US3381843A - Insulation system - Google Patents
Insulation system Download PDFInfo
- Publication number
- US3381843A US3381843A US548309A US54830966A US3381843A US 3381843 A US3381843 A US 3381843A US 548309 A US548309 A US 548309A US 54830966 A US54830966 A US 54830966A US 3381843 A US3381843 A US 3381843A
- Authority
- US
- United States
- Prior art keywords
- panels
- plug
- wall panels
- intersection
- stepped
- 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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Classifications
-
- 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
- F17C13/001—Thermal insulation specially adapted for cryogenic vessels
-
- 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
-
- 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
- F17C2270/0107—Wall panels
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- 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
-
- 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
- Y10S220/902—Foam
Definitions
- the present invention relates to insulated cargo tanks of the type adapted to store liquefied natural gas and the like at cryogenic temperatures and, more particularly, to a new and improved system of interlocking wall panels and plug panels of thermal insulation which form an impervious and stable cargo barrier.
- the insulating wall panels of the invention are generally fiat for flat wall portions, are generally L-shaped for corner portions defined by the intersections of two walls, and are generally boxlike for corner portions defined by the intersections of three walls. All of the wall panels have ascendingly stepped lateral edges.
- the plug panels are interposed in mating relation between the ascendingly stepped edges of the aforementioned wall panels and are correspondingly either of generally fiat or L-shaped configurations and have descendingly stepped side edges.
- the L-shaped and boxlike corner panels are heavily reinforced with internal webbing or stitfeners to provide sufficient strength at the corners of the completed insulation system to safely withstand the accumulated thermal and mechanical stresses which tend to arise at such corners when exposed to cryogenic temperatures.
- the lug panels have end edges which are ascendingly and descendingly stepped and are interlocked to establish extremely rigid joints, the configuration of which substantially reduces the possibility of escaped cryogenic cargo seeping therethrough.
- FIG. 1 is a schematic cross-sectional view of a cargo hold of a double hulled tanker including the insulation system of the present invention
- FIG. 2 is a perspective view of a reinforced, molded three-dimensional corner wall panel embodying the principles of the invention
- FIG. 3 is a fragmentary, perspective view of a corner of an insulted tank showing the interrelationship of the wall panels and plug panels;
- FIG. 4 is a cross-sectional view of a plug panel showing the alternate end edge configurations thereof.
- the overall shape of the insulating barrier of the invention is determined by and generally duplicates that of the inner steel walls 11 of a cargo space 12 of a double hulled vessel 13 of conventional construction.
- the inner walls 11 are completely clad with thermal insulation panels 14 to form a so-called secondary cargo barrier which functions to insulate an inner tank 9 or integral primary cargo barrier (not shown), to provide an impermeable barrier for any leakage of liquefied natural gas and thus protects the vessel structure from the potentially deleterious effects of the supercooled cargo.
- the barrier 10 is established by a series of discrete insulation panels 14, the majority of which are rectangular in shape and characterized as being generally flat. These generally flat panels are designated by reference number 15.
- the panels 16, 17 include transverse internal membranes 18 which provide sufificient strength and rigidity to the corner panels 16, 17 to enable them to withstand the accumulated thermal stress concentrations which tend to localize at the corners of the insulation barrier 10 while it is in service.
- the edges of corner panels 16, 17 are beveled so that they may cooperate with the walls 11 of the supporting structure of triangular cross section to define a channel 19 which may be monitored for gas leakage, the detection of which would, of course, indicate a failure of the cargo barrier.
- the wall panels 15, 16, 17 are fabricated of molded shells 20 of polyester resins reinforced with fiberglass, which shells encapsulate a polyurethane foam filling 21, in accordance with the general teachings of copending application Ser. No. 394,287 of Pratt et al., for Insulation System, filed Sept. 3, 1964.
- the side edges of all of the wall panels 15, 16, 17 are ascendingly stepped with the innermost or cold (in terms of the relation of the installed barrier to the cargo) surfaces of the panels defining the top step 22, and the outermost or warm surfaces of the panels defining the bottom step 23, there being one intermediate step 24, as shown.
- the wall panels 1517 are appropriately afiixed to the walls by suitable means, for example, by using screws and adhesive as described in detail in the above-identified application, in a manner in which their ascendingly stepped edges are parallelly arrayed to define an open grid G.
