WO2020050404A1 - 船舶 - Google Patents
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- WO2020050404A1 WO2020050404A1 PCT/JP2019/035190 JP2019035190W WO2020050404A1 WO 2020050404 A1 WO2020050404 A1 WO 2020050404A1 JP 2019035190 W JP2019035190 W JP 2019035190W WO 2020050404 A1 WO2020050404 A1 WO 2020050404A1
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- WIPO (PCT)
- Prior art keywords
- lpg
- service tank
- temperature
- line
- heater
- Prior art date
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Classifications
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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
- B63B11/00—Interior subdivision of hulls
- B63B11/04—Constructional features of bunkers, e.g. structural fuel tanks, or ballast tanks, e.g. with elastic walls
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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
- B63H—MARINE PROPULSION OR STEERING
- B63H21/00—Use of propulsion power plant or units on vessels
- B63H21/12—Use of propulsion power plant or units on vessels the vessels being motor-driven
- B63H21/14—Use of propulsion power plant or units on vessels the vessels being motor-driven relating to internal-combustion engines
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H21/00—Use of propulsion power plant or units on vessels
- B63H21/38—Apparatus or methods specially adapted for use on marine vessels, for handling power plant or unit liquids, e.g. lubricants, coolants, fuels or the like
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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
- 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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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B43/00—Engines characterised by operating on gaseous fuels; Plants including such engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B43/00—Engines characterised by operating on gaseous fuels; Plants including such engines
- F02B43/10—Engines or plants characterised by use of other specific gases, e.g. acetylene, oxyhydrogen
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
- F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
- F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
- F02M21/0203—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels characterised by the type of gaseous fuel
- F02M21/0209—Hydrocarbon fuels, e.g. methane or acetylene
- F02M21/0212—Hydrocarbon fuels, e.g. methane or acetylene comprising at least 3 C-Atoms, e.g. liquefied petroleum gas [LPG], propane or butane
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
- F02M21/08—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for non-gaseous fuels
- F02M21/10—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for non-gaseous fuels for fuels with low melting point, e.g. apparatus having heating means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/20—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines characterised by means for preventing vapour lock
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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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B43/00—Engines characterised by operating on gaseous fuels; Plants including such engines
- F02B43/10—Engines or plants characterised by use of other specific gases, e.g. acetylene, oxyhydrogen
- F02B2043/103—Natural gas, e.g. methane or LNG used as a fuel
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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
- F17C2221/035—Propane butane, e.g. LPG, GPL
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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
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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
- F17C2227/0337—Heat exchange with the fluid by cooling
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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
- F17C2265/066—Fluid distribution for feeding engines for propulsion
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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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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/30—Use of alternative fuels, e.g. biofuels
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
- Y02T70/50—Measures to reduce greenhouse gas emissions related to the propulsion system
- Y02T70/5218—Less carbon-intensive fuels, e.g. natural gas, biofuels
Definitions
- the present invention relates to a ship including a propulsion engine using LPG as fuel.
- the fuel for the propulsion engine is generally fuel oil such as heavy oil or LNG (Liquefied Natural Gas).
- LNG Liquefied Natural Gas
- LPG Liquefied Petroleum Gas
- Patent Document 1 discloses a ship that supplies LPG as liquid from a fuel tank to a propulsion engine.
- LPG is used as a fuel
- a measure against sulfur oxides is not required as compared with fuel oil and there is a merit that a carbon dioxide emission is small, and the specific gravity is larger than LNG, so that a fuel tank can be downsized.
- LNG specific gravity
- LPG When LPG is used as fuel, it is conceivable that the fuel tank and the propulsion engine are connected by a supply line and a return line, and the LPG is circulated between the fuel tank and the engine and the required amount is used in the engine. .
- the LPG When the LPG is circulated as described above, the LPG is heated when passing through the engine. For this reason, it is desirable to divide the fuel tank into an LPG circulation service tank and an LPG holding storage tank.
- the service tank stores a relatively high temperature LPG
- the storage tank stores a relatively low temperature LPG.
- At least the service tank of the storage tank and the service tank is a pressure vessel that can withstand high pressure, and even if the temperature of the LPG in the service tank becomes higher than the atmospheric temperature, the high pressure in the service tank causes the equilibrium state of the LPG. Will be kept.
- the temperature of the LPG in the storage tank may be equal to or lower than the saturation temperature at atmospheric pressure.
