EP4035985A1 - Cold recovery system, ship including cold recovery system, and cold recovery method - Google Patents
Cold recovery system, ship including cold recovery system, and cold recovery method Download PDFInfo
- Publication number
- EP4035985A1 EP4035985A1 EP20893934.8A EP20893934A EP4035985A1 EP 4035985 A1 EP4035985 A1 EP 4035985A1 EP 20893934 A EP20893934 A EP 20893934A EP 4035985 A1 EP4035985 A1 EP 4035985A1
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- EP
- European Patent Office
- Prior art keywords
- heat exchanger
- working fluid
- liquefied gas
- heat medium
- heat
- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63J—AUXILIARIES ON VESSELS
- B63J2/00—Arrangements of ventilation, heating, cooling, or air-conditioning
- B63J2/12—Heating; Cooling
- B63J2/14—Heating; Cooling of liquid-freight-carrying tanks
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B25/00—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby
- B63B25/02—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods
- B63B25/08—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid
- B63B25/12—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed
- B63B25/16—Load-accommodating arrangements, e.g. stowing, trimming; Vessels characterised thereby for bulk goods fluid closed heat-insulated
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63J—AUXILIARIES ON VESSELS
- B63J2/00—Arrangements of ventilation, heating, cooling, or air-conditioning
- B63J2/12—Heating; Cooling
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63J—AUXILIARIES ON VESSELS
- B63J3/00—Driving of auxiliaries
- B63J3/04—Driving of auxiliaries from power plant other than propulsion power plant
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/10—Arrangements for preventing freezing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C9/00—Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure
- F17C9/02—Methods or apparatus for discharging liquefied or solidified gases from vessels not under pressure with change of state, e.g. vaporisation
- F17C9/04—Recovery of thermal energy
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0031—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other
- F28D9/0037—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the conduits for the other heat-exchange medium also being formed by paired plates touching each other
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/08—Elements constructed for building-up into stacks, e.g. capable of being taken apart for cleaning
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/032—Hydrocarbons
- F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/04—Handled 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
- F17C2223/042—Localisation of the removal point
- F17C2223/046—Localisation of the removal point in the liquid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/01—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the phase
- F17C2225/0107—Single phase
- F17C2225/0123—Single phase gaseous, e.g. CNG, GNC
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
- F17C2225/03—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the pressure level
- F17C2225/035—High pressure, i.e. between 10 and 80 bars
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/01—Propulsion of the fluid
- F17C2227/0128—Propulsion of the fluid with pumps or compressors
- F17C2227/0135—Pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0309—Heat exchange with the fluid by heating using another fluid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0309—Heat exchange with the fluid by heating using another fluid
- F17C2227/0316—Water heating
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0309—Heat exchange with the fluid by heating using another fluid
- F17C2227/0316—Water heating
- F17C2227/0318—Water heating using seawater
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0309—Heat exchange with the fluid by heating using another fluid
- F17C2227/0323—Heat exchange with the fluid by heating using another fluid in a closed loop
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0302—Heat exchange with the fluid by heating
- F17C2227/0327—Heat exchange with the fluid by heating with recovery of heat
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0367—Localisation of heat exchange
- F17C2227/0388—Localisation of heat exchange separate
- F17C2227/0393—Localisation of heat exchange separate using a vaporiser
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/03—Dealing with losses
- F17C2260/031—Dealing with losses due to heat transfer
- F17C2260/032—Avoiding freezing or defrosting
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/04—Reducing risks and environmental impact
- F17C2260/046—Enhancing energy recovery
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2265/00—Effects achieved by gas storage or gas handling
- F17C2265/06—Fluid distribution
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2265/00—Effects achieved by gas storage or gas handling
- F17C2265/07—Generating electrical power as side effect
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS 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
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0102—Applications for fluid transport or storage on or in the water
- F17C2270/0105—Ships
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0033—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for cryogenic applications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2260/00—Heat exchangers or heat exchange elements having special size, e.g. microstructures
- F28F2260/02—Heat exchangers or heat exchange elements having special size, e.g. microstructures having microchannels
Definitions
- a temperature of another heat exchange object is lower than a solidifying point of one heat exchange object (for example, seawater)
- the one heat exchange object is solidified in heat exchange in the heat exchanger, and the solidified heat exchange object may adhere to a surface of the exchanger and block the heat exchanger.
- a small heat exchanger has a higher risk of blockage of the heat exchanger than a large heat exchanger (for example, a shell tube type heat exchanger), and thus has a problem in reliability.
- the cold energy recovery system 2 includes an intermediate heat medium circulation pump 61 disposed on the intermediate heat medium circulation line 6, and a heating water pump 71 disposed on the heating water supply line 7.
- the heating water supply line 7 has one end side 701 which is connected to a heating water supply source 13 disposed outside the cold energy recovery system 2, and another end side 702 which is connected to a heating water discharge destination 14 disposed outside the cold energy recovery system 2.
- the heating water pump 71 the heating water is sent from the heating water supply source 13 to the heating water supply line 7, flows through the heating water supply line 7 from upstream to downstream, and then is sent to the heating water discharge destination 14.
- the above-described cold energy recovery device 41 includes the above-described turbine 42, and the above-described generator 43 configured to generate electricity by driving the turbine 42.
- the cold energy recovery device 41 since the cold energy recovery device 41 includes the turbine 42 and the generator 43, it is possible to generate electricity in the generator 43 by driving the turbine 42 with the working fluid which circulates through the working fluid circulation line 4 and recovers the cold energy from the liquefied gas. In this case, it is possible to effectively utilize the cold energy of the liquefied gas.
- the present disclosure is not limited to the above-described embodiments, and also includes an embodiment obtained by modifying the above-described embodiments and an embodiment obtained by combining these embodiments as appropriate.
- the first heat exchanger (51) compared to a case where the temperature of the liquefied gas is raised only by the first heat exchanger (51), it is possible to reduce the amount of the heat exchange in the first heat exchanger (51), and it is possible to reduce the temperature drop of the working fluid in the first heat exchanger (51). Thus, it is possible to effectively suppress solidification of the intermediate heat medium during the heat exchange between the working fluid and the intermediate heat medium in the second heat exchanger (52). Further, by reducing the amount of the heat exchange in the first heat exchanger (51), it is possible to reduce the size of the first heat exchanger (51).
- the first heat exchange step (S101) includes performing heat exchange between the liquefied gas and the working fluid by the first heat exchanger (51).
- the working fluid that has passed through the first heat exchanger (51) has a low temperature which is not greater than the solidifying point of water.
- the second heat exchange step (S102) includes performing, by the second heat exchanger (52), heat exchange between the working fluid, which is decreased in temperature by the heat exchange in the first heat exchange step (S101), and the intermediate heat medium flowing through the intermediate heat medium circulation line (6). Since the intermediate heat medium has a lower solidifying point than water, the intermediate heat medium is hardly solidified during heat exchange with the low-temperature working fluid in the second heat exchange step. Thus, it is possible to suppress that the solidified intermediate heat medium freezes to the second heat exchanger (52) and blocks the second heat exchanger (52).
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Description
- The present disclosure relates to a cold energy recovery system installed in a ship which includes a liquefied gas storage device configured to store a liquid liquefied gas, a ship having the cold energy recovery system, and a cold energy recovery method by the cold energy recovery system.
- A land LNG (liquefied natural gas) terminal receives and stores liquefied natural gas transported by an LNG carrier. Then, when liquefied natural gas is supplied to a supply destination such as city gas or a thermal power plant, liquefied natural gas is warmed with seawater or the like to be returned to a gas. When liquefied natural gas is vaporized, cryogenic power generation may be performed in which cold energy is recovered as electric power instead of being discarded in seawater (for example, Patent Document 1).
- Providing the land LNG terminal corresponding to each supply destination of liquefied natural gas is difficult due to its cost to, for example, secure land. Thus, a ship, which is equipped with an LNG storage facility for storing liquefied natural gas or a regasification facility for regasifying liquefied natural gas, may be moored on sea, and the liquefied natural gas regasifyied by the ship may be sent to a supply destination on shore or a power gauge (floating power plant) on sea via a pipeline.
- Since the ship is less expandable than an onshore facility, in order to install a cryogenic power generation facility, it is important to reduce the size of the cryogenic power generation system, especially a heat exchanger. As the small heat exchanger, a printed circuit heat exchanger (PCHE), a plate heat exchanger, or the like can be given as an example.
- Patent Document 1:
JP2017-180323A - If a temperature of another heat exchange object is lower than a solidifying point of one heat exchange object (for example, seawater), the one heat exchange object is solidified in heat exchange in the heat exchanger, and the solidified heat exchange object may adhere to a surface of the exchanger and block the heat exchanger. A small heat exchanger has a higher risk of blockage of the heat exchanger than a large heat exchanger (for example, a shell tube type heat exchanger), and thus has a problem in reliability.
- In view of the above issues, an object of at least one embodiment of the present disclosure is to provide a cold energy recovery system capable of suppressing blockage of the heat exchanger due to solidification of a heat medium, and capable of improving reliability of the cold energy recovery system when the small heat exchanger is used.
- A cold energy recovery system according to the present disclosure is a cold energy recovery system installed in a ship which includes a liquefied gas storage device configured to store a liquid liquefied gas, that includes a working fluid circulation line which is configured to circulate a working fluid having a lower solidifying point than water, a cold energy recovery device that includes a turbine which is configured to be driven by the working fluid flowing through the working fluid circulation line, a first heat exchanger which is configured to exchange heat between the liquefied gas and the working fluid flowing through the working fluid circulation line, an intermediate heat medium circulation line which is configured to circulate an intermediate heat medium having a lower solidifying point than water, a second heat exchanger disposed downstream of the first heat exchanger on the working fluid circulation line, the second heat exchanger being configured to exchange heat between the working fluid flowing through the working fluid circulation line and the intermediate heat medium flowing through the intermediate heat medium circulation line, and a third heat exchanger which is configured to exchange heat between the intermediate heat medium flowing through the intermediate heat medium circulation line and heating water introduced from an outside of the cold energy recovery system.
- A ship according to the present disclosure includes the cold energy recovery system.