- the insulating cargo impermeable barrier 10 is completed by filling the spaces between wall panels, i.e., the open grid G, with straight plug panels 26 and L-shaped plug panels 27 formed similarly to the wall panels 15-17 of molded fiberglass reinforced polyester shells which encapsulate polyurethane foam.
- the plug panels 26, 27 may be secured to the wall panels 1517 by adhesives and screws in a manner illustrated in the aforementioned application Ser. No. 394,287.
- the gaps between adjacent wall panels 15-17 are filled with appropriately shaped generally flat plug panels 26 and the gaps of the grid G located at the corners of the tank are filled by L-shaped plug panels 27.
- the illustrated corner intersection of three walls of the barrier 10 embodies all of the shapes of wall panels and plug panels employed in cladding the walls 11 of the cargo hold 12.
- the end edges 28 as well as the side edges 29 of the plug panels are stepped. More specifically, three of the four end edges of the plug panels meeting at every grid intersection are ascendingly stepped and arranged to terminate in alignment with the edges of the wall panels forming the intersection, as shown at the righthand side of the drawing in FIG. 3. The remaining plug-panel which meets at the intersection and completes the joint has a descendingly stepped, extended edge 30 which engages in mating fashion all four of the wall panels at the intersection and the other three lug panels.
- the side edges 29 of all plug panels are descendingly stepped while the end edges may be either ascendingly or descendingly stepped (plug panels with both types of ends being shown in FIG. 4). However, at each grid intersection, only one of the end edges of the four plug panels meeting at the grid intersection is descendingly stepped. Furthermore, the plug panel having the descendingly stepped end edge will be of sufficient length to extend across and to completely fill in the space of the intersection.
- the extended plug panel end edge (which is descendingly stepped) overlaps and mates wit-h the ascendingly stepped edges of the four wall panels, and the three plug panel end edges defining the intersection. Furthermore, all the four side edges of all of the plug panels overlap the ascendingly stepped edges of the wall panels. Therefore, in accordance with the invention, this overlapping, interlocking arrangement of plug and wall panels establishes a substantially rigid barrier, the joints of which provide a tortuous and substantially impenetrable path for escaped cryogenic cargo. Accordingly, the new and improved barrier construction tends to minimize strike through of liquefied natural gas that may have leaked through a primary barrier.
- a continuous insulating barrier construction comprising (a) a closed supporting structure having inner surfaces of predetermined geometric configuration;
- each intersection within the gridlike network being filled by an integral extension of one of said plug pieces;
- said boxlike and said L-shaped wall panels include sufficient reinforcement to withstand stresses developed therein.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
L A T E N A M R O F D c INSULATION SYSTEM Filed May a, 1966 5 SheetsSheet l N A M W F D S E L R A H JOHN REEVES ATTORNEY y 1968 c. D. FORMAN ETAL 3,381,843
INSULATION SYSTEM Filed May 6, 1966 5 Sheets-Sheet 2 r (\WWW co K R. Q Q Q 0 I INVENTORS CHARLES 0. FORMAN w BY JOHN REEVES LL mwommawr y 1968 c. D. FORMAN ETAL 3,381,843
INSULATION SYSTEM Filed May 6, 1966 5 Sheets$heet 5 .INVENTORS CHARLES D. FORMAN BY JOHN F. REEVES Ema/FM ATTORNEY United States Patent 3,381,843 INSULATION SYSTEM Charles D. Forman, Elizabeth, NJ., and John F. Reeves,
Milwaukee, Wis., assignors to Esso Research and Engineering Company, a corporation of Delaware Filed May 6, 1966, Ser. No. 548,309 4 Claims. (Cl. 2209) The present invention relates to insulated cargo tanks of the type adapted to store liquefied natural gas and the like at cryogenic temperatures and, more particularly, to a new and improved system of interlocking wall panels and plug panels of thermal insulation which form an impervious and stable cargo barrier.
The insulating wall panels of the invention are generally fiat for flat wall portions, are generally L-shaped for corner portions defined by the intersections of two walls, and are generally boxlike for corner portions defined by the intersections of three walls. All of the wall panels have ascendingly stepped lateral edges. The plug panels are interposed in mating relation between the ascendingly stepped edges of the aforementioned wall panels and are correspondingly either of generally fiat or L-shaped configurations and have descendingly stepped side edges. As an important aspect of the invention, the L-shaped and boxlike corner panels are heavily reinforced with internal webbing or stitfeners to provide sufficient strength at the corners of the completed insulation system to safely withstand the accumulated thermal and mechanical stresses which tend to arise at such corners when exposed to cryogenic temperatures.