- the storage tank is used as a pressure vessel similarly to the service tank, and the LPG is kept in equilibrium by the high pressure in the storage tank. Good.
- LPG is supplied from the storage tank to the service tank through a transfer line connecting them, in an amount corresponding to the fuel consumption of the engine.
- a pump is provided in the above-mentioned supply line. If the temperature of the LPG in the service tank is lower than the ambient temperature, the LPG may vaporize at the inlet of the pump by receiving heat from the atmosphere while flowing through the supply line from the service tank to the pump. In this case, the pump is damaged or its performance is deteriorated. For example, when an LPG having a temperature lower than the ambient temperature is supplied from the storage tank to the service tank, the temperature of the LPG in the service tank may be lower than the ambient temperature.
- an object of the present invention is to provide a ship that can prevent LPG from being vaporized at an inlet of a pump provided in a supply line.
- a ship includes a propulsion engine using LPG as a fuel, and a service tank storing LPG connected to the propulsion engine through a supply line and a return line.
- a storage tank connected to the service tank by a transfer line, storing LPG having a lower temperature than the LPG in the service tank, a pump provided in the supply line, and a pump provided in the transfer line, A heater that heats the LPG supplied from the storage tank to the service tank so that the temperature of the LPG in the service tank becomes higher than the ambient temperature.
- the above-mentioned ship may further include a control device that adjusts a heating amount of the LPG by the heater so that a temperature of the LPG in the service tank becomes higher than an ambient temperature.
- the above-mentioned ship branches off from the transfer line on the upstream side of the heater and joins the transfer line on the downstream side of the heater, a flow rate of the LPG passing through the heater, and the bypass line.
- a distribution mechanism that changes a ratio of a flow rate of the LPG flowing through the line, wherein the control device controls the distribution mechanism to adjust a heating amount of the LPG in the heater.
- the above-mentioned ship further includes a cooler provided in the return line for cooling the LPG returned from the propulsion engine to the service tank, and the control device is configured to control the temperature of the LPG in the service tank to be high. Not only the heating amount of the LPG in the heater but also the cooling amount of the LPG in the cooler may be adjusted so as to be higher than the air temperature. According to this configuration, since the LPG returned from the engine to the service tank is cooled by the cooler, it is possible to prevent the temperature of the LPG in the service tank from becoming too high. Further, by adjusting the cooling amount of the LPG in addition to the heating amount of the LPG, it is possible to cope with a wide range of situations.
- a vessel includes a propulsion engine using LPG as a fuel, a service tank connected to the propulsion engine via a supply line and a return line, storing a LPG, and a transfer line.
- a storage tank connected to a service tank for storing LPG at a lower temperature than the LPG in the service tank, a pump provided on the supply line, and the service provided from the propulsion engine provided on the return line.
- a cooling device that cools the LPG returned to the tank so that the temperature of the LPG in the service tank becomes higher than the ambient temperature.
- the LPG returned from the engine to the service tank is cooled by the cooler, it is possible to suppress the temperature of the LPG in the service tank from becoming too high. Moreover, according to the above configuration, it is possible to prevent the cooling amount of the LPG in the cooler from becoming excessive and the temperature of the LPG in the service tank from becoming lower than the ambient temperature. Thereby, vaporization of LPG at the inlet of the pump can be prevented.
- the above-mentioned ship may further include a control device that adjusts a cooling amount of the LPG in the cooler so that a temperature of the LPG in the service tank becomes higher than an ambient temperature.
- LPG can be prevented from being vaporized at the inlet of the pump provided in the supply line.
- FIG. 5 is a sectional view taken along line VV in FIG. 4. It is an enlarged view of the service tank in the 2nd alternative means. It is a schematic structure figure of a ship concerning the 3rd substitution means. It is a schematic structure figure of the ship concerning a 4th alternative means. It is an enlarged view of the service tank in the 4th alternative means. It is an enlarged view of a service tank of a modification of the fourth alternative means.
- FIG. 1 shows a ship 1 according to an embodiment of the present invention.
- the ship 1 includes a propulsion engine 11 using LPG as fuel, a storage tank 2 for storing LPG, and a service tank 4.
- LPG may be propane gas containing propane as a main component or propane gas containing butane as a main component.
- the engine 11 is connected to the service tank 4 by a supply line 5 and a return line 6.
- LPG circulates between the service tank 4 and the engine 11 through the supply line 5 and the return line 6.
- the service tank 4 is connected to the storage tank 2 by the transfer line 3.
