US3622030A - Tank for use in storing low-temperature liquefied gas - Google Patents
Tank for use in storing low-temperature liquefied gas Download PDFInfo
- Publication number
- US3622030A US3622030A US876288A US3622030DA US3622030A US 3622030 A US3622030 A US 3622030A US 876288 A US876288 A US 876288A US 3622030D A US3622030D A US 3622030DA US 3622030 A US3622030 A US 3622030A
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- United States
- Prior art keywords
- corrugation
- vessel
- inner vessel
- insulating layer
- tank
- 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
Links
- 238000010276 construction Methods 0.000 abstract description 10
- 239000010409 thin film Substances 0.000 abstract description 8
- 239000007788 liquid Substances 0.000 description 7
- 230000008602 contraction Effects 0.000 description 4
- 238000005452 bending Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 235000019362 perlite Nutrition 0.000 description 1
- 239000010451 perlite Substances 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000037303 wrinkles Effects 0.000 description 1
Images
Classifications
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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
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/022—Land-based bulk storage containers
-
- 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
- F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
-
- 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
- F17C2201/0119—Shape cylindrical with flat end-piece
-
- 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
- F17C2201/03—Orientation
- F17C2201/032—Orientation with substantially vertical main axis
-
- 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
- F17C2203/01—Reinforcing or suspension means
- F17C2203/014—Suspension means
- F17C2203/015—Bars
-
- 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
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0337—Granular
- F17C2203/0341—Perlite
-
- 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
- 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
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0636—Metals
- F17C2203/0639—Steels
-
- 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
- F17C2203/0634—Materials for walls or layers thereof
- F17C2203/0678—Concrete
-
- 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
-
- 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
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/03—Dealing with losses
- F17C2260/031—Dealing with losses due to heat transfer
- F17C2260/033—Dealing with losses due to heat transfer by enhancing insulation
-
- 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
- a tank for use in storing low-temperature liquefied gas has an inner vessel composed of a thin film construction suspended from the top wall of an outer vessel, and is constructed so that corrugations vertically formed on the sidewall of said inner vessel may be contracted under the lowtemperature loaded condition to approach a smooth configuration in close contact with a heat-insulating layer provided between said outer and inner vessels.
- an increase in length is produced along the outer top part of each corrugation due to the difference in length between the outer top part and inner top part of each corrugation, and said increased length appears as an additional corrugation.
- the present invention relates generally to a tank for use in storing low-temperature liquefied gas having an inner vessel of a thin film or membrane construction, and more particularly to a storage tank in which the sidewall of said inner vessel is suspended at its upper end portions from the top wall or the ceiling part of an outer vessel.
- the inner vessel is designed so that the thermal contraction movement in the vertical section may be smooth by connecting the sidewall with the bottom wall of the inner vessel through a curved comer therebetween, but said corrugations stretch out to the curved bottom corner and gradually become null at this curved bottom corner.
- this curved bottom comer needs close contact with the identically curved surface of the heat-insulating layer behind the inner vessel when the corrugations on the curved bottom corner become stretched out.
- the present invention is intended to avoid said defects of the suspended type of a storage tank having a thin film construction.
- the present invention is characterized in that a part of the surface of the heat-insulating layer behind the outer top part is eliminated in advance to form a recess. The deformed outer part of said corrugation is allowed to project into the recess under the lowtemperature loaded condition.
- the pressure given inside the tank can be transmitted to the outer vessel without causing any stress on the inner vessel itself for the reason that the above-described arrangement enables almost the whole surface of the curved bottom corner of the inner vessel to abut the surface of the heat insulating layer.
- FIG. 1 is a view of a vertical section of a suspended type of tank used for storing low-temperature liquefied gas
- FIG. 2 is a view illustrating the curved bottom comer of the inner vessel of the tank
- FIG. 3 is a view illustrating the curved bottom comer of the heat-insulating layer with the present invention adapted thereto;
- FIG. 4 is a deformation at the curved inner vessel of a conventional tank.
- FIG. I shows the whole structure of a suspended type of a tank for use in storing low-temperature liquefied gas having a thin film construction.
- FIG. 1 there is shown the outer vessel 1 composed of such a rigid material as ordinary steel, and the heat-insulating layer 2 composed of perlite concrete of rigid-foamed polyurethane having compression resistant properties.
- the inner vessel composed of thin metallic plate having antilow-temperature property is provided inside this heat-insulating layer 2.
