WO2024069980A1 - 多重殻タンク及び船舶 - Google Patents
多重殻タンク及び船舶 Download PDFInfo
- Publication number
- WO2024069980A1 WO2024069980A1 PCT/JP2022/036844 JP2022036844W WO2024069980A1 WO 2024069980 A1 WO2024069980 A1 WO 2024069980A1 JP 2022036844 W JP2022036844 W JP 2022036844W WO 2024069980 A1 WO2024069980 A1 WO 2024069980A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- tank
- annular plate
- shell
- cylindrical
- protruding direction
- 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.)
- Ceased
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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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D90/00—Component parts, details or accessories for large containers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D90/00—Component parts, details or accessories for large containers
- B65D90/02—Wall construction
- B65D90/028—Wall construction hollow-walled, e.g. double-walled with spacers
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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
- F17C13/004—Details of vessels or of the filling or discharging of vessels for large storage vessels not under pressure
-
- 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
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/025—Bulk storage in barges or on ships
-
- 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
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
-
- 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
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0147—Shape complex
- F17C2201/0157—Polygonal
-
- 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
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/052—Size large (>1000 m3)
-
- 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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0375—Thermal insulations by gas
- F17C2203/0379—Inert
-
- 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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0375—Thermal insulations by gas
- F17C2203/0383—Air
-
- 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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0626—Multiple walls
-
- 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
- F17C2221/01—Pure fluids
- F17C2221/012—Hydrogen
-
- 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
- F17C2221/01—Pure fluids
- F17C2221/014—Nitrogen
-
- 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
- F17C2221/01—Pure fluids
- F17C2221/016—Noble gases (Ar, Kr, Xe)
- F17C2221/017—Helium
-
- 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
-
- 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
-
- 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
-
- 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
Definitions
- This disclosure relates to a multi-shell tank and a vessel equipped therewith.
- Multi-shell tanks have been known as containers for storing low-temperature liquids such as liquefied gas.
- Such multi-shell tanks include an inner tank and at least one outer tank that surrounds the inner tank, with a heat-insulating layer between the tanks that suppresses heat input to the inner tank.
- Patent Document 1 discloses this type of multi-shell tank.
- the double-shell tank disclosed in Patent Document 1 is installed on a liquefied gas carrier.
- This double-shell tank comprises an inner tank and an outer tank.
- the inner tank has an inner tank body that stores liquefied gas, and an inner tank dome that protrudes upward from the inner tank body.
- the outer tank has an outer tank body that surrounds the inner tank body, and an outer tank dome that surrounds the inner tank dome.
- the inner tank dome and outer tank dome have a concentrated arrangement of penetrations for various piping such as liquefied gas transfer piping and electrical piping.
- the inner tank and outer tank dome are connected by being connected with a connecting member.
- This disclosure has been made in consideration of the above circumstances, and its purpose is to provide a multi-shell tank having an inner tank and an outer tank surrounding the inner tank, and equipped with a dome where piping, etc. are concentrated, which can simplify the internal and external access routes.
- a multi-shell tank comprises: an inner tank for containing liquefied gas; An outer tank surrounding the inner tank; a dome joined to the inner tank and the outer tank, a portion of which protrudes from the outer tank in a protruding direction;
- the dome has a first body portion joined to the inner tank, a second body portion positioned away from the first body portion in the protruding direction and joined to the outer tank, and a connecting portion that connects the first body portion and the second body portion and is elastically deformable in response to relative displacement of the first body portion with respect to the second body portion, and the inner space of the first body portion, the inner space of the connecting portion, and the inner space of the second body portion are connected to each other.
- a ship according to one embodiment of the present disclosure comprises a hull and the multi-shell tank supported by the hull.
- the access route between inside and outside the tank can be simplified.
- FIG. 1 is a schematic vertical cross-sectional view of a vessel equipped with a multi-shell tank according to one embodiment of the present disclosure.
- FIG. 2 is an enlarged vertical cross-sectional view of the top of a multi-shell tank.
- FIG. 3 is an enlarged cross-sectional view of the top of the multi-shell tank according to the first modified example.
- FIG. 4 is a diagram for explaining the dimensions of each part of the connecting portion.
- FIG. 5 is an enlarged vertical cross-sectional view of the top of the multi-shell tank after deformation.
- FIG. 6 is an enlarged cross-sectional view of the top of a multi-shell tank showing a deformation-permitting portion according to the first modified example.
- FIG. 1 is a schematic vertical cross-sectional view of a vessel equipped with a multi-shell tank according to one embodiment of the present disclosure.
- FIG. 2 is an enlarged vertical cross-sectional view of the top of a multi-shell tank.
- FIG. 3 is an enlarged cross-section
- FIG. 7 is an enlarged cross-sectional view of the top of a multi-shell tank showing a deformation-permitting portion according to the second modification.
- FIG. 8 is an enlarged cross-sectional view of the top of a multi-shell tank showing a deformation-permitting portion according to the third modified example.