As a further important aspect of the invention, the lug panels have end edges which are ascendingly and descendingly stepped and are interlocked to establish extremely rigid joints, the configuration of which substantially reduces the possibility of escaped cryogenic cargo seeping therethrough.
For a more complete understanding of the invention and its attendant advantages, reference should be made to the following detailed description taken in conjunction with the accompanying drawings, in which:
FIG. 1 is a schematic cross-sectional view of a cargo hold of a double hulled tanker including the insulation system of the present invention;
FIG. 2 is a perspective view of a reinforced, molded three-dimensional corner wall panel embodying the principles of the invention;
FIG. 3 is a fragmentary, perspective view of a corner of an insulted tank showing the interrelationship of the wall panels and plug panels; and
FIG. 4 is a cross-sectional view of a plug panel showing the alternate end edge configurations thereof.
Referring to FIG. 1, the overall shape of the insulating barrier of the invention is determined by and generally duplicates that of the inner steel walls 11 of a cargo space 12 of a double hulled vessel 13 of conventional construction.
Specifically, the inner walls 11 are completely clad with thermal insulation panels 14 to form a so-called secondary cargo barrier which functions to insulate an inner tank 9 or integral primary cargo barrier (not shown), to provide an impermeable barrier for any leakage of liquefied natural gas and thus protects the vessel structure from the potentially deleterious effects of the supercooled cargo.
In accordance with the invention, the barrier 10 is established by a series of discrete insulation panels 14, the majority of which are rectangular in shape and characterized as being generally flat. These generally flat panels are designated by reference number 15.
The corners of the cargo space 12 are clad by new and improved L-shaped panels 16 and boxlike panels 17. In accordance with the inventive principles, the panels 16, 17 include transverse internal membranes 18 which provide sufificient strength and rigidity to the corner panels 16, 17 to enable them to withstand the accumulated thermal stress concentrations which tend to localize at the corners of the insulation barrier 10 while it is in service. As shown, the edges of corner panels 16, 17 are beveled so that they may cooperate with the walls 11 of the supporting structure of triangular cross section to define a channel 19 which may be monitored for gas leakage, the detection of which would, of course, indicate a failure of the cargo barrier. The wall panels 15, 16, 17 are fabricated of molded shells 20 of polyester resins reinforced with fiberglass, which shells encapsulate a polyurethane foam filling 21, in accordance with the general teachings of copending application Ser. No. 394,287 of Pratt et al., for Insulation System, filed Sept. 3, 1964.
In accordance with the invention, the side edges of all of the wall panels 15, 16, 17 are ascendingly stepped with the innermost or cold (in terms of the relation of the installed barrier to the cargo) surfaces of the panels defining the top step 22, and the outermost or warm surfaces of the panels defining the bottom step 23, there being one intermediate step 24, as shown.
The wall panels 1517 are appropriately afiixed to the walls by suitable means, for example, by using screws and adhesive as described in detail in the above-identified application, in a manner in which their ascendingly stepped edges are parallelly arrayed to define an open grid G. In accordance with the invention, the insulating cargo impermeable barrier 10 is completed by filling the spaces between wall panels, i.e., the open grid G, with straight plug panels 26 and L-shaped plug panels 27 formed similarly to the wall panels 15-17 of molded fiberglass reinforced polyester shells which encapsulate polyurethane foam. The plug panels 26, 27 may be secured to the wall panels 1517 by adhesives and screws in a manner illustrated in the aforementioned application Ser. No. 394,287. Thus, as shown in FIG. 3, the gaps between adjacent wall panels 15-17 are filled with appropriately shaped generally flat plug panels 26 and the gaps of the grid G located at the corners of the tank are filled by L-shaped plug panels 27. It should be understood that the illustrated corner intersection of three walls of the barrier 10 embodies all of the shapes of wall panels and plug panels employed in cladding the walls 11 of the cargo hold 12.
