US3814275A - Cryogenic storage vessel - Google Patents

Cryogenic storage vessel Download PDF

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Publication number
US3814275A
US3814275A US00240362A US24036272A US3814275A US 3814275 A US3814275 A US 3814275A US 00240362 A US00240362 A US 00240362A US 24036272 A US24036272 A US 24036272A US 3814275 A US3814275 A US 3814275A
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United States
Prior art keywords
vessel
liner
foam
bonded
insulation
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.)
Expired - Lifetime
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US00240362A
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English (en)
Inventor
C Lemons
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McDonnell Douglas Corp
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McDonnell Douglas Corp
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Filing date
Publication date
Application filed by McDonnell Douglas Corp filed Critical McDonnell Douglas Corp
Priority to US00240362A priority Critical patent/US3814275A/en
Priority to GB1449373A priority patent/GB1412843A/en
Priority to SE7304434A priority patent/SE388262B/sv
Priority to CA167,653A priority patent/CA990227A/en
Priority to ES413249A priority patent/ES413249A1/es
Priority to DE2316859A priority patent/DE2316859C2/de
Priority to FR7311950A priority patent/FR2244122B1/fr
Priority to IT49217/73A priority patent/IT982947B/it
Priority to JP3819373A priority patent/JPS5411925B2/ja
Application granted granted Critical
Publication of US3814275A publication Critical patent/US3814275A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/245—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it being a foam layer
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00—Layered products having a non-planar shape
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • 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
    • F17C3/04—Vessels not under pressure with provision for thermal insulation by insulating layers
    • F17C3/06—Vessels not under pressure with provision for thermal insulation by insulating layers on the inner surface, i.e. in contact with the stored fluid
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/101—Glass fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2439/00—Containers; Receptacles
    • 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
    • F17C2203/0304—Thermal insulations by solid means
    • F17C2203/0329—Foam
    • F17C2203/0333—Polyurethane
    • 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
    • F17C2203/0629—Two 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
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146—Two-phase
    • F17C2223/0153—Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S220/00—Receptacles
    • Y10S220/901—Liquified gas content, cryogenic

