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US3399800A - Tank for liquefied gas - Google Patents

Tank for liquefied gas
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US3399800A
US3399800AUS527254AUS52725466AUS3399800AUS 3399800 AUS3399800 AUS 3399800AUS 527254 AUS527254 AUS 527254AUS 52725466 AUS52725466 AUS 52725466AUS 3399800 AUS3399800 AUS 3399800A
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casing
tight
fluid
tank
ship
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US527254A
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Gilles Auguste
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A RESPONSABILITE DITE GAZ-TRANSPORT Ltee Ste
SARL GAZ TRANSP
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SARL GAZ TRANSP
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Sept. 3, 1968 A. GILLES 3,399,800
' TANK FOR LIQUEFIED GAS Filed Feb. 14, 1966 3 Sheets-Sheet 1 37 -e -5 66 E 5 62 s J57 s5 s5 4' 37 40 i Z 61 i A-h 54 58Q 50 I I 1 44 2 59E Q 46 55 4s 5s 1 f I 1 474s 45 g l l g 1 j/ Invencor A. G \LLES ABwmAQc S A. GILLES TANK FOR LIQUEFIE ID GAS Sept. 3, 1968 3 Sheets-Shae; 2
Filed Feb. 14, 1966 all! IhVen-br A. Glues EZIuJJMLLMJSQLJ;
Sept. 3, 1968 A. GILLES 3,399,800
TANK FOR LIQUEFIED GAS Filed Feb. 14, 1966 Y s Sheets-Sheet s FIG.3
Q l/ E lnveh-l'or A. G ILLE$ Aihrmv United States Patent ABSTRACT OF THE DISCLOSURE An integral tank structure for ships carrying liquefied gas comprising in succession an inner hull, an outer insulating casing, an outer fluid tight casing, an inner insulating casing and an inner fluid tight casing, the two fluid tight casings being made of thin metal having a low coefficient of expansion, reinforced by transverse frames, and supported at their corners by rigid metallic supports projecting through the insulating casings.
This invention relates to the transportation of liquefied gas, and particularly liquefied natural gas having a high methane content, by sea, and to its storage on land. In order to increase the capacity of ships designed for such transport and reduce the cost of construction of isothermal tanks, it has already been suggested that the tanks be made integral with the ship itself by covering the walls of the compartments of the ship with fluid and heat tight sheathing, generally consisting of two layers, but not in itself rigid, so that the hydrostatic pressures are in fact supported solely by the framework of the ship itself.
The principal difiiculty to be overcome in the construction and use of such integral tanks stems from the substantial contractions which result when the temperature of the walls of the tank decreases from the ambient temperature to that of the liquefied gas (-160 C. in the case of methane). To reduce this contraction it is conventional to utilize corrugations running at right angles to each other, which requires an excess of metal. The metals used are ordinarily stainless steel or aluminum alloys, which are not fragile at low temperatures. In view of their complex shapes it is difficult to provide means for supporting them at all ranges of temperature. On the contrary, the principal object of the present invention consists in using a thin smooth wall of an alloy containing 26% nickel, 0.25% carbon and 0.60% manganese, balance substantially all iron, sold under the trademark Invar which is supported at all points by insulatin means which is as rigid as possible. However, it is impossible to avoid any contraction whatsoever, even with this special steel, because the tanks are so large, or to avoid the flexing movements of the framework of the ship caused by the surges of the sea, which flexing movements necessarily affect the walls of the tank.
The effect of all these deformations is concentrated at the dihedral corners, since the tank is usually polygonal for convenience in construction, and especially at trihedral corners which are subjected to alternating strains which tend to destroy the fluid-tight sheathing.
The invention seeks to avoid these difiiculties by so constructing the dihedral and trihedral corners of the transverse walls of the ship that the inevitable contractions will not cause any distortion thereof.