- the capacity of the storage tank 2 is larger than the capacity of the service tank 4.
- the engine 11 is, for example, a diesel cycle or Otto cycle reciprocating engine. Although not shown, the engine 11 includes a main flow path connecting the downstream end of the supply line 5 and the upstream end of the return line 6, and a plurality of fuel injection valves connected in parallel to the main flow path. The fuel injection valve injects LPG as liquid into the air supplied into the cylinder. However, the engine 11 may be a gas turbine engine.
- the supply line 5 is provided with a pump 51, a heater 52, and a shutoff valve 53 in order from the upstream side.
- the number of the pumps 51 may be one or more.
- the heater 52 heats the LPG supplied from the service tank 4 to the engine 11 to a required temperature of the engine 11 (for example, 45 ° C.).
- the upstream end of the supply line 5 is connected to a lower part of the service tank 4.
- the heater 52 is a heat exchanger that performs heat exchange between the heat medium fluid and the LPG.
- the return line 6 is provided with a shutoff valve 61, a first pressure regulating valve 62, a cooler 63, and a second pressure regulating valve 64 in order from the upstream side.
- the positions of the shutoff valve 61 and the first pressure regulating valve 62 may be reversed.
- the cooler 63 cools the LPG returned from the engine 11 to the service tank 4 (the LPG heated by passing through the engine 11) to a predetermined temperature (for example, 40 ° C.). Note that the cooler 63 may be omitted.
- the return line 6 extends to the inside of the service tank 4.
- the cooler 63 is a heat exchanger that performs heat exchange between the heat medium fluid and the LPG.
- the supply line 5 and the return line 6 are connected by a bypass line 71.
- the bypass line 71 branches off from the supply line 5 between the heater 52 and the shut-off valve 53 and joins the return line 6 between the first pressure regulating valve 62 and the cooler 63.
- a shutoff valve 72 is provided in the bypass line 71.
- a flow control valve may be provided in the bypass line 71 instead of the shut-off valve 72.
- the service tank 4 is a pressure vessel that can withstand high pressure.
- the service tank 4 is not covered with a heat insulating material, and the temperature of the LPG in the service tank 4 depends on the ambient temperature, the temperature of the LPG supplied from the storage tank 2, the temperature of the LPG returned from the engine 11, and the like. Change. That is, the high pressure in the service tank 4 keeps the LPG in an equilibrium state. For example, assuming that the temperature of the LPG in the service tank 4 is 0 to 50 ° C., the pressure (saturated vapor pressure) of the gas layer in the service tank 4 is about 0.4 MPa to about 1.8 MPa in gauge pressure. .
- all indications of pressure are gauge pressures.
- the service tank 4 may be covered with a heat insulating material.
- the storage tank 2 is covered with a heat insulating material (not shown) in order to keep the internal LPG at a low temperature.
- This low temperature may be lower than or equal to the saturation temperature at atmospheric pressure (-42 ° C. for propane gas) as long as it is lower than the temperature of LPG in the service tank 4 (more preferably, ambient temperature). It may be higher than the saturation temperature at.
- the storage tank 2 may be a pressure vessel similarly to the service tank 4, and the high pressure in the storage tank 2 may keep the LPG in an equilibrium state.
- a pump 21 is disposed in the storage tank 2.
- the number of the pumps 21 may be one or plural.
- the upstream end of the transfer line 3 described above is connected to the pump 21.
- the transfer line 3 extends to the inside of the service tank 4. However, the pump 21 may be provided outside the storage tank 2 and in the middle of the transfer line 3.
- the LPG is supplied from the storage tank 2 to the service tank 4 through the transfer line 3 in an amount corresponding to the fuel consumption of the engine 11.
- the supply of the LPG may be performed continuously or intermittently.
- the transfer line 3 is provided with a heater 32 for heating the LPG supplied from the storage tank 2 to the service tank 4 to a predetermined temperature (for example, 0 to 45 ° C.).
- the heater 32 is a heat exchanger that performs heat exchange between the heat medium fluid and the LPG.
- a bypass line 33 that bypasses the heater 32 is connected to the transfer line 3.
- the bypass line 33 branches from the transfer line 3 on the upstream side of the heater 32 and joins the transfer line 3 on the downstream side of the heater 32.
- the transfer line 3 is provided with a first flow control valve 31 between the branch point of the bypass line 33 and the heater 32, and the bypass line 33 is provided with a second flow control valve 34.
