US2513749A - Insulated container and method of insulating the same - Google Patents
Insulated container and method of insulating the same Download PDFInfo
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- US2513749A US2513749A US595167A US59516745A US2513749A US 2513749 A US2513749 A US 2513749A US 595167 A US595167 A US 595167A US 59516745 A US59516745 A US 59516745A US 2513749 A US2513749 A US 2513749A
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- vapor
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- jacket
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L59/00—Thermal insulation in general
- F16L59/06—Arrangements using an air layer or vacuum
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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
- F17C3/08—Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
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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
- 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
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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
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/03—Orientation
- F17C2201/035—Orientation with substantially horizontal main axis
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/01—Reinforcing or suspension means
- F17C2203/014—Suspension means
- F17C2203/015—Bars
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0325—Aerogel
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0304—Thermal insulations by solid means
- F17C2203/0345—Fibres
- F17C2203/035—Glass wool
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0375—Thermal insulations by gas
- F17C2203/0387—Cryogen
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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
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0391—Thermal insulations by vacuum
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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
- 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
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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
- 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
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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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/011—Oxygen
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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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/013—Carbone dioxide
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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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/014—Nitrogen
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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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/018—Acetylene
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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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/031—Air
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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
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/03—Mixtures
- F17C2221/032—Hydrocarbons
- F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
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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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/033—Small pressure, e.g. for liquefied gas
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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
- 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
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/901—Liquified gas content, cryogenic
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/918—Spacing element for separating the walls of a spaced-wall container
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S62/00—Refrigeration
- Y10S62/13—Insulation
Definitions
- This invention relates to the insulation of vessels used for the storage of liqueed gases, as for example nitrogen, oxygen, air, methane and ethylene.
- the 'I'he objective of the .present invention is to provide means for producing a vacuum of useful degree in a heat insulating jacket surrounding a storage tank of any size and for reinstating the vacuum in the event it ⁇ becomes impaired after prolonged use of the container, both without the use of exhaust pumps or other evacuat- I ing machinery.
- IB is a liquefied gas storage tank of any preferred form and dimensions. This tank is provided with top and bottom pipe connections li and i2, and with such other fltments as may be desired.
- An outer jacket I3 surrounds the storage tank and is spaced from it by members II-H, which should be of a material of low heat conductivity.
- the jacket should be as nearly air-tight as it is practicable to make it. Tightness is relative and while it is possible to construct a jacket which, when evacuated, will show no appreciable pressure rise over a considerable period, it is very dilcult to build ⁇ a metallic shell which will maintain a vacuum indefinitely.
- the jacket is provided with an inlet connection I5 for the introduction of the functioning vapor and with a vent connection I6 for the displacement of air.
- These tubes are illustrated as entering the jacket near its periphery. It is preferred that these tubes terminate approximately at the center of length of the tank, and that each be provided with afllter as at I7 and I8 and with tent.
- a low subatmospheric pressure which may approach a complete vacuum, in space i9 is produced by first lling it with a suitable vapor, which is afterward liquefied, or liquefied and solidified.
- the air initially filling the jacket must be removed as completely as possible.
- the jacket may be evacuated and vapor admitted to take the place of the removed air, thus economizing vapor.
- the jacket may be charged by admitting a gas or vaportothe jacket space, through one of the connections l5-I6, and venting displaced air through the opposite connection.
- This displacement should vnot be hastened but should be continued until the vent gas shows a sufficiently low air con- If the displacing gas or vapor is materially heavier than air it will naturally be admitted through the lower connection i5 and the air displaced upwardly, while if lighter than air the displacement should be in the opposite direction.
- the choice of a gas or vapor for the above purpose will be governed by the boiling point of the liquid to be stored and by the judgment of the operator as to the degree of pressure reduction which it is desirable to produce in the jacket. If it is preferred to have a close approach to complete vacuum in the jacket space the substance used to displace the air should have a vapor pressure not substantially exceeding 1 mm. mercury ata temperature corresponding to the atmospheric pressure boiling point of the stored liquid, and the quantity of residual air must be' reduced to the minimum. But if the nature of the operation is such that less perfect insulation is required', a substance having a higher vapor pressure may be used or less care need be exer- 3 cited in reducing the quantity of residual air, or both. It is possible to obtain a very useful degrec of heat exclusion with the use of substances having materially higher relative vapor pressures than that above set forth, and with the presence in the jacket of a material quantity of residual air.
- the Wall of the inner vessel ultimately comes to the atmospheric pressure boiling point of the liquid.
- the vapor filling the jacket begins to congeal on the wall of the inner vessel as the freezing-point is reached and, assuming the vapor to be air-free, diii'usion ofvvapor toward the inner wall and solidiiication thereon proceed until the pressure within the jacket equals the vapor pressure of the solid at or vslightly above the temperature of the boiling liquid.
- a high degree of rareiicatio'n of the atmosphere within the jacket is thus produced and the ow of heat through the jacket space and, in consequence, the evaporation of the contents of the inner vessel, substantially cease.