- FIG. 9 is an enlarged cross-sectional view of the top of a multi-shell tank showing a deformation-permitting portion according to the fourth modified example.
- inside refers to the side closer to the center of the space inside the inner tank 3 of the multi-shell tank 2
- outside refers to the side farther from the center of the space inside the inner tank 3 of the multi-shell tank 2.
- FIG. 1 is a schematic vertical cross-sectional view of a ship 1 equipped with a multi-shell tank 2 according to one embodiment of the present disclosure.
- the ship 1 comprises at least one multi-shell tank 2 and a hull 11 supporting the multi-shell tank 2.
- the multi-shell tank 2 contains low-temperature liquefied gas. Examples of liquefied gas include LNG, liquefied nitrogen, liquefied hydrogen, and liquefied helium.
- the ship 1 is a liquefied gas carrier that transports liquefied gas.
- the multi-shell tank 2 according to this embodiment is a loading tank that contains liquefied gas as cargo, but the multi-shell tank 2 may also be a fuel tank.
- the multi-shell tank 2 includes an inner tank 3, an outer tank 4 surrounding the inner tank 3, and a dome 6 penetrating the inner tank 3 and the outer tank 4 in a protruding direction X.
- the protruding direction X is the vertical direction.
- the multi-shell tank 2 according to this embodiment includes a double tank, the inner tank 3 and the outer tank 4, but the multi-shell tank 2 may include three or more tanks.
- the outer tank 4 is surrounded by a tank cover 12 that covers the top, and a retaining wall 14 that covers the sides and bottom.
- a retaining space 53 between the outer tank 4 and the tank cover 12 and the retaining wall 14 is filled with air or an inert gas.
- the top of the dome 6 protrudes upward and is exposed beyond the tank cover 12.
- the inner tank 3 is a container for storing liquefied gas, and has a storage space 51 inside in which the liquefied gas is stored.
- a pipe tower 20 extending in the protruding direction X is arranged in the storage space 51.
- a pump 21 is arranged at the bottom of the pipe tower 20.
- the upper part of the pipe tower 20 is joined to the lower part of the dome 6.
- the top of the inner tank 3 is joined to the inner tank joint 61 of the dome 6.
- the top of the outer tank 4 is joined to the outer tank joint 62 of the dome 6.
- the outer tank joint 62 is located above the inner tank joint 61.
- the inner tank 3 and the outer tank 4 are spaced apart in the radial direction of the multi-shell tank 2.
- An airtight inner/outer tank gap 52 is formed between the inner tank 3 and the outer tank 4, and a heat insulating layer made of a heat insulating material or the like is disposed between the inner and outer tanks 52.
- the inner/outer tank gap 52 is filled with an inter-tank gas.
- the inter-tank gas is, for example, a gas having a boiling point equal to or higher than the boiling point of the liquefied gas stored in the storage space 51.
- the vaporized gas of the liquefied gas in the storage space 51 is used as the inter-tank gas. In this way, when the gas filled in the storage space 51 and the inner/outer tank gap 52 is the same, the inner/outer tank gap 52 may be connected to the inner/outer tank gap 52 in the inner tank 3.
- FIG. 2 is an enlarged vertical cross-sectional view of the top of the multi-shell tank 2.
- the dome 6 has a first body portion 65, a second body portion 66, a roof portion 67, and a connecting portion 68.
- the first body 65 has a cylindrical shape, and an inner tank joint 61 is provided on the first body 65.
- the inner tank 3 is joined to the inner tank joint 61, and the movement of the first body 65 is restrained by the inner tank 3.
- the second body 66 has a cylindrical shape, and an outer tank joint 62 is provided on the second body 66.
- the outer tank 4 is joined to the outer tank joint 62, and the movement of the second body 66 is restrained by the outer tank 4.
- the upper part of the second body 66 is closed by a roof portion 67.
- the first body 65 and the second body 66 are cylindrical, but this is not limited thereto, and the first body 65 and the second body 66 may be cylindrical.
- the second body 66 is arranged above the first body 65, and the first body 65 and the second body 66 are spaced apart in the protruding direction X.
- the gap between the first body 65 and the second body 66 is connected to the space between the inner and outer tanks 52 of the inner tank 3 and the outer tank 4.
- the connecting portion 68 connects the first body portion 65 and the second body portion 66 so that relative displacement between the first body portion 65 restrained to the inner tank 3 and the second body portion 66 restrained to the outer tank 4 is permitted.
- the entirety or a part of the connecting portion 68 is disposed inside the dome 6.
- the connecting portion 68 includes a first annular plate 71, a second annular plate 72, and a cylindrical body 73.
- the connecting portion 68 is interposed between the inner tank 3 and the outer tank 4, and transmits load between the inner tank 3 and the outer tank 4.
- the first annular plate 71 is a hollow circular flat plate having an outer diameter substantially the same as or slightly smaller than that of the first body 65.
- the first annular plate 71 has a main surface that is approximately perpendicular to the protruding direction X when the first annular plate 71 is not deformed.
