163 degrees centigrade), more preferably less than −170 degrees centigrade, and most preferably less than −190 degrees centigrade. In preferred embodiments, the liquid coolant is liquid nitrogen. The boiling point of nitrogen is around −193 degrees centigrade at atmospheric pressure. References to atmospheric pressure refer to a pressure equal to the understood unit of one atmosphere, rather than to prevailing climatic conditions.
  • The system may comprise a storage facility for the liquid coolant. For example, the system may comprise at least one storage tank for storing the liquid coolant. The system may additionally or alternatively comprise a generator for generating the liquid coolant. Equally, the method may comprise a step of generating the liquid coolant. For example, where the system is provided on a maritime vessel, an initial supply of liquid coolant may be provided to the storage facility from an on-shore facility while the vessel is docked, but when the vessel is at sea additional liquid coolant may be provided as needed by the generator.
  • According to a further aspect, a vessel may be provided comprising the system of the second aspect. The vessel may comprise a flow boom arranged to transfer LNG to a second vessel and to receive natural gas vapour from the second vessel. The method may further comprise transferring LNG from a first vessel to a second vessel, and receiving the natural gas vapour from the second vessel. In preferred embodiments, one or both vessels are maritime vessels. In particular, the vessel comprising the system (i.e. the first vessel) may be a bunker vessel while the second vessel may be an LNG fuelled vessel. Alternatively or additionally, the second vessel may be a carrier, particularly an LNG carrier. A bunker vessel is a vessel arranged to re-fuel other vessels while at sea. Preferably, one or both vessels are LNG powered vessels.
  • BRIEF DESCRIPTION OF THE FIGURES
  • A preferred embodiment of the present invention will now be described with reference to the accompanying drawings, in which:
  • FIG. 1 is a schematic diagram showing a bunker vessel comprising a system or handling LNG;
  • FIG. 2 is a schematic diagram showing the connection between various elements of the system in more detail; and
  • FIG. 3 is a schematic diagram illustrating the components of a re-condenser unit.
  • DETAILED DESCRIPTION
  • Referring to FIG. 1, a schematic diagram is provided showing the principle elements of a LNG handling system aboard a bunker vessel 1 for re-fuelling larger ships. The system comprises two LNG storage tanks 10, port and starboard manifolds 20, a liquid nitrogen tank 30, a gaseous nitrogen tank 40, a liquid nitrogen generator 50, a re-condenser unit 60, engines 70 and a flow boom 80. FIG. 1 illustrates functional connections between the various illustrated elements of the system for the transfer of LNG (indicated as “L”, dotted lines), natural gas vapour (indicated as “V”, thick lines) and nitrogen (both liquid and gaseous indicated as “N”, thin lines).
  • The port and starboard manifolds 20 are arranged to allow transfer of LNG, natural gas vapour, and nitrogen between the bunker vessel and an on-shore facility. LNG received from the port and starboard manifolds is stored in the storage tanks 10. In this embodiment, the storage tanks are pressurised, C-class, storage tanks which may operate at up to 10 bar, but the skilled person will recognize that alternative tanks may be used. Indeed, the storage tanks may be any type of chamber or container suitable to act as a reservoir for LNG. Pressurised tanks, particularly pressurised “C” Type tanks, allow a wider range of operating temperature and pressure within the bunker vessel. The storage tanks store LNG at around −163 degrees centigrade.
  • Liquid nitrogen received from the manifolds 20 is stored in liquid nitrogen tank 30. Nitrogen that evaporates from liquid nitrogen tank 30 may be received in gas nitrogen tank 40 from where it is passed to the ship's systems for use in for purging of cargo/fuel lines, inerting tanks and hold spaces and so on. Alternatively or additionally, nitrogen may be vented to the atmosphere or re-used by liquid nitrogen generator 50. The liquid nitrogen tank 30 and the gas nitrogen tank 40 may be any suitable container or chamber suitable to act as a reservoir for liquid nitrogen and gaseous nitrogen respectively.