- the vapor When the evacuation is not complete and some residual air remains in the jacket space, the vapor is largely congealed on the outer surface of the inner container, as previously described, and is thereby largely eliminated as a heat conducting material.
- the mean temperature of the residual air in the insulating space is reduced, and its heat conductivity is thereby lessened as the vac- ⁇ uum is improved.
- a partial or complete precooling of the inner vessel and establishment ⁇ of the reduced pressure in the jacket space may be produced by initially filling the container with some less valuable liquid of low boiling point, or by passing through it a stream of a cold gas.
- the inner vessel is emptied and the unit allowed to come to atmospheric temperature.
- A'gas bottle indicated at 20 is then connected to inlet tube I5 and vent I6 is opened, the heavy vapor being introduced slowly until air is completely or substantially displaced.
- the two openings are then closed and sealed and liquefied gas again placed in the inner vessel, this step reestablishing the heat insulating value of the jacket space.
- the recharging operation may be begun immediately after emptying the inner container and while the unit is still cold.
- a heavy vapor such as that of a halogenated hydrocarbon
- the supply is shut oft', the unit allowed to warm up by absorbing atmospheric heat and, when the jacket space has reached at least atmospheric pressure, the valve in upper connection I6 is opened.
- the congealed substance is slowly vaporized, forming a vapor pool which displaces the air upwardly as it increases in volume. This displacement is at a low rate which avoids turbulence and intermixture of air with vapor, and accomplishes the recharging with the minimum consumption of Freon or other congealable substance.
- the stored liquid may be maintained at any pressure to whichthe inner vessel is adapted.
- a superatmospheric pressure on the stored liquid raises the actual temperature at which it boils and, in consequence, the maximum temperature at which the vapor must congeal, permitting the use of a wider variety of substances as the source of vapor.
- 'I'he essential is that the vapor should solidify, and should have a low vapor pressure, at a temperature determined by the boiling point of the stored liquid at the pressure under which it is stored.
- a storage tank adapted to retain a liquefied gas, comprising: an inner, liquid-retaining shell; a jacket surrounding and spaced from said shell to form a sealed insulating space, said space containing at the most some residual air at a very low partial pressure and containing the vapor of a substance which is in the vapor phase at atmospheric temperature and pressure and which solidenders at a temperature above the boiling point of said liquefied gas at the pressure existing in said tank and which has a very low vapor pressure at said boiling point.
- the vapor contained in said space is the vapor of a substance which solidies at a temperature above 90 Kelvin and which has a vapor pressure not substantially exceeding 1 mm. of mercury, absolute, at 90 Kelvin.
- a storage tank adapted to retain a liquefied gas, comprising: an inner, liquid-retaining shell; a jacket surrounding and spaced from said shell to form a sealed insulating space; a filling of porous material within said space, and a vapor within the voids of said iilling, said vapor being of a substance which is in the vapor phase at atmospheric temperature and pressure and which solidies at a temperature above the boiling point of said liquefied gas at the pressure existing in said tank and which has a very low vapor preslure at said boiling point.
- the method of insulating a storage tank for volatile liquids having a jacket providing an enclosure of space surrounding said tank comprising: replacing the air initially present in said space with a vapor which solidifies at a temperature above the boiling point of the liquid to be stored in said tank and which has a low vapor pressure in the solid state; sealing said vaporlled jacket to prevent leakage of air into said space when the pressure therein falls below atmospheric; placing in said tank a volatile liquid which boils at a temperature below the solidifying point of said vapor, and permitting said liquid t boil and thereby to cool the wall of said tank to the solidifying point of said vapor.
- the method of insulating a liquid oxygen storage tank having a jacket providing an enclosure of space surrounding said tank comprising: introducing into the lower portion of said space a vapor heavier than air which solidiiies to prevent leakage of air into said space when u at a temperature above K. and which has a low vapor pressure in the solid state; venting the upper portion of said space while introducing said heavy vapor and thereby replacing with said heavy vapor a material proportion of the atmosphere previously present in said space; sealing said vapor-filled jacket to prevent leakage of air into said space when the pressure therein falls below atmospheric, and causing liquid oxygen to boil in said tank until a substantial portion of said heavy vapor is solidified and the pressure in said space correspondingly reduced.
- the method of insulating a liqueedgas storage tank having a jacket providing an enclosure of space surrounding said tank comprising: introducing into thelower portion of said space a vapor heavier than air which soliditles at a temperature above the atmospheric pressure boiling point of said liquefied gas and which has a low vapor pressure in the solid state; venting the upper portion of said space while introducing said heavy vapor and thereby replacing with said heavy vapor a material proportion of the atmosphere previously present in said space; sealing said vapor-filled jacket to prevent leakage of air into said space when the pressure therein falls below atmospheric, and causing liqueiied gas to boil in said. tank until .a substantial portion of said heavy vapor is solidified and the pressure in said space correspondingly reduced.