- the outer edge of the first annular plate 71 is joined to the upper end of the first body 65.
- the outer edge of the first annular plate 71 may be joined to the inner peripheral surface of the first body 65. Since the movement of the first body 65 is restrained by the inner tank 3, the movement of the outer edge of the first annular plate 71 is also restrained by the inner tank 3.
- the second annular plate 72 is a hollow circular flat plate having an outer diameter substantially the same as or slightly smaller than that of the second body 66.
- the second annular plate 72 has a main surface that is approximately perpendicular to the protruding direction X when the second annular plate 72 is not deformed.
- the outer edge of the second annular plate 72 is joined to the inner peripheral surface of the second body 66.
- the outer edge of the second annular plate 72 may be joined to the lower end of the second body 66. Since the movement of the second body 66 is restrained by the outer tank 4, the movement of the outer edge of the second annular plate 72 is also restrained by the outer tank 4.
- the first annular plate 71 and the second annular plate 72 are spaced apart in the protruding direction X.
- the first body portion 65 and the second body portion 66 have substantially the same outer diameter, and therefore the first annular plate 71 and the second annular plate 72 have substantially the same outer diameter.
- the outer diameters of the first body portion 65 and the second body portion 66 may be different, and the outer diameters of the first annular plate 71 and the second annular plate 72 may be different from each other.
- the cylindrical body 73 is a cylindrical member extending in the protruding direction X.
- the outer diameter of the cylindrical body 73 is smaller than the inner diameters of the first body portion 65 and the second body portion 66, and the cylindrical body 73 is disposed inside the first body portion 65 and the second body portion 66.
- the outer diameter of the cylindrical body 73 is substantially the same as the inner diameters of the first annular plate 71 and the second annular plate 72.
- the inner edge portions of the first annular plate 71 and the second annular plate 72, which are separated in the protruding direction X, are connected by the cylindrical body 73.
- the connecting portion 68 formed by the first annular plate 71, the cylindrical body 73, and the second annular plate 72 has a C-shaped cross section parallel to the protruding direction X that opens toward the outer periphery.
- the connecting portion 68 has a higher elastic deformation ability while reducing the radial dimension.
- the outer diameter of the first annular plate 71 and the inner diameter of the second annular plate 72 may be substantially the same, the cylindrical body 73 may connect the outer edge of the first annular plate 71 and the inner edge of the second annular plate 72, and the first annular plate 71, the cylindrical body 73, and the second annular plate 72 may form the connecting portion 68 having a crank-shaped cross section parallel to the protruding direction X.
- the inner diameter of the first annular plate 71 and the outer diameter of the second annular plate 72 may be substantially the same, the inner edge of the first annular plate 71 and the outer edge of the second annular plate 72 may be connected by the cylindrical body 73, and the first annular plate 71, the cylindrical body 73, and the second annular plate 72 may form the connecting portion 68 having a crank-shaped cross section parallel to the protruding direction X.
- the upper end of the cylindrical body 73 is joined to the inner edge of the second annular plate 72, and the lower end of the cylindrical body 73 is joined to the inner edge of the first annular plate 71.
- the cylindrical body 73, the first annular plate 71, and the second annular plate 72 are joined so as to be approximately perpendicular in the vertical cross section of the multi-shell tank 2.
- the corners of at least one of the connection parts between the cylindrical body 73 and the first annular plate 71 and the second annular plate 72 may be rounded.
- the cylinder 73 and the first annular plate 71 are connected via a ring member 70 having an arc-shaped vertical cross section.
- the cross section of the connection between the cylinder 73 and the first annular plate 71 in the protruding direction X is smoothly curved, and stress concentration at the connection is suppressed.
- the cylinder 73 and the second annular plate 72 are connected via a ring member 70 having an arc-shaped cross section in the protruding direction X.
- the vertical cross section of the connection between the cylinder 73 and the second annular plate 72 is smoothly curved, and stress concentration at the connection is suppressed.
- FIG. 1 the example shown in FIG.
- the first annular plate 71 and the first body 65 are connected via a ring member 70 having an arc-shaped cross section in the protruding direction X.
- the corners of the connection between the connecting part 68 and the first body 65 or the second body 66 may also be rounded.
- the first annular plate 71 is disposed between the inner tank joint 61 and the outer tank joint 62 in the protruding direction X.
- the outer peripheral space 74 of the cylinder 73 surrounded by the first annular plate 71, the second annular plate 72, and the cylinder 73 is connected to the space between the inner and outer tanks 52.
- the second annular plate 72 is disposed farther away from the inner tank joint 61 in the protruding direction X than the outer tank joint 62.
- the outer peripheral space 74 of the cylinder 73 has an area separated from the exposed or retained space 53 only by the second body 66 of the dome 6.
- the outer peripheral space 74 connected to the inner and outer tank space 52 can be used as a wiring space for the inter-tank piping 92 (or inter-tank wiring) passing through the inner and outer tank space 52.