- the sidewall 3 and the bottom wall 6 of the inner vessel are connected with each other through the curved bottom comer 5 and form a kind of a liquid-tight bag.
- the upper end portion 7 of the inner vessel is suspended from the top structure 9 of the outer vessel through the means of balancing counterweight members 8.
- the lower end portion of the corrugations reaches the curved bottom center 5, wherein the corrugations gradually diminish and finally become null.
- the outer topline l0'-l0" and the inner top line 1 l'1 l of the corrugation 4 are different from each other in length; the outer topline 10'l0" is longer than the inner top line ll'll" Therefore if the surface of the bottom corner of the heat-insulating layer is formed in the shape of a simple curved surface, and when the curved corner of the inner vessel contacts closely with the heat-insulating layer afier being stretched out by liquid pressure, the curved bottom comer of the inner vessel may be deformed as shown in FIG. 4. In FIG.
- a two-dotted chain line 4 shows the state of a corrugation before the curved bottom corner 5 is deformed by liquid pressure.
- the point 11 on the corrugation comes to the point 11" and contacts with the heat-insulating layer, and the curved bottom comer 5 at this stage is shown by a full line.
- the point 10' on the outer part of the corrugation comes to the point 10" by the effects of thermal contraction of the inner vessel in the vertical section and by those of shearing force working in the material of the inner vessel.
- the outer top line 10l0" rugation is longer than the topline ll '-11" which is equal to the line ll'l1" in length, and therefore the surplus produced by the difference of the two lines in length appears as a new corrugation or a projecting part 12.
- a projecting part is unfavorable since it causes an extremely sharp bending or collapse at this part due to liquid pressure thereupon.
- a part of the heat-insulating layer situated just behind the outer part of the corrugation is recessed, as shown at 13 in FIG. 3, in accordance with the present invention.
- the outer part 10 of a corrugation 4 at the curved bottom corner 5 of the inner vessel is allowed to bottom comer of the of the corproject outward when it is deformed by liquid pressure, and it is prevented from forming an inwardly projecting part 12, or a part projecting toward the center of the tank.
- the deformed outer part of a corrugation, projecting outward fits in the dent formed in advance and contacts closely with the wall surface of the dent 13, thereby alleviating any extremely concentrated stress on the inner vessel.
- the internal pressure on the tank is transmitted to the outer ve$el through the heat-insulating layer and is supported by this outer vessel; and as mentioned above, according to the present invention, substantially all of the surface of the curved bottom corner of the inner vessel contacts closely with the surface of the heat-insulating layer under the low-temperature loaded condition.
- a tank for use in storing low-temperature liquefied gas comprising an outer vessel of a rigid construction, a compression-resistant heat-insulating layer of material provided as a lining in contact with the inner surfaces of said outer vessel, and an inner vessel of a deformable thin film or membranous construction provided inwardly of said heat-insulating layer, said inner vessel having a sidewall suspended at its upper end portions from the top part of said outer vessel and connected at its lower end by a curved comer portion to the bottom wall of said inner vessel, said inner vessel sidewall having vertical corrugations defining inner and outer crests and additional corrugations which are continuations of said vertical corrugations and which taper from an upper region of said curved comer portion toward and finally flatten out at said bottom wall, said heat-insulating layer having a sidewall and a bottom wall interconnected by a curved comer portion, wherein an inner surface of said curved portion of said insulating layer has a plurality of recesses therein, said recesses being align
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
A tank for use in storing low-temperature liquefied gas has an inner vessel composed of a thin film construction suspended from the top wall of an outer vessel, and is constructed so that corrugations vertically formed on the sidewall of said inner vessel may be contracted under the low-temperature loaded condition to approach a smooth configuration in close contact with a heat-insulating layer provided between said outer and inner vessels. At the curved bottom corner of said inner vessel, an increase in length is produced along the outer top part of each corrugation due to the difference in length between the outer top part and inner top part of each corrugation, and said increased length appears as an additional corrugation. To prevent collapse of the additional corrugation, when the vessel is loaded, a part of the heat-insulating layer is eliminated to form a recess for the outer part of the additional corrugation, thereby providing it with a smooth deformation.