The object of the present invention is accordingly to provide a new fluid-tight isothermal tank integrated into the framework of a ship between two transverse bulkheads therein and comprising two successive fluid-tight primary and secondary casings, commonly referred to by the US. Coast Guard and Marine Insurers as primary and secondary barriers. These cases are alternated with "Ice two primary and secondary isothermal insulatin casings, said tank being characterized by the fact that the primary and secondary fluid-tight casings terminate near the transverse bulkheads of the ship in a rigid polygonal ring made of strips of the same metal substantially thicker and stronger than the sheets forming the fluidtight casings. One of these strips is positioned in alignment with the transverse bulkhead and screwed along its two edges onto planks, while the other st-rip completing the dihedral angle is welded along one of its edges perpendicular to the said one strip, between the two points of attach-ment thereof, and along its other edge to another plank. The assembly formed by these planks which may comprise several sections free to contract, is connected to a corner of the framework of the ship by supporting hangers suitably spaced and attached directly to this structure in the case of the dihedral angles of the secondary casing, and to supporting chairs interconnected by rods extending through fluid-tight seals in the secondary casing in the case of the dihedral angles of the primary casing. At each corner of the rigid ring are two trihedral corner members made of a special steel, one of which is fastened to, the secondary casin and connected directly to the inner hull or double bulkhead by three connecting members, preferably consisting of three stainless steel tubes, and the other of which is fastened to the primary casing and connected to the first corner member by three metallic connecting tubes or rods. The strips forming the dihedral angles of the ring are rigidly welded to the trihedral corner members for the two casings, and the corresponding planks are fastened within each of the corner members by screws spaced from these welds. The screws are covered over after insertion and the rigid ring formed by the dihedral and trihedral corner members are built while strain free at normal temperatures so as to be under elastic strain at the temperature at which the tank holds liquid gas.
In order that the invention may be clearly understood, one representative embodiment thereof will now be described, purely by way of illustration, in connection with the annexed drawings, in which:
FIG. 1 is a partial horizontal cross-section showing one of the dihedral corners;
FIG. 2 is a partial vertical section taken near a transverse bulkhead to show in detail a trihedral corner; and
FIG. 3 is a horizontal section taken along the line IIIIII of FIG. 2.
In order to build a tank according to the invention, the starting point is naturally a ship comprisingan outer hull and its essential supporting framework, and an inner hull, the framework of the boat being positioned between the inner and outer hulls. For convenience in construction the inner hull may have the same general contour as the outer hull, but be more polygonal in character, usually octagonal, that is to say, like a rectangle with four beveled corners. The ship also comp-rises, from how to stern, a series of compartments for transporting liquid gas and separated each from the other by double bulkheads comprising two parallel walls spaced by the necessary supporting framework.
Inside each of these compartments is an integral tank comprising two fluid-tight casings alternating with two heat insulating casings. As shown on FIG. 1, there are successively from the inside out the primary fluid-tight casing consisting of thethin plates 37 which are made of a metal which has a low coefiicient of expansion and connected together by means of theirflanges 40; the heat insulating casing consisting of theinsulating boxes 14, the secondary fluid-tight casing consisting of .plates 8 connected at theirflanges 9, the secondary heat insulating casing consisting of theinsulating boxes 1, theinner hull 3, the framework of the ship, and finally the outer hull (not shown).
The transverse walls of the ship, that is to say, those positioned against thedouble bulkheads 4, are made in the same way as the lateral walls and are each encircled by a rigid ring.
Two of the walls comprising the secondary fluid-tight casing 8 are connected at a dihedral angle in the following manner: Twothick planks 43 and 44, positioned as shown in FIG. 1 are each supported as required by chairs made of twoiron plates 45 and 46 welded at right angles to each other and resting on athick metal bracket 47 which lies in a plane parallel to that of FIG. 1. Thisbracket 47 is welded to both theplates 45 and 46 and thewalls 3 and 4 of the double bulkhead. Theplanks 43 and 44 are connected to theplates 45 and 46 by means of screws (not shown) which extend perpendicularly into the plank, but are not so tight as to eliminate all play longitudinally of the planks.