- the method of insulating a liquefied gas storage tank having a jacket providing an enclosure of space surrounding said tank comprising: introducing into said space a vapor which solidies at a temperature above the atmospheric pressure boiling point of said liqueed gas and which has a low vapor pressure in the solid state; venting said space during said introduction at a point substantially opposite the point at which said vapor is introduced and thereby replacing with said vapor a material proportion of the atmosphere previously present in said space; sealing said jacket after introducing said vapor to prevent leakage of air into said space when the pressure therein falls below atmospheric, and vaporizing liquid gas in said tank until a substantial portion of said vapor is solidiiied and the pressure in said space correspondingly reduced.
- the method of insulating a liquefied gas storage tank having a Jacket providing an enclosure of space surrounding said tank and a packing of porous material substantially filling said space comprising: bringing said packing to substantially atmospheric temperature; introducing into said space a stream of the vapor of a substance which is in the vapor phase at atmospheric temperature and pressure, which is a solid at thefatmospheric pressure boiling point of said liqueiied gas and which has a low vapor pressure in the solid state; venting from said space gases and vapors displaced from the voids in said porous material by the introduction of said vapor; sealing said jacket after introducing said vapor to retain vapor and exclude air from said space, and cooling said tank to the is correspondingly reduced.
- the method of insulating a liquefied gas storage tank having a jacketproviding an en closure of space surrounding said tank and a packing of porous material substantially lling said space comprising: introducing into the voids in said packing material the vapor of a substance which is in the vapor phase at atmospheric temperature and pressure, which is a solid at the atmospheric pressure boiling point of said i liquefied gas and which has a low vapor pressure in the solid state; bringing a solid surface in contact with said vapor to a temperature at which a portion of said vapor is solidified and intro- 8 vapor remaining in said space is partially solidiiied on the wall of said tank and the pressure within said space is correspondingly reduced.
- the method of insulating a chamber having walls anda jacket providing an enclosure of space surrounding the chamber walls comprising: at least substantially replacing the air initially present in the space with a vapor which is a solid under conditions of use of the chamber and .which has a low vapor pressure in the solid state, the quantity of vapor being such that when at least a major portion is solidified av vacuum is formed in the space; sealing the vapor-filled jacket to preventleakage of air into the space when the pressure therein falls below atmospheric; and cooling the walls of the chamber below the solidifying point of the vapor, whereby a vacuum is formed within the space.
- the method of insulating a chamber having walls and a jacket providing an enclosure of space surrounding the chamber walls and a packing of porous material substantially iilling the space comprising: bringing the packing to substantially atmospheric temperature; at least substantially -replacing the air initially present in the space with the vapor of a substance which is in the vapor phase at 'atmospheric temperature and pressure, which is a solid under conditions oi' use of the chamber and which has a low vapor pressure in the solid state, the quantity of vapor being such that when at least a major portion is solidified a vacuum is formed; sealing the vapor-illlcd jacket to prevent leakage of air into the space when the pressure therein falls below atmospheric; cooling the walls of the chamber below the solidifying point of Ythe vapor whereby a vacuum is formed within the space.
Description
July 4, 1950 c. J. scHlLLlNG 2,513,749
INSULATED CONTAINER AND METHOD OF INSULATING THE SAME Filed May 22, 1945 CLARENCE j sKCHlLUNG INVENTOR @M Ld; f-MM.
ATTORNEY Patented 'July 4, i959 uNrrEoI 'STATES Per asians INSULATED CONTAINER AND METHOD F INSULATHNG THE SAME Clarence J. Schilling, Chattanooga, Tenn., as
signor to Air Products, Incorporated, Chattanooga, Tenn., a corporation ci Michigan Application May 22, 1945, Serial No. 595,167
(Ci. (i2-l) 16 Claims.
This invention relates to the insulation of vessels used for the storage of liqueed gases, as for example nitrogen, oxygen, air, methane and ethylene.
It is very old practice to store liqueed gases in so-called vacuum vessels, having an evacuated jacket surrounding a storage space maintained at or close to atmospheric pressure. On the small scale in which it is possible to use glass vessels, this method is highly effective in retarding heat flow into the liquid and thereby minimizing evaporation.
The same principle has been applied to storage in quantity, but the difficulty has been encountered that metallic vessels, however carefully constructed, are liable to slow inward leakage of air by which the vacuum is reduced and nally destroyed. To again evacuate the jacket, after this occurrence, requires apparatus the cost of which is not burdensome in a. stationary plant including numerous storage vessels but is prohibitive in connection with single or portable tanks.
'I'he objective of the .present invention is to provide means for producing a vacuum of useful degree in a heat insulating jacket surrounding a storage tank of any size and for reinstating the vacuum in the event it` becomes impaired after prolonged use of the container, both without the use of exhaust pumps or other evacuat- I ing machinery.