- A cold energy recovery method according to the present disclosure is a cold energy recovery method by a cold energy recovery system installed in a ship which includes a liquefied gas storage device configured to store a liquid liquefied gas, the cold energy recovery system including a working fluid circulation line which is configured to circulate a working fluid having a lower solidifying point than water, a cold energy recovery device that includes a turbine which is configured to be driven by the working fluid flowing through the working fluid circulation line, a first heat exchanger which is configured to exchange heat between the liquefied gas and the working fluid flowing through the working fluid circulation line, an intermediate heat medium circulation line which is configured to circulate an intermediate heat medium having a lower solidifying point than water, a second heat exchanger disposed downstream of the first heat exchanger on the working fluid circulation line, the second heat exchanger being configured to exchange heat between the working fluid flowing through the working fluid circulation line and the intermediate heat medium flowing through the intermediate heat medium circulation line, and a third heat exchanger which is configured to exchange heat between the intermediate heat medium flowing through the intermediate heat medium circulation line and heating water introduced from an outside of the cold energy recovery system, the cold energy recovery method including a first heat exchange step of performing heat exchange between the liquefied gas and the working fluid by the first heat exchanger, a second heat exchange step of performing, by the second heat exchanger, heat exchange between the intermediate heat medium and the working fluid that has exchanged heat with the liquefied gas in the first heat exchange step, and a third heat exchange step of performing, by the third heat exchanger, heat exchange between the heating water and the intermediate heat medium that has exchanged heat with the working fluid in the second heat exchange step.
- According to at least one embodiment of the present disclosure, a cold energy recovery system is provided which is capable of suppressing blockage of a heat exchanger due to solidification of a heat medium, and is capable of improving reliability of a cold energy recovery system when a small heat exchanger is used.
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FIG. 1 is a schematic configuration diagram schematically showing the configuration of a ship having a cold energy recovery system according to an embodiment of the present disclosure. -
FIG. 2 is a schematic configuration diagram schematically showing the overall configuration of the cold energy recovery system according to the first embodiment of the present disclosure. -
FIG. 3 is a schematic configuration diagram schematically showing the overall configuration of the cold energy recovery system according to the second embodiment of the present disclosure. -
FIG. 4 is a schematic configuration diagram schematically showing the overall configuration of the cold energy recovery system according to the third embodiment of the present disclosure. -
FIG. 5 is a schematic configuration diagram schematically showing the overall configuration of the cold energy recovery system according a comparative example. -
FIG. 6 is an explanatory view for describing an example of a heat exchanger in an embodiment of the present disclosure. -
FIG. 7 is a flowchart of a cold energy recovery method according to an embodiment of the present disclosure. - Embodiments of the present disclosure will be described below with reference to the accompanying drawings. It is intended, however, that unless particularly identified, dimensions, materials, shapes, relative positions and the like of components described or shown in the drawings as the embodiments shall be interpreted as illustrative only and not intended to limit the scope of the present disclosure.
- For instance, an expression of relative or absolute arrangement such as "in a direction", "along a direction", "parallel", "orthogonal", "centered", "concentric" and "coaxial" shall not be construed as indicating only the arrangement in a strict literal sense, but also includes a state where the arrangement is relatively displaced by a tolerance, or by an angle or a distance whereby it is possible to achieve the same function.
- For instance, an expression of an equal state such as "same", "equal", and "uniform" shall not be construed as indicating only the state in which the feature is strictly equal, but also includes a state in which there is a tolerance or a difference that can still achieve the same function.
- Further, for instance, an expression of a shape such as a rectangular shape or a tubular shape shall not be construed as only the geometrically strict shape, but also includes a shape with unevenness or chamfered corners within the range in which the same effect can be achieved.
- On the other hand, the expressions "comprising", "including" or "having" one constitutional element is not an exclusive expression that excludes the presence of other constitutional elements.
- The same configurations are indicated by the same reference characters and may not be described again in detail.
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FIG. 1 is a schematic configuration diagram schematically showing the configuration of a ship having a cold energy recovery system according to an embodiment of the present disclosure. - As shown in
FIG. 1 , a coldenergy recovery system 2 according to some embodiments is installed in aship 1. As shown inFIG. 1 , theship 1 includes ahull 10, and the coldenergy recovery system 2 mounted on thehull 10. In the illustrated embodiment, theship 1 further includes a liquefied gas storage device (for example, a liquefied gas tank) 11 mounted on thehull 10. The liquefiedgas storage device 11 is configured to store a liquid liquefied gas (for example, liquefied natural gas). - In the illustrated embodiment, the
hull 10 internally forms anengine room 15. Theengine room 15 is equipped with an engine (for example, a marine diesel engine) 16 for applying a propulsive force to theship 1. In this case, by driving theengine 16, theship 1 can be moved from a liquefied gas supply source to the vicinity of a liquefied gas supply destination. -
FIG. 2 is a schematic configuration diagram schematically showing the overall configuration of the cold energy recovery system according to the first embodiment of the present disclosure.FIG. 3 is a schematic configuration diagram schematically showing the overall configuration of the cold energy recovery system according to the second embodiment of the present disclosure.FIG. 4 is a schematic configuration diagram schematically showing the overall configuration of the cold energy recovery system according to the third embodiment of the present disclosure. - As shown in
FIGs. 2 to 4 , the coldenergy recovery system 2 according to some embodiments includes a liquefiedgas supply line 3, a workingfluid circulation line 4, a coldenergy recovery device 41, an intermediate heatmedium circulation line 6, a heatingwater supply line 7, afirst heat exchanger 51, asecond heat exchanger 52, and athird heat exchanger 53. Each of the liquefiedgas supply line 3, the workingfluid circulation line 4, the intermediate heatmedium circulation line 6, and the heatingwater supply line 7 includes a flow passage through which a fluid flows. - The liquefied
gas supply line 3 is configured to send a liquefied gas from the liquefiedgas storage device 11. The workingfluid circulation line 4 is configured to circulate a working fluid having a lower solidifying point than water. Hereinafter, liquefied natural gas (LNG) will be described as a specific example of the liquefied gas, and propane will be described as a specific example of the working fluid. However, the present disclosure is also applicable to a liquefied gas other than liquefied natural gas, and further is also applicable to a case where a heat medium other than propane is used as the working fluid. - In the illustrated embodiment, the cold
energy recovery system 2 includes aliquefied gas pump 31 disposed on the liquefiedgas supply line 3, and a workingfluid circulation pump 44 disposed on the workingfluid circulation line 4. The liquefiedgas supply line 3 has oneend side 301 connected to the liquefiedgas storage device 11, and has anotherend side 302 which is connected to liquefiedgas equipment 12 disposed outside the coldenergy recovery system 2. As the liquefiedgas equipment 12, a gas holder (seeFIG. 1 ) disposed on shore, a gas pipe connected to the gas holder, or the like can be given as an example. By driving theliquefied gas pump 31, the liquefied gas stored in the liquefiedgas storage device 11 is sent to the liquefiedgas supply line 3, flows through the liquefiedgas supply line 3 from upstream to downstream, and then is sent to the liquefiedgas equipment 12. Further, by driving the workingfluid circulation pump 44, the working fluid circulates through the workingfluid circulation line 4. - The cold
energy recovery device 41 includes aturbine 42 configured to be driven by the working fluid flowing through the workingfluid circulation line 4. In the illustrated embodiment, the coldenergy recovery device 41 further includes agenerator 43 configured to generate electricity by driving theturbine 42. Theturbine 42 includes aturbine rotor 421 disposed on the workingfluid circulation line 4. Theturbine rotor 421 is configured to be rotatable by the working fluid flowing through the workingfluid circulation line 4. In some other embodiments, the coldenergy recovery device 41 may not convert a rotational force of theturbine rotor 421 into electric power, but may recover the rotational force as power as it is by a power transmission device (for example, a coupling, a belt, a pulley, or the like). - The intermediate heat
medium circulation line 6 is configured to circulate an intermediate heat medium having a lower solidifying point than water. The heatingwater supply line 7 is configured to send heating water introduced from the outside of the coldenergy recovery system 2. The "heating water" can be water for heating a heat exchange object as a heat medium in the heat exchanger, and may be water at room temperature. The heating water is preferably water that is easily available in the ship 1 (for example, outboard water such as seawater, cooling water that has cooled an engine of theship 1, or the like). - In the illustrated embodiment, the cold
energy recovery system 2 includes an intermediate heatmedium circulation pump 61 disposed on the intermediate heatmedium circulation line 6, and aheating water pump 71 disposed on the heatingwater supply line 7. By driving the intermediate heatmedium circulation pump 61, the intermediate heat medium circulates through the intermediate heatmedium circulation line 6. The heatingwater supply line 7 has oneend side 701 which is connected to a heatingwater supply source 13 disposed outside the coldenergy recovery system 2, and anotherend side 702 which is connected to a heatingwater discharge destination 14 disposed outside the coldenergy recovery system 2. By driving theheating water pump 71, the heating water is sent from the heatingwater supply source 13 to the heatingwater supply line 7, flows through the heatingwater supply line 7 from upstream to downstream, and then is sent to the heatingwater discharge destination 14. - As the heating
water supply source 13, a water inlet 17 (seeFIG. 1 ) provided in thehull 10 to introduce outboard water, a cooling water flow passage 18 (seeFIG. 1 ) where the cooling water that has cooled the engine of the ship 1 (for example, the engine 16) flows, or the like can be given as an example. Further, as the heatingwater discharge destination 14, a water outlet 19 (seeFIG. 1 ) provided in thehull 10 to discharge water outboard, or the like can be given as an example. - The intermediate heat medium may be the same type of heat medium as the working fluid, or may be a different type of heat medium. In the embodiment shown in