- the inter-tank piping 92 is led from the inner and outer tank space 52 to the outer peripheral space 74 of the cylinder 73, and is led to the exposure through the penetration part of the second body part 66 of the dome 6.
- the inter-tank piping 92 is led directly to the exposure through the space connected to the inner and outer tank space 52 and the inner and outer tank space 52, without passing through the storage space 51 or the holding space 53.
- the penetration part through which the inter-tank piping 92 passes through in the dome 6 may be subjected to airtight construction to ensure airtightness between the inner and outer tank space 52, or heat insulation construction similar to that of the tank.
- inter-tank wiring may be laid in the same manner as the inter-tank piping 92.
- the inner space of the first body 65, the inner space of the connecting portion 68, and the inner space of the second body 66 (excluding the portion where the connecting portion 68 is located on the inner periphery) are connected to each other, forming a space extending in the protruding direction X.
- the in-tank piping 91 passed through the pipe tower 20 is passed through a space extending in the protruding direction X inside the dome 6 that is connected to the pipe tower 20, and is led to the exposure through the second body 66 or the roof portion 67 of the dome 6.
- an in-tank wiring may be laid in the same manner as the in-tank piping 91. In this way, the penetrations of the in-tank piping 91 and the inter-tank piping 92 are arranged in a concentrated manner in the dome 6, and each of the in-tank piping 91 and the inter-tank piping 92 is led out of the tank through one penetration arranged in the dome 6.
- the cylindrical body 73 has a first cylindrical portion 731, a second cylindrical portion 732, and a deformable portion 7 arranged between the first cylindrical portion 731 and the second cylindrical portion 732.
- the deformable portion 7 is elastically deformable in response to the relative displacement of the second cylindrical portion 732 with respect to the first cylindrical portion 731.
- the deformable portion 7 is composed of a combination of multiple ring plates 7a, or a combination of a ring plate 7a and a third cylindrical portion 7b.
- the ring plate 7a is a hollow circular flat member having a main surface that is approximately perpendicular to the protruding direction X when not deformed.
- the third cylindrical portion 7b is a cylindrical member that extends substantially parallel to the protruding direction X.
- the ring plate 7a and the third cylindrical portion 7b have a thickness of, for example, 10 mm or more and 60 mm or less.
- a cylindrical body 73 including such a deformable portion 7 can still transmit load between the first annular plate 71 and the second annular plate 72.
- the deformation-permitting portion 7 is composed of a pair of ring plates 7a spaced apart in the protruding direction X, and a third tubular portion 7b that connects the pair of ring plates 7a in the protruding direction X.
- the inner edges of the pair of ring plates 7a are joined to the tubular body 73.
- the outer edges of the pair of ring plates 7a are joined to the third tubular portion 7b.
- the pair of ring plates 7a are joined in such a manner that the third tubular portion 7b is sandwiched between them.
- the arrangement of the deformation-permitting portion 7 in the cylindrical body 73 is not particularly limited, but it is desirable that the joints of the members are not extremely close to each other.
- the first end 73a of the cylindrical body 73 joined to the first annular plate 71 and the deformation-permitting portion 7 are separated by H1 in the protruding direction X.
- H1 is a value that does not cause the joint between the first annular plate 71 and the cylindrical body 73 to be narrow, and is not particularly limited, but is 500 mm or more.
- the second end 73b of the cylindrical body 73 joined to the second annular plate 72 and the deformation-permitting portion 7 are separated by H2 in the protruding direction X.
- H2 is a value that does not cause the joint between the second annular plate 72 and the cylindrical body 73 to be narrow, and is not particularly limited, but is 500 mm or more.
- the dimension of the third cylindrical portion 7b in the protruding direction X i.e., the distance between the pair of ring plates 7a, is H3.
- H3 is a value that ensures that the joint between the ring plate 7a and the third cylindrical portion 7b is not narrow, and is not particularly limited, but is 500 mm or more.
- the outer wall of the cylinder 73 including the deformable portion 7 and the inner wall of the second body portion 66 of the dome 6 are radially spaced apart by R1.
- the maximum diameter of the cylinder 73 is the outer diameter of the ring plate 7a of the deformable portion 7.
- R1 is a value that prevents the outer peripheral space 74 of the cylinder 73 from being extremely narrow and allows the passage of workers, piping, and wiring, and is not particularly limited, but is 500 mm or more.
- the inner tank 3 and the outer tank 4 contract due to the cold heat.
- the inner tank 3 is at a lower temperature than the outer tank 4, so the inner tank 3 thermally contracts to a greater extent than the outer tank 4.
- Figure 5 is a diagram showing the relative displacement caused by thermal contraction between the inner tank joint 61 and the outer tank joint 62.
- the deformation of the connection part 68 and the inner tank 3 is shown exaggerated.
- the connecting portions 68 mainly the first annular plate 71, the second annular plate 72, and the ring plate 7a of the cylindrical body 73 each elastically deform so that the outer edge and the inner edge move away from each other in the protruding direction X, causing the connecting portion 68 to extend in the protruding direction X as a whole.