- the first flow control valve 31 and the second flow control valve 34 constitute a distribution mechanism 35 that changes the ratio of the flow rate of the LPG passing through the heater 32 to the flow rate of the LPG flowing through the bypass line 33.
- a distribution valve three-way valve provided at a branch point of the bypass line 33 in the transfer line 3 is used instead of the first flow control valve 31 and the second flow control valve 34. You may.
- the above-described pump 51 and various valves are controlled by the control device 8. However, in FIG. 1, only some signal lines are drawn for simplification of the drawing.
- the control device 8 is, for example, a computer having a memory such as a ROM and a RAM and a CPU, and a program stored in the ROM is executed by the CPU.
- the control device 8 may be a single device or may be divided into a plurality of devices (for example, an engine control device and a fuel supply control device).
- the control device 8 closes the shutoff valves 53 and 61 while the engine 11 is stopped, and opens the shutoff valves 53 and 61 while the engine 11 is operating. While the engine 11 is stopped, the flow path between the shutoff valves 53 and 61 (the downstream part of the supply line 5, the main flow path of the engine 11 and the upstream part of the return line 6) is purged with an inert gas.
- the control device 8 controls the pump 51 so that the discharge flow rate of the pump 51 changes according to the fuel consumption of the engine 11. For example, when the load of the engine 11 is high, a surplus flow rate, which is the flow rate of the LPG flowing from the engine 11 to the return line 6, is detected by a flowmeter (not shown), and the surplus flow rate is constant with respect to the fuel consumption of the engine 11.
- the pump 51 is controlled so that the ratio becomes as follows. Instead of the surplus flow rate, a supply flow rate which is a flow rate of LPG flowing from the supply line 5 to the engine 11 may be employed. Conversely, when the load on the engine 11 is low, the discharge flow rate of the pump 51 is kept constant.
- the control device 8 opens the shutoff valve 72 and closes the shutoff valve 53 before the operation of the engine 11 until the flow rate of the pump 51 is stabilized.
- the control device 8 closes the shutoff valve 72 and opens the shutoff valve 53.
- the control device 8 opens the shut-off valve 72 to open the shut-off valve 72. Suppress increase in engine supply pressure.
- Control device 8 is electrically connected to first pressure gauge 91 and second pressure gauge 92.
- the first pressure gauge 91 is provided on the supply line 5 downstream of the branch point of the first bypass line 71 and detects the pressure of LPG supplied to the engine 11.
- the second pressure gauge 92 is provided in the return line 6 between the first pressure regulating valve 62 and the second pressure regulating valve 64, and detects the pressure of the LPG after the pressure is reduced by the first pressure regulating valve 62. I do.
- the controller 8 controls the first pressure regulating valve 62 so that the pressure detected by the first pressure gauge 91 becomes the required pressure of the engine 11 (for example, 5 to 6 MPa when the engine 11 is a reciprocating engine of a diesel cycle). Control.
- the control device 8 determines that the pressure detected by the second pressure gauge 92 is lower than the saturated vapor pressure at the assumed maximum temperature. Also, the second pressure regulating valve 64 is controlled so as to have a high set value (for example, 3.5 MPa).
- the control device 8 is also electrically connected to the first thermometer 81 and the second thermometer 82.
- the first thermometer 81 detects an atmospheric temperature.
- the second thermometer 82 is provided in the service tank 4 and detects the temperature of the LPG in the service tank 4.
- the controller 8 controls the first flow control valve 31 and the first flow control valve 31 so that the temperature of the LPG in the service tank 4 detected by the second thermometer 82 becomes higher than the atmospheric temperature detected by the first thermometer 81.
- the second flow control valve 34 distributed mechanism 35
- the heating amount of LPG in the heater 32 is adjusted.
- an estimated value such as a weather forecast may be used as the large air temperature.
- the heating amount of the LPG of the heater 32 is appropriately adjusted. It is suppressed that the temperature becomes lower than the ambient temperature. Thus, LPG vaporization at the inlet of the pump 51 can be prevented.
- the temperature of the LPG in the service tank 4 can be prevented from becoming too high.
- thermometer 83 detects a transfer temperature that is the temperature of the LPG after the LPG that has passed through the heater 32 and the LPG that has flowed through the bypass line 33 are mixed.
- the control device 8 first determines the service flow rate from the return flow rate, which is the flow rate of LPG flowing from the return line 6 to the service tank 4, the transfer flow rate, which is the flow rate of LPG flowing from the transfer line 3 to the service tank 4, and the ambient temperature.