FIG. 2 , the intermediate heat medium is constituted by propane, and the heating water is constituted by the cooling water (engine jacket water) having cooled the engine. The cooling water draws heat from the engine and has a higher temperature than seawater at room temperature. In the embodiment shown inFIG. 3 , the intermediate heat medium is constituted by propane, and the heating water is constituted by seawater acquired from the outside of the ship. In the embodiment shown inFIG. 4 , the intermediate heat medium is constituted by antifreeze (more specifically, glycol water), and the heating water is constituted by seawater acquired from the outside of the ship. For reference,FIGs. 2 to 4 each show an example of a temperature and a pressure in each flow passage. - The
first heat exchanger 51 is configured to exchange heat between the liquefied gas flowing through the liquefiedgas supply line 3 and the working fluid flowing through the workingfluid circulation line 4. In the illustrated embodiment, thefirst heat exchanger 51 forms a liquefiedgas flow passage 511 which is disposed on the liquefiedgas supply line 3 and through which the liquefied gas flows, and a workingfluid flow passage 512 which is disposed on the workingfluid circulation line 4 and in which the working fluid flows. The workingfluid flow passage 512 is disposed at least partially adjacent to the liquefiedgas flow passage 511, and heat exchange is performed between the working fluid flowing through the workingfluid flow passage 512 and the liquefied gas flowing through the liquefiedgas flow passage 511. - The
second heat exchanger 52 is configured to exchange heat between the working fluid flowing through the workingfluid circulation line 4 and the intermediate heat medium flowing through the intermediate heatmedium circulation line 6. In the illustrated embodiment, thesecond heat exchanger 52 forms a workingfluid flow passage 521 which is disposed on the workingfluid circulation line 4 and through which the working fluid flows, and an intermediate heatmedium flow passage 522 which is disposed on the intermediate heatmedium circulation line 6 and in which the intermediate heat medium flows. The intermediate heatmedium flow passage 522 is disposed at least partially adjacent to the workingfluid flow passage 521, and heat exchange is performed between the intermediate heat medium flowing through the intermediate heatmedium flow passage 522 and the working fluid flowing through the workingfluid flow passage 521. - The
third heat exchanger 53 is configured to exchange heat between the intermediate heat medium flowing through the intermediate heatmedium circulation line 6 and the heating water flowing through the heatingwater supply line 7. In the illustrated embodiment, thethird heat exchanger 53 forms an intermediate heatmedium flow passage 531 which is disposed on the intermediate heatmedium circulation line 6 and through which the intermediate heat medium flows, and a heatingwater flow passage 532 which is disposed on the heatingwater supply line 7 and through which the heating water flows. The heatingwater flow passage 532 is disposed at least partially adjacent to the intermediate heatmedium flow passage 531, and heat exchange is performed between the intermediate heat medium flowing through the heatingwater flow passage 532 and the working fluid flowing through the intermediate heatmedium flow passage 531. - The first heat exchanger 51 (more specifically, the liquefied gas flow passage 511) is disposed downstream of the liquefied
gas pump 31 on the liquefiedgas supply line 3 and upstream of the liquefiedgas equipment 12. The liquefiedgas pump 31 is disposed downstream of the liquefiedgas storage device 11 on the liquefiedgas supply line 3. Further, the first heat exchanger 51 (more specifically, the working fluid flow passage 512) is disposed downstream of theturbine 42 on the workingfluid circulation line 4 and upstream of the workingfluid circulation pump 44. - The second heat exchanger 52 (more specifically, the working fluid flow passage 521) is disposed downstream of the working
fluid circulation pump 44 on the workingfluid circulation line 4 and upstream of theturbine 42. Further, the second heat exchanger 52 (more specifically, the intermediate heat medium flow passage 522) is disposed downstream of the third heat exchanger (more specifically, the intermediate heat medium flow passage 531) on the intermediate heatmedium circulation line 6 and upstream of the intermediate heatmedium circulation pump 61. - The third heat exchanger (more specifically, the heating water flow passage 532) is disposed downstream of the
heating water pump 71 on the heatingwater supply line 7 and upstream of the heatingwater discharge destination 14. Theheating water pump 71 is disposed downstream of the heatingwater supply source 13 on the heatingwater supply line 7. - The liquid liquefied gas boosted by the liquefied
gas pump 31 is sent to the liquefiedgas flow passage 511 of thefirst heat exchanger 51. The heat exchange in thefirst heat exchanger 51 heats the liquefied gas flowing through the liquefiedgas flow passage 511 and cools the working fluid flowing through the workingfluid flow passage 512. That is, the cold energy of the liquefied gas flowing through the liquefiedgas flow passage 511 is recovered by the working fluid flowing through the workingfluid flow passage 512. The heat exchange in thefirst heat exchanger 51 causes the working fluid flowing through the workingfluid flow passage 512 to have the temperature lower than the solidifying point of water (heating water). - The intermediate heat medium boosted by the intermediate heat
medium circulation pump 61 is sent to the intermediate heatmedium flow passage 531 of thethird heat exchanger 53. Further, the heating water boosted by theheating water pump 71 is sent to the heatingwater flow passage 532. The heat exchange in thethird heat exchanger 53 heats the intermediate heat medium flowing through the intermediate heatmedium flow passage 531. - The working fluid boosted by the working fluid the
circulation pump 44 after being cooled by thefirst heat exchanger 51 is sent to the workingfluid flow passage 521 of thesecond heat exchanger 52. Further, the intermediate heat medium heated by thethird heat exchanger 53 is sent to the intermediate heatmedium flow passage 522. The heat exchange in thesecond heat exchanger 52 heats the working fluid flowing through the workingfluid flow passage 521 and cools the intermediate heatmedium flow passage 522. Herein, since the intermediate heat medium has the lower solidifying point than water, it is possible to suppress solidification during the heat exchange with the low-temperature working fluid in the second heat exchanger. In the embodiments shown inFIGs. 2 to 4 , the coldenergy recovery system 2 decides a condition of each equipment in the coldenergy recovery system 2 such that the intermediate heat medium flowing through the intermediate heatmedium circulation line 6 has the temperature higher than the solidifying point of water. - The intermediate heat medium flowing through the intermediate heat
medium flow passage 531 of thethird heat exchanger 53 has a higher temperature than the working fluid flowing through the workingfluid flow passage 521 of thesecond heat exchanger 52. In the illustrated embodiment, the intermediate heat medium flowing through the intermediate heatmedium flow passage 531 has the temperature higher than the solidifying point of water (heating water). As described above, although the intermediate heat medium is cooled by the heat exchange with the working fluid in thesecond heat exchanger 52, the temperature higher than the solidifying point of water is maintained even after the cooling. Thus, it is possible to suppress solidification of the heating water during the heat exchange between the intermediate heat medium and the heating water in thethird heat exchanger 53. -
FIG. 5 is a schematic configuration diagram schematically showing the overall configuration of the cold energy recovery system according a comparative example. A coldenergy recovery system 20 according to the comparative example includes the liquefiedgas supply line 3, the workingfluid circulation line 4, the coldenergy recovery device 41, the heatingwater supply line 7, and thefirst heat exchanger 51. Then, the coldenergy recovery system 20 further includes aheat exchanger 50 configured to exchange heat between the working fluid flowing through the workingfluid circulation line 4 and the heating water flowing through the heatingwater supply line 7. In the comparative example shown inFIG. 5 , the liquefied gas is constituted by liquefied natural gas, the working fluid is constituted by R1234ZE, and the heating water the heating water is constituted by seawater acquired from the outside of the ship. For reference,FIG. 5 shows an example of the temperature and the pressure in each flow passage. - The
heat exchanger 50 forms a workingfluid flow passage 501 disposed at a position corresponding to the above-described second heat exchanger 52 (working fluid flow passage 521) on the workingfluid circulation line 4, and a heatingwater flow passage 502 disposed at a position corresponding to the above-described third heat exchanger 53 (heating water flow passage 532) on the heatingwater supply line 7. The heatingwater flow passage 502 is disposed at least partially adjacent to the workingfluid flow passage 501, and heat exchange is performed between the heating water flowing through the heatingwater flow passage 502 and the working fluid flowing through the workingfluid flow passage 501. - The working fluid flowing through the working
fluid flow passage 501 has a temperature lower than the solidifying point of water (heating water) like the working fluid flowing through the workingfluid flow passage 521. Thus, the heating water is solidified by the heat exchange between the working fluid and the heating water in theheat exchanger 50, the solidified heating water may freeze to the heatingwater flow passage 502 of theheat exchanger 50, and may block theheat exchanger 50. - As shown in
FIGs. 2 to 4 , the coldenergy recovery system 2 according to some embodiments includes the above-described workingfluid circulation line 4, the coldenergy recovery device 41 including theturbine 42 described above, and the above-described intermediate heatmedium circulation line 6, the above-describedfirst heat exchanger 51, the above-describedsecond heat exchanger 52, and the above-describedthird heat exchanger 53. - With the above configuration, the cold
energy recovery system 2 at least includes the intermediate heatmedium circulation line 6, thesecond heat exchanger 52, and thethird heat exchanger 53. In such coldenergy recovery system 2, the heating water and the working fluid circulating through the workingfluid circulation line 4 indirectly exchange heat via the intermediate heat medium circulating through the intermediate heatmedium circulation line 6, making it possible to suppress solidification of the heat medium (the intermediate heat medium, the heating water) during the heat exchange. Thus, it is possible to suppress that the solidified heat medium freezes to the heat exchanger (thesecond heat exchanger 52, the third heat exchanger 53) and blocks the heat exchanger. - More specifically, the working fluid circulating through the working
fluid circulation line 4 has a temperature which is not greater than the solidifying point of water by the heat exchange with the liquefied gas in thefirst heat exchanger 51. In thesecond heat exchanger 52, heat exchange is performed between the working fluid which has passed through thefirst heat exchanger 51 and is decreased in temperature, and the intermediate heat medium circulating through the intermediate heatmedium circulation line 6. Since the intermediate heat medium has a lower solidifying point than water, the intermediate heat medium is hardly solidified during heat exchange with the low-temperature working fluid in thesecond heat exchanger 52. Thus, it is possible to suppress that the solidified intermediate heat medium freezes to thesecond heat exchanger 52 and blocks thesecond heat exchanger 52. - Meanwhile, in the