- the configuration of the deformation-permitting portion 7 of the cylindrical body 73 is not limited to the above, and it is sufficient if the cylindrical body 73 can be extended in the protruding direction X by elastic deformation. Modified examples of the cylindrical body 73 are described below.
- the deformable portion 7 of the cylindrical body 73 shown in FIG. 2 protrudes toward the outer diameter side relative to the main body of the cylindrical body 73. However, the deformable portion 7 may protrude toward the inner diameter side relative to the main body of the cylindrical body 73.
- the deformable portion 7 of the cylindrical body 73 according to the modified example shown in FIG. 6 has a pair of ring plates 7a whose outer edge is joined to the cylindrical body 73, and a third cylindrical portion 7b that connects the inner edge portions of the pair of ring plates 7a.
- the inner diameter of the cylindrical body 73 including the deformable portion 7 is a value that does not narrow the inner circumference of the cylindrical body 73 and allows the pump 21, piping, and wiring to pass through, and is not particularly limited, but is 1000 mm or more.
- the minimum diameter of the cylindrical body 73 is the inner diameter of the ring plate 7a of the deformable portion 7, and the ring plate 7a has an inner diameter of 1000 mm or more.
- the cylindrical body 73 shown in Fig. 2 has one deformation allowance portion 7, but may have multiple deformation allowance portions 7 spaced apart in the protruding direction X.
- the cylindrical body 73 according to a modified example shown in Fig. 7 has two deformation allowance portions 7.
- the two deformation allowance portions 7 are spaced apart by H4 in the protruding direction X.
- H4 is a value that ensures that the joint between the ring plate 7a and the main body of the cylindrical body 73 is not narrow, and is not particularly limited, but is 500 mm or more.
- the deformable portion 7 of the cylindrical body 73 shown in Fig. 2 is composed of a pair of ring plates 7a and a third cylindrical portion 7b, but the third cylindrical portion 7b may be omitted.
- the deformable portion 7 of the cylindrical body 73 according to the modified example shown in Fig. 8 is composed of a pair of ring plates 7a whose inner edges are joined together. The outer edges of the pair of ring plates 7a are both joined to the main body of the cylindrical body 73.
- the deformable portion 7 may be composed of a pair of ring plates 7a whose outer edges are joined together.
- the deformable portion 7 of the cylindrical body 73 shown in Fig. 2 is composed of a pair of ring plates 7a and a third cylindrical portion 7b, but it is sufficient that the deformable portion 7 is capable of transmitting a load and capable of elastically expanding and contracting deformation in the protruding direction X.
- the deformable portion 7 of the cylindrical body 73 according to the modified example shown in Fig. 9 is a protrusion 7c having a curved cross section in the protruding direction X and protruding inward or outward beyond the first cylindrical portion 731 and the second cylindrical portion 732.
- the protrusion 7c is continuous in the circumferential direction on the surface of the cylindrical body 73.
- the cross section of the protrusion 7c may be wave-shaped, and the deformable portion 7 may be composed of a corrugated pipe, for example.
- the multi-shell tank 2 comprises: An inner tank 3 for containing liquefied gas; An outer tank 4 surrounding the inner tank 3; a dome 6 joined to the inner tub 3 and the outer tub 4, a portion of which protrudes from the outer tub 4 in a protruding direction X;
- the dome 6 has a first body 65 joined to the inner tank 3, a second body 66 arranged away from the first body 65 in the protruding direction X and joined to the outer tank 4, and a connecting part 68 that connects the first body 65 and the second body 66 and is elastically deformable in response to the relative displacement of the first body 65 with respect to the second body 66, and the inner space of the first body 65, the inner space of the connecting part 68, and the inner space of the second body 66 are connected to each other.
- the multi-shell tank 2 according to the second item of the present disclosure is the multi-shell tank 2 according to the first item, in which the connecting portion 68 includes a first annular plate 71 having an outer edge portion joined to the first body portion 65, a second annular plate 72 having an outer edge portion joined to the second body portion 66 and positioned away from the first annular plate 71 in the protruding direction X, and a cylindrical body 73 having a first end portion 73a connected to the inner edge portion of the first annular plate 71 and a second end portion 73b connected to the inner edge portion of the second annular plate 72 and extending in the protruding direction X.
- the inner tank 3 and the outer tank 4 are connected via the dome 6, so that a portion of the dome 6 is not enclosed by the outer tank 4. Therefore, by accessing the inner tank 3 through the wall of the dome 6 without passing through the wall of the outer tank 4, a simple internal and external access route that does not pass through the space between the inner and outer tanks 52 can be realized.
- a space extending in the protruding direction X is formed on the inner circumference of the first body 65, the connecting portion 68, and the connecting portion 68, so that this space can be used for wiring or piping inside the dome 6.