Definitions

  • Resin impregnated fabric and perforated foil comprise a porous liner UNITED STATES PATENTS bonded to fiber-reinforced foam layers to form gase- 2,676,773 4/1954 Sanz ct a1.
  • 220/9 LG ous boundary layer insulation.
  • 3,009,601 11/1961 Matsch 220/9 LG 3,243,931 4/1966 Becherer 220/9 R X 10 Claims, 7 Drawing Figures 3,267,685 8/1966 Schroeder 220/9 LG 1 CRYOGENIC STORAGE VESSEL BACKGROUND.
  • An ocean going vessel has been developed with a multiple of liquid fluid storage compartments, each having inner liners which are porous and have a permeability that may be achieved with'a single ply of glass fabric impregnated with a polyurethane or epoxy resin,
  • the porosity of the liner allows the pressure within the reinforced foam insulation to reach a state of equilibrium or near equilibrium with the liquid inside the vessel compartments as they are being filled, emptied or stored;
  • the cryogenic liquid is thus contained within a gaseous envelope within the insulative foam composite within the container or vessel compartment.
  • the gas-liquid interface occurs very near the liner and most often appears somewhat inside the insulation.
  • the insulation consists of a plurality of pre-fabricated 3D foam blocks or segments bonded together to form long and narrow segments with interlocking edges to provide for maximum flexibility in mating with the contours of the marine vessel, and to permit a significant area of liner-insulation composite to be applied with a minimum of time of installation inside the vessel.
  • a perforated electrically conducting film or strip may be bonded to the liner outer surface (the surface exposed to the liquid) to serve as a static electrical discharge element and to serve as a barrier against flame propagation.
  • these strips are mechanically held in position until a vacuum bag could be installed thereover/These strips are vacuum bonded to the walls of the vessel.
  • Damage to the insulation is readily detectable by visual examination and easily repaired with a splice. Debonding can be detected before reaching a serious stage by observing frost patterns on the vessel. Thus, the insulation materialmay be accomplished at low cost and is highly reliable in use.
  • These internally insulated tanks may be used for transporting or storage of liquified gas at cryogenic temperatures as low as 423F. (liquid hydrogen) and can be used for transporting or storage of fluids under high pressure or at atmospheric pressure.
  • FIG. 1 is a sectional view illustrating the insulation system installed within a ships hull
  • FIG. 2 is a perspective view showing the construction detail of one prefabricated segment or LOG" of insulation to be bonded to the tank wall;
  • FIG. 3 is an elevational view taken along line 3-3 in FIG. 1;
  • FIGS. 4, 5 and 6 are sectional views showing corner joints.
  • FIG. 7 is an elevational view showing hooks on ceiling or overhead tank wall insulation attachments.
  • FIG. 1 shows a marine vessel 10 for the transportation of liquified natural gas such as liquid methane and including thermally insulated cargo tanks 12 integrally supported inside the cargo holds and having the general configuration of the cargo holds.
  • the ship 10 is provided with an outer hull l4 and an inner hull l6 spaced from outer hull 14 by spacers 18.
  • the space 20 between the inner and outer hull may be used for storage or water ballast asdesired.
  • the inner hull I6 is integrally lined with heat insulation material comprising an inner insulation layer 22 covered with a porous liner 24; A second or outer insulation layer 26 with porous liner 28 is bonded to the first and a perforated conductive foil 30 completes'the insulative composite.
  • Retention fasteners 32 in the ceiling are used to retain the composite until the vacuum bonding has been accomplished upon installation.
  • Other retention fasteners 33 such as glass fiber or other non-metallic cord may be anchored to the walls 35 and floor 37 of the container hull 16. These fasteners extend through the insulation and liners to serve as high load attach points to support slosh baffles and other internal structures not shown.
  • the insulation layers 22, 26 and liners 24, 28 are shown in FIG. 2 as elongated strips or logs 34, 36. Typically, these logs will be about 90 feet long, about 2 feet wide and 6 inches thick.
  • Each log consists of a plurality of blocks of three-dimensional reinforced foam covered with a fiber glass cloth liner in a manner to be more fully explained hereinafter.
  • a strip of perforated aluminum foil 30 with pin holes approximately one-half inch on center is applied to the inner liner to reduce fire hazard, particularly when the logs are installed.
  • each of the layers 22, 26 are made from a plurality of blocks 38' which consist of foam 40 having X, Y and Z reinforcing fibers 42, 44 and 46.
