US2927437A - Tank for storing low temperature liquids in ambient surroundings - Google Patents
Tank for storing low temperature liquids in ambient surroundings Download PDFInfo
- Publication number
- US2927437A US2927437A US457174A US45717454A US2927437A US 2927437 A US2927437 A US 2927437A US 457174 A US457174 A US 457174A US 45717454 A US45717454 A US 45717454A US 2927437 A US2927437 A US 2927437A
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- United States
- Prior art keywords
- tank
- passage
- liquid
- gas
- low temperature
- Prior art date
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- Expired - Lifetime
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/10—Vessels not under pressure with provision for thermal insulation by liquid-circulating or vapour-circulating jackets
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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
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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
- F17C2203/0639—Steels
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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
- F17C2203/0658—Synthetics
- F17C2203/066—Plastics
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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
- F17C2221/012—Hydrogen
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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
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/04—Handled 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
- F17C2223/042—Localisation of the removal point
- F17C2223/046—Localisation of the removal point in the liquid
- F17C2223/047—Localisation of the removal point in the liquid with a dip tube
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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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0337—Heat exchange with the fluid by cooling
- F17C2227/0341—Heat exchange with the fluid by cooling using another fluid
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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
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0367—Localisation of heat exchange
- F17C2227/0388—Localisation of heat exchange separate
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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
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/016—Preventing slosh
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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
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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
- F17C2265/00—Effects achieved by gas storage or gas handling
- F17C2265/03—Treating the boil-off
- F17C2265/032—Treating the boil-off by recovery
- F17C2265/033—Treating the boil-off by recovery with cooling
- F17C2265/034—Treating the boil-off by recovery with cooling with condensing the gas phase
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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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/32—Hydrogen storage
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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
- Y10S62/00—Refrigeration
- Y10S62/19—Ionic thompson effect
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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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4935—Heat exchanger or boiler making
Definitions
- This invention relates to a tank for storing low temperature liquids in ambient surroundings and more particularly to the storage tank which includes both means for cooling the low temperature liquid and means for maintaining the outside surface of said tank at about ambient temperature in order to prevent the formation of excessive frost on the exterior of the tank.
- the tirst passage ⁇ means is for vthe recirculation of the evaporated gases in order to continually cool the liquid within the tank and these recirculated gases are cooled to a low temperature by passing through a heat exchanger connected to the low temperature liquid supply.
- a quantity of the evaporated gas is circulated around the outer shell of the tank and is heated to about ambient temperature in order to maintain the outer skin of the tank at about ambient ternperature and thereby eliminate the formation of frost on the exterior of the tank.
- the gas circulated in this passage means can be heated by the engine exhaust or by burning a portion of this circulate gas in a combustion chamber. Also, provision is made to supply gas to the second passage means from the rst passage means when the pressure in the iirst passage means exceeds a predetermined value.
- the tank of this invention is particularly suitable for storage of liquid hydrogen which, in gas form, can be combusted to heat the outer skin of the tank.
- Another object of the invention is to provide a tank for storing low temperature liquids in which the evaporated liquid is recirculated around the inner container to prevent excessive evaporation and a portion of the evaporated liquid is supplied to a heating cycle which c discharge f rorn the outer chamber is connected with;
- Another object of the invention is to provide a liquid storage tank having inner passage means associated with the inner container to maintain the low temperature liquid with minimum evaporation and having an outer passage means containing evaporated gas at about ambient temperature in order to prevent formation of frost 0n the exterior of the tank.
- Figure 1 is a perspective view of the storage tank of the present invention illustrating the shape of the tank.
- Figure 2 is -a transverse vertical section along line 2-2 of Figure 1 illustrating the inner and outer passages for the tank and the baffles for the tank.
- Figure 3 is a vertical section along line 3--3 of Figure 2 illustrating the apparatus associated with the tank for cooling the low temperature liquid and for heating the outside skin of the tank.
- the tank is illustrated as having a cylindrical center section with dome shaped ends.
- the tank is formed of an inner container 5 which can be constructed ofany suitable material, such as steel or plastic, and an outer skin 6 which can likewise be constructed of any suitable material.
- the inner container supports a pair of vertical articless 7 and 8 which have openings 9 and 10, respectively, in order to permit some movement of the liquid within the tank.
- a horizontal bafe 11 is supported by the inner container and has openings 12 for permitting some vertical movement of the liquid within the tank.
- An inlet passage 13 passes through the outer skin and the inner container and is secured to a fitting 14. The inlet passage discharges near the bottom of the tank and has a cap 15 to seal the passage when not in use.
- the outer shell and inner container are separated by an insulating member 16 in which is formed a plurality of inner passages 17 and a plurality of outer passages 18.
- the outer passages 18 are closed by the outer skin 6 of the tank while the inner passages 17 are in contact with an insulating layer 19 of uniform thickness which surrounds the inner container 5.
- Each of the passages 17 and 18 pass completely around the tank and are separated from one another by projections 20 and 21, respectively, of member 16.
- the passages 17 all communicate with a header space 22 at one end of the tank and with a header space 23 at the other end of the tank and these header spaces are closed by circular enlargements 24 and 25, respectively, formed at each end of the member 16.
- the outer skin 6 has circular extensions 26 and 27 at opposite dome ends of the tank and these circular members are larger in diameter than the enlargements 24 and 25, respectively, in order to form header spaces 28 and 29 at the end of the tank with which the passages ⁇ 18 connect.