Theplank 43 in alignment with thecasing 8 parallel to thewall 4 of the double bulkhead is first attached, and then covered by astrip 48 of metal having a high nickel content, preferably identical to that from which the plates forming thecasing 8 are made, but substantially thicker, for example, 1.5 mm. This strip has anedge 49 bent out at a right angle and attached to theplank 43 byscrews 50 while its other edge is attached thereto by means ofscrews 51. Then theplank 44 is put in place, followed by anotherstrip 52 and analogous to thestrip 48, but having two flanges, one, 53, attached by means ofscrews 54, While the other, 55, abuts thestrip 48 to which it is welded in situ after inserting between thestrip 48 and the plank a strip of asbestos, not shown.
Thestrip 48 is then connected to the edge of thesecondary casing 8 by means of a cover-joint 56, Welded at both edges. In like manner thestrip 52 is connected to the secondary casing by means of a cover-joint 57.
Tworods 58, welded to the chairs formed by themembers 45, 46 and 47, extend through fluid-tight seals in the cover-joints 56 and 57, using sealing rings, not shown, and support a second chair comprising tworectangular steel plates 59 and 60 welded together at right angles to each other. This second chair supports two planks '61 and 62 which serve the same purpose with respect to the primary casing that theplanks 43 and 44 serve with respect to the secondary casing.Metallic strips 63 and 64, like thestrips 48 and 52, are fastened in like manner to each other and to theplanks 61 and 62. Finally, the cover-joints 65 and 66 connect thestrips 63 and 64 to the primary casing in the same way as the saidcoverjoints 56 and 57.
In order to form each of the rigid rings hereinbefore mentioned it is necessary to connect the ends of each of the angle members formed by the assembly of thestrips 48 and 52 or 63 and 64 together to form the corners of the ring, which is polygonal, and generally octagonal. Each trihedral angle is positioned at the intersection of three planes, two of which are parallel to the longitudinal axis of the ship, while the other is perpendicular thereto.
These connections are made by means of trihedral metallic corner members, made of a special steel, for example a steel containing 9% nickel, thicker than the previously mentioned strips, about 8 thick, for example. Thecorner member 67, formed from three fiat plates welded to each other, is connected to the hull of the ship (either the inner hull or the double bulkhead) by connectingmembers 68 which must be strong enough to resist compression, tension, and buckling, yet have a small section for the transmission of heat. For this reason, recourse is preferably had to sections of stainless steel tubing having a large diameter and thin walls.
Theplanks 43 and 44 are attached to thiscorner member 67 by means ofscrews 69 passing through suitable holes in said corner member, and thestrips 48 and 52 have theirends 70 welded to this corner member so as to cover the heads of thescrews 69 and insure overall impermeability. The cover-joints 56 and 57 are also welded to the three plates forming the corner member so as to ensure the impermeability of the secondary casing, as well as the transfer of those forces which act directly in the direction of the plane of the transverse wall of the tank, and in the direction of the dihedral anglemembers parallel thereto.
It is easy to understand that, since the assembly is welded together at room temperature, when the temperature falls the transverse wall of the tank contracts and exerts traction on the dihedral corners in the direction of thestrips 48. These corners concentrate the forces and transmit them to the trihedral corner members. However, since as will be hereinafter seen, the trihedral corner members are rigidly connected to the basic structure of the ship, these forces cannot cause deformation, but only an elastic strain by tensioning the corresponding members. In effect, in view of the high mechanical strength of the materials employed and their very low coefficient of expansion, even at temperatures of the order of l60, the mechanical strains thus developed as a consequence of temperature changes do not exceed 5 kg./mm. which is far below the elastic limit of these high nickel content steels.
This embodiment thus resists any tendency toward free play resulting from contractions by mechanically tensioning the entire ring formed by the dihedral corner members. It will also be seen that the effects of tension longitudinally of the dihedral corners is absorbed by the rigidity of theplanks 43 and 44 and referred thereby to the supporting chairs.