  • These blocks may be of the type, and made by the method, set forth in U.S. Pat. No. 3,322,868 for Three-Dimensional Reinforced Structure by Kruse and Rossello which issued May 30, [967, the subject matter of which is hereby incorporated by reference. Of course, other materials and methods of fabrication may also be used as desired provided they serve the purpose intended.
  • a fiber glass liner 24 is bonded to the outer ends of the Z fibers 46. and the abutting ends of the blocks 38 are also bonded together to form the elongated strips or logs. These are then bonded to the inner surface of the inner hull 16 of the vessel. The edges of the liner 24 are then taped with splices 48. The second layer 26 with fiberglass liner 28 is vthen bonded to the first liner' 24, and splices 50"applied.
  • a polyurethane or epoxy resin may be used to impregnate and bond (while wet) the liner to the fiber ends.
  • the amount of resin used preferably is about 1.5 times the weight of the dry glass fabric. This usually is referred to as a 60 percent by weight resin content laminate. It has been found that resin in the amount of 2 /2 times the weight of the fabric causes cracking due to contraction at a -423F. temperature and,-in the amount of only one, the bond strength to the foam is marginal and a high reliability bond is not achieved
  • FIGS. 4, and 6 there are shown several comer connections.
  • four columns or posts 52, 54, 56 and 58 of foam wrapped in a fiber glass lining are placed in a corner at the intersection of container walls 60, 62.
  • Fiber glass splices 64 are applied to the inner corners of the inner and outer layers 66, 68 of insulation having liners 70, 72 on their inner faces.
  • a comer splice 74 then completes the porous seal.
  • FIG. 5 the corner formed by container walls 76, 78 has the end 80 of inner layer 82 abutting wall 78, with end 84 of inner layer 86 abutting end 80.
  • the fiber glass liner 88 is then wrapped around the corner over the inner ends of Z fibers 90 of both layers.
  • outer layer 92 is ap- 4 plied with its end 94 abutting end 84 of layer 86, and end 96 of layer 98 is then placed against end 94.
  • Fiber glass liner 100 and a perforated aluminum foil 102 is then applied.
  • the inner layers 104 and 106 have tapered abutting ends 108, 110 meeting at the corner of container walls 112, 114. Their respective fiber glass liners 116, 118 wrap around their ends and contact the container walls 112, 114.
  • the outer layers 120, 122 have tapered abutting ends 124, 126 with fiber glass liners 128, I30 extending around the ends for bonding to liners 116 and 118 respectively.
  • FIG. 7 there is shown a technique for attaching the insulation to the top of the container.
  • a scaffold support hook 134 In the upper corner 132 is a scaffold support hook 134.
  • the side insulation 136 is applied to side wall 138, leaving hook 134,
  • Insulation fastening devices 140 are attached to the underside of roof or top 142. Preferably, they may be shafts with barbs on the end since they are needed only to hold the adhesive-coated insulation strips 144 in position against the ceiling until a vacuum bag can be installed for the bonding process.
  • sections 146 and 148 of the insulation are shown as yet to be pushed onto fasteners 150. When installed, the hooks lock under the X and Y fibers within the foam. After the ceiling insulation has been applied, the scaffolding is removed and insulation wedge 154 is applied to the corner 132.
  • a vacuum bag isthen used to apply'pressure (about 20 inches of mercury or 10 p.s.i.) during the cure cycle of the adhesive.
  • the adhesive resin bonds at ambient temperature (77F.) for 24 hours or at F. for 3 hours. This sequence is repeated to bond all strips of insulation to the vessel.
  • the liner splices are then applied but no external pressure is needed in liner-to-liner bonding. This process allows the critical bonds of liner-to-reinforced foam to be made outside the cryogenic container and under best environmental conditions, using preferred quality control measures. Only the bond to the vessel and the less critical liner splices need be accomplished inside the vessel.
  • cryogenic fluid As the insulated vessel is filled with cryogenic fluid, a small'amount of fluid will permeate slowly through the porous liner where the warmer temperature promptly turns liquid to gas thus creating a reverse or offsetting pressure to prevent further liquid penetration.
  • This conversion of cryogenic liquid to gas taking place at, or just under,the liner surface occurs within the cell size of the foam or in such minute volume that the porosity within the liner provides ample escape paths which prevent the reverse gas pressure from exceeding the liner bond rupture strength.
