US2329765A - Low temperature storage tank - Google Patents

Low temperature storage tank Download PDF

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Publication number
US2329765A
US2329765A US418734A US41873441A US2329765A US 2329765 A US2329765 A US 2329765A US 418734 A US418734 A US 418734A US 41873441 A US41873441 A US 41873441A US 2329765 A US2329765 A US 2329765A
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shell
container
attached
shells
spherical
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US418734A
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James O Jackson
Howell C Cooper
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C3/00Vessels not under pressure
    • F17C3/02Vessels not under pressure with provision for thermal insulation
    • F17C3/08Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0128Shape spherical or elliptical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/03Orientation
    • F17C2201/032Orientation with substantially vertical main axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/01Reinforcing or suspension means
    • F17C2203/011Reinforcing means
    • F17C2203/012Reinforcing means on or in the wall, e.g. ribs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0345Fibres
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0304Thermal insulations by solid means
    • F17C2203/0354Wood
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0391Thermal insulations by vacuum
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0626Multiple walls
    • F17C2203/0629Two walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0639Steels
    • F17C2203/0643Stainless steels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634Materials for walls or layers thereof
    • F17C2203/0636Metals
    • F17C2203/0648Alloys or compositions of metals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01Mounting arrangements
    • F17C2205/0103Exterior arrangements
    • F17C2205/0107Frames
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01Mounting arrangements
    • F17C2205/0153Details of mounting arrangements
    • F17C2205/018Supporting feet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0323Valves
    • F17C2205/0332Safety valves or pressure relief valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2209/00Vessel construction, in particular methods of manufacturing
    • F17C2209/22Assembling processes
    • F17C2209/221Welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/011Oxygen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/014Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/03Mixtures
    • F17C2221/031Air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/033Small pressure, e.g. for liquefied gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/04Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
    • F17C2223/042Localisation of the removal point
    • F17C2223/046Localisation of the removal point in the liquid
    • F17C2223/047Localisation of the removal point in the liquid with a dip tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2260/00Purposes of gas storage and gas handling
    • F17C2260/01Improving mechanical properties or manufacturing
    • F17C2260/011Improving strength
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0102Applications for fluid transport or storage on or in the water
    • F17C2270/0105Ships
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS 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
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0102Applications for fluid transport or storage on or in the water
    • F17C2270/011Barges
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S220/00Receptacles
    • Y10S220/901Liquified gas content, cryogenic

Definitions

  • This invention relates to storage tanks and particularly to metallic tanks or containers for the storage of liquids and vapors (fluids) at low temperatures.
  • Containers consisting of double-walled glass or metallic vessels having an evacuated space between the double walls have been used for many years for the storage of extremely cold liquids and vapors such as liquid oxygen, liquid nitrogen, etc. These containers have, however, been of rather small capacity, the largest of which we have knowledge having a capacity of less than 10 gallons. To allow for internal expansion and contraction due to temperature changes and to ensure good insulating properties, such containers have invariably been constructed in such manner that the inner vessel is suspended at its neck from the neck of the outer vessel. For these reasons it has not been practicable to produce containers of this type which have larger volumetric capacity. In many cases buffers made of felt or other materials having good insulating properties have been placed at advantageous positions between the two vessels to assist in the support of the inner vessel but even under such conditions the practical limit of the present glass or metallic vacuum bottle has been definitely reached at about the capacity stated.
  • Another object of the invention resides in the provision of a large container for low temperature fluids which is so constructed that it not only has the requisite strength but also has excellent insulating characteristics while at the same time making necessary provision for internal expansion and contraction due to temperature changes.
  • An additional object of the invention resides in the provision of a container which has a spherical body portion and a conical polar portion, the conical portion being arranged tangentially to the spherical portion.
  • a still further object of the invention resides in providing a large tank for low temperature fluids which has a spherical body portion and a tangentially disposed conical portion and wherein the said portions are provided with girders arranged in the manner of lines of latitude and meridians of longitude on the earths surface.
  • a still further object of the invention resides in a double-walled container for low temperature fluids, the inner wall of which is composed of an austenitic material such as chromium-nickel steel, particularly one containing approximately 18% chromium and 8% nickel, and the outer surface of which is highly polished.
  • an austenitic material such as chromium-nickel steel, particularly one containing approximately 18% chromium and 8% nickel, and the outer surface of which is highly polished.
  • Fig. 1 illustrates a double-walled evacuated container for low temperature fluids responding to the present invention partially in elevation and partially in vertical section;
  • Fig. 1a is a fragmentary view of a modification of the invention in which the double-walled container is filled with heat insulating material between its walls;
  • Fig. 1b is a fragmentary view of a modified valve arrangement for the form of inventionillustrated in Fig. 1a;
  • Fig. 2 is a view similar to Fig. 1 of a structurally modified form of the invention.
  • the container there shown has an inner shell which consists of a hollow segmental spherical shell portion 20 formed of sheet metal parts united as by welding and a conical polar portion 2
  • , 23 is composed of two integrally united parts but may equally well be a single unitary member. Both variations are deemed to be a part of the invention.
  • a relatively heavy flanged ring-like member 24 is strongly attached as by welding.
  • Member 24 isprovided with a perforated closure 25 also secured in place as by welding.
  • This arrangement provides a compartment or chamber 26 which is loosely packed with a ma terial which is capable of absorbing a relatively large quantity of gas, especially at low temperatures.