In accordance with the invention, the end edges 28 as well as the side edges 29 of the plug panels are stepped. More specifically, three of the four end edges of the plug panels meeting at every grid intersection are ascendingly stepped and arranged to terminate in alignment with the edges of the wall panels forming the intersection, as shown at the righthand side of the drawing in FIG. 3. The remaining plug-panel which meets at the intersection and completes the joint has a descendingly stepped, extended edge 30 which engages in mating fashion all four of the wall panels at the intersection and the other three lug panels. As will be understood, the side edges 29 of all plug panels are descendingly stepped while the end edges may be either ascendingly or descendingly stepped (plug panels with both types of ends being shown in FIG. 4). However, at each grid intersection, only one of the end edges of the four plug panels meeting at the grid intersection is descendingly stepped. Furthermore, the plug panel having the descendingly stepped end edge will be of sufficient length to extend across and to completely fill in the space of the intersection.
Accordingly, it should be understood, at every grid intersection, the extended plug panel end edge (which is descendingly stepped) overlaps and mates wit-h the ascendingly stepped edges of the four wall panels, and the three plug panel end edges defining the intersection. Furthermore, all the four side edges of all of the plug panels overlap the ascendingly stepped edges of the wall panels. Therefore, in accordance with the invention, this overlapping, interlocking arrangement of plug and wall panels establishes a substantially rigid barrier, the joints of which provide a tortuous and substantially impenetrable path for escaped cryogenic cargo. Accordingly, the new and improved barrier construction tends to minimize strike through of liquefied natural gas that may have leaked through a primary barrier.
It should be understood that the specific structure herein illustrated and described is intended to be representative only, as certain changes may be made therein with out departing from the clear teachings of the disclosure. Accordingly, reference should be made to the following appended claims in determining the full scope of the in vention.
What is claimed is:
1. A continuous insulating barrier construction comprising (a) a closed supporting structure having inner surfaces of predetermined geometric configuration;
(b) a plurality of insulation wall panels secured to said inner surfaces of said supporting structure;
(c) said wall panels having ascendingly stepped side edges defining a gridlike network of gaps therebetween;
(d) a plurality of insulation plug panels filling the gaps between opposed longitudinal sides of said wall panels;
(e) each intersection within the gridlike network being filled by an integral extension of one of said plug pieces;
(f) said extension engaging the ends of three other plug pieces terminating at said grid intersection;
(g) the innermost layer of said extension being superimposed upon the intermediate layers of said three other plug pieces and the intermediate layers of at least portions of the four wall panels defining said grid intersection.
2. A barrier construction in accordance with claim 1,
in which (a) the intersections of adjacent walls of said barrier being formed -by molded L-shaped wall panels and plug panels;
(b) the corner intersections of three walls of said barrier being formed by molded boxlike wall panels having portions coplanar with each of the intersecting walls.
3. A barrier construction in accordance with claim 2,
in which (a) said boxlike and said L-shaped wall panels include sufficient reinforcement to withstand stresses developed therein.
4. A barrier construction in accordance with claim 1,
in which (a) all of the side edges of said plug panels are descendingly stepped;
(b) one of the four end edges of the plug panels meeting at each intersection is descendingly stepped;
(c) the end edges of the other three plug panels meeting at said intersection are ascendingly stepped.
References Cited UNITED STATES PATENTS 3,158,459 11/1964 Guilhem 22015 3,298,345 1/ 1967 Pratt.
3,339,780 9/1967 Forman et a1.
3,341,051 9/1967 Forman et al.
THERON E. CONDON, Primary Examiner.