Referring to the attached drawing, whichis a longitudinal section through an exemplary storagetank and its jacket: IB is a liquefied gas storage tank of any preferred form and dimensions. This tank is provided with top and bottom pipe connections li and i2, and with such other fltments as may be desired.
An outer jacket I3 surrounds the storage tank and is spaced from it by members II-H, which should be of a material of low heat conductivity. The jacket should be as nearly air-tight as it is practicable to make it. Tightness is relative and while it is possible to construct a jacket which, when evacuated, will show no appreciable pressure rise over a considerable period, it is very dilcult to build `a metallic shell which will maintain a vacuum indefinitely. l
The jacket is provided with an inlet connection I5 for the introduction of the functioning vapor and with a vent connection I6 for the displacement of air. These tubes are illustrated as entering the jacket near its periphery. It is preferred that these tubes terminate approximately at the center of length of the tank, and that each be provided with afllter as at I7 and I8 and with tent.
' tight valves as at 2i and 22. The points at which the tubes are brought out oi the shell may be as convenient.
While not strictly essential, it is preferable to lill the space I9 between the jacket and the storage vessel proper with some light, porous, incombustible material, such as glass wool, finely comminuted diatomaceous earth or an aerogel, for example, the form of silica known commercially as Santocel This filling reduces radin ation across the insulating space, prevents convection currents and assists in the displacement of air by vapor in a step later described. The packing should be placed with care so as to ce evenly porous throughout.
The establishment of a low subatmospheric pressure, which may approach a complete vacuum, in space i9 is produced by first lling it with a suitable vapor, which is afterward liquefied, or liquefied and solidified. The air initially filling the jacket must be removed as completely as possible. In the Shop, where the necessary apparatus is available, the jacket may be evacuated and vapor admitted to take the place of the removed air, thus economizing vapor. In the iield, or in any location at which vacuum-producing machinery is not at hand, the jacket may be charged by admitting a gas or vaportothe jacket space, through one of the connections l5-I6, and venting displaced air through the opposite connection. This displacement should vnot be hastened but should be continued until the vent gas shows a sufficiently low air con- If the displacing gas or vapor is materially heavier than air it will naturally be admitted through the lower connection i5 and the air displaced upwardly, while if lighter than air the displacement should be in the opposite direction.
The choice of a gas or vapor for the above purpose will be governed by the boiling point of the liquid to be stored and by the judgment of the operator as to the degree of pressure reduction which it is desirable to produce in the jacket. If it is preferred to have a close approach to complete vacuum in the jacket space the substance used to displace the air should have a vapor pressure not substantially exceeding 1 mm. mercury ata temperature corresponding to the atmospheric pressure boiling point of the stored liquid, and the quantity of residual air must be' reduced to the minimum. But if the nature of the operation is such that less perfect insulation is required', a substance having a higher vapor pressure may be used or less care need be exer- 3 cited in reducing the quantity of residual air, or both. It is possible to obtain a very useful degrec of heat exclusion with the use of substances having materially higher relative vapor pressures than that above set forth, and with the presence in the jacket of a material quantity of residual air.
The following list of substances is suggested as I including members suitable for the storage oi' almost all liquids boiling materially below atmospheric temperature under normal atmospheric prsure:
Melting Boiling Point Point K. C'. Carbon dioxide 216 -78 Freon 114 (dichlorotetraiiuoroethane) 203 3 Sulfur iMMe 200 Freon 12 (dlchlorodiduoromethane) 195 5 Aoetylenn 191 -84 Frecn 2l (dichloromonoiiuoromethane) 173 -9 Ethylene oxide.- 162 l1 Ethgl ether. 150 35 Met yiene chloride 173 40 unit to a superatmospheric temperature in order to vaporize the agent and thus displace the jacket air.
The above examples should be considered illustrative only as any substance may be usedwhich has the requisite relation of melting point and boiling point for the specic conditions existing in each case. The Freons and other halogenated hydrocarbons are preferred displacing agents by reason of their high molecular weight.
When the inner or storage vessel is charged with a liquefied gas, such as one of those above mentioned. and is maintained at atmospheric pressure, the Wall of the inner vessel ultimately comes to the atmospheric pressure boiling point of the liquid. The vapor filling the jacket begins to congeal on the wall of the inner vessel as the freezing-point is reached and, assuming the vapor to be air-free, diii'usion ofvvapor toward the inner wall and solidiiication thereon proceed until the pressure within the jacket equals the vapor pressure of the solid at or vslightly above the temperature of the boiling liquid. A high degree of rareiicatio'n of the atmosphere within the jacket is thus produced and the ow of heat through the jacket space and, in consequence, the evaporation of the contents of the inner vessel, substantially cease.
When the evacuation is not complete and some residual air remains in the jacket space, the vapor is largely congealed on the outer surface of the inner container, as previously described, and is thereby largely eliminated as a heat conducting material. The mean temperature of the residual air in the insulating space is reduced, and its heat conductivity is thereby lessened as the vac-` uum is improved.