Description
United States Patent 72] inventor Katsuro Yamamoto Tokyo, Japan [21 Appl. No. 876,288 [22] Filed Nov. 13, 1969 [45] Patented Nov. 23, 11971 [73] Assignee Bridgestone Liquefied Gas Company Limited Tokyo, Japan [32] Priority Nov. 15, 1968 [33] Japan [31 43/83397 l 54] TANK FOR USE IN STORING LOW- TEMPERATURE LIQUEFIED GAS 1 Claim, 4 Drawing Figs. [52] 11.8. CI 220/10, 220/9 LG [51 Int. Cl 865d 7/22 [50] Field of Search 220/10, 9 LG, 9 F; 62/45 [5 6] References Cited UNITED STATES PATENTS 685,832 11/1901 Gender 220/72 2,889,953 6/1959 Morrison 220/9 LG 3,047,184 7/l 962 Van Bergen et al. 2 20/l8 X 3,085,708 4/1963 Dosker 220/9 LG 3,150,795 9/1964 Schlumberger 220/9 LG FOREIGN PATENTS 924,803 5/1963 Great Britain 220/9 LG Primary E.\'aminer.loseph R. Leclair Assistant Examiner-James R. Garrett Attorneys-Robert E. Burns and Emmanuel J. Lobato ABSTRACT: A tank for use in storing low-temperature liquefied gas has an inner vessel composed of a thin film construction suspended from the top wall of an outer vessel, and is constructed so that corrugations vertically formed on the sidewall of said inner vessel may be contracted under the lowtemperature loaded condition to approach a smooth configuration in close contact with a heat-insulating layer provided between said outer and inner vessels. At the curved bottom corner of said inner vessel, an increase in length is produced along the outer top part of each corrugation due to the difference in length between the outer top part and inner top part of each corrugation, and said increased length appears as an additional corrugation. To prevent collapse of the additional corrugation, when the vessel is loaded, a part of the heat-insulating layer is eliminated to form a recess for the outer part of the additional corrugation. thereby providing it with a smooth QS EUIW i I iiinkibmwa l z z y t t A e E 1 -02? I I I [III I I III III I II I I I TANK FOR USE IN STORING LOW-TEMPERA'IUiZE LIQUEFIED GAS The present invention relates generally to a tank for use in storing low-temperature liquefied gas having an inner vessel of a thin film or membrane construction, and more particularly to a storage tank in which the sidewall of said inner vessel is suspended at its upper end portions from the top wall or the ceiling part of an outer vessel.
In this suspended type of storage tank having a thin film construction, of an inner vessel. These vertical corrugations are prepared to be stretched out so as to approach contact with the surface of a heat-insulating layer, disposed between the inner and outer vessels, under the low-temperature loaded condition, that is, when low-temperature liquefied gas is supplied into the storage tank and liquid pressure acts thereupon.
Accordingly, pressure inside the tank is transmitted, through the above-mentioned heat-insulating layer having compression resistant properties, to the outer vessel having a rigid construction, and is finally received by the outer vessel. Therefore, stresses do not act substantially upon the inner vessel which may be designed primarily to prevent the leakage of liquid. However, suspended-type storage tanks having a thin film construction involve other problems. In particular, the inner vessel is designed so that the thermal contraction movement in the vertical section may be smooth by connecting the sidewall with the bottom wall of the inner vessel through a curved comer therebetween, but said corrugations stretch out to the curved bottom corner and gradually become null at this curved bottom corner. Under the low-temperature loaded condition, this curved bottom comer needs close contact with the identically curved surface of the heat-insulating layer behind the inner vessel when the corrugations on the curved bottom corner become stretched out. Actually, however, at such a curved bottom comer, there is a difference in length between the outer top part of the corrugation and the inner top part of the corrugation in the vertical section of the corrugation. That is, the outer topline of a corrugation (the part of a corrugation closer to the heat-insulating layer) is longer than the inner topline of a corrugation. Therefore, when the curved bottom comer with corrugations thereupon is stretched out to establish a close contact with the heat-insulating layer, an extra or a surplus length of the outer topline is produced. This surplus length appears as a new-formed corrugation or a projecting part, which easily results in a sharp-bending or collapse when acted upon by liquid pressure in the tank because of the empty space therebehind. This sharp bending or collapse is apt to damage the inner vessel made of a thin metallic plate at this part. In other words, the inner vessel, which is designed to be relieved of any stress, will be subject to stress upon the above-mentioned part.
The present invention is intended to avoid said defects of the suspended type of a storage tank having a thin film construction. For the purpose of absorbing the surplus length of the outer part of a corrugation produced by the difference in length between the inner topline and the outer topline of a corrugation in the vertical section at the curved bottom comer under the low-temperature loaded condition, the present invention is characterized in that a part of the surface of the heat-insulating layer behind the outer top part is eliminated in advance to form a recess. The deformed outer part of said corrugation is allowed to project into the recess under the lowtemperature loaded condition. Thus, the pressure given inside the tank can be transmitted to the outer vessel without causing any stress on the inner vessel itself for the reason that the above-described arrangement enables almost the whole surface of the curved bottom corner of the inner vessel to abut the surface of the heat insulating layer.