- the target transfer temperature required for the temperature of the LPG in the tank 4 to become higher than the ambient temperature is calculated.
- the control device 8 controls the first flow control valve 31 and the second flow control valve 34 (distribution mechanism 35) such that the transfer temperature detected by the second thermometer 83 becomes the target transfer temperature.
- the heater 32 is a heat exchanger that exchanges heat between the heat medium fluid and the LPG, and when the temperature of the heat medium fluid supplied to the heater 32 can be changed, the bypass line 33 and the flow control valve 31 and 34 may be omitted, and the control device 8 may adjust the heating amount of the LPG in the heater 32 by changing the temperature of the heating medium fluid supplied to the heater 32.
- control device 8 adjusts not only the heating amount of the LPG in the heater 32 but also the cooling amount of the LPG in the cooler 63 so that the temperature of the LPG in the service tank 4 becomes higher than the ambient temperature. Is also good.
- the cooling amount of the LPG in addition to the heating amount of the LPG, it is possible to cope with a wide range of situations.
- a bypass line is connected to the return line 6 so as to bypass the cooler 63, and the flow rate of the LPG passing through the cooler 63 and the bypass line
- the cooling amount of the LPG in the cooler 63 may be adjusted by changing the ratio of the flow rate of the LPG flowing through the LPG.
- the cooler 63 is a heat exchanger that exchanges heat between the heat medium fluid and the LPG, and when the temperature of the heat medium fluid supplied to the cooler 63 can be changed, the heat supplied to the cooler 63 can be changed.
- the cooling amount of the LPG in the cooler 63 may be adjusted by changing the temperature of the medium fluid.
- the LPG heating amount in the heater 32 When adjusting not only the LPG heating amount in the heater 32 but also the LPG cooling amount in the cooler 63, for example, the LPG heating amount in the heater 32 In addition, the cooling amount of the LPG in the cooler 63 may be reduced.
- control device 8 adjusts only the amount of cooling of the LPG in the cooler 63 without adjusting the amount of heating of the LPG in the heater 32 so that the temperature of the LPG in the service tank 4 becomes higher than the ambient temperature. May be adjusted. According to this configuration, it is possible to prevent the cooling amount of the LPG in the cooler 63 from becoming excessive and the temperature of the LPG in the service tank 4 from becoming lower than the ambient temperature. Thus, LPG vaporization at the inlet of the pump 51 can be prevented. Needless to say, when only the cooling amount of the LPG in the cooler 63 is adjusted, the heater 32 can be omitted.
- the service tank 4 has a vertically long cylindrical shape, but the service tank 4 may have other shapes such as a horizontally long cylindrical shape, a spherical shape, a cubic shape, and a rectangular parallelepiped shape. .
- the shape of the storage tank 2 can be arbitrarily changed.
- the relatively low temperature LPG supplied through the transfer line 3 supply LPG
- the relatively high temperature LPG returned through the return line 6 return LPG
- the return LPG having a relatively high temperature flows out of the service tank 4 through the supply line 5
- the LPG is introduced at the inlet of the pump 51 provided in the supply line 5. May vaporize. In this case, the pump 51 is damaged or performance is deteriorated.
- first to fourth alternative means as described below are conceivable.
- the same components as those of the above-described embodiment are denoted by the same reference numerals, and redundant description will be omitted.
- FIG. 3 shows a boat 1A according to a first alternative means.
- the marine vessel 1A is different from the marine vessel 1 shown in FIG. 1 in that the marine vessel 1A does not include the bypass line 33, the first flow control valve 31, and the second flow control valve.
- the marine vessel 1A includes a bypass line 33, a first flow control valve 31, and a second flow control valve 34, and the first flow control valve 31 and the second flow control valve are different from those in the first embodiment. It may be controlled similarly.
- a special measure is taken for the service tank 4.
- the service tank 4 will be described in more detail with reference to FIGS. 4 and 5.
- a downstream portion of the return line 6 extending from the outside of the service tank 4 to the inside and a downstream side of the transfer line 3 extending from the outside to the inside of the service tank 4.
- the portion is configured such that the LPG flowing from the downstream end of the return line 6 and the downstream end of the transfer line 3 forms a swirling flow.
- a mortar-shaped (inverted conical) guide member 45 whose diameter decreases downward is arranged in the service tank 4 (more precisely, in the liquid layer 40 made of LPG).
- the downstream end of the return line 6 and the downstream end of the transfer line 3 are located above the guide member 45, and the upstream end of the supply line 5 is connected to the service tank 4 below the guide member 45.