  • a ma terial which is capable of absorbing a relatively large quantity of gas, especially at low temperatures.
  • and branch pipe 32 located laterally near the top of member 3
  • passes vertically through and is attached to cover plate 28 which is provided with a central aperture for such purpose.
  • may be by welding.
  • Tubular branch pipe 32 terminates in a flange 33 to which may be bolted a continuation of the vent pipe which may carry the vented vapors through a line provided with proper safety valves to special condensing machinery for the purpose of re-liquefying and conserving such vented vapors.
  • End piece 34 closes the upper end of tube 3
  • Member 34 has a central opening through which tube 35 extends downwardly nearly to the bottom of the container.
  • Members 34 and 35 are united in gastight relationship, preferably by welding.
  • the contents of the container may be withdrawn through tube 35 by removing the cap 36 normally in place thereon and connecting tube 35 to a pipe or hose or other suitable conduit.
  • suificient pressure through branch pipe 32 the contents of the container may be forced up through tube 35 and directed to any desired point.
  • conical sheet metal portion 38 Attached to flange 21, as by welding, and extending downwardly and outwardly therefrom is the conical sheet metal portion 38 which is very close to or in contact with portion 23 at its top but which thereafter diverges therefrom so as to produce an annular chamber or space 56 between the inner spherical member 20 and the outer spherical member 39 of the container, the member 39 being composed of sheet metal parts assembled and secured as by welding.
  • the lower polar portion of member 39 is cut out and member 40 secured thereto as by welding.
  • Member 40 is made up of a cylindrical portion and a lower concave-convex closure of disc shape which is welded or otherwise secured to the cylindrical portion.
  • extend radially inwardly through the vertical cylindrical portion of member 40 and are welded in such position.
  • terminate in truncated conical ends which are slightly spaced from the outer surface of the vertical cylindrical member 24.
  • member 24 is incapable of appreciable lateral movement, being held thereagainst by members 4
  • a plurality of horizontal continuous sheet metal rings 42, 43, 44 and 45 are attached, a by welding, to outer shell 38, 39.
  • a plurality of vertical bar-like sheet metal ribs 46 are disposed around the periphery of the outer shell and are attached to it and to the horizontal rings 42, 43, 44 and 45 and member 40 as by Welding.
  • the purpose of these bar-like members is to strengthen or stiffen the outer shell against collapse due to the pressure of the atmosphere on the external surface thereof after the space 56 has been evacuated.
  • the horizontal rings and vertical ribs are arranged in the manner of lines of latitude and meridians of longitude on the earths surface. Depending upon the size of the tank, the sections of metal employed, etc., the members 46 may be omitted where their strengthening effect i not essential.
  • a thin cylindrical sheet metal shell 41 is suitably attached to the outer shell and extends vertically to about the level of flange 21.
  • This cylindrical shell is spaced from the periphery of flange 21 and hence forms an annular opening between the upper end of member 38 and the said cylindrical shell.
  • This opening is filled with a heat insulating material 48, such a cork blocks.
  • a cover member 49 consisting of a hollow cylindrical shell having an annular substantially flat top forming a roof which fits loosely over member 41 in telescoping fashion. Cover member 49 encloses an annular body of solid heat insulating material 50, such as cork blocks, cemented in place to the cover member.
  • of the cover member the sides of which are defined b the solid insulating material 50 is filled after the cover member is in position with a loose granular or fibrous heat insulating material such as granulated cork.
  • is to permit the cap to be withdrawn over tube 3
  • a cylindrical sheet metal shell 52 having a substantially flat bottom, is attached as shown to the exterior shell as b welding it to ring 45.
  • This sheet metal shell is provided with a number of openings each of which is normally closed by a bolted-on closure plate 53 through which the chamber 54 may be filled with a granular or iibrous heat insulating material such as granulated cork.
  • Fig. 2 the modified structure of Fig. 2 is fundamentally the same as that of Fig. 1 alread described. This will be apparent by the use of the same numerals to designate like parts.
  • the inner shell 20 is secured to a frusto-conical shell portion 2
  • outer shell 39 of Fig. 2 has the frustoconical portion 38 as a continuation thereof, the shell terminating in a converging cylindrical collar-like outer neck 31 which rises to meet flange 2! and is welded thereto.
  • horizontal ring 42 is welded in place at the juncture of parts 38 and 31.
  • parts 24 and 40 are a little diiferent from parts 24 and 40 as will be readily ascertainable upon inspection. In other respects there is no material difference between the two containers such as would alter the nature of the inventive concept.
  • the container we proportioned the interior surfaces to resist an internal pressure equal to one atmosphere (due to the evacuation of the space between the two shells) plus the weight of the liquid at its highest elevation plus whatev'er pressure might have to be applied in order to remove the liquid from the vessel.
  • the spherical portion of the interior shell is proportioned as for spherical surfaces, using commonly known methods for obtaining the stress caused by the weight of the stored liquid and also that caused by the atmospheric and imposed inside vapor pressures.
  • the conical portion is designed the same as the spherical portion except that the cone radius is used in the customary way in determining the maximum stress.
  • the horizontal circular reinforcing ring 23 is proportioned to withstand the horizontal component' of the radial stress in cone portion 2], 23 at its juncture with ring 23'.
  • the exterior shell is designed so that in cooperation with the barlike stiffeners, when used, it will have sufficient strength to resist the external atmospheric pressure on the entire outer shell.