For a better understanding of the invention, reference will be taken to the accompanying drawings as an embodiment of the present invention.
FIG. 1 is a view of a vertical section of a suspended type of tank used for storing low-temperature liquefied gas;
vertical corrugations are formed in the sidewall FIG. 2 is a view illustrating the curved bottom comer of the inner vessel of the tank;
FIG. 3 is a view illustrating the curved bottom comer of the heat-insulating layer with the present invention adapted thereto;
. FIG. 4 is a deformation at the curved inner vessel of a conventional tank.
Referring more particularly to the drawings, FIG. I shows the whole structure of a suspended type of a tank for use in storing low-temperature liquefied gas having a thin film construction.
In FIG. 1 there is shown the outer vessel 1 composed of such a rigid material as ordinary steel, and the heat-insulating layer 2 composed of perlite concrete of rigid-foamed polyurethane having compression resistant properties. Inside this heat-insulating layer 2, the inner vessel composed of thin metallic plate having antilow-temperature property is provided. The sidewall 3 and the bottom wall 6 of the inner vessel are connected with each other through the curved bottom comer 5 and form a kind of a liquid-tight bag. The upper end portion 7 of the inner vessel is suspended from the top structure 9 of the outer vessel through the means of balancing counterweight members 8.
Thennal contraction of the inner vessel in the vertical section is possible without any trouble since each portion of the inner vessel moves smoothly in the direction of the arrowhead (A). The curved bottom comer enables said movement; that is, the sliding movement of the sidewall of the inner vessel toward the bottom comer proceeds smoothly.
Vertically running corrugations or wrinkles 4 are formed on the sidewall 3 of the inner vessel. When the inner vessel is subject to low-temperature load, these corrugations are stretch out by the internal pressure on the tank, so that the thermal contraction of the inner vessel in the circumferential direction is compensated, and finally the surface of the inner vessel becomes almost flat into a close contact with the surface of the heat-insulating layer 2. Thus, the internal pressure on the tank is transmitted through the heat-insulating layer to the outer vessel which has a rigid construction, and any substantial stress does not act upon the inner vessel.
The lower end portion of the corrugations reaches the curved bottom center 5, wherein the corrugations gradually diminish and finally become null. At this curved bottom comer, the outer topline l0'-l0" and the inner top line 1 l'1 l of the corrugation 4 are different from each other in length; the outer topline 10'l0" is longer than the inner top line ll'll" Therefore if the surface of the bottom corner of the heat-insulating layer is formed in the shape of a simple curved surface, and when the curved corner of the inner vessel contacts closely with the heat-insulating layer afier being stretched out by liquid pressure, the curved bottom comer of the inner vessel may be deformed as shown in FIG. 4. In FIG. 4, a two-dotted chain line 4 shows the state of a corrugation before the curved bottom corner 5 is deformed by liquid pressure. After the corrugation is stretched out, the point 11 on the corrugation comes to the point 11" and contacts with the heat-insulating layer, and the curved bottom comer 5 at this stage is shown by a full line. The point 10' on the outer part of the corrugation comes to the point 10" by the effects of thermal contraction of the inner vessel in the vertical section and by those of shearing force working in the material of the inner vessel.
As mentioned above, the outer top line 10l0" rugation is longer than the topline ll '-11" which is equal to the line ll'l1" in length, and therefore the surplus produced by the difference of the two lines in length appears as a new corrugation or a projecting part 12. But such a projecting part is unfavorable since it causes an extremely sharp bending or collapse at this part due to liquid pressure thereupon. In order to solve this problem, a part of the heat-insulating layer situated just behind the outer part of the corrugation, is recessed, as shown at 13 in FIG. 3, in accordance with the present invention. Thus, the outer part 10 of a corrugation 4 at the curved bottom corner 5 of the inner vessel is allowed to bottom comer of the of the corproject outward when it is deformed by liquid pressure, and it is prevented from forming an inwardly projecting part 12, or a part projecting toward the center of the tank. The deformed outer part of a corrugation, projecting outward, fits in the dent formed in advance and contacts closely with the wall surface of the dent 13, thereby alleviating any extremely concentrated stress on the inner vessel. Thus, the internal pressure on the tank is transmitted to the outer ve$el through the heat-insulating layer and is supported by this outer vessel; and as mentioned above, according to the present invention, substantially all of the surface of the curved bottom corner of the inner vessel contacts closely with the surface of the heat-insulating layer under the low-temperature loaded condition.