- the downstream portion of the return line 6 is located in the circumferential direction of the guide member 45 and slightly downward with respect to the horizontal direction so that the LPG flowing from the downstream end of the return line 6 collides with the upper surface of the guide member 45 at an angle. It is bent.
- the downstream portion of the transfer line 3 is arranged in the circumferential direction of the guide member 45 and in the horizontal direction so that the LPG flowing from the downstream end of the transfer line 3 collides obliquely with the upper surface of the guide member 45. It is bent slightly downward. Therefore, the LPG flowing from the downstream end of the return line 6 and the downstream end of the transfer line 3 forms a swirling flow along the upper surface of the guide member 45.
- the return LPG having a relatively high temperature (the LPG returned to the service tank 4 through the return line 6) and the supply LPG having a relatively low temperature (the service tank 4 having the service tank 4 through the transfer line 3).
- LPG supplied to the LPG are mixed by the swirling flow. Thereby, the temperature of the LPG in the service tank 4 becomes uniform, and the vaporization of the LPG at the inlet of the pump 51 can be prevented.
- the guide member 45 is disposed in the service tank 4, but the downstream portion of the return line 6 and the downstream portion of the transfer line 3 are bent in the circumferential direction of the guide member 45 and in the horizontal direction. In this case, the guide member 45 may be omitted. However, if the guide member 45 is provided as in the first alternative means, a swirling flow can be reliably formed above the guide member 45.
- downstream end of the return line 6 is located below the downstream end of the transfer line 3 in the service tank 4.
- the partition member 46 is disposed in the service tank 4.
- the partition member 46 partitions the liquid layer 40 made of LPG (the gas layer is made of PG vaporized from LPG) into a first region 41 and a second region 42.
- the upstream end of the supply line 5 communicates with the first area 41, and the downstream end of the return line 6 and the downstream end of the transfer line 3 are located in the second area 42.
- the partition member 46 is a plate parallel to the vertical direction, and the first area 41 and the second area 42 are arranged in the horizontal direction.
- the partition member 46 may be a plate parallel to the horizontal direction, and the first region 41 may be located below the second region 42.
- the partition member 46 may be a perforated plate such as a mesh material or a punched metal.
- the partition member 46 may have a cylindrical shape that extends in the vertical direction such that the first area 41 is located at the center of the service tank 4 and the second area 42 is located around the first area 41.
- the return LPG is returned in the service tank 4 as shown by an arrow in FIG. 6 due to the density difference between the return LPG having a relatively high temperature and the supply LPG having a relatively low temperature. rises and the supplied LPG falls. Therefore, the return LPG and the supply LPG are mixed by convection. Thereby, the temperature of the LPG in the service tank 4 becomes uniform, and the vaporization of the LPG at the inlet of the pump 51 can be prevented.
- FIG. 7 shows a boat 1B according to the third alternative means.
- the return line 6 and the transfer line merge with each other outside the service tank 4. For this reason, the downstream portion of the return line 6 and the downstream portion of the transfer line 3 form a common flow path extending from the outside to the inside of the service tank 4.
- the return line 6 joins the transfer line 3 on the downstream side of the second pressure regulating valve 64.
- the return line 6 is provided with a check valve 65 between the second pressure regulating valve 64 and the junction of the transfer line 3.
- the transfer line 3 joins the return line 6 on the downstream side of the heater 32.
- the transfer line 3 is provided with a check valve 36 between the heater 32 and the junction of the return line 6.
- the mode of merging the return line 6 and the transfer line may be such that three pipes are connected in a T-shape or a Y-shape.
- a container may be provided at the junction of the return line 6 and the transfer line, and three pipes may be connected to this container.
- the return LPG having a relatively high temperature and the supply LPG having a relatively low temperature flow into the service tank 4 after being mixed with each other. Thereby, the temperature of the LPG in the service tank 4 becomes uniform, and the vaporization of the LPG at the inlet of the pump 51 can be prevented.
- FIG. 8 shows a ship 1C according to the fourth alternative means.
- This ship 1C includes a bypass line 33, a first flow control valve 31, and a second flow control valve 34, as in the above embodiment.
- the first flow control valve 31 and the second flow control valve 34 are provided with the distribution mechanism 35 that changes the ratio of the flow rate of the LPG passing through the heater 32 to the flow rate of the LPG flowing through the bypass line 33. Is configured.