third heat exchanger 53, heat exchange is performed between the heating water and the intermediate heat medium which has passed through thesecond heat exchanger 52 and is decreased in temperature. Although the intermediate heat medium is cooled by the heat exchange with the working fluid in thesecond heat exchanger 52, the temperature higher than the solidifying point of water is maintained even after the cooling. Thus, it is possible to suppress solidification of the heating water during the heat exchange between the intermediate heat medium and the heating water in thethird heat exchanger 53. Thus, it is possible to suppress that the solidified heating water freezes to thethird heat exchanger 53 and blocks thethird heat exchanger 53. - Thus, with the above configuration, since the cold
energy recovery system 2 can suppress that the solidified heat medium (the intermediate heat medium, the heating water) freezes to the heat exchanger (thesecond heat exchanger 52, the third heat exchanger 53) and blocks the heat exchanger, it is possible to improve reliability of the coldenergy recovery system 2 when the small heat exchanger is used. - In the embodiments shown in
FIGs. 2 to 4 , the above-described workingfluid circulation line 4 includes abypass flow passage 45 branches from downstream of thesecond heat exchanger 52, bypasses theturbine 42, and is connected to upstream of thefirst heat exchanger 51. A flow passage other than thebypass flow passage 45 of the workingfluid circulation line 4 described above (a flow passage passing through theturbine 42 or the first heat exchanger 51) will be referred to as amain flow passage 40. Thebypass flow passage 45 branches from themain flow passage 40 at abranch portion 451 and joins themain flow passage 40 at amerge portion 452. The above-described coldenergy recovery system 2 further includes an on-offvalve 46 disposed downstream of thebranch portion 451 of themain flow passage 40 and upstream of theturbine 42, and an on-offvalve 47 disposed on thebypass flow passage 45. When the coldenergy recovery system 2 is started, the on-offvalve 46 is closed and the on-offvalve 47 is opened to allow the working fluid to bypass theturbine 42. After a predetermined period has elapsed, the on-offvalve 46 is opened and the on-offvalve 47 is closed to allow the working flow passage to pass through theturbine 42. - In the embodiments shown in
FIGs. 2 to 4 , the above-described coldenergy recovery system 2 is configured to evaporate the intermediate heat medium flowing through the intermediate heatmedium circulation line 6 in thethird heat exchanger 53, and is configured to condense the intermediate heat medium flowing through the intermediate heatmedium circulation line 6 in thesecond heat exchanger 52. In this case, it is possible to improve the overall efficiency of the coldenergy recovery system 2 by utilizing latent heat or sensible heat. - In some embodiments, as shown in
FIGs. 3 and4 , the above-described coldenergy recovery system 2 further includes the above-described liquefiedgas supply line 3, and anauxiliary heat exchanger 81 disposed downstream of thefirst heat exchanger 51 on the liquefiedgas supply line 3. Theauxiliary heat exchanger 81 is configured to exchange heat between the liquefied gas flowing downstream of thefirst heat exchanger 51 through the liquefiedgas supply line 3 and a heating medium circulating in the coldenergy recovery system 2. - In the illustrated embodiment, the heating medium has a lower solidifying point than water. The
auxiliary heat exchanger 81 forms a liquefiedgas flow passage 811 which is disposed downstream of the first heat exchanger on the liquefiedgas supply line 3 and through which the liquefied gas flows, and a heatingmedium flow passage 812 through which the heating medium circulating in the coldenergy recovery system 2 flows. The heatingmedium flow passage 812 is disposed at least partially adjacent to the liquefiedgas flow passage 811, and heat exchange is performed between the heating medium flowing through the heatingmedium flow passage 812 and the liquefiedgas flow passage 811 flowing through the liquefiedgas flow passage 811. - The liquefied gas heated by the
first heat exchanger 51 is sent to the liquefiedgas flow passage 811 of theauxiliary heat exchanger 81. The heat exchange in theauxiliary heat exchanger 81 heats the liquefied gas flowing through the liquefiedgas flow passage 811 and cools the heating medium flowing through the heatingmedium flow passage 812. Herein, since the heating medium has the lower solidifying point than water, it is possible to suppress solidification during the heat exchange with the liquefied gas in theauxiliary heat exchanger 81. - With the above configuration, the cold
energy recovery system 2 includes the liquefiedgas supply line 3, thefirst heat exchanger 51 disposed on the liquefiedgas supply line 3, and theauxiliary heat exchanger 81 disposed downstream of thefirst heat exchanger 51 on the liquefiedgas supply line 3. In such coldenergy recovery system 2, the heat exchange in thefirst heat exchanger 51 and theauxiliary heat exchanger 81 raises the temperature of the liquefied gas and vaporizes the liquefied gas. In this case, it is not necessary to raise the temperature to a temperature, at which the liquid liquefied gas is completely vaporized, by the heat exchange in thefirst heat exchanger 51. Thus, compared to a case where the temperature of the liquefied gas is raised only by thefirst heat exchanger 51, it is possible to reduce the amount of the heat exchange in thefirst heat exchanger 51, and it is possible to reduce the temperature drop of the working fluid in thefirst heat exchanger 51. Thus, it is possible to effectively suppress solidification of the intermediate heat medium during the heat exchange between the working fluid and the intermediate heat medium in thesecond heat exchanger 52. Further, by reducing the amount of the heat exchange in thefirst heat exchanger 51, it is possible to reduce the size of thefirst heat exchanger 51. - In some embodiments, the above-described cold
energy recovery system 2 is configured such that the above-described liquefiedgas supply line 3 does not include a heat exchanger other than thefirst heat exchanger 51, as shown inFIG. 2 . In this case, the liquefied gas is vaporized by the heat exchange in thefirst heat exchanger 51. With the above configuration, it is possible to simplify the structure of the coldenergy recovery system 2. - In some embodiments, as shown in
FIG. 3 , the heating medium that exchanges heat with the liquefied gas in theauxiliary heat exchanger 81 described above is constituted by the intermediate heat medium heated by thethird heat exchanger 53 and flowing through the intermediate heatmedium circulation line 6. In this case, in theauxiliary heat exchanger 81, heat exchange is performed between the liquefied gas which has passed through thefirst heat exchanger 51 and is raised in temperature, and the intermediate heat medium heated by thethird heat exchanger 53. Since the intermediate heat medium has the lower solidifying point than water, it is possible to suppress solidification during the heat exchange with the liquefied gas in theauxiliary heat exchanger 81. Thus, it is possible to suppress that the solidified intermediate heat medium freezes to theauxiliary heat exchanger 81 and blocks theauxiliary heat exchanger 81. Thus, it is possible to effectively heat the liquefied gas by theauxiliary heat exchanger 81. - If a heat medium circulating through a circulation line different from the intermediate heat
medium circulation line 6 is used as the heating medium, a circulation pump for circulating the heat medium becomes necessary. With the above configuration, by using the intermediate heat medium circulating through the intermediate heatmedium circulation line 6 as the heating medium, the above-described circulation pump becomes unnecessary, making it possible to suppress an equipment cost of the coldenergy recovery system 2. - In some embodiments, as shown in
FIG. 3 , the above-described intermediate heatmedium circulation line 6 includes abypass flow passage 63 which branches from downstream of thethird heat exchanger 53, bypasses thesecond heat exchanger 52, and is connected to upstream of thethird heat exchanger 53. The above-describedauxiliary heat exchanger 81 is configured to exchange heat between the liquefied gas flowing through the liquefiedgas supply line 3 and the intermediate heat medium flowing through thebypass flow passage 63. - As shown in
FIG. 3 , a flow passage other than thebypass flow passage 63 of the intermediate heatmedium circulation line 6 described above (a flow passage passing through thesecond heat exchanger 52 or the third heat exchanger 53) will be referred to as amain flow passage 62. In the illustrated embodiment, the coldenergy recovery system 2 includes: an intermediate heat medium storage device (for example, a buffer tank) 64 which is disposed downstream of thesecond heat exchanger 52 on themain flow passage 62 and upstream of the intermediate heatmedium circulation pump 61, and is configured to store the intermediate heat medium; and aflow regulating valve 65 which is disposed downstream of theauxiliary heat exchanger 81 on thebypass flow passage 63 and is configured to regulate the flow rate of the intermediate heat medium flowing through thebypass flow passage 63. - The
bypass flow passage 63 has oneend side 631 which is connected to downstream of thethird heat exchanger 53 on themain flow passage 62 and upstream of thesecond heat exchanger 52, and another end side 632 connected to the intermediate heatmedium storage device 64. The intermediate heat medium that has passed through thebypass flow passage 63 joins the intermediate heat medium that has passed through thesecond heat exchanger 52 on themain flow passage 62, in the intermediate heatmedium storage device 64. The another end side 632 of thebypass flow passage 63 may be connected to downstream of thesecond heat exchanger 52 on themain flow passage 62 and upstream of the intermediate heatmedium storage device 64. - The
flow regulating valve 65 is disposed downstream of the auxiliary heat exchanger 81 (more specifically, the heating medium flow passage 812) on thebypass flow passage 63. By regulating the flow rate of the intermediate heat medium flowing through thebypass flow passage 63 with theflow regulating valve 65, the flow rate of the intermediate heat medium passing through thesecond heat exchanger 52 on themain flow passage 62 is also regulated. - Since the intermediate heat medium is a heat medium responsible for heating in the
second heat exchanger 52 and theauxiliary heat exchanger 81, the intermediate heat medium is cooled by heat exchange in these heat exchangers. With the above configuration, theauxiliary heat exchanger 81 is configured to exchange heat between the liquefied gas and the intermediate heat medium which flows through thebypass flow passage 63 bypassing thesecond heat exchanger 52. That is, since the intermediate heatmedium circulation line 6 does not form the flow passage passing through both thesecond heat exchanger 52 and theauxiliary heat exchanger 81, it is possible to prevent the temperature of the intermediate heat medium circulating through the intermediate heatmedium circulation line 6 from becoming too low. Thus, it is possible to suppress solidification of the heating water during the heat exchange with the intermediate heat medium in thethird heat exchanger 53. - In some embodiments, as shown in
FIG. 4 , the above-described coldenergy recovery system 2 further includes a second intermediate heatmedium circulation line 9 which is configured to circulate a second intermediate heat medium having a lower solidifying point than water. The heating medium which exchanges heat with the liquefied gas in theauxiliary heat exchanger 81 described above is constituted by the second intermediate heat medium flowing through the second intermediate heatmedium circulation line 9. The heatingmedium flow passage 812 of theauxiliary heat exchanger 81 is disposed on the second intermediate heatmedium circulation line 9. - In the illustrated embodiment, the cold