Although the present invention has been particularly shown and described, it is a matter of course that various changes and modifications may be made without departing from the scope of the present invention.
What is claimed is:
l. A tank for use in storing low-temperature liquefied gas, comprising an outer vessel of a rigid construction, a compression-resistant heat-insulating layer of material provided as a lining in contact with the inner surfaces of said outer vessel, and an inner vessel of a deformable thin film or membranous construction provided inwardly of said heat-insulating layer, said inner vessel having a sidewall suspended at its upper end portions from the top part of said outer vessel and connected at its lower end by a curved comer portion to the bottom wall of said inner vessel, said inner vessel sidewall having vertical corrugations defining inner and outer crests and additional corrugations which are continuations of said vertical corrugations and which taper from an upper region of said curved comer portion toward and finally flatten out at said bottom wall, said heat-insulating layer having a sidewall and a bottom wall interconnected by a curved comer portion, wherein an inner surface of said curved portion of said insulating layer has a plurality of recesses therein, said recesses being aligned with the outer crests of said inner vessel corrugations so that when the inner vessel is filled with a low-temperature liquified gas which flattens out the corrugations, the portions of the inner vessel in the region of the outer crests of the corrugations in said curved comer portion can deform to project outwardly into said recesses to compensate for a surplus length of the outer crests of said corrugations over the inner crests in the region of said curved comer portion, to provide supported outward deformation of said inner vessel at said recesses.
* 4! t i i
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP43083397A JPS4831569B1 (en) | 1968-11-15 | 1968-11-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3622030A true US3622030A (en) | 1971-11-23 |
Family
ID=13801281
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US876288A Expired - Lifetime US3622030A (en) | 1968-11-15 | 1969-11-13 | Tank for use in storing low-temperature liquefied gas |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3622030A (en) |
| JP (1) | JPS4831569B1 (en) |
| DE (1) | DE1956289A1 (en) |
| FR (1) | FR2023428A1 (en) |
| GB (1) | GB1261258A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3712500A (en) * | 1971-08-06 | 1973-01-23 | Preload Eng Co | Liner for cryogenic container |
| US3827135A (en) * | 1972-03-13 | 1974-08-06 | Bridgestone Liquefied Gas Co | Method of constructing a low temperature liquefied gas tank of a membrane type |
| US3827136A (en) * | 1972-03-25 | 1974-08-06 | Bridgestone Liquefied Gas Co | Method of constructing a low temperature liquefied gas tank of a membrane type |
| US3861553A (en) * | 1971-11-24 | 1975-01-21 | Bridgestone Liquefied Gas Co | Means for supporting an inner membranous vessel of a low temperature liquefied gas tank of a membrane type |
| US3904067A (en) * | 1972-09-22 | 1975-09-09 | Ishikawajima Harima Heavy Ind | Membrane tank for liquefied gases |
| US4919366A (en) * | 1988-09-23 | 1990-04-24 | Mmi Incorporated | Heat resistive wall assembly for a space vehicle |
| US20080209918A1 (en) * | 2007-03-02 | 2008-09-04 | Enersea Transport Llc | Storing, transporting and handling compressed fluids |
| US20090152278A1 (en) * | 2007-12-14 | 2009-06-18 | Markus Lindner | Inner shell for a pressure vessel |
| US20090321452A1 (en) * | 2006-06-14 | 2009-12-31 | L'Air Liquide Societe Anonyme Pour L'Etude Et L'Expolitation Des Procedes Georges Claude | System for Insulating a Cyrogenic Tank and Method of Insulating said Tank |
| US20110168722A1 (en) * | 2010-01-13 | 2011-07-14 | BDT Consultants Inc. | Full containment tank |