  • Members 24 and 24' are designed so as to safely resist the internal pressure and weight of the contents and the depending flanges thereof are proportioned so as to safely transmit to bar-like members 4
  • Members M] and 40' are designed to resist the external pressure and to receive the reactions from bars 4
  • Our vacuum containers may be used either for stationary storage purposes or as a component partof trucks, railroad cars, barges, ships, airplanes, etc. for the transportation of the stored contents.
  • the design is considered especially suitable for use in barges and ships where the longitudinal and transverse bulkheads are partitions of the ships and could be rigidly attached, as by welding, to the vertical stiifeners 46 which would not only form an excellent support for the vacuum vessels themselves but which, because of their very great rigidity, would act to stifien the vessels and to divide the interior of the vessels or barges into' bulkheaded spaces, which is considered desirable in boat building.
  • the bar-like members El have a body of sufficient diameter to enable them to carry the stresses imposed upon them as a column.
  • the ends are truncated and the extreme ends may be hard-faced so as to provide a very high unit bearing value.
  • the spots on the vertical flanges of members 24 and 24' against which members M bear may alsoibe hard-faced so as to provide a corresponding high unit bearing on that member.
  • the remaining source of heat infiltration is the black body radiation from the outer to the inner shell. This may be considerable especially if the temperature of the contents being stored is several hundred degrees Fahrenheit below the temperature of the outside shell.
  • the inner shell 20 of sheet metal having a very high polish bn the exterior surface, which effectively reflects any radiated heat back to the outer shell.
  • austenitic stainless steel contain ing from about 23-24% chromium and about 2 -l2% nickel with the remainder iron and the usual impurities is entirely satisfactory, and we prefer to use so-called 18-8 which has a chromium content of approximately 18% and a nickel content of approximately 8% for the construction of the inner shell.
  • Fig. 1a The form of the invention illustrated in Fig. 1a is the same as that of Fig. 1 except that in addition to employing an evacuated space 56 between the shells and necks we fill such space with a suitable heat insulating medium 56a such as granulated cork, charcoal or pulverized balsa wood.
  • a suitable heat insulating medium 56a such as granulated cork, charcoal or pulverized balsa wood.
  • valve 55 and tube 55' are modified as shown in Fig. 1b to provide a chamber 39' filled with a straining or filtering material 39 such as coarse steel wool to prevent loss of insulating material into the evacuating line.
  • a polished outer surface on the inner shell is unessential and therefore may be dispensed with. This form of container is less expensive and for many purposes entirely satisfactory.
  • the heat insulating medium above mentioned also acts to prevent black body heat radiation into the inner shell in the same manner that a polished surface, provided on the outer surface of the inner shell, prevents such by refiecting heat back toward the outer shell. Such constitutes another effective mode of realizing the present results. It should further be understood that the construction of Fig. 2 may likewise be modified to utilize a filling of insulating or radiation blocking material in accordance with Fig. 1a.,
  • An insulated container comprising inner and outer metal shells having substantially spherical spaced apart lower portions and upper portions which are attached to said lower portions and which converge to a common line of contact, said upper portions being substantially conical at their lines of attachment to their lower portions and substantially tangent thereto, said outer shell being reinforced by stifiening means adapted to enable it to support the weight and contents of said inner sriell, said stifiening means being attached to the upper extremities of said shells at said common line of contact.
  • an outer metal shell having a substantially spherical lower portion and a substantially conical upper portion which is substantially tangent thereto, an inner metal shell having a substantially spherical lower portion spaced from the spherical portion of the outer shell and a substantially conical portion above said spherical portion and which is substantially tangent thereto; the upper extremities of the outer and inner shells being in contact one with the other and attached to a metal member which extends laterally beyond the outer periphery of the upper extremity of the outer shell, said outer shell being reinforced by stiffening means attached to its outer surface and to said metal member.
  • An insulated container comprising inner and outer metal shells having substantially spherical spaced apart lower portions and upper portions which are attached to said lower portions and which contact one with the other at their upper extremities, said upper portions being substantially conical at their lines of attachment to the lower portions and substantially tangent thereto, a metal member to which the upper extremities of both shells are attached, said outer shell being reinforced by vertically and horizontally extending stiffening means adapted to enable it to support the weight and contents of said inner shell, said vertically extending stiffening means being attached to the metal member to which the upper extremities of both shells are attached.
  • an outer metal shell having a substantially spherical lower portion and asubstantially conical upper portion which is substantially tangent thereto, an inner metal shell having a substantially spherical lower portion spaced from the spherical portion of the outer shell and a substantially conical portion above said spherical portion and which is substantially tangent thereto; the upper extremities of both shells being in contact one with the other and attached to a metal member which extends laterally beyond the upper extremity of the outer shell, said outer shell being reinforced by stiffening means attached to its outer surface and to said metal member and means carried partially by each shell adjacent its lower polar region for limiting relative horizontal movement between the shells at such regions While permitting relative vertical movement of the same.
  • an outer shell having a substantially spherical lower portion and a substantially conical upper portion substantially tangent thereto
  • an inner shell having a substantially spherical lower portion spaced from the spherical portion of the outer shell and a substantially conical portion above said spherical portion and which is substantially tangent thereto
  • a laterally extending member to which the upper extremities of said shells are attached as by welding
  • stiffening means welded to the exterior of the outer shell and to such laterally extending member
  • means carried partially by each shell adjacent its lower polar region for limiting relative lateral movement of said shells at such region while permitting relative vertical movement of the same and heat insulating means carried by the outer shell and surrounding said movement limiting means.