To avoid wastage of valuable liquids such, for example, as liquid oxygen, a partial or complete precooling of the inner vessel and establishment` of the reduced pressure in the jacket space may be produced by initially filling the container with some less valuable liquid of low boiling point, or by passing through it a stream of a cold gas.
When, with the passage of time, air leakage into the jacket space appreciably reduces its heat insulating value, the process of charging the jacket may be repeated. Two procedures are available, differing somewhat in manipulation but producing approximately the same ultimate result. f
In the first procedure, the inner vessel is emptied and the unit allowed to come to atmospheric temperature. A'gas bottle indicated at 20 is then connected to inlet tube I5 and vent I6 is opened, the heavy vapor being introduced slowly until air is completely or substantially displaced. The two openings are then closed and sealed and liquefied gas again placed in the inner vessel, this step reestablishing the heat insulating value of the jacket space.
Alternatively, the recharging operation may be begun immediately after emptying the inner container and while the unit is still cold. In this operation a heavy vapor, such as that of a halogenated hydrocarbon, is first introduced through the bottom connection I8, this vapor freezing in contact with the cold inner vessel as it enters the jacket. When a quantity of vapor equal to or somewhat greater than that which would ll the jacket space at atmospheric temperature and pressure has been introduced the supply is shut oft', the unit allowed to warm up by absorbing atmospheric heat and, when the jacket space has reached at least atmospheric pressure, the valve in upper connection I6 is opened. As the temperature rises the congealed substance is slowly vaporized, forming a vapor pool which displaces the air upwardly as it increases in volume. This displacement is at a low rate which avoids turbulence and intermixture of air with vapor, and accomplishes the recharging with the minimum consumption of Freon or other congealable substance.
If the vapor used should be lighter than air it would, of course, be introduced at the top of the jacket and the air would be displaced downwardly, the operation in all other respects being as above described.
During periods of nonuse of the unit it returns to atmospheric temperature and the vapor in the jacket space comes back to the pressure at which it was originally charged, plus that'due to air leakage, if any has occurred. This may be atmospheric ormaterially above atmospheric, as may be preferred. In either case, no inward leakage of air can occur during such periods of idleness.
In the event of severe leakage of air into the jacket space, a material improvement in insulating value may be produced, even in the absence of a supply of Freon or other vapor suitable for recharging. A considerable proportion of the leakage air may be eliminated by merely allowl ing the unit to warm up, or even heating it to a temperature materially above atmospheric, and venting the jacket space, preferably on the side opposite that which the vapor would seek by reason of its relative weight. lThis will cause air containing only a minor proportion of vapor to be discharged and on again sealing and cooling the jacket space a material reduction in pressure and a correspondingly improved insulating value will be observed.
The above descriptions refer to the storage of the liquid at atmospheric pressure, but it will be 10 undel'StOQd that this is by no means essential.
guance The stored liquid may be maintained at any pressure to whichthe inner vessel is adapted. A superatmospheric pressure on the stored liquid raises the actual temperature at which it boils and, in consequence, the maximum temperature at which the vapor must congeal, permitting the use of a wider variety of substances as the source of vapor. 'I'he essential is that the vapor should solidify, and should have a low vapor pressure, at a temperature determined by the boiling point of the stored liquid at the pressure under which it is stored.
I claim as my invention:
1. A storage tank adapted to retain a liquefied gas, comprising: an inner, liquid-retaining shell; a jacket surrounding and spaced from said shell to form a sealed insulating space, said space containing at the most some residual air at a very low partial pressure and containing the vapor of a substance which is in the vapor phase at atmospheric temperature and pressure and which solidiiles at a temperature above the boiling point of said liquefied gas at the pressure existing in said tank and which has a very low vapor pressure at said boiling point.
2. Apparatus as and for the purpose set forth in claim 1, in which the vapor contained in said space is the vapor of a halogenated hydrocarbon.
3. Apparatus as set forth in claim l, in which the vapor contained in said space is the vapor of dichlorodifluoromethane.
4. Apparatus as set forth in claim 1, in which the vapor contained in said space is the vapor of a substance which solidies at a temperature above 90 Kelvin and which has a vapor pressure not substantially exceeding 1 mm. of mercury, absolute, at 90 Kelvin.
5. A storage tank adapted to retain a liquefied gas, comprising: an inner, liquid-retaining shell; a jacket surrounding and spaced from said shell to form a sealed insulating space; a filling of porous material within said space, and a vapor within the voids of said iilling, said vapor being of a substance which is in the vapor phase at atmospheric temperature and pressure and which solidies at a temperature above the boiling point of said liquefied gas at the pressure existing in said tank and which has a very low vapor preslure at said boiling point.