energy recovery system 2 includes a second intermediate heatmedium circulation pump 91 disposed downstream of theauxiliary heat exchanger 81 on the second intermediate heatmedium circulation line 9. By driving thecirculation pump 91, the second intermediate heat medium circulates through the second intermediate heatmedium circulation line 9. - The second intermediate heat medium may be the same type of heat medium as the first intermediate heat medium which is the intermediate heat medium flowing through the intermediate heat
medium circulation line 6, or may be a different type of heat medium. In the embodiment shown inFIG. 4 , the second intermediate heat medium is constituted by R1234ZE. - With the above configuration, the heating medium which exchanges heat with the liquefied gas in the
auxiliary heat exchanger 81 is constituted by the second intermediate heat medium flowing through the second intermediate heatmedium circulation line 9. In this case, in theauxiliary heat exchanger 81, heat exchange is performed between the liquefied gas which has passed through thefirst heat exchanger 51 and is raised in temperature, and the second intermediate heat medium circulating through the second intermediate heatmedium circulation line 9. Since the second intermediate heat medium has the lower solidifying point than water, it is possible to suppress solidification during the heat exchange with the liquefied gas in theauxiliary heat exchanger 81. Thus, it is possible to suppress that the solidified second intermediate heat medium freezes to theauxiliary heat exchanger 81 and blocks theauxiliary heat exchanger 81. - Further, with the above configuration, since the second intermediate heat
medium circulation line 9 is different from the intermediate heatmedium circulation line 6, it is possible to use, as the second intermediate heat medium, a heat medium different from the intermediate heat medium circulating through the intermediate heatmedium circulation line 6. For example, as the second intermediate heat medium, it is possible to use a heat medium which is more suitable for conditions of the heat exchange in theauxiliary heat exchanger 81 than the intermediate heat medium circulating through the intermediate heatmedium circulation line 6. - In some embodiments, as shown in
FIG. 4 , the above-described coldenergy recovery system 2 further includes a secondauxiliary heat exchanger 82 which is configured to exchange heat between the second intermediate heat medium flowing through the second intermediate heatmedium circulation line 9 and the heating water introduced from the outside of the coldenergy recovery system 2. - In the illustrated embodiment, the second
auxiliary heat exchanger 82 forms a second intermediate heatmedium flow passage 821 which is disposed downstream of thecirculation pump 91 on the second intermediate heatmedium circulation line 9 and through which the second intermediate heat medium flows, and a heatingwater flow passage 822 through which the heating water introduced from the outside of the coldenergy recovery system 2 flows. The heatingwater flow passage 822 is disposed at least partially adjacent to the second intermediate heatmedium flow passage 821, and heat exchange is performed between the heating water flowing through the heatingwater flow passage 822 and the second intermediate heat medium flowing through the second intermediate heatmedium flow passage 821. - In the embodiment shown in
FIG. 4 , the above-described heatingwater supply line 7 includes asub flow passage 72 which branches from downstream of theheating water pump 71 and upstream of thethird heat exchanger 53, and is connected to a heatingwater discharge destination 14B. The heatingwater flow passage 822 of the secondauxiliary heat exchanger 82 is disposed on thesub flow passage 72. As shown inFIG. 4 , a flow passage other than thesub flow passage 72 of the heatingwater supply line 7 described above (a flow passage passing through theheating water pump 71 or the third heat exchanger 53) will be referred to as amain flow passage 70. Thesub flow passage 72 has oneend side 721 which is connected to downstream of theheating water pump 71 on themain flow passage 70 and upstream of thethird heat exchanger 53, and anotherend side 722 connected to the heatingwater discharge destination 14B. In this case, since it is possible to send the heating water to each of themain flow passage 70 and thesub flow passage 72 by theheating water pump 71, a dedicated pump for flowing the heating water to thesub flow passage 72 becomes unnecessary. Thus, it is possible to suppress the equipment cost of the coldenergy recovery system 2. The anotherend side 722 of thesub flow passage 72 may be connected to downstream of thethird heat exchanger 53 on themain flow passage 70 or the heatingwater discharge destination 14. - The second intermediate heat medium, which is boosted by the
circulation pump 91 after being cooled by theauxiliary heat exchanger 81, is sent to the second intermediate heatmedium flow passage 821. Further, the heating water boosted by theheating water pump 71 is sent to the heatingwater flow passage 822. The second intermediate heat medium flowing through the second intermediate heatmedium flow passage 821 has a higher temperature than the heating water flowing through the heatingwater flow passage 822. The heat exchange in the secondauxiliary heat exchanger 82 heats the second intermediate heat medium flowing through the second intermediate heatmedium flow passage 821. The second intermediate heat medium heated by the secondauxiliary heat exchanger 82 is sent to theauxiliary heat exchanger 81. - In the illustrated embodiment, the second intermediate heat medium flowing through the second intermediate heat
medium flow passage 821 has the temperature higher than the solidifying point of water (heating water). Although the second intermediate heat medium flowing through the second intermediate heatmedium circulation line 9 is cooled by the heat exchange with the liquefied gas in theauxiliary heat exchanger 81, the temperature higher than the solidifying point of water is maintained even after the cooling. Thus, it is possible to suppress solidification of the heating water during the heat exchange between the second intermediate heat medium and the heating water in the secondauxiliary heat exchanger 82. - In the cold
energy recovery system 2, since the heat exchange in thefirst heat exchanger 51 and theauxiliary heat exchanger 81 raises the temperature of the liquefied gas, the amount of the heat exchange in theauxiliary heat exchanger 81 is small, and the amount of temperature drop of the second intermediate heat medium (heating medium) in theauxiliary heat exchanger 81 is small. With the above configuration, it is possible to suppress solidification of the heating water during the heat exchange between the heating water and the second intermediate heat medium in the secondauxiliary heat exchanger 82. - In some embodiments, as shown in
FIGs. 2 to 4 , the above-described coldenergy recovery device 41 includes the above-describedturbine 42, and the above-describedgenerator 43 configured to generate electricity by driving theturbine 42. In this case, since the coldenergy recovery device 41 includes theturbine 42 and thegenerator 43, it is possible to generate electricity in thegenerator 43 by driving theturbine 42 with the working fluid which circulates through the workingfluid circulation line 4 and recovers the cold energy from the liquefied gas. In this case, it is possible to effectively utilize the cold energy of the liquefied gas. - In some embodiments, as shown in
FIGs. 2 to 4 , the above-described coldenergy recovery system 2 at least includes the liquefiedgas supply line 3 configured to send the liquefied gas from the liquefiedgas storage device 11, and the liquefiedgas pump 31 disposed on the liquefiedgas supply line 3. The liquefiedgas pump 31 is configured to be driven by the electric power generated by thegenerator 43. In the illustrated embodiment, each of thecirculation pump 44, thecirculation pump 61, theheating water pump 71, and the second intermediate heatmedium circulation pump 91 is also configured to be driven by the electric power generated by thegenerator 43. Not all of the liquefiedgas pump 31, thecirculation pump 44, thecirculation pump 61, theheating water pump 71, and the second intermediate heatmedium circulation pump 91, but one or not less than one of them may be configured to be driven by the electric power generated by thegenerator 43. - With the above configuration, it is possible to drive the liquefied
gas pump 31 disposed on the liquefiedgas supply line 3 by the electric power generated by thegenerator 43. In this case, an electric power system for supplying electric power from the onshore electric power equipment to the liquefiedgas pump 31 becomes unnecessary, making it possible to reduce the size of theship 1 provided with the liquefiedgas pump 31. Alternatively, since it is possible to reduce the occupied space of the coldenergy recovery system 2 in theship 1, it is possible to increase the occupied space of the liquefiedgas storage device 11 in theship 1. -
FIG. 6 is an explanatory view for describing an example of the heat exchanger in an embodiment of the present disclosure. - In some embodiments, as shown in
FIG. 6 , thethird heat exchanger 53 is constituted by a microchannel heat exchanger 53A. The microchannel heat exchanger 53A includes afirst microchannel 531A through which the intermediate heat medium flows, and asecond microchannel 532A at least a part of which is disposed adjacent to thefirst microchannel 531A and through which the heating water flows. - In the illustrated embodiment, the microchannel heat exchanger 53Ais constituted by a PCHE (Printed Circuit Heat Exchanger) which is created by alternately stacking and joining to each other
first metal plates 533 each in which a plurality offirst microchannels 531A are formed andsecond metal plates 534 each in which a plurality ofsecond microchannels 532A are formed. In some other embodiments, the microchannel heat exchanger 53A may be a plate heat exchanger or the like. - With the above configuration, since the
third heat exchanger 53 is constituted by the microchannel heat exchanger 53A which allows for the heat exchange between the intermediate heat medium flowing through thefirst microchannels 531A and the heating water flowing through thesecond microchannels 532A, thethird heat exchanger 53 is compact and can improve a heat-transfer coefficient. Since the cold energy recovery system2 using such heat exchanger can reduce the occupied space of the coldenergy recovery system 2 in theship 1, it is possible to increase the occupied space of the liquefiedgas storage device 11 in theship 1. The heat exchanger other than thethird heat exchanger 53 may also be the microchannel heat exchanger. - As shown in
FIG. 1 , theship 1 according to some embodiments includes the above-described coldenergy recovery system 2. In this case, since it is possible to reduce the size of the coldenergy recovery system 2 by using the small heat exchanger for the heat exchanger of the cold energy recovery system 2 (for example, thethird heat exchanger 53 or the like), it is possible to reduce the size of theship 1 having the coldenergy recovery system 2. Alternatively, since it is possible to reduce the occupied space of the coldenergy recovery system 2 in theship 1, it is possible to increase the occupied space of the liquefiedgas storage device 11 in theship 1. -
FIG. 7 is a flowchart of a cold energy recovery method according to an embodiment of the present disclosure. - A cold energy recovery method100 according to some embodiments is a cold energy recovery method by the above-described cold
energy recovery system 2 which is installed in theship 1 including the liquefiedgas storage device 11 and as shown inFIG. 7 , at least includes a first heat exchange step S101, a second heat exchange step S102, and a third heat exchange step S103. - The first heat exchange step S101 includes performing heat exchange between the liquefied gas and the working fluid by the