  • the temperature gradient across the insulation thickness reaches a measure of stability and the gas pressure within the foam insulation will approach near equilibrium with the fluid pressure at the liner surface.
  • the foam insulation will eventually become permeated with the gas type being carried in liquid form, such as hydrogen gas when LH (liquid hydrogen) is being carried, or methane when LNG (liquid natural gas) is being carried.
  • the thermal conductivity of the insulation therefore, will be slightly less than that of the gas type being carried and thus the container is insulated from the liquid gas.
  • the reinforcing fibers within the foam are firmly bonded to the vessel wall and are also firmly bonded to the liner.
  • Both of these bonds must be sufficiently strong to withstand the momentary pressure differential fluctuations during filling the vessel with cryogenic fluid and when emptying the vessel. In addition, these bonds must withstand the loads transmitted to the insulation composite by racking and bending of the vessel in rough seas, along with the forces generated by the cryogenic fluid creating sloshing waves against the surface of the liner.
  • this invention constitutes a novel but realistic approach toward achieving the degree of reliability vital to the successful performance and required service life span of the vessel.
  • Damage to the insulation in the form of liner cracks is readily detected by visual examination of the liner surface and easily repaired with a splice. Debonds between liner and fiber-reinforced foam are also readily detected using proven methods with sonic brush examination, and are repaired by replacing the damaged area.
  • the high tolerance of the insulation system to sustain damage or personnel abuse and still function reliably as cryogenic insulation is noteworthy and small areas of surface damage need only be repaired to maintain the insulation required to achieve minimum boiloff rates of the liquified gas cargo.
  • a vessel for receiving liquified gas at cryogenic temperatures as low as 423F. said vessel having a supporting wall to which is bonded oriented fiberreinforced plastic foam to which a permeable liner is adhesively bonded to its outer surface, said liner being porous to the extent of allowing cryogenic temperature fluids in a liquid state within said vessel to permeate as a gas into said fiber-reinforced foam insulation resulting in a gaseous envelope and a gaseous-liquid interface within the insulation and a state of near equilibrium pressure across said liner, thereby containing said cryogenic fluids in a liquid state in spaced relationship to said supporting wall.
  • a vessel for receiving liquified gas at cryogenic temperatures as set forth in claim 1 wherein a second thickness of foam with a second permeable liner thereon is bonded in overlapping relationship to the first mentioned liner.
  • a vessel for receiving liquified gas at cryogenic temperatures as set forth in claim 6 wherein vertical corners are formed at the intersection of inner hull walls, said vertical corners comprising foam posts wrapped in a fiber glass lining, vertical edges of said foam bonded to said inner hull abutting said foam posts, and fiber glass splices applied over abuttin edges.
  • Avessel for receiving liquified gas at cryogenic I temperatures as set forth in claim 1 wherein said foam with liner bonded thereto is prefabricated in segments and is bonded together with overlapping liner strips bonded to splice adjacent liner edges together to prevent heat leakage paths between segments.
  • a vessel for receiving liquified gas at cryogenic temperatures as in claim 1 wherein said foam has X, Y and Z oriented reinforcing fibers therein, said Z fibers passing through the thickness of said foam with Z fiber ends on one side bonded to said vessel and Z fiber ends on the other of said foam being bonded to said liner.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
US00240362A 1972-04-03 1972-04-03 Cryogenic storage vessel Expired - Lifetime US3814275A (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
US00240362A US3814275A (en) 1972-04-03 1972-04-03 Cryogenic storage vessel
GB1449373A GB1412843A (en) 1972-04-03 1973-03-26 Cryogenic storage vessel
SE7304434A SE388262B (sv) 1972-04-03 1973-03-29 Behallare for inneslutning av i vetskeform overford gas vid kryotemperaturer
ES413249A ES413249A1 (es) 1972-04-03 1973-04-02 Perfeccionamientos en naves oceanicas para el almacenamien-to y transporte de fluidos a temperaturas criogenicas.
CA167,653A CA990227A (en) 1972-04-03 1973-04-02 Cryogenic storage vessel
DE2316859A DE2316859C2 (de) 1972-04-03 1973-04-02 Speicherbehälter zur Aufnahme von verflüssigtem Gas mit Temperaturen bis-253°C
FR7311950A FR2244122B1 (sv) 1972-04-03 1973-04-03
IT49217/73A IT982947B (it) 1972-04-03 1973-04-03 Nave da carico con compartimenti per immagazzinamento criogenico di gas liquidi
JP3819373A JPS5411925B2 (sv) 1972-04-03 1973-04-03