  • The liquid nitrogen generator 50 passes generated liquid nitrogen back to the liquid nitrogen tank 30. The liquid nitrogen generator 50 may be a compression cooling system, and is preferably powered by the vessel's electrical systems. For example, the liquid nitrogen generator 50 may be arranged to filter and compress atmospheric air before carbon dioxide water and residual hydrocarbons are removed in an air purification unit. The air is then passed to a cold box where it is cooled and liquefied. The liquid air is distilled then in a distillation column to yield pure nitrogen gas which is condensed in a condenser to yield pure liquid nitrogen.
  • The system comprises a flow boom 80 for transferring LNG to another vessel, such as an LNG carrier. The flow boom 80 is a transfer boom in this embodiment. The transfer boom 80 receives LNG from LNG storage tank 10 and may also receive natural gas vapour from the other vessel. Natural gas vapour received by the transfer boom is passed to the re-condenser unit 60.
  • The re-condenser unit 60 also receives natural gas vapour from the LNG storage tank 10. The re-condenser unit 60 is arranged to re-liquefy the natural gas vapour to return it to an LNG state. Once re-liquefied the LNG may be passed back to the LNG storage tank 10.
  • The re-condenser unit 60 also receives liquid nitrogen from the liquid nitrogen tank 30 and LNG from the LNG tanks 10. These liquids are used during the processes of cooling the natural gas vapour at the re-condenser unit, as will be explained in greater detail below with reference to FIG. 3.
  • In the embodiment shown in FIG. 1, the engines 70 of the bunker vessel use the stored LNG as a fuel source. In practice, natural gas vapour is used for combustion in the engines. The natural gas vapour used for this purpose may be boil-off gas (BOG) spontaneously occurring in the LNG storage tanks 10, or may be deliberately vaporised LNG from the LNG storage tanks. LNG from the storage tank may be vaporised by a forcing vaporizer, for example.
  • FIG. 2 shows in more detail the connections between various elements of the system of FIG. 1. In particular, FIG. 2 illustrates the LNG storage tanks 10 and the port and starboard manifolds 20. As shown, a variety of valves are provided to control the flows and pressures of gas and liquid in the system. FIG. 2 also illustrates various connection points to other elements of the system. In particular, connection points 201 are provided for LNG returning from the re-condenser unit 60, while connection points 202 are provided for natural gas vapour passed to the re-condensing unit 60. There is also provided connection point 210 for passing LNG to the re-condensing unit 60 for use during a re-liquefaction process implemented by the re-condensing unit 60 and a connection point 214 for receiving LNG from the re-condensing unit that has been used for this purpose. LNG that is extracted from the LNG storage tanks 10 but is not ultimately used in the engine 70 or the re-condensing unit 60 may be returned to the LNG storage tanks via connection points 215.
  • Connection point 203 is shown for passing LNG to the transfer boom 80, while connection point 204 receives natural gas vapour from the transfer boom 80. In this manner, LG can be transferred to another vessel, while excess boil-off as from the vessel can be retrieved for handling on the bunker vessel.
  • Connection point 205 is provided for passing gas vapour to the engines 70. There is also provided a connection point 206 for transferring natural gas vapour to a gas combustion unit (GCU). In an emergency situation, this GCU may be used to burn and thus dispose of natural gas vapour that is not otherwise handled by the system. There is also provided a vent 208 to vent natural gas vapour to the atmosphere where this is appropriate.
  • Connection point 207 is provided for the receipt of nitrogen vapour for purging of lines, and inerting spaces as required. Excess vapour would be vented via the GCU. The vapour may be received from the gas nitrogen tank 40 which receives boil-off from the liquid nitrogen tank 30. Connection point 210 is for supply of liquid nitrogen via the manifolds 20 from shore for charging the liquid nitrogen storage tank 30.