- the piping or wiring passed through the dome 6 can be led out to the outside by penetrating the roof portion 67 or the second body 66 of the dome 6, so that a simple piping or wiring route with a reduced number of penetration points can be formed. Furthermore, with the multi-shell tank 2 configured as described above, when the inner tank 3 contains low-temperature liquefied gas and the degree of thermal contraction between the inner tank 3 and the outer tank 4 differs, causing the inner tank 3 to displace relative to the outer tank 4. The stress caused by the relative displacement is suppressed by the elastic deformation of mainly the first annular plate 71 and the second annular plate 72 of the connecting portion 68.
- the multi-shell tank 2 according to the third item of the present disclosure is the multi-shell tank 2 according to the second item, in which the cylindrical body 73 includes a first cylindrical portion 731 and a second cylindrical portion 732 spaced apart in the protruding direction X, and a deformation-permitting portion 7 that is elastically deformable in response to the relative displacement of the second cylindrical portion 732 with respect to the first cylindrical portion 731.
- the first annular plate 71 and the second annular plate 72 and the deformation-permitting portion 7 elastically deform the connecting portion 68 in response to the relative displacement of the inner tank 3 relative to the outer tank 4.
- the connecting portion 68 can be elastically deformed to a larger extent and with greater flexibility.
- the multi-shell tank 2 according to the fourth item of the present disclosure is the multi-shell tank 2 according to the third item, in which the deformation-permitting portion 7 includes a pair of ring plates 7a spaced apart in the protruding direction X, and a third tubular portion 7b connecting between the pair of ring plates 7a.
- the multi-shell tank 2 according to the fifth item of the present disclosure is the multi-shell tank 2 according to the third item, in which the deformation-permitting portion 7 includes a pair of ring plates 7a whose outer edges or inner edges are joined together.
- the multi-shell tank 2 according to the sixth item of the present disclosure is the multi-shell tank 2 according to the third item, in which the deformation-permitting portion 7 has a curved cross section in the protruding direction X and includes a ridge 7c that continues circumferentially on the surface of the cylindrical body 73.
- the multi-shell tank 2 according to the fourth to sixth items above allows for a simple construction of the deformation-permitting portion 7 that can transmit load in the cylindrical body 73.
- the multi-shell tank 2 according to the seventh item of the present disclosure is a multi-shell tank 2 according to any one of the second to sixth items, in which the corners of the connection between at least one of the first annular plate 71 and the second annular plate 72 and the cylindrical body 73 are rounded.
- the multi-shell tank 2 according to the eighth item of the present disclosure is the multi-shell tank 2 according to the seventh item, in which the annular plate and the cylinder 73 are connected via a ring member 70 whose cross section in the protruding direction X is curved.
- the multi-shell tank 2 according to the seventh and eighth items can suppress stress concentration at the connection between the annular plates 71, 72 and the cylindrical body 73.
- the multi-shell tank 2 according to the ninth item of the present disclosure is a multi-shell tank 2 according to any one of the second to eighth items, which has an outer peripheral space 74 between the inner wall of the second body 66 and the outer wall of the cylindrical body 73, the outer peripheral space 74 being connected to the space between the inner and outer tanks 52 between the inner tank 3 and the outer tank 4.
- the multi-shell tank 2 according to the tenth item of the present disclosure is the multi-shell tank 2 according to the ninth item, in which the second body 66 has a penetration that connects the outer peripheral space 74 with the exposure, and is equipped with an inner and outer tank space 52, the outer peripheral space 74, and an inter-tank piping 92 that passes through the penetration.
- the inter-tank piping 92 can be extended to the outside through the penetration in the wall of the dome 6, without passing through the wall of the outer tank 4.
- the multi-shell tank 2 according to the eleventh item of the present disclosure is the multi-shell tank 2 according to the ninth or tenth item, in which the inner wall of the second body 66 and the outer wall of the cylinder 73 are spaced apart to allow workers to access the outer peripheral space 74.
- the outer space 74 can be used as a passageway for workers.
- the multi-shell tank 2 according to the twelfth item of the present disclosure is the multi-shell tank 2 according to any one of the second to eleventh items, further comprising a pipe tower 20 disposed within the inner tank 3 and connected to the lower part of the dome 6, and a pump 21 disposed at the lower part of the pipe tower 20, and the cylindrical body 73 has an inner diameter that allows the pump 21 to pass through.
- the pump 21 can be transported to and from the bottom of the pipe tower 20 through the dome 6.
- the ship 1 according to the thirteenth item of the present disclosure comprises a hull 11 and a multi-shell tank 2 according to any one of the first to twelfth items supported by the hull 11.
- the above-mentioned multi-shell tank 2 is suitable as a cargo tank or fuel tank to be installed on the ship 1.