first heat exchanger 51. The second heat exchange step S102 includes performing, by thesecond heat exchanger 52, heat exchange between the intermediate heat medium and the working fluid that has exchanged heat with the liquefied gas in the first heat exchange step S101. The third heat exchange step S103 includes performing, by thethird heat exchanger 53, heat exchange between the heating water and the intermediate heat medium that has exchanged heat with the working fluid in the second heat exchange step S102. - The above method includes the first heat exchange step S101, the second heat exchange step S102, and the third heat exchange step S103. In such cold
energy recovery method 100, the second heat exchange step S102 and the third heat exchange step S103 cause the heating water and the working fluid circulating through the workingfluid circulation line 4 to indirectly exchange heat via the intermediate heat medium circulating through the intermediate heatmedium circulation line 6, making it possible to suppress solidification of the heat medium (the intermediate heat medium, the heating water) during the heat exchange. Thus, it is possible to suppress that the solidified heat medium freezes to the heat exchanger (thesecond heat exchanger 52, the third heat exchanger 53) and blocks the heat exchanger. - More specifically, the first heat exchange step S101 includes performing heat exchange between the liquefied gas and the working fluid by the
first heat exchanger 51. The working fluid that has passed through thefirst heat exchanger 51 has a low temperature which is not greater than the solidifying point of water. The second heat exchange step S102 includes performing, by thesecond heat exchanger 52, heat exchange between the working fluid, which is decreased in temperature by the heat exchange in the first heat exchange step S101, and the intermediate heat medium flowing through the intermediate heatmedium circulation line 6. Since the intermediate heat medium has a lower solidifying point than water, the intermediate heat medium is hardly solidified during heat exchange with the low-temperature working fluid in the second heat exchange step S102. Thus, it is possible to suppress that the solidified intermediate heat medium freezes to thesecond heat exchanger 52 and blocks thesecond heat exchanger 52. - Meanwhile, the third heat exchange step S103 includes performing, by the
third heat exchanger 53, heat exchange between the heating water and the intermediate heat medium which is decreased in temperature by the heat exchange in the second heat exchange step S102. Although the intermediate heat medium is cooled by the heat exchange with the working fluid in the second heat exchange step S102, the temperature higher than the solidifying point of water is maintained even after the cooling. Thus, it is possible to suppress solidification of the heating water during the heat exchange between the intermediate heat medium and the heating water in the third heat exchange step S103. Thus, it is possible to suppress that the solidified heating water freezes to thethird heat exchanger 53 and blocks thethird heat exchanger 53. - With the above method, since it is possible to suppress that the solidified heat medium (the intermediate heat medium, the heating water) freezes to the heat exchanger (the
second heat exchanger 52, the third heat exchanger 53) and blocks the heat exchanger, it is possible to improve reliability of the coldenergy recovery system 2 when the small heat exchanger is used. - As shown in
FIG. 7 , the coldenergy recovery method 100 may further include a first auxiliary heat exchange step S201 or a second auxiliary heat exchange step S202. The first auxiliary heat exchange step S201 includes performing, by theauxiliary heat exchanger 81, heat exchange between the above-described heating water and the liquefied gas which is raised in temperature by the heat exchange in the first heat exchange step S101. The second auxiliary heat exchange step S202 includes performing, by the secondauxiliary heat exchanger 82, heat exchange between the heating water and the second intermediate heat medium flowing through the second intermediate heatmedium circulation line 9. - The present disclosure is not limited to the above-described embodiments, and also includes an embodiment obtained by modifying the above-described embodiments and an embodiment obtained by combining these embodiments as appropriate.
- The contents described in some embodiments described above would be understood as follows, for instance.
- 1) A cold energy recovery system (2) according to at least one embodiment of the present disclosure is a cold energy recovery system (2) installed in a ship (1) which includes a liquefied gas storage device (11) configured to store a liquid liquefied gas, that includes a working fluid circulation line (4) which is configured to circulate a working fluid having a lower solidifying point than water, a cold energy recovery device (41) that includes a turbine (42) which is configured to be driven by the working fluid flowing through the working fluid circulation line (4), a first heat exchanger (51) which is configured to exchange heat between the liquefied gas and the working fluid flowing through the working fluid circulation line (4), an intermediate heat medium circulation line (6) which is configured to circulate an intermediate heat medium having a lower solidifying point than water, a second heat exchanger (52) disposed downstream of the first heat exchanger (51) on the working fluid circulation line (4), the second heat exchanger (52) being configured to exchange heat between the working fluid flowing through the working fluid circulation line (4) and the intermediate heat medium flowing through the intermediate heat medium circulation line (6), and a third heat exchanger (53) which is configured to exchange heat between the intermediate heat medium flowing through the intermediate heat medium circulation line (6) and heating water introduced from an outside of the cold energy recovery system (2).
- With the above configuration 1), the cold energy recovery system (2) includes the intermediate heat medium circulation line (6), the second heat exchanger (52), and the third heat exchanger (53). In such cold energy recovery system (2), the heating water and the working fluid circulating through the working fluid circulation line (4) indirectly exchange heat via the intermediate heat medium circulating through the intermediate heat medium circulation line (6), making it possible to suppress solidification of the heat medium (the intermediate heat medium, the heating water) during heat exchange. Thus, it is possible to suppress that the solidified heat medium freezes to the heat exchanger (the
second heat exchanger 52, the third heat exchanger 53) and blocks the heat exchanger. - More specifically, the working fluid circulating through the working fluid circulation line (4) has a temperature which is not greater than the solidifying point of water by the heat exchange with the liquefied gas in the first heat exchanger (51). In the second heat exchanger (52), heat exchange is performed between the working fluid which has passed through the first heat exchanger (51) and is decreased in temperature, and the intermediate heat medium circulating through the intermediate heat medium circulation line (6). Since the intermediate heat medium has a lower solidifying point than water, the intermediate heat medium is hardly solidified during heat exchange with the low-temperature working fluid in the second heat exchanger (52). Thus, it is possible to suppress that the solidified intermediate heat medium freezes to the second heat exchanger (52) and blocks the second heat exchanger (52).
- Meanwhile, in the third heat exchanger (53), heat exchange is performed between the heating water and the intermediate heat medium which has passed through the second heat exchanger (51) and is decreased in temperature. Although the intermediate heat medium is cooled by the heat exchange with the working fluid in the second heat exchanger (51), the temperature higher than the solidifying point of water is maintained even after the cooling. Thus, it is possible to suppress solidification of the heating water during the heat exchange between the intermediate heat medium and the heating water in the third heat exchanger (53). Thus, it is possible to suppress that the solidified heating water freezes to the third heat exchanger (53) and blocks the third heat exchanger (53).
- With the above configuration, since the cold energy recovery system (2) can suppress that the solidified heat medium (the intermediate heat medium, the heating water) freezes to the heat exchanger (the
second heat exchanger 52, the third heat exchanger 53) and blocks the heat exchanger, it is possible to improve reliability of the cold energy recovery system (2) when the small heat exchanger is used. - 2) In some embodiments, the cold energy recovery system (2) according to the above 1) further includes a liquefied gas supply line (3) configured to send the liquefied gas from the liquefied gas storage device (11), and an auxiliary heat exchanger (81) disposed downstream of the first heat exchanger (51) on the liquefied gas supply line (3), the auxiliary heat exchanger (81) being configured to exchange heat between the liquefied gas flowing through the liquefied gas supply line (3) and a heating medium circulating in the cold energy recovery system (2).
- With the above configuration 2), the cold energy recovery system (2) includes the liquefied gas supply line (3), the above-described first heat exchanger (51), and the auxiliary heat exchanger (81). In such cold energy recovery system (2), the heat exchange in the first heat exchanger (51) and the auxiliary heat exchanger (81) raises the temperature of the liquefied gas and vaporizes the liquefied gas. In this case, it is not necessary to raise the temperature to a temperature, at which the liquid liquefied gas is completely vaporized, by the heat exchange in the first heat exchanger (51). Thus, compared to a case where the temperature of the liquefied gas is raised only by the first heat exchanger (51), it is possible to reduce the amount of the heat exchange in the first heat exchanger (51), and it is possible to reduce the temperature drop of the working fluid in the first heat exchanger (51). Thus, it is possible to effectively suppress solidification of the intermediate heat medium during the heat exchange between the working fluid and the intermediate heat medium in the second heat exchanger (52). Further, by reducing the amount of the heat exchange in the first heat exchanger (51), it is possible to reduce the size of the first heat exchanger (51).
- 3) In some embodiments, in the cold energy recovery system (2) according to the above 2), the heating medium is constituted by the intermediate heat medium heated by the third heat exchanger (53) and flowing through the intermediate heat medium circulation line (6).
- With the above configuration 3), in the auxiliary heat exchanger (81), heat exchange is performed between the liquefied gas which has passed through the first heat exchanger (51) and is raised in temperature, and the intermediate heat medium heated by the third heat exchanger (53). Since the intermediate heat medium has the lower solidifying point than water, it is possible to suppress solidification during the heat exchange with the liquefied gas in the auxiliary heat exchanger (81). Thus, it is possible to suppress that the solidified intermediate heat medium freezes to the auxiliary heat exchanger (81) and blocks the auxiliary heat exchanger (81). Thus, it is possible to effectively heat the liquefied gas by the auxiliary heat exchanger (81).
- If a heat medium circulating through a circulation line different from the intermediate heat medium circulation line (6) is used as the heating medium, a circulation pump for circulating the heat medium becomes necessary. With the above configuration 3), by using the intermediate heat medium circulating through the intermediate heat medium circulation line (6) as the heating medium, the above-described circulation pump becomes unnecessary, making it possible to suppress an equipment cost of the cold energy recovery system (2).