- a distribution valve three-way valve provided at a branch point of the bypass line 33 in the transfer line 3 is used instead of the first flow control valve 31 and the second flow control valve 34. You may.
- the partition member 47 is disposed in the service tank 4.
- the partition member 47 partitions the liquid layer 40 made of LPG (the gas layer is made of PG vaporized from LPG) into a first region 41 and a second region 42.
- the upstream end of the supply line 5 communicates with the first area 41, the downstream end of the transfer line 3 is located in the first area 41, and the downstream end of the return line 6 is located in the second area 42.
- the partition member 47 is a horizontal perforated plate
- the first region 41 is a region below the partition member 47
- the second region is a region above the partition member 47.
- a perforated plate for example, a mesh material or a punched metal is used.
- Control device 8 is also electrically connected to first thermometer 84 and second thermometer 85.
- the first thermometer 84 is provided in the service tank 4 and detects the temperature of the upper part of the liquid layer 40 in the service tank 4 (in the present embodiment, the second area 42).
- the temperature of the upper part of the liquid layer 40 is equal to or lower than the temperature of the liquid level in the service tank 4 due to the temperature distribution (density distribution) in the service tank 4.
- the second thermometer 85 is provided in the transfer line 3 on the downstream side of the junction of the bypass line 33, and the LPG flowing from the transfer line 3 to the service tank 4 (the LPG flowing through the heater 32 and the LPG flowing through the bypass line 33). The temperature of the LPG after the mixed LPG is detected.
- the controller 8 keeps the temperature of the LPG detected by the second thermometer 85 lower than the temperature of the LPG detected by the first thermometer 84 (a temperature equal to or lower than the temperature of the liquid level in the service tank 4).
- the heating amount of the LPG in the heater 32 is adjusted so that the LPG is heated.
- the return LPG (the service tank through the return line 6)
- the supply LPG (LPG supplied to the service tank 4 through the transfer line 3) having a lower temperature than the LPG returned to the supply tank 4 preferentially flows out of the service tank 4 through the supply line 5.
- LPG vaporization at the inlet of the pump 51 can be prevented.
- the service tank 4 can be made of a general steel material instead of a special steel material for low temperature (for example, a steel material having toughness even at ⁇ 46 ° C. or lower).
- the heating amount of the supplied LPG is adjusted such that the temperature of the LPG flowing from the transfer line 3 to the service tank 4 is kept lower than the temperature of the upper part of the liquid layer 40 in the service tank 4.
- the effect that the above-mentioned low-temperature supply LPG preferentially flows out can be reliably obtained.