6. Apparatus substantially as and for the purpose set forth in claim 5, in which said lling material is an aerogel.
7. The method of insulating a storage tank for volatile liquids having a jacket providing an enclosure of space surrounding said tank, comprising: replacing the air initially present in said space with a vapor which solidifies at a temperature above the boiling point of the liquid to be stored in said tank and which has a low vapor pressure in the solid state; sealing said vaporlled jacket to prevent leakage of air into said space when the pressure therein falls below atmospheric; placing in said tank a volatile liquid which boils at a temperature below the solidifying point of said vapor, and permitting said liquid t boil and thereby to cool the wall of said tank to the solidifying point of said vapor.
8. The method of insulating a storage tank for liquid oxygen having a jacket providing an enclosure of space surrounding said tank, comprising: replacing the air initially present in said space with a vapor which solidliles at a temperature above the atmospheric pressure boiling point of liquid oxygen; sealing said vapor-filled jacket the pressure therein vfalls below atmospheric; placing liquid oxygen in said tank, and permitting said oxygen to boil until theA wall of said tank is cooled to the solidii'ying point of said vapor, whereby the pressure within said space is reduced by the solidiiication of a portion of said vapor.
9. The method of insulating a liquid oxygen storage tank having a jacket providing an enclosure of space surrounding said tank, comprising: introducing into the lower portion of said space a vapor heavier than air which solidiiies to prevent leakage of air into said space when u at a temperature above K. and which has a low vapor pressure in the solid state; venting the upper portion of said space while introducing said heavy vapor and thereby replacing with said heavy vapor a material proportion of the atmosphere previously present in said space; sealing said vapor-filled jacket to prevent leakage of air into said space when the pressure therein falls below atmospheric, and causing liquid oxygen to boil in said tank until a substantial portion of said heavy vapor is solidified and the pressure in said space correspondingly reduced.
10. The method of insulating a liqueedgas storage tank having a jacket providing an enclosure of space surrounding said tank, comprising: introducing into thelower portion of said space a vapor heavier than air which soliditles at a temperature above the atmospheric pressure boiling point of said liquefied gas and which has a low vapor pressure in the solid state; venting the upper portion of said space while introducing said heavy vapor and thereby replacing with said heavy vapor a material proportion of the atmosphere previously present in said space; sealing said vapor-filled jacket to prevent leakage of air into said space when the pressure therein falls below atmospheric, and causing liqueiied gas to boil in said. tank until .a substantial portion of said heavy vapor is solidified and the pressure in said space correspondingly reduced.
l1. The method of insulating a liquefied gas storage tank having a jacket providing an enclosure of space surrounding said tank, comprising: introducing into said space a vapor which solidies at a temperature above the atmospheric pressure boiling point of said liqueed gas and which has a low vapor pressure in the solid state; venting said space during said introduction at a point substantially opposite the point at which said vapor is introduced and thereby replacing with said vapor a material proportion of the atmosphere previously present in said space; sealing said jacket after introducing said vapor to prevent leakage of air into said space when the pressure therein falls below atmospheric, and vaporizing liquid gas in said tank until a substantial portion of said vapor is solidiiied and the pressure in said space correspondingly reduced.
12. 'I'he method of insulating a liqueed gas storage tank having a jacket providing an enclosure of space surrounding said tank, comprising: introducing into said space a vapor which solidiiies at a temperature above the atmospheric pressure yboiling point of said liquefied gas and which has a low vapor pressure in the solid state; venting said space during said introduction at a point substantially opposite the point at which said vapor is introduced and thereby replacing with said vapor a material proportion of the atmosphere previously present in said space; sealing said jacket after said introduction to exclude air from and retain vapor in said space; reducing the temperature of the wall of said tank below the solidifying point of said vapor; storing said liquefied gas in said cooled tank, and permitting vaporization of the contents of said tank sufficient to maintain the wall of said tank below the solidiiled point of said vapor. thereby maintaining a rarened, heat-insulating atmosphere in said space.
13. The method of insulating a liquefied gas storage tank having a Jacket providing an enclosure of space surrounding said tank and a packing of porous material substantially filling said space, comprising: bringing said packing to substantially atmospheric temperature; introducing into said space a stream of the vapor of a substance which is in the vapor phase at atmospheric temperature and pressure, which is a solid at thefatmospheric pressure boiling point of said liqueiied gas and which has a low vapor pressure in the solid state; venting from said space gases and vapors displaced from the voids in said porous material by the introduction of said vapor; sealing said jacket after introducing said vapor to retain vapor and exclude air from said space, and cooling said tank to the is correspondingly reduced.
14. The method of insulating a liquefied gas storage tank having a jacketproviding an en closure of space surrounding said tank and a packing of porous material substantially lling said space, comprising: introducing into the voids in said packing material the vapor of a substance which is in the vapor phase at atmospheric temperature and pressure, which is a solid at the atmospheric pressure boiling point of said i liquefied gas and which has a low vapor pressure in the solid state; bringing a solid surface in contact with said vapor to a temperature at which a portion of said vapor is solidified and intro- 8 vapor remaining in said space is partially solidiiied on the wall of said tank and the pressure within said space is correspondingly reduced.