  • inner and outer metal shells having substantially spherical spaced apart lower portions and upper portions which are substantially conical and which at their upper extremities are in contact one with the other, a metal member to which the upper contacting extremities of the shells are attached, which extends laterally beyond such extremities and has an opening extending vertically therethrough giving access to the interior of the inner shell, a closure element removably attached to said member and carrying a tubular member which extends through said opening and has its lower end open to the interior of the inner shell, a walled compartment which surrounds the upper end of the outer shell, extends upwardly from said shell to a position adjacent said removable element and has a removable cover provided with an opening in its top around said tubular member and heat insulating material within said compartment.
  • a container as defined in claim 2 in which the terminal upper portion of the inner shell is cylindrical and the terminal upper portion of the outer shell while conical is of a steeper angle than the conical portion which is substantially tangent to the spherical portion of the outer s e 8.
  • a container as defined in claim 5 in which that part of the movement limiting means carried by the inner shell is hollow, has a perforated closure positioned in its lower end and contains a body of gas absorbing material which contacts with the inner shell and is in communication with the space between the shells.
  • a container as defined in claim 4 in which the outer shell adjacent its lower polar region carries means for heat insulating the means for limiting relative horizontal movement between the shells at the lower polar regions thereof.
  • a container as defined in claim 5 in which the outer shell carries heat insulating means which surrounds the upper extremities of the shells and the laterally extending member to which such upper extremities are attached, and the outer shell adjacent the lower polar region thereof carries heat insulating means which surrounds the, means for limiting the relative lateral movement of the shells at the lower polar regions thereof.

Description

Sept. 21, 1943. JAC N TA 2,329,765
LOW TEMPERATURE STORAGE TANK Filed Nov. 12, 1941 2 Sheefs-Sheet 1 W ATTORN EYS P 1943- J. o. JACKSON ET AL 2,329,765
LOW TEMPERATURE STORAGE TANK Filed NOV. 12, 1941 2 Sheets-Sheet 2 I 36 3 Inn! 6 .33 5/ 49 5/ J E 49 Z9 Z6 M Z7 57 47 48 30 n. 2
4 I I 46 I 5 I mun h|lu 38 IN I 23 k I Hinh, H" Z/ 4 In I Huh! h h 56 I l u I 44 I ||l v 44' n 59 4 In, 20 44 II II 46 46 I f 4% "In II I i ll 55 55' n, I
\J 52 J Z5 Z6- 1 F19, 2 ISVNTRS I 6 Q w ATTORNEYS Patented Sept. 21, 1943 LOW TEMPERATURE STORAGE TANK James 0. Jackson, Cratton, and Howell C. Cooper, Sewickley, Pa.
Application November 12, 1941, Serial No. 418,734
l1 Claims.
This invention relates to storage tanks and particularly to metallic tanks or containers for the storage of liquids and vapors (fluids) at low temperatures.
Containers consisting of double-walled glass or metallic vessels having an evacuated space between the double walls have been used for many years for the storage of extremely cold liquids and vapors such as liquid oxygen, liquid nitrogen, etc. These containers have, however, been of rather small capacity, the largest of which we have knowledge having a capacity of less than 10 gallons. To allow for internal expansion and contraction due to temperature changes and to ensure good insulating properties, such containers have invariably been constructed in such manner that the inner vessel is suspended at its neck from the neck of the outer vessel. For these reasons it has not been practicable to produce containers of this type which have larger volumetric capacity. In many cases buffers made of felt or other materials having good insulating properties have been placed at advantageous positions between the two vessels to assist in the support of the inner vessel but even under such conditions the practical limit of the present glass or metallic vacuum bottle has been definitely reached at about the capacity stated.
It is, therefore, one of the objects of this invenion to provide a container which is capable of holding large amounts of fluidseither liquids or vapors-at low temperatures and particularly at the extremely low temperatures involved by liquid air, liquid oxygen, liquid nitrogen, etc.
Another object of the invention resides in the provision of a large container for low temperature fluids which is so constructed that it not only has the requisite strength but also has excellent insulating characteristics while at the same time making necessary provision for internal expansion and contraction due to temperature changes.
An additional object of the invention resides in the provision of a container which has a spherical body portion and a conical polar portion, the conical portion being arranged tangentially to the spherical portion.
A still further object of the invention resides in providing a large tank for low temperature fluids which has a spherical body portion and a tangentially disposed conical portion and wherein the said portions are provided with girders arranged in the manner of lines of latitude and meridians of longitude on the earths surface.
A still further object of the invention resides in a double-walled container for low temperature fluids, the inner wall of which is composed of an austenitic material such as chromium-nickel steel, particularly one containing approximately 18% chromium and 8% nickel, and the outer surface of which is highly polished.
Other andfurther objects and advantages reside in the various combinations, subcombinations and details hereinafter described and claimed and in such other and further matters as will be understood by those skilled in the art or pointed out hereinafter. Such include the provision of either an evacuated chamber or the use of a heat insulating medium between the spaced container walls.
In the accompanying drawings:
Fig. 1 illustrates a double-walled evacuated container for low temperature fluids responding to the present invention partially in elevation and partially in vertical section;
Fig. 1a is a fragmentary view of a modification of the invention in which the double-walled container is filled with heat insulating material between its walls;
Fig. 1b is a fragmentary view of a modified valve arrangement for the form of inventionillustrated in Fig. 1a; and
Fig. 2 is a view similar to Fig. 1 of a structurally modified form of the invention.