  • Each LNG storage tank is provided with a discharge pump 11 for pumping LNG to the transfer boom 80 and a LNG fuel pump 12 for pumping LNG to the engines 70. Various connections allow the LNG pumped by either the discharge pump 11 or the LNG fuel pump 12 to be re-directed as appropriate.
  • Each LNG storage tank 10 also comprises a first LNG inlet 13 and a second LNG inlet 14. LNG can be received at the LNG storage tanks 10 from the re-condenser unit 60 via connection points 201 and from the port and starboard manifolds 20. The LNG storage tanks also comprise a gas dome 15 above the storage tanks, where boil off gas (BOG) from the stored LNG is collected. The LNG storage tanks 10 comprise a gas outlet 17 for passing this natural gas vapour to other elements of the system.
  • The LNG storage tanks 10 also comprise a return spray header 16. The spray header returns a proportion of the LNG extracted from the LNG storage tank 10 as a spray applied to the surface of the stored LNG in the tank. This helps to maintain uniform temperature within the stored LNG and thereby reduces the rate of generation of boil off gas.
  • The port and starboard manifolds 20 comprise a first LNG interface 21. A second LNG interface 22, a natural gas vapour interface 23 and a nitrogen interface 24. When the bunker vessel is docked, LNG may be provided to the LNG storage tanks 10 via the LNG interfaces 21, 22 while natural gas vapour may be returned to shore via the gas vapour interface 23. Liquid nitrogen may also be provided to the liquid nitrogen tank 30 via the nitrogen interface 24.
  • FIG. 2 also illustrates a forcing vaporiser 211 on the line between the LNG storage tanks and connection point 205 to the engines 70. This is used to vaporise LNG to produce natural gas vapour which can be combusted by the engines 70 to generate power for the bunker vessel's propulsion and electrical systems. The system further comprises a compressor 212 for compressing gas passed through the vaporiser 211 before it reaches the engines 70. A further compressor 213 may also be provided for natural gas vapour being returned to the port and starboard manifolds 20.
  • FIG. 3 illustrates the re-condensing unit 60 in more detail. In order to facilitate comparison with FIG. 2, various functionally equivalent connections portions are shown in FIG. 3 using the same reference numerals as used in FIG. 2. For example, FIG. 3 shows connection points 202 for providing natural gas vapour, particularly BOG, to the re-condensing unit 60. Moreover, connection points 201 for receiving the re-liquefied LNG from the re-condensing unit 60 and returning this to the LNG storage tanks 10 are also shown.
  • FIG. 3 also illustrates liquid nitrogen tank 30 and gaseous nitrogen tank 40. The liquid nitrogen tank 30 is filled from the port and starboard manifolds via connection point 209 (also shown in FIG. 2) and may also be filled from bunker vessel's liquid nitrogen generator 50 via connection point 301. Nitrogen which evaporates from the liquid nitrogen tank 30 may be passed to the gaseous nitrogen tank 40, from where it may be vented via connection point 302 or passed to consumers via connection point 303. Consumers in this case may include systems aboard the vessel; for example, nitrogen vapour may be used for purging of cargo/fuel lines, inerting tanks and hold spaces and so on.
  • The re-condensing unit 60 comprises a first heat exchanger 62, a second heat exchanger 64 and a compressor 66. The first heat exchanger 62 is an LNG sub-cooler and is coupled to the liquid nitrogen tank 30 and to LNG outlets of the LNG tanks 10. LNG from the LNG tanks 10 is cooled using liquid nitrogen from the liquid nitrogen tank 30 to below its temperature in the LNG tanks 10. The LNG cooled in this manner is referred to as “sub-cooled”.
  • The second heat exchanger 64 is coupled to the first heat exchanger 62 so as to receive the sub-cooled LNG therefrom. The second heat exchanger 64 is also arranged to receive natural gas vapour. The natural gas vapour may originate either at the LNG tanks 10 or be received from another vessel via the transfer boom 80. Typically, the natural gas vapour is BOG that has occurred by evaporation of LNG.