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00240362A US3814275A (en) 1972-04-03 1972-04-03 Cryogenic storage vessel

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US3814275A true US3814275A (en) 1974-06-04

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Application Number Title Priority Date Filing Date
US00240362A Expired - Lifetime US3814275A (en) 1972-04-03 1972-04-03 Cryogenic storage vessel

Country Status (9)

Country Link
US (1) US3814275A (sv)
JP (1) JPS5411925B2 (sv)
CA (1) CA990227A (sv)
DE (1) DE2316859C2 (sv)
ES (1) ES413249A1 (sv)
FR (1) FR2244122B1 (sv)
GB (1) GB1412843A (sv)
IT (1) IT982947B (sv)
SE (1) SE388262B (sv)

Cited By (34)

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US3931908A (en) * 1973-08-02 1976-01-13 Kaiser Aluminum & Chemical Corporation Insulated tank
US3968764A (en) * 1974-10-31 1976-07-13 Moss Rosenberg Verft A/S Ships for transport of liquefied gases
US3988995A (en) * 1974-05-14 1976-11-02 Ulrich Finsterwalder Container for liquefied gas
US3993213A (en) * 1975-09-04 1976-11-23 Mcdonnell Douglas Corporation Thermally insulated cryogenic container
DE2638427A1 (de) * 1975-09-02 1977-03-10 Dow Chemical Co Verfahren zur herstellung eines thermisch isolierenden laminats
DE2710338A1 (de) * 1976-03-09 1977-09-15 Mc Donnell Douglas Corp Tiefsttemperatur-isoliersystem
US4091160A (en) * 1976-03-31 1978-05-23 Rohr Industries, Inc. Acoustical laminate
US4116150A (en) * 1976-03-09 1978-09-26 Mcdonnell Douglas Corporation Cryogenic insulation system
US4155482A (en) * 1975-11-03 1979-05-22 Owens-Corning Fiberglas Corporation Insulated cryogenic liquid container
US4366917A (en) * 1975-03-04 1983-01-04 Technigaz Cryogenic tank
US4660594A (en) * 1985-08-05 1987-04-28 Gocze Thomas E Portable collapsible tank for storing liquid
US4993581A (en) * 1989-05-02 1991-02-19 Mitchell A Ross Dual wall tank
USH943H (en) 1989-12-13 1991-08-06 The United States Of America As Represented By The United States Department Of Energy Organic liner for thermoset composite tank
US5090586A (en) * 1989-05-02 1992-02-25 Madison Chemical Industries Inc. Dual wall tank
US5098795A (en) * 1988-08-10 1992-03-24 Battelle Memorial Institute Composite metal foil and ceramic fabric materials
US5183176A (en) * 1989-11-14 1993-02-02 Meier & Niehaus Gmbh Lining for receptacles
US5611453A (en) * 1993-06-10 1997-03-18 Schwartz; Ian F. Vessel formed of polymeric composite materials
WO2002029311A1 (de) * 2000-10-04 2002-04-11 Mi Developments Austria Ag & Cokg Rohrartige leitung oder behälter zum transport bzw. zum aufbewahren kryogener medien und verfahren zur herstellung
US20050150443A1 (en) * 2004-01-09 2005-07-14 Conocophillips Company High volume liquid containment system for ships
US20060169704A1 (en) * 2003-02-18 2006-08-03 Klaus Brunnhofer Double-walled container for cryogenic liquids
US20070245941A1 (en) * 2004-07-02 2007-10-25 Sandstrom Robert E Lng Sloshing Impact Reduction System
DE102006056821A1 (de) * 2006-12-01 2008-06-05 Institut für Luft- und Kältetechnik gGmbH Thermisches Isolationssystem, insbesondere für LNG-Tankschiffe und Verfahren zu dessen Herstellung
US20090283176A1 (en) * 2008-05-16 2009-11-19 Berry Gene D Cryogenic Capable High Pressure Containers for Compact Storage of Hydrogen Onboard Vehicles
US20100001005A1 (en) * 2008-07-01 2010-01-07 The Boeing Company Composite Cryogenic Tank with Thermal Strain Reducer Coating
US20100012787A1 (en) * 2008-07-18 2010-01-21 Michael Leslie Hand Strong bonded joints for cryogenic application
US20100236312A1 (en) * 2006-06-22 2010-09-23 Matthias Kipping Coiler mandrel
US20110168722A1 (en) * 2010-01-13 2011-07-14 BDT Consultants Inc. Full containment tank
US20120018587A1 (en) * 2010-07-22 2012-01-26 The Boeing Company Fabric Preform Insert for a Composite Tank Y-Joint
US20130136527A1 (en) * 2008-07-18 2013-05-30 The Boeing Company Device for Controlling Stress in Joints at Cryogenic Temperatures and Method of Making the Same
WO2014035510A3 (en) * 2012-07-03 2014-07-03 The Boeing Company Composite tank having joint with softening strip and method of making the tank
US8939407B2 (en) 2011-02-15 2015-01-27 The Boeing Company Common bulkhead for composite propellant tanks
US9453293B2 (en) 2008-07-18 2016-09-27 The Boeing Company Method of making a composite tank having joint with softening strip
US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials