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Abstract
Description
液化ガスを収容する内槽と、
前記内槽を囲む外槽と、
前記内槽及び前記外槽と接合されており、一部分が前記外槽から突出方向へ突出したドームとを、備え、
前記ドームは、前記内槽と接合された第1胴部、前記第1胴部から前記突出方向へ離れて配置され前記外槽と接合された第2胴部、及び、前記第1胴部と前記第2胴部とを連結し、前記第2胴部に対する前記第1胴部の相対的変位に追従して弾性変形可能な連結部を有し、前記第1胴部の内周空間、前記連結部の内周空間、及び前記第2胴部の内周空間が連通しているものである。
多重殻タンク2は、内槽3と、内槽3を囲む外槽4と、内槽3及び外槽4を突出方向Xに貫くドーム6とを備える。本実施形態において突出方向Xは上下方向である。本実施形態に係る多重殻タンク2は内槽3と外槽4の二重の槽を備えるが、多重殻タンク2は三重以上の槽を備えていてもよい。外槽4は、上部を覆うタンクカバー12と、側部及び底部を覆う保持壁14により包囲されている。外槽4と、タンクカバー12及び保持壁14との間の保持空間53には、空気又は不活性ガスが充填されている。ドーム6の頂部は、タンクカバー12よりも上方へ突出して暴露されている。
図2は、多重殻タンク2の頂部の拡大垂直断面図である。図2に示すように、ドーム6は、第1胴部65、第2胴部66、屋根部67、及び連結部68を有する。
図2に示す筒体73の変形許容部7は、筒体73の本体に対し外径側へ突出している。但し、変形許容部7は、筒体73の本体に対し内径側へ突出するものであってもよい。図6に示す変形例に係る筒体73の変形許容部7は、筒体73と外縁部が接合された一対のリング板7aと、一対のリング板7aの内縁部を接続する第3筒部7bとを有する。変形許容部7を含む筒体73の内径は、筒体73の内周が狭隘とならず且つポンプ21や配管や配線を通せる程度の値であり、特に限定されないが、1000mm以上である。図6に示す例では、筒体73の最小径は変形許容部7のリング板7aの内径であり、リング板7aは1000mm以上の内径を有する。
図2に示す筒体73は、一か所の変形許容部7を有するが、突出方向Xに離れた複数箇所の変形許容部7を有していてもよい。図7に示す変形例に係る筒体73は、2か所の変形許容部7を有する。2か所の変形許容部7は、突出方向XにH4だけ離れている。H4は、リング板7aと筒体73の本体の接合部が狭隘とならない程度の値であり、特に限定されないが、500mm以上である。
図2に示す筒体73の変形許容部7は、一対のリング板7aと第3筒部7bとからなるが、第3筒部7bが省略されてもよい。図8に示す変形例に係る筒体73の変形許容部7は、内縁部同士が接合された一対のリング板7aからなる。一対のリング板7aの外縁部は、いずれも、筒体73の本体と接合されている。但し、変形許容部7は、外縁部同士が接合された一対のリング板7aで構成されていてもよい。
図2に示す筒体73の変形許容部7は、一対のリング板7aと第3筒部7bとからなるが、変形許容部7は荷重を伝達可能であり且つ突出方向Xに弾性伸縮変形可能であればよい。図9に示す変形例に係る筒体73の変形許容部7は、突出方向Xの断面が曲線状であって第1筒部731及び第2筒部732よりも内側又は外側へ突出する突条7cである。突条7cは、筒体73の表面で周方向に連続している。突条7cの断面は波型であってもよく、変形許容部7は例えばコルゲート管で構成されていてもよい。
本開示の第1の項目に係る多重殻タンク2は、
液化ガスを収容する内槽3と、
内槽3を囲む外槽4と、
内槽3及び外槽4と接合されており、一部分が外槽4から突出方向Xへ突出したドーム6とを、備え、
ドーム6は、内槽3と接合された第1胴部65、第1胴部65から突出方向Xへ離れて配置され外槽4と接合された第2胴部66、及び、第1胴部65と第2胴部66とを連結し、第2胴部66に対する第1胴部65の相対的変位に追従して弾性変形可能な連結部68を有し、第1胴部65の内周空間、連結部68の内周空間、及び第2胴部66の内周空間が連通しているものである。
Claims (13)
- 液化ガスを収容する内槽と、
前記内槽を囲む外槽と、
前記内槽及び前記外槽と接合されており、一部分が前記外槽から突出方向へ突出したドームとを、備え、
前記ドームは、前記内槽と接合された第1胴部、前記第1胴部から前記突出方向へ離れて配置され前記外槽と接合された第2胴部、及び、前記第1胴部と前記第2胴部とを連結し、前記第2胴部に対する前記第1胴部の相対的変位に追従して弾性変形可能な連結部を有し、前記第1胴部の内周空間、前記連結部の内周空間、及び前記第2胴部の内周空間が連通している、
多重殻タンク。 - 前記連結部は、前記第1胴部に接合された外縁部を有する第1環状板、前記第2胴部に接合された外縁部を有し且つ前記第1環状板から前記突出方向へ離れて配置された第2環状板、及び、前記第1環状板の内縁部と接続された第1端部と前記第2環状板の内縁部と接続された第2端部とを有し前記突出方向に延びる筒体を含む、
請求項1に記載の多重殻タンク。 - 前記筒体は、前記突出方向に離れて配置された第1筒部及び第2筒部と、前記第1筒部に対する前記第2筒部の相対的変位に追従して弾性変形可能な変形許容部を含む、
請求項2に記載の多重殻タンク。 - 前記変形許容部は、前記突出方向に離れて配置された一対のリング板と、前記一対のリング板の間を接続する第3筒部とを含む、
請求項3に記載の多重殻タンク。 - 前記変形許容部は、外縁部同士又は内縁部同士が接合された一対のリング板を含む、
請求項3に記載の多重殻タンク。 - 前記変形許容部は、前記突出方向の断面が曲線状であり前記筒体の表面で周方向に連続する突条を含む、
請求項3に記載の多重殻タンク。 - 前記第1環状板及び前記第2環状板のうち少なくとも一方の環状板と前記筒体との接続部の角が丸められている、