- 4) In some embodiments, in the cold energy recovery system (2) according to the above 3), the intermediate heat medium circulation line (6) includes a bypass flow passage (63) which branches from downstream of the third heat exchanger (53), bypasses the second heat exchanger (52), and is connected to upstream of the third heat exchanger (53), and the auxiliary heat exchanger (81) is configured to exchange heat between the liquefied gas flowing through the liquefied gas supply line (3) and the intermediate heat medium flowing through the bypass flow passage (63).
- Since the intermediate heat medium is a heat medium responsible for heating in the second heat exchanger (52) and the auxiliary heat exchanger (81), the intermediate heat medium is cooled by heat exchange in these heat exchangers. With the above configuration 4), the auxiliary heat exchanger (81) is configured to exchange heat between the liquefied gas and the intermediate heat medium which flows through the bypass flow passage (63) bypassing the second heat exchanger (52). That is, since the intermediate heat medium circulation line (6) does not form the flow passage passing through both the second heat exchanger (52) and the auxiliary heat exchanger (81), it is possible to prevent the temperature of the intermediate heat medium circulating through the intermediate heat medium circulation line (6) from becoming too low. Thus, it is possible to suppress solidification of the heating water during the heat exchange with the intermediate heat medium in the third heat exchanger (53).
- 5) In some embodiments, the cold energy recovery system (2) according to the above 2) further includes a second intermediate heat medium circulation line (9) which is configured to circulate a second intermediate heat medium having a lower solidifying point than water. The heating medium is constituted by the second intermediate heat medium flowing through the second intermediate heat medium circulation line (9).
- With the above configuration 5), the heating medium which exchanges heat with the liquefied gas in the auxiliary heat exchanger (81) is constituted by the second intermediate heat medium flowing through the second intermediate heat medium circulation line (9). In this case, in the auxiliary heat exchanger (81), heat exchange is performed between the liquefied gas which has passed through the first heat exchanger (51) and is raised in temperature, and the second intermediate heat medium circulating through the second intermediate heat medium circulation line (9). Since the second intermediate heat medium has the lower solidifying point than water, it is possible to suppress solidification during the heat exchange with the liquefied gas in the auxiliary heat exchanger (81). Thus, it is possible to suppress that the solidified second intermediate heat medium freezes to the auxiliary heat exchanger (81) and blocks the auxiliary heat exchanger (81).
- Further, with the above configuration 5), since the second intermediate heat medium circulation line (9) is different from the intermediate heat medium circulation line (6), it is possible to use, as the second intermediate heat medium, a heat medium different from the intermediate heat medium circulating through the intermediate heat medium circulation line (6). For example, as the second intermediate heat medium, it is possible to use a heat medium which is more suitable for conditions of the heat exchange in the auxiliary heat exchanger (81) than the intermediate heat medium circulating through the intermediate heat medium circulation line (6).
- 6) In some embodiments, the cold energy recovery system (2) according to the above 5) further includes a second auxiliary heat exchanger (82) which is configured to exchange heat between the second intermediate heat medium flowing through the second intermediate heat medium circulation line (9) and heating water introduced from an outside of the cold energy recovery system (2).
- In the cold energy recovery system (2), since the heat exchange in the first heat exchanger (51) and the auxiliary heat exchanger (81) raises the temperature of the liquefied gas, the amount of the heat exchange in the auxiliary heat exchanger (81) is small, and the amount of temperature drop of the second intermediate heat medium (heating medium) in the auxiliary heat exchanger (81) is small. With the above configuration 6), it is possible to suppress solidification of the heating water during the heat exchange between the heating water and the second intermediate heat medium in the second auxiliary heat exchanger (82).
- 7) In some embodiments, in the cold energy recovery system (2) according to any one of the above 1) to 6), the cold energy recovery device (41) further includes a generator (43) configured to generate electricity by driving the turbine (42).
- With the above configuration 7), since the cold energy recovery device (41) includes the turbine (42) and the generator (43), it is possible to generate electricity in the generator (43) by driving the turbine (42) with the working fluid which circulates through the working
fluid circulation line 4 and recovers the cold energy from the liquefied gas. In this case, it is possible to effectively utilize the cold energy of the liquefied gas. - 8) In some embodiments, the cold energy recovery system (2) according to the above 7) further includes a liquefied gas supply line (3) configured to send the liquefied gas from the liquefied gas storage device (11), and a liquefied gas pump (31) disposed on the liquefied gas supply line (3). The liquefied gas pump (31) is configured to be driven by electric power generated by the generator (43).
- With the above configuration 8), it is possible to drive the liquefied gas pump (31) disposed on the liquefied gas supply line (3) by the electric power generated by the generator (43). In this case, an electric power system for supplying electric power from the onshore electric power equipment to the liquefied gas pump (31) becomes unnecessary, making it possible to reduce the size of the ship (1) provided with the liquefied gas pump (31). Alternatively, since it is possible to reduce the occupied space of the cold energy recovery system (2) in the ship (1), it is possible to increase the occupied space of the liquefied gas storage device (11) in the ship (1).
- 9) In some embodiments, in the cold energy recovery system (2) according to any one of the above 1) to 8), the third heat exchanger (53) is constituted by a microchannel heat exchanger (53A) that includes a first microchannel (531A) through which the intermediate heat medium flows, and a second microchannel (532A) through which the heating water flows, at least a part of the second microchannel (532A) being disposed adjacent to the first microchannel (531A).
- With the above configuration 9), since the third heat exchanger (53) is constituted by the microchannel heat exchanger (53A) which allows for the heat exchange between the intermediate heat medium flowing through the first microchannel (531A) and the heating water flowing through the second microchannel (532A), the third heat exchanger (53) is compact and can improve a heat-transfer coefficient.
- 10) A ship (1) according to at least one embodiment of the present disclosure includes the cold energy recovery system (2) according to any one of the above 1) to 9).
- With the above configuration 10), since it is possible to reduce the size of the cold energy recovery system (2) by using the small heat exchanger, it is possible to reduce the size of the ship (1) having the cold energy recovery system (2). Alternatively, since it is possible to reduce the occupied space of the cold energy recovery system (2) in the ship (1), it is possible to increase the occupied space of the liquefied gas storage device (11) in the ship (1).
- 11) A cold energy recovery method (100) according to at least one embodiment of the present disclosure is a cold energy recovery method (100) by a cold energy recovery system (2) installed in a ship (1) which includes a liquefied gas storage device (11) configured to store a liquid liquefied gas, the cold energy recovery system (2) including a working fluid circulation line (4) which is configured to circulate a working fluid having a lower solidifying point than water, a cold energy recovery device (41) that includes a turbine (42) which is configured to be driven by the working fluid flowing through the working fluid circulation line (4), a first heat exchanger (51) which is configured to exchange heat between the liquefied gas and the working fluid flowing through the working fluid circulation line (4), an intermediate heat medium circulation line (6) which is configured to circulate an intermediate heat medium having a lower solidifying point than water, a second heat exchanger (52) disposed downstream of the first heat exchanger (51) on the working fluid circulation line (4), the second heat exchanger (52) being configured to exchange heat between the working fluid flowing through the working fluid circulation line (4) and the intermediate heat medium flowing through the intermediate heat medium circulation line (6), and a third heat exchanger (53) which is configured to exchange heat between the intermediate heat medium flowing through the intermediate heat medium circulation line (6) and heating water introduced from an outside of the cold energy recovery system (2), the cold energy recovery method (100) including a first heat exchange step (S101) of performing heat exchange between the liquefied gas and the working fluid by the first heat exchanger (51), a second heat exchange step (S102) of performing, by the second heat exchanger (52), heat exchange between the intermediate heat medium and the working fluid that has exchanged heat with the liquefied gas in the first heat exchange step (S101), and a third heat exchange step (S103) of performing, by the third heat exchanger (53), heat exchange between the heating water and the intermediate heat medium that has exchanged heat with the working fluid in the second heat exchange step (S102).
- The above method 11) includes the first heat exchange step (S101), the second heat exchange step (S102), and the third heat exchange step (S103). In such cold energy recovery method (100), the second heat exchange step (S102) and the third heat exchange step (S103) cause the heating water and the working fluid circulating through the working fluid circulation line (4) to indirectly exchange heat via the intermediate heat medium circulating through the intermediate heat medium circulation line (6), making it possible to suppress solidification of the heat medium (the intermediate heat medium, the heating water) during heat exchange. Thus, it is possible to suppress that the solidified heat medium freezes to the heat exchanger (the
second heat exchanger 52, the third heat exchanger 53) and blocks the heat exchanger. - More specifically, the first heat exchange step (S101) includes performing heat exchange between the liquefied gas and the working fluid by the first heat exchanger (51). The working fluid that has passed through the first heat exchanger (51) has a low temperature which is not greater than the solidifying point of water. The second heat exchange step (S102) includes performing, by the second heat exchanger (52), heat exchange between the working fluid, which is decreased in temperature by the heat exchange in the first heat exchange step (S101), and the intermediate heat medium flowing through the intermediate heat medium circulation line (6). Since the intermediate heat medium has a lower solidifying point than water, the intermediate heat medium is hardly solidified during heat exchange with the low-temperature working fluid in the second heat exchange step. Thus, it is possible to suppress that the solidified intermediate heat medium freezes to the second heat exchanger (52) and blocks the second heat exchanger (52).
- Meanwhile, the third heat exchange step (S103) includes performing, by the third heat exchanger (53), heat exchange between the heating water and the intermediate heat medium which is decreased in temperature by the heat exchange in the second heat exchange step (SI02). Although the intermediate heat medium is cooled by the heat exchange with the working fluid in the second heat exchange step (S102), the temperature higher than the solidifying point of water is maintained even after the cooling. Thus, it is possible to suppress solidification of the heating water during the heat exchange between the intermediate heat medium and the heating water in the third heat exchange step. Thus, it is possible to suppress that the solidified heating water freezes to the third heat exchanger (53) and blocks the third heat exchanger (53).