- the partition member 47 does not necessarily have to be a horizontal perforated plate, and may have an inverted L-shaped cross section as shown in FIG. 10 or may have another shape. Alternatively, the partition member 475 itself may be omitted.
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Abstract
Description
本発明は上述した実施形態に限定されるものではなく、本発明の要旨を逸脱しない範囲で種々の変形が可能である。
前記実施形態では、ポンプ51の入口でのLPGの気化を防止するために、サービスタンク4内のLPGの温度を大気温よりも高くする手段が採用されていた。しかし、ポンプ51の入口でのLPGの気化を防止するためには、別の手段を採用することも可能である。
図3に、第1代替手段に係る船舶1Aを示す。この船舶1Aが、図1に示す船舶1と異なるのは、バイパスライン33、第1流量制御弁31および第2流量制御弁34を含まないことである。ただし、第1実施形態と同様に、船舶1Aがバイパスライン33、第1流量制御弁31および第2流量制御弁34を含み、第1流量制御弁31および第2流量制御弁が前記実施形態と同様に制御されてもよい。また、第1代替手段では、サービスタンク4に特別な対策がなされている。
第1代替手段では、サービスタンク4内にガイド部材45が配置されていたが、返送ライン6の下流側部分および移送ライン3の下流側部分をガイド部材45の周方向であって水平方向に折り曲げた場合には、ガイド部材45が省略されてもよい。ただし、第1代替手段のようにガイド部材45が設けられていれば、ガイド部材45の上方で旋回流を確実に形成することができる。
次に、図6を参照して、第2代替手段に係る船舶を説明する。第2代替手段の船舶が第1代替手段の船舶1Aと異なるのは、サービスタンク4内の構造だけである。
仕切部材46が無くても返送LPGと供給LPGとが対流によって混ぜ合わされるので、仕切部材46は省略されてもよい。ただし、仕切部材46が設けられていれば、第2領域42内で返送LPGと供給LPGとを十分に混ぜ合わせることができる。
図7に、第3代替手段に係る船舶1Bを示す。第3代替手段では、返送ライン6と移送ラインとがサービスタンク4の外部で互いに合流している。このため、返送ライン6の下流側部分と移送ライン3の下流側部分は、サービスタンク4の外部から内部へ延びる共通の流路となっている。
図8に、第4代替手段に係る船舶1Cを示す。この船舶1Cは、前記実施形態と同様に、バイパスライン33、第1流量制御弁31および第2流量制御弁34を含む。前記実施形態で説明したように、第1流量制御弁31および第2流量制御弁34は、加熱器32を通過するLPGの流量とバイパスライン33を流れるLPGの流量の比率を変更する分配機構35を構成する。
仕切部材47は、必ずしも水平な多孔板である必要はなく、図10に示すような断面逆L字状の形状を有してもよいし、その他の形状を有してもよい。あるいは、仕切部材475自体が省略されてもよい。
11 推進用エンジン
2 ストレージタンク
3 移送ライン
32 加熱器
33 バイパスライン
35 分配機構
4 サービスタンク
5 供給ライン
51 ポンプ
6 返送ライン
63 冷却器
8 制御装置
Claims (6)
- LPGを燃料とする推進用エンジンと、
供給ラインおよび返送ラインにより前記推進用エンジンと接続された、LPGを貯留するサービスタンクと、
移送ラインにより前記サービスタンクと接続された、前記サービスタンク内のLPGよりも低温のLPGを貯留するストレージタンクと、
前記供給ラインに設けられたポンプと、
前記移送ラインに設けられた、前記ストレージタンクから前記サービスタンクへ供給されるLPGを、前記サービスタンク内のLPGの温度が大気温よりも高くなるように加熱する加熱器と、
を備える、船舶。 - 前記サービスタンク内のLPGの温度が大気温よりも高くなるように、前記加熱器でのLPGの加熱量を調整する制御装置をさらに備える、請求項1に記載の船舶。
- 前記加熱器の上流側で前記移送ラインから分岐し、前記加熱器の下流側で前記移送ラインに合流するバイパスラインと、
前記加熱器を通過するLPGの流量と前記バイパスラインを流れるLPGの流量の比率を変更する分配機構と、をさらに備え、
前記制御装置は、前記分配機構を制御して前記加熱器でのLPGの加熱量を調整する、請求項2に記載の船舶。 - 前記返送ラインに設けられた、前記推進用エンジンから前記サービスタンクへ返送されるLPGを冷却する冷却器をさらに備え、
前記制御装置は、前記サービスタンク内のLPGの温度が大気温よりも高くなるように、前記加熱器でのLPGの加熱量だけでなく前記冷却器でのLPGの冷却量も調整する、請求項2または3に記載の船舶。 - LPGを燃料とする推進用エンジンと、
供給ラインおよび返送ラインにより前記推進用エンジンと接続された、LPGを貯留するサービスタンクと、
移送ラインにより前記サービスタンクと接続された、前記サービスタンク内のLPGよりも低温のLPGを貯留するストレージタンクと、
前記供給ラインに設けられたポンプと、
前記返送ラインに設けられた、前記推進用エンジンから前記サービスタンクへ返送されるLPGを、前記サービスタンク内のLPGの温度が大気温よりも高くなるように冷却する冷却器と、
を備える、船舶。 - 前記サービスタンク内のLPGの温度が大気温よりも高くなるように、前記冷却器でのLPGの冷却量を調整する制御装置をさらに備える、請求項5に記載の船舶。
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KR20160031662A (ko) * | 2014-09-12 | 2016-03-23 | 현대중공업 주식회사 | Bog를 연료로 사용하는 부유식 발전선 |
KR20170009577A (ko) * | 2015-07-17 | 2017-01-25 | 대우조선해양 주식회사 | 엔진을 포함하는 선박 |
KR20180062240A (ko) * | 2016-11-30 | 2018-06-08 | 한국항공우주연구원 | 연료 공급 장치 |
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KR102404713B1 (ko) | 2022-06-08 |
CN112638763B (zh) | 2023-08-22 |
JP7049469B2 (ja) | 2022-04-06 |
KR20210048520A (ko) | 2021-05-03 |
SG11202102112QA (en) | 2021-04-29 |
JPWO2020050404A1 (ja) | 2021-08-30 |
CN112638763A (zh) | 2021-04-09 |
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