| WO2024261466A1 (en) * | 2023-06-20 | 2024-12-26 | Salamander Pumped Shower Systems Ltd | Improvements in liquide storage |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US685832A (en) * | 1897-09-08 | 1901-11-05 | William Gender | Sheet-metal vessel. |
| US2889953A (en) * | 1954-02-04 | 1959-06-09 | Constock Liquid Methane Corp | Insulated tank with impervious lining |
| US3047184A (en) * | 1960-01-15 | 1962-07-31 | Shell Oil Co | Storage tank |
| US3085708A (en) * | 1960-12-19 | 1963-04-16 | Conch Int Methane Ltd | Membrane type storage tank |
| GB924803A (en) * | 1961-06-20 | 1963-05-01 | Conch Int Methane Ltd | Membrane tanks |
| US3150795A (en) * | 1961-06-20 | 1964-09-29 | Conch Int Methane Ltd | Membrane tanks |
-
1968
- 1968-11-15 JP JP43083397A patent/JPS4831569B1/ja active Pending
-
1969
- 1969-11-08 DE DE19691956289 patent/DE1956289A1/en active Pending
- 1969-11-13 US US876288A patent/US3622030A/en not_active Expired - Lifetime
- 1969-11-14 FR FR6939278A patent/FR2023428A1/fr not_active Withdrawn
- 1969-11-14 GB GB55829/69A patent/GB1261258A/en not_active Expired
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US685832A (en) * | 1897-09-08 | 1901-11-05 | William Gender | Sheet-metal vessel. |
| US2889953A (en) * | 1954-02-04 | 1959-06-09 | Constock Liquid Methane Corp | Insulated tank with impervious lining |
| US3047184A (en) * | 1960-01-15 | 1962-07-31 | Shell Oil Co | Storage tank |
| US3085708A (en) * | 1960-12-19 | 1963-04-16 | Conch Int Methane Ltd | Membrane type storage tank |
| GB924803A (en) * | 1961-06-20 | 1963-05-01 | Conch Int Methane Ltd | Membrane tanks |
| US3150795A (en) * | 1961-06-20 | 1964-09-29 | Conch Int Methane Ltd | Membrane tanks |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3712500A (en) * | 1971-08-06 | 1973-01-23 | Preload Eng Co | Liner for cryogenic container |
| US3861553A (en) * | 1971-11-24 | 1975-01-21 | Bridgestone Liquefied Gas Co | Means for supporting an inner membranous vessel of a low temperature liquefied gas tank of a membrane type |
| US3827135A (en) * | 1972-03-13 | 1974-08-06 | Bridgestone Liquefied Gas Co | Method of constructing a low temperature liquefied gas tank of a membrane type |
| US3827136A (en) * | 1972-03-25 | 1974-08-06 | Bridgestone Liquefied Gas Co | Method of constructing a low temperature liquefied gas tank of a membrane type |
| US3904067A (en) * | 1972-09-22 | 1975-09-09 | Ishikawajima Harima Heavy Ind | Membrane tank for liquefied gases |
| US4919366A (en) * | 1988-09-23 | 1990-04-24 | Mmi Incorporated | Heat resistive wall assembly for a space vehicle |
| US20090321452A1 (en) * | 2006-06-14 | 2009-12-31 | L'Air Liquide Societe Anonyme Pour L'Etude Et L'Expolitation Des Procedes Georges Claude | System for Insulating a Cyrogenic Tank and Method of Insulating said Tank |
| US8141738B2 (en) * | 2006-06-14 | 2012-03-27 | L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude | System for insulating a cryogenic tank and method of insulating said tank |
| US20080209918A1 (en) * | 2007-03-02 | 2008-09-04 | Enersea Transport Llc | Storing, transporting and handling compressed fluids |
| US9033178B2 (en) | 2007-03-02 | 2015-05-19 | Enersea Transport Llc | Storing, transporting and handling compressed fluids |
| US20100237081A1 (en) * | 2007-12-14 | 2010-09-23 | Gm Global Technology Operations, Inc. | Inner shell for a pressure vessel |
| US20090152278A1 (en) * | 2007-12-14 | 2009-06-18 | Markus Lindner | Inner shell for a pressure vessel |
| US20110168722A1 (en) * | 2010-01-13 | 2011-07-14 | BDT Consultants Inc. | Full containment tank |
| WO2024261466A1 (en) * | 2023-06-20 | 2024-12-26 | Salamander Pumped Shower Systems Ltd | Improvements in liquide storage |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2023428A1 (en) | 1970-08-21 |
| GB1261258A (en) | 1972-01-26 |
| DE1956289A1 (en) | 1970-05-27 |
| JPS4831569B1 (en) | 1973-09-29 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: MITSUI LIQUEFIED GAS CO., LTD., NO. 1-1, KYOBASHI Free format text: CHANGE OF NAME;ASSIGNOR:BRIDGESTONE LIQUIFIED GAS CO., LTD.,;REEL/FRAME:003862/0001 Effective date: 19810611 |