15. The method of insulating a chamber having walls anda jacket providing an enclosure of space surrounding the chamber walls comprising: at least substantially replacing the air initially present in the space with a vapor which is a solid under conditions of use of the chamber and .which has a low vapor pressure in the solid state, the quantity of vapor being such that when at least a major portion is solidified av vacuum is formed in the space; sealing the vapor-filled jacket to preventleakage of air into the space when the pressure therein falls below atmospheric; and cooling the walls of the chamber below the solidifying point of the vapor, whereby a vacuum is formed within the space.
16. The method of insulating a chamber having walls and a jacket providing an enclosure of space surrounding the chamber walls and a packing of porous material substantially iilling the space, comprising: bringing the packing to substantially atmospheric temperature; at least substantially -replacing the air initially present in the space with the vapor of a substance which is in the vapor phase at 'atmospheric temperature and pressure, which is a solid under conditions oi' use of the chamber and which has a low vapor pressure in the solid state, the quantity of vapor being such that when at least a major portion is solidified a vacuum is formed; sealing the vapor-illlcd jacket to prevent leakage of air into the space when the pressure therein falls below atmospheric; cooling the walls of the chamber below the solidifying point of Ythe vapor whereby a vacuum is formed within the space.
CLARENCE J. SCHILLING.
REFERENCES CITED The following references are of record in the ille of this patent:
AUNITED STATES PATENTS Hill et al Mar. 30, 1943
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US595167A US2513749A (en) | 1945-05-22 | 1945-05-22 | Insulated container and method of insulating the same |
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US595167A US2513749A (en) | 1945-05-22 | 1945-05-22 | Insulated container and method of insulating the same |
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US2742115A (en) * | 1952-06-24 | 1956-04-17 | Gen Electric | Insulated construction panel |
US2776776A (en) * | 1952-07-11 | 1957-01-08 | Gen Electric | Liquefied gas container |
US2779066A (en) * | 1952-05-23 | 1957-01-29 | Gen Motors Corp | Insulated refrigerator wall |
US2863584A (en) * | 1955-07-05 | 1958-12-09 | Little Inc A | Evacuating a mass of powdery insulation |
US2871042A (en) * | 1954-06-02 | 1959-01-27 | Bascom W Birmingham | Supporting and heat insulating means |
US2929221A (en) * | 1956-10-09 | 1960-03-22 | Texaco Inc | Method and apparatus for the transportation of liquefied petroleum products |
US2961116A (en) * | 1956-01-03 | 1960-11-22 | Applied Radiation Corp | Thermally insulated wall structure |
US2974496A (en) * | 1958-02-10 | 1961-03-14 | Conch Int Methane Ltd | Low-temperature fluid container |
US2986891A (en) * | 1958-02-10 | 1961-06-06 | Little Inc A | Low-temperature vessels |
US3007596A (en) * | 1956-07-16 | 1961-11-07 | Union Carbide Corp | Thermal insulation |
US3012407A (en) * | 1960-12-20 | 1961-12-12 | Dale L Burrows | Insulating structure |
US3021027A (en) * | 1958-10-08 | 1962-02-13 | David R Claxton | Means for supporting the inner member of a double-walled tank |
US3024941A (en) * | 1958-11-28 | 1962-03-13 | North American Aviation Inc | Temperature controlled insulation |
US3094071A (en) * | 1959-06-30 | 1963-06-18 | Union Carbide Corp | Vacuum insulated storage tanks for missile use |
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US3105148A (en) * | 1960-02-26 | 1963-09-24 | Well Surveys Inc | Variable thermal-conductance vacuum-walled container for scintillation detectors |
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US3270802A (en) * | 1963-01-10 | 1966-09-06 | Jay G Lindberg | Method and apparatus for varying thermal conductivity |
US3309884A (en) * | 1965-10-11 | 1967-03-21 | Richard S Pauliukonis | Dewar design for storage and transportation of low temperature fluids |
US3313116A (en) * | 1965-03-15 | 1967-04-11 | Mcmullen Ass John J | Method for cooling and filling liquefied gas transport and storage tanks |
US3339515A (en) * | 1965-07-06 | 1967-09-05 | Phillips Petroleum Co | Atmospheric pressure storage and transportation of volatile liquids |
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US2779066A (en) * | 1952-05-23 | 1957-01-29 | Gen Motors Corp | Insulated refrigerator wall |
US2742115A (en) * | 1952-06-24 | 1956-04-17 | Gen Electric | Insulated construction panel |