Turning now to the primary casing, all that has just been said about the secondary casing applies thereto. The othertrihedral corner member 71 serves in a manner analagous to that served by thetrihedral corner member 67, but on a smaller scale, being supported by threerods 72 fixed to thecorner member 67. The planks '61 and 62 are fastened in like manner to this trihedral corner member by means ofscrews 73, the heads of which are covered by the ends of thestrips 63 and 64. These strips, aswell as the cover-joints 65 and 66 are welded in a fluid-tight manner directly to thetrihedral corner member 71. The method of construction and the manner of functioning under tension is naturally the same.
To sum "up, it will be seen that each of the primary and secondary fluid-tight casings of the tank comprises at each end an inflexible transverse wall stretched on a rigid ring which cannot itself be deformed and which is supported at its eight corners as Well as by a certain number of intermediate chairs, so that this transverse wall does not undergo any deformation, but only a variation in elastic strain.
In like manner the lateral walls of the tank, which are attached at their ends to the rigid ring, undergo, in response to the decrease in temperature and deformations of the hull of the ship, only an elastic tension.
-It will be appreciated that the foregoing embodiment has been described purely by way of example, and may be modified as to detail without thereby departing from the basic principles of the invention as defined by the following claims.
What is claimed is:
1. In combination with a ship having an inner hull and transverse bulkheads, the improved fluid-tight tank for holding liquefied gases which comprises thin inner and outer fluid-tight casings positioned within said inner hull and made of a metal having a low coefficient of expansion, inner and outer insulating casings comprising a material which is a poor conductor of heat, said inner insulating casing being positioned between said fluidtight casings and said outer insulating casing being positioned between the outer fluid-tight casing and the inner hull and bulkhead, said casings having polygonal sides extending transversely of said ship and longitudinal sides connected to said transverse sides to form trihedral corners at the connections between each polygonal side and two adjacent longitudinal sides, a rigid frame peripherally supporting each polygonal side of each fluid-tight casing, rigid metallic support means extending from points near each trihedral corner of the outer fluid-tight casing through the outer insulating casing to said inner hull and to a transverse bulkhead, and additional rigid metallic supporting means extending from points near each trihed-ral corner of said inner fluid-tight casing to the peripheral supporting frame of said outer fluid-tight casing.
2. The combination claimed inclaim 1, according to which said rigid metallic support means are thin walled tubes of stainless steel having a cross-section which is large in proportion to the thickness of the tube walls.
3. The combination claimed inclaim 1, according to which said rigid frames are strain free at normal temperatures so as to be stressed by contractions at the temperature of liquefied gas.
4. The combination claimed inclaim 1 in which said casings are made of an alloy containing 26% nickel, 0.25% carbon, 0.6% manganese, balance substantially all iron.
5. The combination according toclaim 1 in which said peripheral supporting frames comprise wooden planks.
6. The combination according to claim 5 comprising metallic chairs intermediate said trihedral corners, each resting on said inner hull and one of said bulkheads and supporting the wooden planks comprised by the rigid frame of said outer fluid-tight casing.
7. The combination claimed in claim 6 accordin to which each of said peripheral supporting frames comprises L-section metallic members on which said planks are seated, and comprising supporting rods extending between the L-section members associated with the inner fluid-tight casing and those associated with the outer fluid-tight casing whereby the former L-section members are supported by the latter.
8. The combination claimed in claim 7 according to which said last mentioned supporting rods pass through openings in the outer fluid-tight casing and said openings are sealed fluid tight.
9. The combination claimed in claim 7 according to which said L-section metallic members are made of the same material as said fluid-tight casings but are thicker.