Like numerals designate corresponding parts in the various views of the drawings.
Referring now to Fig. 1 of the drawings, the container there shown has an inner shell which consists of a hollow segmental spherical shell portion 20 formed of sheet metal parts united as by welding and a conical polar portion 2|, 23 forming a continuation of the said spherical portion and united to it as by welding. Portion 2|, 23 is composed of two integrally united parts but may equally well be a single unitary member. Both variations are deemed to be a part of the invention. At the lower polar portion of spherical portion 20 a relatively heavy flanged ring-like member 24 is strongly attached as by welding. Member 24 isprovided with a perforated closure 25 also secured in place as by welding. This arrangement provides a compartment or chamber 26 which is loosely packed with a ma terial which is capable of absorbing a relatively large quantity of gas, especially at low temperatures. A number of materials can be employed with success and we mention, purely by way of example, activated carbon, silica gel, and charcoal derived from woods and shells among which beechnut shell charcoal is particularly effective.
The upper edge of conical portion 2|, 23 is firmly secured, as by welding, to a relatively thick horizontally disposed centerless annular flange member 21. Superimposed on flange 21 is a cover plate 28 secured to flange 21 by fastening means such as the cap screws 29. The joint between members 21 and 28 is gas-tight, being sealed by a ring gasket 30 of suitable material.
In containers of the present type some slight heat infiltration inevitably occurs which causes vaporization. In the present construction such vapors can escape by way of tubular member 3| and branch pipe 32 located laterally near the top of member 3|. Member 3| passes vertically through and is attached to cover plate 28 which is provided with a central aperture for such purpose. The uniting of member 28 and 3| may be by welding. Tubular branch pipe 32 terminates in a flange 33 to which may be bolted a continuation of the vent pipe which may carry the vented vapors through a line provided with proper safety valves to special condensing machinery for the purpose of re-liquefying and conserving such vented vapors.
End piece 34 closes the upper end of tube 3| and is attached thereto as by welding. Member 34 has a central opening through which tube 35 extends downwardly nearly to the bottom of the container. Members 34 and 35 are united in gastight relationship, preferably by welding. The contents of the container may be withdrawn through tube 35 by removing the cap 36 normally in place thereon and connecting tube 35 to a pipe or hose or other suitable conduit. By applying suificient pressure through branch pipe 32 the contents of the container may be forced up through tube 35 and directed to any desired point.
Attached to flange 21, as by welding, and extending downwardly and outwardly therefrom is the conical sheet metal portion 38 which is very close to or in contact with portion 23 at its top but which thereafter diverges therefrom so as to produce an annular chamber or space 56 between the inner spherical member 20 and the outer spherical member 39 of the container, the member 39 being composed of sheet metal parts assembled and secured as by welding. The lower polar portion of member 39 is cut out and member 40 secured thereto as by welding. Member 40 is made up of a cylindrical portion and a lower concave-convex closure of disc shape which is welded or otherwise secured to the cylindrical portion. A plurality of angularly disposed short bar-like members 4| extend radially inwardly through the vertical cylindrical portion of member 40 and are welded in such position. Members 4| terminate in truncated conical ends which are slightly spaced from the outer surface of the vertical cylindrical member 24. Thus member 24 is incapable of appreciable lateral movement, being held thereagainst by members 4|, but is enabled to move vertically without undue restriction.
A plurality of horizontal continuous sheet metal rings 42, 43, 44 and 45 are attached, a by welding, to outer shell 38, 39. A plurality of vertical bar-like sheet metal ribs 46 are disposed around the periphery of the outer shell and are attached to it and to the horizontal rings 42, 43, 44 and 45 and member 40 as by Welding. The purpose of these bar-like members is to strengthen or stiffen the outer shell against collapse due to the pressure of the atmosphere on the external surface thereof after the space 56 has been evacuated. It will be noted that the horizontal rings and vertical ribs are arranged in the manner of lines of latitude and meridians of longitude on the earths surface. Depending upon the size of the tank, the sections of metal employed, etc., the members 46 may be omitted where their strengthening effect i not essential.
A thin cylindrical sheet metal shell 41 is suitably attached to the outer shell and extends vertically to about the level of flange 21. This cylindrical shell is spaced from the periphery of flange 21 and hence forms an annular opening between the upper end of member 38 and the said cylindrical shell. This opening is filled with a heat insulating material 48, such a cork blocks. A cover member 49 consisting of a hollow cylindrical shell having an annular substantially flat top forming a roof which fits loosely over member 41 in telescoping fashion. Cover member 49 encloses an annular body of solid heat insulating material 50, such as cork blocks, cemented in place to the cover member. The interior portion 5| of the cover member the sides of which are defined b the solid insulating material 50 is filled after the cover member is in position with a loose granular or fibrous heat insulating material such as granulated cork. The purpose of the space 5| is to permit the cap to be withdrawn over tube 3| and flange 33 so that bolts 29 may be removed, whenever necessary, to gain access to the interior of the container.
A cylindrical sheet metal shell 52, having a substantially flat bottom, is attached as shown to the exterior shell as b welding it to ring 45. This sheet metal shell is provided with a number of openings each of which is normally closed by a bolted-on closure plate 53 through which the chamber 54 may be filled with a granular or iibrous heat insulating material such as granulated cork. Communicating with the space 56 between the two shells and attached to the outer shell, as by welding, is hermetically tight needle valve 55 provided at one end with a copper tube connection 55', which is substantially or entirely leak-proof.