- With the above method, since it is possible to suppress that the solidified heat medium (the intermediate heat medium, the heating water) freezes to the heat exchanger (the
second heat exchanger 52, the third heat exchanger 53) and blocks the heat exchanger, it is possible to improve reliability of the cold energy recovery system (2) when the small heat exchanger is used. -
- 1
- Ship
- 2
- Cold energy recovery system
- 20
- Cold energy recovery system according to comparative example
- 3
- Liquefied gas supply line
- 301
- One end side
- 302
- Another end side
- 31
- Liquefied gas pump
- 4
- Working fluid circulation line
- 41
- Cold energy recovery device
- 42
- Turbine
- 421
- Turbine rotor
- 43
- Generator
- 44
- (Working fluid) circulation pump
- 50
- Heat exchanger (of comparative example)
- 501
- Working fluid flow passage
- 502
- Heating water flow passage
- 51
- First heat exchanger
- 511
- Liquefied gas flow passage
- 512
- Working fluid flow passage
- 52
- Second heat exchanger
- 521
- Working fluid flow passage
- 522
- Intermediate heat medium flow passage
- 53
- Third heat exchanger
- 531
- Intermediate heat medium flow passage
- 531A
- First microchannel
- 532
- Heating water flow passage
- 532A
- Second microchannel
- 6
- Intermediate heat medium circulation line
- 61
- (Intermediate heat medium) circulation pump
- 62
- Main flow passage
- 63
- Bypass flow passage
- 631
- One end side
- 632
- Another end side
- 64
- Intermediate heat medium storage device
- 65
- Flow regulating valve
- 7
- Heating water supply line
- 701
- One end side
- 702
- Another end side
- 71
- Heating water pump
- 81
- Auxiliary heat exchanger
- 811
- Liquefied gas flow passage
- 812
- Heating medium flow passage
- 82
- Second auxiliary heat exchanger
- 821
- Second intermediate heat medium flow passage
- 822
- Heating water flow passage
- 9
- Second intermediate heat medium circulation line
- 10
- Hull
- 11
- Liquefied gas storage device
- 12
- Equipment
- 13
- Heating water supply source
- 14
- Heating water discharge destination
- 15
- Engine room
- 16
- Engine
- 17
- Water inlet
- 18
- Cooling water flow passage
- 19
- Water outlet
Claims (11)
- A cold energy recovery system installed in a ship which includes a liquefied gas storage device configured to store a liquid liquefied gas, comprising:a working fluid circulation line which is configured to circulate a working fluid having a lower solidifying point than water;a cold energy recovery device that includes a turbine which is configured to be driven by the working fluid flowing through the working fluid circulation line;a first heat exchanger which is configured to exchange heat between the liquefied gas and the working fluid flowing through the working fluid circulation line;an intermediate heat medium circulation line which is configured to circulate an intermediate heat medium having a lower solidifying point than water;a second heat exchanger disposed downstream of the first heat exchanger on the working fluid circulation line, the second heat exchanger being configured to exchange heat between the working fluid flowing through the working fluid circulation line and the intermediate heat medium flowing through the intermediate heat medium circulation line; anda third heat exchanger which is configured to exchange heat between the intermediate heat medium flowing through the intermediate heat medium circulation line and heating water introduced from an outside of the cold energy recovery system.
- The cold energy recovery system according to claim 1, further comprising:a liquefied gas supply line configured to send the liquefied gas from the liquefied gas storage device; andan auxiliary heat exchanger disposed downstream of the first heat exchanger on the liquefied gas supply line, the auxiliary heat exchanger being configured to exchange heat between the liquefied gas flowing through the liquefied gas supply line and a heating medium circulating in the cold energy recovery system.
- The cold energy recovery system according to claim 2,
wherein the heating medium is constituted by the intermediate heat medium heated by the third heat exchanger and flowing through the intermediate heat medium circulation line. - The cold energy recovery system according to claim 3,wherein the intermediate heat medium circulation line includes a bypass flow passage which branches from downstream of the third heat exchanger, bypasses the second heat exchanger, and is connected to upstream of the third heat exchanger, andwherein the auxiliary heat exchanger is configured to exchange heat between the liquefied gas flowing through the liquefied gas supply line and the intermediate heat medium flowing through the bypass flow passage.
- The cold energy recovery system according to claim 2,further comprising a second intermediate heat medium circulation line which is configured to circulate a second intermediate heat medium having a lower solidifying point than water,wherein the heating medium is constituted by the second intermediate heat medium flowing through the second intermediate heat medium circulation line.
- The cold energy recovery system according to claim 5, further comprising a second auxiliary heat exchanger which is configured to exchange heat between the second intermediate heat medium flowing through the second intermediate heat medium circulation line and heating water introduced from an outside of the cold energy recovery system.
- The cold energy recovery system according to any one of claims 1 to 6,
wherein the cold energy recovery device further includes a generator configured to generate electricity by driving the turbine. - The cold energy recovery system according to claim 7, further comprising:a liquefied gas supply line configured to send the liquefied gas from the liquefied gas storage device; anda liquefied gas pump disposed on the liquefied gas supply line,wherein the liquefied gas pump is configured to be driven by electric power generated by the generator.
- The cold energy recovery system according to any one of claims 1 to 8,
wherein the third heat exchanger is constituted by a microchannel heat exchanger that includes:a first microchannel through which the intermediate heat medium flows; anda second microchannel through which the heating water flows, at least a part of the second microchannel being disposed adjacent to the first microchannel. - A ship comprising the cold energy recovery system according to any one of claims 1 to 9.
- A cold energy recovery method by a cold energy recovery system installed in a ship which includes a liquefied gas storage device configured to store a liquid liquefied gas,
the cold energy recovery system including:a working fluid circulation line which is configured to circulate a working fluid having a lower solidifying point than water;a cold energy recovery device that includes a turbine which is configured to be driven by the working fluid flowing through the working fluid circulation line;a first heat exchanger which is configured to exchange heat between the liquefied gas and the working fluid flowing through the working fluid circulation line;an intermediate heat medium circulation line which is configured to circulate an intermediate heat medium having a lower solidifying point than water;a second heat exchanger disposed downstream of the first heat exchanger on the working fluid circulation line, the second heat exchanger being configured to exchange heat between the working fluid flowing through the working fluid circulation line and the intermediate heat medium flowing through the intermediate heat medium circulation line; anda third heat exchanger which is configured to exchange heat between the intermediate heat medium flowing through the intermediate heat medium circulation line and heating water introduced from an outside of the cold energy recovery system,the cold energy recovery method comprising:a first heat exchange step of performing heat exchange between the liquefied gas and the working fluid by the first heat exchanger;a second heat exchange step of performing, by the second heat exchanger, heat exchange between the intermediate heat medium and the working fluid that has exchanged heat with the liquefied gas in the first heat exchange step; anda third heat exchange step of performing, by the third heat exchanger, heat exchange between the heating water and the intermediate heat medium that has exchanged heat with the working fluid in the second heat exchange step.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2019213558A JP7288842B2 (en) | 2019-11-26 | 2019-11-26 | Cold heat recovery system, ship with cold heat recovery system, and cold heat recovery method |
PCT/JP2020/043956 WO2021106984A1 (en) | 2019-11-26 | 2020-11-26 | Cold recovery system, ship including cold recovery system, and cold recovery method |
Publications (2)
Publication Number | Publication Date |
---|---|
EP4035985A1 true EP4035985A1 (en) | 2022-08-03 |
EP4035985A4 EP4035985A4 (en) | 2022-11-23 |
Family
ID=76087207
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20893934.8A Pending EP4035985A4 (en) | 2019-11-26 | 2020-11-26 | Cold recovery system, ship including cold recovery system, and cold recovery method |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP4035985A4 (en) |
JP (1) | JP7288842B2 (en) |
KR (1) | KR20220062651A (en) |
CN (1) | CN114651148B (en) |
WO (1) | WO2021106984A1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
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JP2023020523A (en) * | 2021-07-30 | 2023-02-09 | 三菱重工マリンマシナリ株式会社 | Cold recovery system and starting method for cold recovery system |
CN114030582B (en) * | 2021-10-19 | 2024-01-26 | 中国舰船研究设计中心 | Integrated cabin seawater cooling system |
WO2023191523A1 (en) * | 2022-03-30 | 2023-10-05 | 주식회사 엔엑스엔시스템즈 | System using cold heat |
CN114923361A (en) * | 2022-04-06 | 2022-08-19 | 东南大学 | Fluid channel structure, printed circuit board heat exchanger and LNG transport ship |
KR102487017B1 (en) * | 2022-05-03 | 2023-01-11 | 에너진(주) | Gasification device for liquefied natural gas |
CN115158625B (en) * | 2022-07-15 | 2024-04-16 | 上海外高桥造船有限公司 | Ship low-temperature fuel cold energy recycling system and method and ship |
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EP0009387A1 (en) * | 1978-09-18 | 1980-04-02 | Fluor Corporation | Process for obtaining energy during the regasification of liquefied gases |
JPS5930887B2 (en) * | 1979-10-11 | 1984-07-30 | 大阪瓦斯株式会社 | Intermediate heat medium type liquefied natural gas cold power generation system |
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JP4404010B2 (en) * | 2005-05-26 | 2010-01-27 | Jfeエンジニアリング株式会社 | Combined refrigeration generator |
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JP5662313B2 (en) * | 2008-07-15 | 2015-01-28 | クライオスター・ソシエテ・パール・アクシオンス・サンプリフィエ | Conversion of liquefied natural gas |
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-
2019
- 2019-11-26 JP JP2019213558A patent/JP7288842B2/en active Active
-
2020
- 2020-11-26 EP EP20893934.8A patent/EP4035985A4/en active Pending
- 2020-11-26 WO PCT/JP2020/043956 patent/WO2021106984A1/en unknown
- 2020-11-26 KR KR1020227013263A patent/KR20220062651A/en not_active Application Discontinuation
- 2020-11-26 CN CN202080078074.0A patent/CN114651148B/en active Active
Also Published As
Publication number | Publication date |
---|---|
KR20220062651A (en) | 2022-05-17 |
WO2021106984A1 (en) | 2021-06-03 |
CN114651148A (en) | 2022-06-21 |
CN114651148B (en) | 2023-12-01 |
JP7288842B2 (en) | 2023-06-08 |
JP2021085443A (en) | 2021-06-03 |
EP4035985A4 (en) | 2022-11-23 |
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