References Cited UNITED STATES PATENTS 1,269,197 6/1918 Mendenhall 220-15 2,053,251 9/1936 Cook et a1. 2209 2,220,501 11/ 1940 Wallach 220-9 2,239,128 4/1941 Sykes 220-15 3,007,596 11/ 1961 Matsch 2209 3,071,094 1/1963 Leroux 11474 3,093,260 6/1963 Macorrnack et al 22015 3,112,043 11/1963 Tucker 220-10 THERON E. CONDON, Primary Examiner.
JAMES R. GARRETT, Assistant Examiner.
US527254A1965-03-051966-02-14Tank for liquefied gasExpired - LifetimeUS3399800A (en)

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FR8149AFR1438330A (en)1965-03-051965-03-05 Integrated tank improved for the transport of liquefied gases

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US527263AExpired - LifetimeUS3403651A (en)1965-03-051966-02-14Integral tank for transporting liquefied gas
US527254AExpired - LifetimeUS3399800A (en)1965-03-051966-02-14Tank for liquefied gas

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US (2)US3403651A (en)
BE (1)BE676015A (en)
DE (2)DE1506252A1 (en)
DK (2)DK128153B (en)
ES (1)ES322862A1 (en)
FI (2)FI49752C (en)
FR (1)FR1438330A (en)
GB (2)GB1131811A (en)
NL (2)NL6602773A (en)
SE (2)SE328498B (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3595424A (en)*1969-02-241971-07-27Conch Int Methane LtdContainers for liquefied gases
US3896961A (en)*1972-04-051975-07-29Gaz TransportInsulated storage tank for liquid or liquefied products
US4065019A (en)*1975-08-221977-12-27Gaz-TransportFluid-tight isothermal tank for liquefied gas
US4116150A (en)*1976-03-091978-09-26Mcdonnell Douglas CorporationCryogenic insulation system
US4170952A (en)*1976-03-091979-10-16Mcdonnell Douglas CorporationCryogenic insulation system
US4452162A (en)*1978-05-261984-06-05Mcdonnell Douglas CorporationCorner structure for cryogenic insulation system
US5450806A (en)*1993-09-091995-09-19Gaz TransportWatertight and thermally insulating tank built into the bearing structure of a ship having a simplified corner structure
US5586513A (en)*1994-09-201996-12-24Gaztransport & TechnigazWatertight and thermally insulating tank built into a bearing structure
US20060118019A1 (en)*2004-12-082006-06-08Yang Young MShip with liquid tank
US7204195B2 (en)2004-12-082007-04-17Korea Gas CorporationShip with liquid tank
US20070246473A1 (en)*2006-04-202007-10-25Korea Gas CorporationLng tank and vehicle with the same
US20100018225A1 (en)*2006-09-012010-01-28Korea Gas CorporationStructure for liquefied natural gas storage tank
US20170320549A1 (en)*2014-09-222017-11-09Daewoo Shipbuilding & Marine Engineering Co., Ltd.Heat-insulation system for liquefied natural gas cargo hold
CN113874651A (en)*2019-04-162021-12-31韩国Gas公社 Liquefied gas tank capable of lifting inner shell and lifting method of inner shell of liquefied gas tank

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
USRE29463E (en)*1969-10-101977-11-01Kvaerner Brug A/STanker for liquified and/or compressed gas
BE757663A (en)*1969-10-181971-04-01Kvaerner Brug As IMPROVEMENTS IN TANKS MOUNTED SEPARATELY ON BOARD A SHIP