It will be observed that the modified structure of Fig. 2 is fundamentally the same as that of Fig. 1 alread described. This will be apparent by the use of the same numerals to designate like parts. In Fig. 2, however, the inner shell 20 is secured to a frusto-conical shell portion 2|, 23 which terminates in a vertical cylindrical inner neck 22, the juncture between 22 and 23 being provided with a girder-like ring member 23'. Since the entire weight of the inner shell is suspended by neck 22 this latter member is made of adequate strength and thickness to prevent damaging stresses and strains from arising in the structure.
Further, outer shell 39 of Fig. 2 has the frustoconical portion 38 as a continuation thereof, the shell terminating in a converging cylindrical collar-like outer neck 31 which rises to meet flange 2! and is welded thereto. In this case, horizontal ring 42 is welded in place at the juncture of parts 38 and 31. In Fig. 2 also the parts 24 and 40 are a little diiferent from parts 24 and 40 as will be readily ascertainable upon inspection. In other respects there is no material difference between the two containers such as would alter the nature of the inventive concept.
In designing the container we proportioned the interior surfaces to resist an internal pressure equal to one atmosphere (due to the evacuation of the space between the two shells) plus the weight of the liquid at its highest elevation plus whatev'er pressure might have to be applied in order to remove the liquid from the vessel. The spherical portion of the interior shell is proportioned as for spherical surfaces, using commonly known methods for obtaining the stress caused by the weight of the stored liquid and also that caused by the atmospheric and imposed inside vapor pressures. The conical portion is designed the same as the spherical portion except that the cone radius is used in the customary way in determining the maximum stress.
The horizontal circular reinforcing ring 23 is proportioned to withstand the horizontal component' of the radial stress in cone portion 2], 23 at its juncture with ring 23'. The exterior shell is designed so that in cooperation with the barlike stiffeners, when used, it will have sufficient strength to resist the external atmospheric pressure on the entire outer shell. Members 24 and 24' are designed so as to safely resist the internal pressure and weight of the contents and the depending flanges thereof are proportioned so as to safely transmit to bar-like members 4| any horizontal forces which may be present. Members M] and 40' are designed to resist the external pressure and to receive the reactions from bars 4| and to transmit the same into the outer shell with the cooperation of vertical stiffeners 66, when used.
Our vacuum containers may be used either for stationary storage purposes or as a component partof trucks, railroad cars, barges, ships, airplanes, etc. for the transportation of the stored contents. The design is considered especially suitable for use in barges and ships where the longitudinal and transverse bulkheads are partitions of the ships and could be rigidly attached, as by welding, to the vertical stiifeners 46 which would not only form an excellent support for the vacuum vessels themselves but which, because of their very great rigidity, would act to stifien the vessels and to divide the interior of the vessels or barges into' bulkheaded spaces, which is considered desirable in boat building.
In the use of our vacuum tank we have found that even though extreme care is taken in making all of the welded joints, after a period of use there will be some infiltration of air or gases, perhaps through very tiny pores in the sheet metal itself or perhaps from gas entrapped in the metalduring its manufacture. We, therefore, provide a gas absorbing material, such as activated carbon, which has the property of absorbing gas, especially at the very low temperature of the fluid which we contemplate storing. This gas-absorbing material is, therefore, placed in contact with the inner vessel so that it will be maintained at a very cold temperature where its efilciency in absorbing gases is the greatest. ditions it might be desirable to further evacuate the space 56 between the two vessels. For example, in a barge containing several of our tanks, a vacuum pump might be provided and connected with very tightly sealed copper tubing to needle valve 55 so that a very high vacuum could be maintained at all times.
We have determined that a vacuum of the order of of a millimeter of mercury (absolute pressure) will reduce the heat infiltration from the outer to the inner shell by conduction or convection through any possible remnant of unevacuated gases to almost zero. ever, heat infiltration from the outer to the inner shell through the neck and through the lateral stabilizing members 4!. We have found that Under certain con- There remains, howthese losses may be greatly reduced by increasing the distance over which the heat must travel in reaching the inner'shell. For example, (referring now to Fig. 2) for heat to reach the inner shell through the neck it must travel the entire length of the path from the intersection of members 41 and 38 up through the outer neck to the intersection with flange 21, then down the inner neck 22, then down 2|, until contact with the liquid is established. Since the heat conductivity of a metal is inversely proportional to the length of the metal path through which the heat must travel, it is apparent that this method of insulation is very efiectlve in reducing neck heat losses.
The same thing is true of the insulation at the bottom of the vessel and, in addition, the special construction of members 41 further reduces the heat infiltration at this point. The bar-like members El have a body of sufficient diameter to enable them to carry the stresses imposed upon them as a column. The ends, however, are truncated and the extreme ends may be hard-faced so as to provide a very high unit bearing value. Likewise, the spots on the vertical flanges of members 24 and 24' against which members M bear may alsoibe hard-faced so as to provide a corresponding high unit bearing on that member. As a result of this construction the actual metal ts metal contact between members 24 and 24 and 4| is not large and, since when member 26 cools it tends to contract somewhat there is normally no actual contact except when the vessel is tilted slightly so that the weight of the contents tends to force member 26 or 2 8 to press against one or more of the members 8|.