  • The second heat exchanger 64 is a condenser arranged to cool the natural gas vapour using the sub-cooled LNG received from the first heat exchanger such that it is liquefied. The second heat exchanger thus generates LNG which is returned to the LNG tanks 10. Furthermore, once it has passed through the second heat exchanger, the sub-cooled LNG is returned to the LNG tanks 10.
  • The re-condensing unit also comprises a compressor 66. The compressor 66 is used to compress natural gas vapour prior to its injection into the second heat exchanger 64. This is found to increase the efficiency of heat exchange at the second heat exchanger 64.
  • In use, the bunker vessel comprising the system illustrated in FIG. 1 is docked with another vessel which it is to re-fuel. In particular examples, this other ship is an LNG fuelled vessel.
  • The transfer boom 80 is used to transfer LNG from the LNG tanks 10 to the LNG carrier. During this process, natural gas vapour is displaced from the tanks aboard the LNG carrier, and boil-off gas is also generated from the LNG tanks 10 on the bunker vessel and at other points in the system. This natural gas vapour is directed towards the re-condensing unit, where it first encounters 60 the compressor 66. The compressor 66 acts to increase the pressure within the natural gas vapour by compressing the vapour, and the compressed vapour is then passed to the second heat exchanger 64. The second heat exchanger 64 transfers heat between sub-cooled LNG and the compressed vapour, thereby cooling the compressed vapour until it condenses (i.e. liquefies), and creating LNG. This LNG is then passed to the LNG storage tanks 10.
  • As mentioned above, the sub-cooled LNG used in the second heat exchanger 64 is also passed to the LNG storage tanks 10 after passing through the second heat exchanger 64. Prior to this, the sub-cooled LNG is generated by cooling using liquid nitrogen at the first heat exchanger 62.
  • As described above, the preferred embodiment is designed for use upon a bunker vessel used to refuel another ship. However, it will be understood that variations may be proposed for alternative types of marine vessels, and indeed to shore-based transport and storage.
  • Other variations and modifications will be apparent to the skilled person. Such variations and modifications may involve equivalent and other features which are already known and which may be used instead of, or in addition to, features described herein. Features that are described in the context of separate embodiments may be provided in combination in a single embodiment. Conversely, features which are described in the context of a single embodiment may also be provided separately or in any suitable sub-combination. It should be noted that the term “comprising” does not exclude other elements or steps, the term “a” or “an” does not exclude a plurality, a single feature may fulfill the functions of several features recited in the claims and reference signs in the claims shall not be construed as limiting the scope of the claims. It should also be noted that the Figures are not necessarily to scale; emphasis instead generally being placed upon illustrating the principles of the present disclosure.

Claims (15)

1. A method for condensing natural gas vapour to generate liquefied natural gas (LNG), comprising:
providing a liquid coolant, wherein the liquid coolant has a boiling point less than that of natural gas;
cooling LNG at a first heat exchanger using the liquid coolant to generate sub-cooled LNG; and
condensing natural gas vapour at a second heat exchanger using the sub-cooled LNG to liquefy the natural gas vapour and thereby generate further LNG.
2. A method according to claim 1, further comprising:
obtaining the LNG for cooling at the first heat exchanger from at least one LNG storage tank; and
returning the sub-cooled LNG to the at least one LNG storage tank after it is used at the second heat exchanger.
3. A method according to claim 2, further comprising delivering the further LNG to the at least one LNG storage tank.
4. A method according to claim 1, wherein the natural gas vapour is boil-off gas.
5. A method according to claim 1, wherein the liquid coolant is liquid nitrogen.
6. A method according to claim 1, further comprising compressing the natural gas vapour.
7. A method according to claim 1, further comprising:
delivering LNG from a first vessel to a second vessel; and
receiving the natural gas vapour from the second vessel.