BE757662A (en)*1969-10-181971-04-01Kvaerner Brug As DEVICE FOR MOUNTING SEPARATE TANKS ON BOARD A SHIP
US3785320A (en)*1970-09-171974-01-15Gaz TransportIntegral tank for transporting liquefied gas
USRE29424E (en)*1970-10-151977-10-04Kvaerner Brug AsTank construction for liquified and/or compressed gas
US3782581A (en)*1971-12-271974-01-01Phillips Petroleum CoFluid containment system
DE2247220A1 (en)*1972-09-271974-03-28Linde Ag DEVICE FOR TRANSPORTING LOW-BOILING LIQUID GASES
US3929247A (en)*1973-07-111975-12-30Kaiser Aluminium Chem CorpCryogenic tank
FR2264712B1 (en)*1974-03-211976-12-17Gaz Transport
BE847581A (en)*1975-11-031977-02-14 INSULATED TANK FOR CRYOGENIC LIQUIDS,
US4066184A (en)*1976-07-131978-01-03Conch L.N.G.Thermal insulation systems
CA1088438A (en)*1978-05-261980-10-28Donal E. HarbaughCorner structure for cryogenic insulation system
FR2462336A1 (en)*1979-07-271981-02-13Gaz TransportTank for transporting liquefied gases by sea - incorporates fluid tightness and insulating barriers simply realised, necessitating only small sweeping nitrogen flow
FR2527544B1 (en)*1982-06-011987-01-09Gaz Transport WATERPROOF AND THERMALLY INSULATING TANK INTEGRATED INTO THE CARRIER STRUCTURE OF A VESSEL AND VESSEL COMPRISING SAME
JPS58214093A (en)*1982-06-051983-12-13Kawasaki Heavy Ind LtdDouble shell type low temperature tank
RU2125099C1 (en)*1997-10-221999-01-20Открытое акционерное общество "Северсталь"Method of steel melting in converter
KR100499710B1 (en)*2004-12-082005-07-05한국가스공사Lng storage tank installed inside the ship and manufacturing method the tank
KR101122292B1 (en)*2008-06-192012-03-21삼성중공업 주식회사 Insulation structure of LNG carrier cargo hold and its construction method
FR2944335B1 (en)*2009-04-142011-05-06Gaztransp Et Technigaz STOPPING THE SECONDARY MEMBRANE FROM AN LNG TANK

Citations (8)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US1269197A (en)*1917-04-031918-06-11John J MendenhallHeat-insulating container.
US2053251A (en)*1930-11-031936-09-08Gen Motors CorpRefrigerating apparatus
US2220501A (en)*1935-12-051940-11-05American Flange And Mfg CompanRefrigerator structure and corner construction therefor
US2239128A (en)*1935-06-201941-04-22American Flange & MfgPortable insulated container
US3007596A (en)*1956-07-161961-11-07Union Carbide CorpThermal insulation
US3071094A (en)*1959-06-021963-01-01Anciens Chantiers Dubigeon SaVessel for transporting liquefied hydrocarbons
US3093260A (en)*1960-04-081963-06-11Alumiseal CorpInsulated refrigeration tank structures
US3112043A (en)*1962-03-121963-11-26Conch Int Methane LtdContainer for storing a liquid at a low temperature

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
FR599750A (en)*1925-02-211926-01-19 Hatch cover enhancements
NL127373C (en)*1957-01-16
NL110538C (en)*1959-09-10
NL295593A (en)*1962-07-24
NL128973C (en)*1963-04-24
US3339783A (en)*1965-02-241967-09-05Exxon Research Engineering CoCryogenic container

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US1269197A (en)*1917-04-031918-06-11John J MendenhallHeat-insulating container.