The remaining source of heat infiltration is the black body radiation from the outer to the inner shell. This may be considerable especially if the temperature of the contents being stored is several hundred degrees Fahrenheit below the temperature of the outside shell. In order to reduce this loss to a minimum we construct the inner shell 20 of sheet metal having a very high polish bn the exterior surface, which effectively reflects any radiated heat back to the outer shell. We have found that austenitic stainless steel contain ing from about 23-24% chromium and about 2 -l2% nickel with the remainder iron and the usual impurities is entirely satisfactory, and we prefer to use so-called 18-8 which has a chromium content of approximately 18% and a nickel content of approximately 8% for the construction of the inner shell. These steels, being austenitic in nature, do not become brittle at low temperatures and satisfactory welds may be made, using welding rods of the same or slightly higher chromium and nickel content, e. g., 9-25% chromium and 2-12 nickel, which welds also are satisfactory at low temperatures. We, therefore, construct the entire inner shell from material of the above range of composition as well as the outer neck and the outer conical portion down to ap proximately the juncture with 41. We also use stainless steel of the composition stated or an alloy consisting of approximately 3 /2% nickel, the balance ordinary mild steel, for tubes 3| and 35 and connecting parts. We have found cork board to be the best insulating material for the neck insulation and granulated cork the best for the insulation in spaces 5| and 54, although there are other materials which are entirely satisfactory.
The form of the invention illustrated in Fig. 1a is the same as that of Fig. 1 except that in addition to employing an evacuated space 56 between the shells and necks we fill such space with a suitable heat insulating medium 56a such as granulated cork, charcoal or pulverized balsa wood. 'In such case it is to be understood that valve 55 and tube 55' are modified as shown in Fig. 1b to provide a chamber 39' filled with a straining or filtering material 39 such as coarse steel wool to prevent loss of insulating material into the evacuating line. A polished outer surface on the inner shell is unessential and therefore may be dispensed with. This form of container is less expensive and for many purposes entirely satisfactory. The heat insulating medium above mentioned also acts to prevent black body heat radiation into the inner shell in the same manner that a polished surface, provided on the outer surface of the inner shell, prevents such by refiecting heat back toward the outer shell. Such constitutes another effective mode of realizing the present results. It should further be understood that the construction of Fig. 2 may likewise be modified to utilize a filling of insulating or radiation blocking material in accordance with Fig. 1a.,
We have described two particular forms of the invention, with the understanding that other and further additions, omissions, substitutions and variations may be made both as to construction and as to materials of construction. The invention is rather that defined by the appended claims.
Having thus described our invention, what we claim as new and desire to secure by Letters Patent is:
1. An insulated container comprising inner and outer metal shells having substantially spherical spaced apart lower portions and upper portions which are attached to said lower portions and which converge to a common line of contact, said upper portions being substantially conical at their lines of attachment to their lower portions and substantially tangent thereto, said outer shell being reinforced by stifiening means adapted to enable it to support the weight and contents of said inner sriell, said stifiening means being attached to the upper extremities of said shells at said common line of contact.
2. In an insulated container, an outer metal shell having a substantially spherical lower portion and a substantially conical upper portion which is substantially tangent thereto, an inner metal shell having a substantially spherical lower portion spaced from the spherical portion of the outer shell and a substantially conical portion above said spherical portion and which is substantially tangent thereto; the upper extremities of the outer and inner shells being in contact one with the other and attached to a metal member which extends laterally beyond the outer periphery of the upper extremity of the outer shell, said outer shell being reinforced by stiffening means attached to its outer surface and to said metal member.
3. An insulated container comprising inner and outer metal shells having substantially spherical spaced apart lower portions and upper portions which are attached to said lower portions and which contact one with the other at their upper extremities, said upper portions being substantially conical at their lines of attachment to the lower portions and substantially tangent thereto, a metal member to which the upper extremities of both shells are attached, said outer shell being reinforced by vertically and horizontally extending stiffening means adapted to enable it to support the weight and contents of said inner shell, said vertically extending stiffening means being attached to the metal member to which the upper extremities of both shells are attached.
4. In an insulated container, an outer metal shell having a substantially spherical lower portion and asubstantially conical upper portion which is substantially tangent thereto, an inner metal shell having a substantially spherical lower portion spaced from the spherical portion of the outer shell and a substantially conical portion above said spherical portion and which is substantially tangent thereto; the upper extremities of both shells being in contact one with the other and attached to a metal member which extends laterally beyond the upper extremity of the outer shell, said outer shell being reinforced by stiffening means attached to its outer surface and to said metal member and means carried partially by each shell adjacent its lower polar region for limiting relative horizontal movement between the shells at such regions While permitting relative vertical movement of the same.
5. In an insulated container, an outer shell having a substantially spherical lower portion and a substantially conical upper portion substantially tangent thereto, an inner shell having a substantially spherical lower portion spaced from the spherical portion of the outer shell and a substantially conical portion above said spherical portion and which is substantially tangent thereto, a laterally extending member to which the upper extremities of said shells are attached as by welding, stiffening means welded to the exterior of the outer shell and to such laterally extending member, means carried partially by each shell adjacent its lower polar region for limiting relative lateral movement of said shells at such region while permitting relative vertical movement of the same and heat insulating means carried by the outer shell and surrounding said movement limiting means.