J. R. GARRETT, Examiner.
Claims (1)
1. A CONTINUOUS INSULATING BARRIER CONSTRUCTION COMPRISING (A) A CLOSED SUPPORTING STRUCTURE HAVING INNER SURFACES OF PREDETERMINED GEOMETRIC CONFIGURATION; (B) A PLURALITY OF INSULATION WALL PANELS SECURED TO SAID INNER SURFACES OF SAID SUPPORTING STRUCTURE; (C) SAID WALL PANELS HAVING ASCENDINGLY STEPPED SIDE EDGES DEFINING A GRIDLIKE NETWORK OF GAPS THEREBETWEEN; (D) A PLURALITY OF INSULATION PLUG PANELS FILLING THE GAPS BETWEEN OPPOSED LONGITUDINAL SIDES OF SAID WALL PANELS; (E) EACH INTERSECTION WITHIN THE GRIDLIKE NETWORK BEING FILLED BY AN INTEGRAL EXTENSION OF ONE OF SAID PLUG PIECES; (F) SAID EXTENSION ENGAGING THE ENDS OF THREE OTHER PLUG PIECES TERMINATING AT SAID GRID INTERSECTION; (G) THE INNERMOST LAYER OF SAID EXTENSION BEING SUPERIMPOSED UPON THE INTERMEDIATE LAYERS OF SAID THREE OTHER PLUG PIECES AND THE INTERMEDIATE LAYERS OF AT LEAST PORTIONS OF THE FOUR WALL PANELS DEFINING SAID GRID INTERSECTION.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US548309A US3381843A (en) | 1966-05-06 | 1966-05-06 | Insulation system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US548309A US3381843A (en) | 1966-05-06 | 1966-05-06 | Insulation system |
Publications (1)
Publication Number | Publication Date |
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US3381843A true US3381843A (en) | 1968-05-07 |
Family
ID=24188274
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US548309A Expired - Lifetime US3381843A (en) | 1966-05-06 | 1966-05-06 | Insulation system |
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US (1) | US3381843A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3557992A (en) * | 1968-05-29 | 1971-01-26 | Litewate Transport Equipment C | Unitary molded plastic structures |
US3765558A (en) * | 1971-01-04 | 1973-10-16 | Arctic Tanker Group Inc | Cryogenic tank design and method of manufacture |
US5258159A (en) * | 1990-05-02 | 1993-11-02 | The Budd Company | Process for making a fiber reinforced fuel tank |
US5344038A (en) * | 1988-10-14 | 1994-09-06 | The Budd Company | Composite fuel tank |
WO2015132498A1 (en) * | 2014-03-04 | 2015-09-11 | Gaztransport Et Technigaz | Sealed and insulating vessel comprising a deflection element allowing the flow of gas at a corner |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3158459A (en) * | 1960-03-22 | 1964-11-24 | & Chantiers De La Seine Mariti | Self-discharging container for conveying and storing low temperature fluids or othermaterials |
US3298345A (en) * | 1964-11-13 | 1967-01-17 | Exxon Research Engineering Co | Double hulled ship |
US3339780A (en) * | 1964-11-06 | 1967-09-05 | Exxon Research Engineering Co | Duplex insulating panel |
US3341051A (en) * | 1964-12-24 | 1967-09-12 | Exxon Research Engineering Co | Cryogenic insulation system |
-
1966
- 1966-05-06 US US548309A patent/US3381843A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3158459A (en) * | 1960-03-22 | 1964-11-24 | & Chantiers De La Seine Mariti | Self-discharging container for conveying and storing low temperature fluids or othermaterials |
US3339780A (en) * | 1964-11-06 | 1967-09-05 | Exxon Research Engineering Co | Duplex insulating panel |
US3298345A (en) * | 1964-11-13 | 1967-01-17 | Exxon Research Engineering Co | Double hulled ship |
US3341051A (en) * | 1964-12-24 | 1967-09-12 | Exxon Research Engineering Co | Cryogenic insulation system |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3557992A (en) * | 1968-05-29 | 1971-01-26 | Litewate Transport Equipment C | Unitary molded plastic structures |
US3765558A (en) * | 1971-01-04 | 1973-10-16 | Arctic Tanker Group Inc | Cryogenic tank design and method of manufacture |
US5344038A (en) * | 1988-10-14 | 1994-09-06 | The Budd Company | Composite fuel tank |
US5258159A (en) * | 1990-05-02 | 1993-11-02 | The Budd Company | Process for making a fiber reinforced fuel tank |
WO2015132498A1 (en) * | 2014-03-04 | 2015-09-11 | Gaztransport Et Technigaz | Sealed and insulating vessel comprising a deflection element allowing the flow of gas at a corner |
FR3018338A1 (en) * | 2014-03-04 | 2015-09-11 | Gaztransp Et Technigaz | SEALED AND INSULATING TANK WITH A DEFLECTION ELEMENT FOR GAS FLOW AT AN ANGLE |
CN106164564A (en) * | 2014-03-04 | 2016-11-23 | 气体运输技术公司 | A kind of sealing comprising the deflecting element allowing corner gas flowing and insulating vessel |
JP2017512284A (en) * | 2014-03-04 | 2017-05-18 | ギャズトランスポルト エ テクニギャズ | Sealed insulated container with deflecting elements allowing gas flow in the corners |
CN106164564B (en) * | 2014-03-04 | 2018-03-27 | 气体运输技术公司 | A kind of sealing comprising the deflecting element for allowing corner gas to flow and insulating vessel |
AU2015226021B2 (en) * | 2014-03-04 | 2019-03-28 | Gaztransport Et Technigaz | Sealed and insulating vessel comprising a deflection element allowing the flow of gas at a corner |
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