US2053251A (en)*1930-11-031936-09-08Gen Motors CorpRefrigerating apparatus
US2239128A (en)*1935-06-201941-04-22American Flange & MfgPortable insulated container
US2220501A (en)*1935-12-051940-11-05American Flange And Mfg CompanRefrigerator structure and corner construction therefor
US3007596A (en)*1956-07-161961-11-07Union Carbide CorpThermal insulation
US3071094A (en)*1959-06-021963-01-01Anciens Chantiers Dubigeon SaVessel for transporting liquefied hydrocarbons
US3093260A (en)*1960-04-081963-06-11Alumiseal CorpInsulated refrigeration tank structures
US3112043A (en)*1962-03-121963-11-26Conch Int Methane LtdContainer for storing a liquid at a low temperature

Cited By (25)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3595424A (en)*1969-02-241971-07-27Conch Int Methane LtdContainers for liquefied gases
US3896961A (en)*1972-04-051975-07-29Gaz TransportInsulated storage tank for liquid or liquefied products
US4065019A (en)*1975-08-221977-12-27Gaz-TransportFluid-tight isothermal tank for liquefied gas
US4116150A (en)*1976-03-091978-09-26Mcdonnell Douglas CorporationCryogenic insulation system
US4170952A (en)*1976-03-091979-10-16Mcdonnell Douglas CorporationCryogenic insulation system
US4452162A (en)*1978-05-261984-06-05Mcdonnell Douglas CorporationCorner structure for cryogenic insulation system
US5450806A (en)*1993-09-091995-09-19Gaz TransportWatertight and thermally insulating tank built into the bearing structure of a ship having a simplified corner structure
US5586513A (en)*1994-09-201996-12-24Gaztransport & TechnigazWatertight and thermally insulating tank built into a bearing structure
US7171916B2 (en)*2004-12-082007-02-06Korea Gas CorporationShip with liquid tank
US20060118018A1 (en)*2004-12-082006-06-08Yang Young MModular walls for use in building liquid tank
US20060131304A1 (en)*2004-12-082006-06-22Yang Young MLiquid tank system
US20060118019A1 (en)*2004-12-082006-06-08Yang Young MShip with liquid tank
US7204195B2 (en)2004-12-082007-04-17Korea Gas CorporationShip with liquid tank
US7325288B2 (en)2004-12-082008-02-05Korea Gas CorporationMethod for manufacturing liquid tank and ship with liquid tank
US7597212B2 (en)2004-12-082009-10-06Korea Gas CorporationModular walls for use in building liquid tank
US20060117566A1 (en)*2004-12-082006-06-08Yang Young MMethod for manufacturing liquid tank and ship with liquid tank
US7717288B2 (en)2004-12-082010-05-18Korea Gas CorporationLiquid tank system
US7819273B2 (en)2006-04-202010-10-26Korea Gas CorporationLiquid natural gas tank with wrinkled portion and spaced layers and vehicle with the same
US20070246473A1 (en)*2006-04-202007-10-25Korea Gas CorporationLng tank and vehicle with the same
US20100018225A1 (en)*2006-09-012010-01-28Korea Gas CorporationStructure for liquefied natural gas storage tank
US7938287B2 (en)*2006-09-012011-05-10Korea Gas CorporationStructure for liquefied natural gas storage tank
US20170320549A1 (en)*2014-09-222017-11-09Daewoo Shipbuilding & Marine Engineering Co., Ltd.Heat-insulation system for liquefied natural gas cargo hold
US10023270B2 (en)*2014-09-222018-07-17Daewoo Shipbuilding & Marine Engineering Co., Ltd.Heat-insulation system for liquefied natural gas cargo hold
CN113874651A (en)*2019-04-162021-12-31韩国Gas公社 Liquefied gas tank capable of lifting inner shell and lifting method of inner shell of liquefied gas tank
CN113874651B (en)*2019-04-162023-06-27韩国Gas公社Liquefied gas tank capable of lifting inner shell and lifting method of liquefied gas tank inner shell

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ES322862A1 (en)1966-11-16
SE328498B (en)1970-09-14
GB1136164A (en)1968-12-11
DK137351B (en)1978-02-20
NL140956B (en)1974-01-15
FI49752C (en)1975-09-10
FI49648C (en)1975-08-11
DK128153B (en)1974-03-11
FI49752B (en)1975-06-02
DK137351C (en)1978-07-17
DE1294842B (en)1969-05-08
NL6602773A (en)1966-09-06
FI49648B (en)1975-04-30
SE328497B (en)1970-09-14
DE1506252A1 (en)1970-04-23
BE676015A (en)1966-06-16
FR1438330A (en)1966-05-13
US3403651A (en)1968-10-01
NL6602772A (en)1966-09-06
GB1131811A (en)1968-10-30

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