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FR2235330B1 (sv) * 1973-06-27 1977-06-24 Mitsubishi Chem Ind
FR2303230A1 (fr) * 1975-03-03 1976-10-01 Secmapp Systeme, outillage et methode de construction de cuves cryogeniques pour navires methaniers et reservoirs terrestres
GB1530458A (en) * 1975-11-22 1978-11-01 Conch Int Methane Ltd Insulation system for liquefied gas tanks
CN109094741A (zh) * 2018-07-06 2018-12-28 浙江海洋大学 船运易流态货物防流态化的电解减饱和装置及方法
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US4170952A (en) * 1976-03-09 1979-10-16 Mcdonnell Douglas Corporation Cryogenic insulation system
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US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
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US7743940B2 (en) * 2003-02-18 2010-06-29 Magna Steyr Fahrezeugtechnik AG & Co. KG Double-walled container having supports for positioning the inner and outer walls
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US20100001005A1 (en) * 2008-07-01 2010-01-07 The Boeing Company Composite Cryogenic Tank with Thermal Strain Reducer Coating
US8656571B2 (en) 2008-07-18 2014-02-25 The Boeing Company Strong bonded joints for cryogenic applications
US20130136527A1 (en) * 2008-07-18 2013-05-30 The Boeing Company Device for Controlling Stress in Joints at Cryogenic Temperatures and Method of Making the Same
US10399709B2 (en) * 2008-07-18 2019-09-03 The Boeing Company Method of making a device for controlling stress in joints at cryogenic temperatures
US10759547B2 (en) 2008-07-18 2020-09-01 The Boeing Company Strong bonded joints for cryogenic applications
US9453293B2 (en) 2008-07-18 2016-09-27 The Boeing Company Method of making a composite tank having joint with softening strip
US20100012787A1 (en) * 2008-07-18 2010-01-21 Michael Leslie Hand Strong bonded joints for cryogenic application
US10407188B2 (en) 2008-07-18 2019-09-10 The Boeing Company Composite tank having joint with softening strip
US10005570B2 (en) 2008-07-18 2018-06-26 The Boeing Company Strong bonded joints for cryogenic applications
US20110168722A1 (en) * 2010-01-13 2011-07-14 BDT Consultants Inc. Full containment tank
US20120018587A1 (en) * 2010-07-22 2012-01-26 The Boeing Company Fabric Preform Insert for a Composite Tank Y-Joint
US8974135B2 (en) * 2010-07-22 2015-03-10 The Boeing Company Fabric preform insert for a composite tank Y-joint
US10562239B2 (en) 2010-07-22 2020-02-18 The Boeing Company Method for forming a fabric preform insert for a composite tank Y-joint
US8939407B2 (en) 2011-02-15 2015-01-27 The Boeing Company Common bulkhead for composite propellant tanks
CN104428578B (zh) * 2012-07-03 2017-07-28 波音公司 具有带有软化带的接头的复合罐及制造该罐的方法
CN104428578A (zh) * 2012-07-03 2015-03-18 波音公司 具有带有软化带的接头的复合罐及制造该罐的方法
WO2014035510A3 (en) * 2012-07-03 2014-07-03 The Boeing Company Composite tank having joint with softening strip and method of making the tank

Also Published As

Publication number Publication date
GB1412843A (en) 1975-11-05
DE2316859C2 (de) 1981-10-08
JPS4947926A (sv) 1974-05-09
JPS5411925B2 (sv) 1979-05-18
IT982947B (it) 1974-10-21
SE388262B (sv) 1976-09-27
ES413249A1 (es) 1976-01-01
FR2244122B1 (sv) 1977-02-04
DE2316859A1 (de) 1973-10-04
CA990227A (en) 1976-06-01
FR2244122A1 (sv) 1975-04-11

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