請求項2乃至6のいずれか一項に記載の多重殻タンク。 - 前記環状板と前記筒体は、前記突出方向の断面が曲線状のリング部材を介して接続されている、
請求項7に記載の多重殻タンク。 - 前記第2胴部の内壁と前記筒体の外壁の間に、前記内槽と前記外槽の内外槽間と連通された外周空間を有する、
請求項2乃至8のいずれか一項に記載の多重殻タンク。 - 前記第2胴部は前記外周空間と暴露とを連通する貫通部を有し、
前記内外槽間、前記外周空間、及び前記貫通部を通された槽間配管を備える、
請求項9に記載の多重殻タンク。 - 前記第2胴部の内壁と前記筒体の外壁は、前記外周空間を作業者が交通可能に離間している、
請求項9又は10に記載の多重殻タンク。 - 前記内槽内に配置されて前記ドームの下部と接続されたパイプタワーと、
前記パイプタワーの下部に配置されたポンプとを更に備え、
前記筒体は前記ポンプが通過可能な内径を有する、
請求項2乃至11のいずれか一項に記載の多重殻タンク。 - 船体と、
前記船体に支持された請求項1乃至12のいずれか一項に記載の多重殻タンクとを、備えた、
船舶。
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| KR1020257011237A KR20250067153A (ko) | 2022-09-30 | 2022-09-30 | 다중각 탱크 및 선박 |
| CN202280097399.2A CN119486948A (zh) | 2022-09-30 | 2022-09-30 | 多层壳罐和船舶 |
| PCT/JP2022/036844 WO2024069980A1 (ja) | 2022-09-30 | 2022-09-30 | 多重殻タンク及び船舶 |
| JP2024549063A JP7793807B2 (ja) | 2022-09-30 | 2022-09-30 | 多重殻タンク及び船舶 |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS636300A (ja) * | 1986-06-26 | 1988-01-12 | Kawasaki Heavy Ind Ltd | 二重殻低温タンクの内部点検用ロボツト搬入方法 |
| DE4019278A1 (de) * | 1990-06-16 | 1991-12-19 | Marine Service Gmbh | Behaelter zur lagerung oder zum transport verfluessigter gase |
| JP2001031185A (ja) * | 1999-07-19 | 2001-02-06 | Nisso Engineering Co Ltd | 流体貯槽及び貯槽設備 |
| JP2015004383A (ja) * | 2013-06-19 | 2015-01-08 | 川崎重工業株式会社 | 二重殻タンクおよび液化ガス運搬船 |
| CN111442184A (zh) * | 2020-04-20 | 2020-07-24 | 辰一(上海)石油天然气工程技术有限公司 | 一种双层球罐用接管连接结构及双层球罐 |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9702557B2 (en) | 2012-04-20 | 2017-07-11 | Ngk Spark Plug Co., Ltd. | Glow plug |
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2022
- 2022-09-30 WO PCT/JP2022/036844 patent/WO2024069980A1/ja not_active Ceased
- 2022-09-30 JP JP2024549063A patent/JP7793807B2/ja active Active
- 2022-09-30 KR KR1020257011237A patent/KR20250067153A/ko active Pending
- 2022-09-30 CN CN202280097399.2A patent/CN119486948A/zh active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS636300A (ja) * | 1986-06-26 | 1988-01-12 | Kawasaki Heavy Ind Ltd | 二重殻低温タンクの内部点検用ロボツト搬入方法 |
| DE4019278A1 (de) * | 1990-06-16 | 1991-12-19 | Marine Service Gmbh | Behaelter zur lagerung oder zum transport verfluessigter gase |
| JP2001031185A (ja) * | 1999-07-19 | 2001-02-06 | Nisso Engineering Co Ltd | 流体貯槽及び貯槽設備 |
| JP2015004383A (ja) * | 2013-06-19 | 2015-01-08 | 川崎重工業株式会社 | 二重殻タンクおよび液化ガス運搬船 |
| CN111442184A (zh) * | 2020-04-20 | 2020-07-24 | 辰一(上海)石油天然气工程技术有限公司 | 一种双层球罐用接管连接结构及双层球罐 |
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| JP7793807B2 (ja) | 2026-01-05 |
| CN119486948A (zh) | 2025-02-18 |
| KR20250067153A (ko) | 2025-05-14 |
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