6. In an insulated container, inner and outer metal shells having substantially spherical spaced apart lower portions and upper portions which are substantially conical and which at their upper extremities are in contact one with the other, a metal member to which the upper contacting extremities of the shells are attached, which extends laterally beyond such extremities and has an opening extending vertically therethrough giving access to the interior of the inner shell, a closure element removably attached to said member and carrying a tubular member which extends through said opening and has its lower end open to the interior of the inner shell, a walled compartment which surrounds the upper end of the outer shell, extends upwardly from said shell to a position adjacent said removable element and has a removable cover provided with an opening in its top around said tubular member and heat insulating material within said compartment.
7. A container as defined in claim 2 in which the terminal upper portion of the inner shell is cylindrical and the terminal upper portion of the outer shell while conical is of a steeper angle than the conical portion which is substantially tangent to the spherical portion of the outer s e 8. A container as defined in claim 5 in which that part of the movement limiting means carried by the inner shell is hollow, has a perforated closure positioned in its lower end and contains a body of gas absorbing material which contacts with the inner shell and is in communication with the space between the shells.
9. A container as defined in claim 4 in which the outer shell adjacent its lower polar region carries means for heat insulating the means for limiting relative horizontal movement between the shells at the lower polar regions thereof.
10. A container as defined in claim 4 in which the outer shell in addition to the stiffening means which are attached to the metal member to which the upper extremities of both shells are attached, is provided with spaced horizontal outwardly extending rings welded thereto and arranged in the manner of lines of latitude of the earth's surface.
11. A container as defined in claim 5 in which the outer shell carries heat insulating means which surrounds the upper extremities of the shells and the laterally extending member to which such upper extremities are attached, and the outer shell adjacent the lower polar region thereof carries heat insulating means which surrounds the, means for limiting the relative lateral movement of the shells at the lower polar regions thereof.
- JAMES O. JACKSON.
HOWELL C. COOPER.
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US2426630A (en) * 1943-09-27 1947-09-02 Specialties Dev Corp High-pressure gaseous oxygen package
US2439806A (en) * 1943-08-11 1948-04-20 Guardite Corp Testing chamber
US2451486A (en) * 1944-09-01 1948-10-19 Chicago Bridge & Iron Co Vacuum tank for storing liquids at high or low temperatures
US2462064A (en) * 1944-10-09 1949-02-15 Chicago Bridge & Iron Co Pressure vessel for storage of liquids at abnormally high or low temperatures
US2563118A (en) * 1945-02-02 1951-08-07 Pittsburgh Des Moines Company Double walled insulated tank or container for storing low-tem-perature liquefied gases
US2648953A (en) * 1951-06-22 1953-08-18 Hofman Lab Inc Liquid helium container with insertable heat exchanger
US2677938A (en) * 1950-11-16 1954-05-11 Union Carbide & Carbon Corp Vacuum-insulated container and process for evacuating same
US2823822A (en) * 1955-10-10 1958-02-18 Aro Equipment Corp Vacuum bottle
US2892564A (en) * 1957-04-10 1959-06-30 Union Stock Yard & Transit Co Chicago Shipper container
US2954892A (en) * 1958-07-09 1960-10-04 Conch Int Methane Ltd Vessel for storing cold liquids
US2965218A (en) * 1956-08-16 1960-12-20 Rand Dev Corp Getter
US3108706A (en) * 1959-08-31 1963-10-29 Union Carbide Corp Apparatus for improving vacuum insulation
US3130561A (en) * 1961-06-30 1964-04-28 Nat Res Corp Insulation device
US3147877A (en) * 1958-01-09 1964-09-08 Union Carbide Corp Liquefied gas container
US3306058A (en) * 1964-10-23 1967-02-28 Keilin Victor Efimovich Cryostat
US5408832A (en) * 1992-06-08 1995-04-25 Saes Getters, S.P.A. Thermally insulating jacket and related process
US5865037A (en) * 1996-08-30 1999-02-02 Vesture Corporation Insulated chest and method
US5918478A (en) * 1996-08-30 1999-07-06 Vesture Corporation Insulated chest and method
US20040047745A1 (en) * 2002-09-06 2004-03-11 Burkholder Robert F. Air compressor assembly having enclosed unpainted air tank
US20060104834A1 (en) * 2003-04-02 2006-05-18 Stilwell J C Air compressor enclosed in shroud having tab isolator
US20080116211A1 (en) * 2005-02-03 2008-05-22 Jan Ericson Container and Method of Manufacturing a Container
US20160153614A1 (en) * 2013-04-30 2016-06-02 St Reproductive Technologies, Llc Transportation and/or storage device comprising a double-walled insulating bulb
US11408563B1 (en) * 2022-02-17 2022-08-09 Pipl Limited Pressure vessel and method of manufacturing thereof

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2439806A (en) * 1943-08-11 1948-04-20 Guardite Corp Testing chamber
US2426630A (en) * 1943-09-27 1947-09-02 Specialties Dev Corp High-pressure gaseous oxygen package
US2451486A (en) * 1944-09-01 1948-10-19 Chicago Bridge & Iron Co Vacuum tank for storing liquids at high or low temperatures
US2462064A (en) * 1944-10-09 1949-02-15 Chicago Bridge & Iron Co Pressure vessel for storage of liquids at abnormally high or low temperatures
US2563118A (en) * 1945-02-02 1951-08-07 Pittsburgh Des Moines Company Double walled insulated tank or container for storing low-tem-perature liquefied gases
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