8. A system for condensing natural gas vapour to generate liquefied natural gas (LNG); comprising:
a first heat exchanger arranged to cool LNG using a liquid coolant to generate sub-cooled LNG, wherein the liquid coolant has a boiling point less than that of natural gas; and
a second heat exchanger arranged to condense natural gas vapour using the sub-cooled LNG to liquefy the natural gas vapour and thereby generate further LNG.
9. A system according to claim 8, further comprising at least one LNG storage tank, wherein the first heat exchanger is arranged to receive the LNG for cooling at the first heat exchanger from the at least one LNG storage tank, and wherein the system is arranged to return the sub-cooled LNG to the LNG storage tank after it is used at the second heat exchanger.
10. A system according to claim 9, wherein the system is arranged to deliver the further LNG to the at least one LNG storage tank.
11. A system according to claim 8, wherein the natural gas vapour is boil-off gas.
12. A system according to claim 8, wherein the liquid coolant is liquid nitrogen.
13. A system according to claim 8, further comprising a compressor for compressing the natural gas vapour.
14. A vessel having a system for condensing natural gas vapour to generate liquefied natural gas, the vessel comprising:
a first heat exchange exchanger arranged to cool LNG using a liquid coolant to generate sub-cooled LNG, wherein the liquid coolant has a boiling point less than that of natural gas;
a second heat exchanger arranged to condense natural gas vapour using the sub-cooled LNG to liquefy the natural gas vapour and thereby generate further LNG; and
a transfer boom arranged to transfer LNG to a second vessel and to receive natural gas vapour from the second vessel.
15. A vessel according to claim 14, wherein the vessel is a bunker vessel.
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US20150219280A1 (en) * 2014-02-05 2015-08-06 Air Liquide Industrial U.S. Lp Method and apparatus for reducing boil-off gas losses from a liquid storage tank
WO2017114815A1 (en) * 2015-12-31 2017-07-06 Shell Internationale Research Maatschappij B.V. Liquefied fuel gas system and method
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JP2019035502A (en) * 2017-08-18 2019-03-07 アリアーネグループ ゲーエムベーハー Cooling of boil off gas of liquefied gas for supplying power to machines, plant, or vehicle
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FR3106874A1 (en) * 2020-02-05 2021-08-06 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Liquefied gas delivery process
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US11402152B2 (en) * 2017-07-07 2022-08-02 Tor Christensen Large scale coastal liquefaction
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US20150219280A1 (en) * 2014-02-05 2015-08-06 Air Liquide Industrial U.S. Lp Method and apparatus for reducing boil-off gas losses from a liquid storage tank
WO2017114815A1 (en) * 2015-12-31 2017-07-06 Shell Internationale Research Maatschappij B.V. Liquefied fuel gas system and method
CN108474520A (en) * 2015-12-31 2018-08-31 国际壳牌研究有限公司 liquefied fuel gas system and method
JP2018080738A (en) * 2016-11-15 2018-05-24 レール・リキード−ソシエテ・アノニム・プール・レテュード・エ・レクスプロワタシオン・デ・プロセデ・ジョルジュ・クロード Boil off gas recondenser and lng supply system equipped with the same
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US11698169B2 (en) 2016-12-23 2023-07-11 Shell Usa, Inc. Vessel for the transport of liquefied gas and method of operating the vessel
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US11402152B2 (en) * 2017-07-07 2022-08-02 Tor Christensen Large scale coastal liquefaction
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JP2019035502A (en) * 2017-08-18 2019-03-07 アリアーネグループ ゲーエムベーハー Cooling of boil off gas of liquefied gas for supplying power to machines, plant, or vehicle
CN111758003A (en) * 2018-01-23 2020-10-09 气体运输技术公司 Cryogenic heat pump and its use in liquefied gas treatment
CN113767246A (en) * 2019-03-15 2021-12-07 气体运输技术公司 System for controlling pressure in a liquefied natural gas vessel
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