US2776776A (en) * | 1952-07-11 | 1957-01-08 | Gen Electric | Liquefied gas container |
US2871042A (en) * | 1954-06-02 | 1959-01-27 | Bascom W Birmingham | Supporting and heat insulating means |
US2863584A (en) * | 1955-07-05 | 1958-12-09 | Little Inc A | Evacuating a mass of powdery insulation |
US2961116A (en) * | 1956-01-03 | 1960-11-22 | Applied Radiation Corp | Thermally insulated wall structure |
US3007596A (en) * | 1956-07-16 | 1961-11-07 | Union Carbide Corp | Thermal insulation |
US2929221A (en) * | 1956-10-09 | 1960-03-22 | Texaco Inc | Method and apparatus for the transportation of liquefied petroleum products |
US3101862A (en) * | 1958-01-15 | 1963-08-27 | Union Carbide Corp | Container construction using load carrying insulation |
US2986891A (en) * | 1958-02-10 | 1961-06-06 | Little Inc A | Low-temperature vessels |
US2974496A (en) * | 1958-02-10 | 1961-03-14 | Conch Int Methane Ltd | Low-temperature fluid container |
US3021027A (en) * | 1958-10-08 | 1962-02-13 | David R Claxton | Means for supporting the inner member of a double-walled tank |
US3024941A (en) * | 1958-11-28 | 1962-03-13 | North American Aviation Inc | Temperature controlled insulation |
US3094071A (en) * | 1959-06-30 | 1963-06-18 | Union Carbide Corp | Vacuum insulated storage tanks for missile use |
US3105148A (en) * | 1960-02-26 | 1963-09-24 | Well Surveys Inc | Variable thermal-conductance vacuum-walled container for scintillation detectors |
US3012407A (en) * | 1960-12-20 | 1961-12-12 | Dale L Burrows | Insulating structure |
US3122004A (en) * | 1961-03-27 | 1964-02-25 | Union Carbide Corp | Apparatus for cryogenic refrigeration |
US3137143A (en) * | 1962-04-23 | 1964-06-16 | Robert B Jacobs | Condensing vacuum insulation |
US3270802A (en) * | 1963-01-10 | 1966-09-06 | Jay G Lindberg | Method and apparatus for varying thermal conductivity |
US3349574A (en) * | 1964-07-31 | 1967-10-31 | Little Inc A | Inflatable flexible double-wall insulating sealed containers for transporting perishables in a controlled atmosphere |
US3466196A (en) * | 1964-11-13 | 1969-09-09 | Thomson Houston Comp Francaise | Isothermal assembly |
US3313116A (en) * | 1965-03-15 | 1967-04-11 | Mcmullen Ass John J | Method for cooling and filling liquefied gas transport and storage tanks |
US3339515A (en) * | 1965-07-06 | 1967-09-05 | Phillips Petroleum Co | Atmospheric pressure storage and transportation of volatile liquids |
US3309884A (en) * | 1965-10-11 | 1967-03-21 | Richard S Pauliukonis | Dewar design for storage and transportation of low temperature fluids |
US3369370A (en) * | 1965-12-03 | 1968-02-20 | Hughes Aircraft Co | Method of detector cooling and device therefor |
DE2333933A1 (en) * | 1972-07-05 | 1974-01-24 | Midwesco Enterprise Inc | LOW TEMPERATURE INSULATING JACKET |
US3812886A (en) * | 1972-07-05 | 1974-05-28 | Midwesco Enterprise Inc | Cryogenic insulation |
US4349051A (en) * | 1979-03-23 | 1982-09-14 | Lothar Schilf | Thermal insulation of vessels and method of fabrication |
US4417428A (en) * | 1981-02-19 | 1983-11-29 | Boeing Aerospace Company | Integral purged multi-layer insulation design |
FR2502289A1 (en) * | 1981-03-19 | 1982-09-24 | Applied Thermodynamics Lonog S | LIQUEFIED NATURAL GAS RESERVOIR, IN PARTICULAR METHANE |
EP0064887A1 (en) * | 1981-03-19 | 1982-11-17 | APPLIED THERMODYNAMICS & L.N.G. SERVICE Société à Responsabilité Limiteé de droit français | Reservoir for liquefied gas, particularly for methane gas |
US4388810A (en) * | 1981-03-19 | 1983-06-21 | Gaz De France | Storage tank for liquefied gas such as methane |
US4636415A (en) * | 1985-02-08 | 1987-01-13 | General Electric Company | Precipitated silica insulation |
US4681788A (en) * | 1986-07-31 | 1987-07-21 | General Electric Company | Insulation formed of precipitated silica and fly ash |
US4972967A (en) * | 1990-01-16 | 1990-11-27 | Soltech, Inc. | Water heater construction and sealing device therefor |
US5228585A (en) * | 1991-08-28 | 1993-07-20 | Minnesota Valley Engineering, Inc. | Variable capacity vehicle-mounted cryogenic storage vessels and method of making same |
US20070039967A1 (en) * | 2003-05-02 | 2007-02-22 | Nippon Oil Corporation | Method of manufacturing gas cylinder, gas cylinder, and method of occluding and discharging gas |
US7669727B2 (en) * | 2003-09-04 | 2010-03-02 | Millipore Corporation | Bag support system |
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US8240344B2 (en) * | 2008-08-05 | 2012-08-14 | Chicago Bridge & Iron Company | Method and apparatus for insulating a component of a low-temperature or cryogenic storage tank |
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