- passage 31 the gases evaporating from the level 30 of the low temperature liquid are led through passage 31 to the center passage 17.
- Passage 31 is protected by a plate 32 secured to the underside of the inner container 5 and by bafes 33. These evaporated gases pass to header space 23 where they are intermingled with previously evaporated gases received from all of the passages y17.
- a passage 34 extends through enlargement member 2'5 and connects with header space 23 and is also connected to a passage 35 through a litting 36. Passage 35 connectsv with the outer chamber 37 of heat exchanger 38 and the Y3 hesiter ze -thgh pss'gess and brewer 4o.
- blower 40 serves to continually recirculte the cooled evaporated gases through the heat exchanger 38 and through the passages 17.
- the 4lowu temperature liquid within the nner container -sV is withdrawn atraiga pas: sage-41 containing a pump 42 and the passage 41. leads" to the inner chamber '43 of heat exchanger 38 which in tutti is connected by passage 44 to the point of use, such as non-air breathing engine or other process.
- the low temperature liquid will be evaporated in inner cham# ber 43 by the heat absorbed from the recirculated Vgases in chamber 37 and the recirculated gas in passage 39 will be at about the liquilication temperatureof the low temperature liquid.
- a passage 45 connects with fitting 36 and has an enlarged portion 46 which contains apacking 47, the enlarged portion being connected with a passage 48 through a tting ⁇ 49.
- the packing 47 acts as aresistant to the flow of evaporated gas throughpassage 4S to' passage 48 and permits flow only when the pressure of the gas in passage 45 exceeds a predetermined value. Therefore, the packing serves as a release valve to prevent the pressure in the cooling passages 17 from exceeding a set va 1ue.
- the heating system which serves tomaintain the outer skin of the tank at about ambient temperature, will now be described.
- the passage 48 connects with the diseharge header 29 and with the outer chamber 50 of heat exchanger 51.
- the outer chamber 50 is also conneeted with the inlet header 28 through passage 52 which contains blower 53 to maintain circulation of the gases through passages 18.
- the inner chamber 54 of heat exchanger 51 is connected to iitting 55 through passage 56 and. two alternate passages are connected with fitting 55 in order to supply heating gases through passage 6 to chamber 54.
- the exhaust of the engine can be con-Y nected Vto fitting 55 through passage 57 which contains avalve 58 for regulating the amount of exhaust supplied to the chamber 54.
- a combustion chamber '59 is connected to fitting 55 and is supplied with oxygen gas or other oxidant through passage r60 which contains a' valve 61 for regulating the supply.
- the fuel supplied to the combustion chamber is withdrawn from passage 52 through passage 62 which also contains a valve 63 for regulating the fuel supply to the combustion chamber.
- valve 58 When the valve 58 is closed and the valves 61 and 61'y are regulated, a portion of, the evaporated gas in the heating cycle is continually withdrawn and combusted in combustion chamber 59, and the combustion products are discharged to atmosphere through a passage 64, which contains a release valve 65 in order to prevent the pressure in the combustion chamber from exceeding a predetermined value.
- a passage 64 which contains a release valve 65 in order to prevent the pressure in the combustion chamber from exceeding a predetermined value.
- valves 61 and 63 When it is desired to heat the gases in the heating system by engine exhaust only, the valves 61 and 63 are closed and the valve yS8 is regulated to supply the desired amount of heat to heat exchanger 51, and theex# haust gases are exhausted to atmosphere through passage 6 4 and the pressure of the exhaust is rnaintained a t ⁇ the desired value by release valve 6 5.
- both valves 61 and ⁇ 6.?) are closed, there willbe Vno evaporated gas withf drawn from the heating system and therefre a release Valve' 66 is placed in passage 48 in'order td prevent the pressure in the heating system; from exceeding a preselected value.
- a portion of the evaporated gas is supplied 4to this system through passage 45 to passage 48 and the gases are heated in heat exchanger 51 to about ambient temperature.
- the circulation of these heated gases through passages 18 serve to maintain the outer skin 6 of the tank at about ambient temperature so that frost will not form on the outer skin of the tank.
- the heated gases entering header 28 will be at somewhat higher temperature than the gases leaving header 29 and that the heat exchanger 51 can be regulated to rnaiiitaintli average temperature of the outer skin at about ambient temperature.
- frost of course, is un desirable since it adds weight to the tank and *makes it difficult to utilize the tank in eonnectionwith other structure.
- the oxygen supply passage 60 can connect with any available oxygen supply and the heat exchangers can beof any desired construction, 0f course, both engine exhaust and the combustionchamber 59, ⁇ c an he used at the vsante time by proper regulation of valves 58, 61 and 6 While the tankhas been describedas containinv4 a low temperature liquid, it is apparent that this low temper Vture substance must be in the form of a fuel, lsuch as liquid hydrogen, if combustion vchamber y59 is to' be utilized.
- a storage tank for a low temperature liquid has been provided in which the inner container of thetank is continually cooled byold gases evaporating from the liquid and these gases are' further cooled by the low-temperature liquid itself.
- the tank is supplied with aheating system "cli warms the outer skin of the tank to about ambient 'ternl perature and prevents the formation of frost on the tank.
- This heatingcycle can utilize either the exhaust'frofrnf an engine or can continually utilize a portion 4ofthe evaporated gases in a combustion chamber.l Itis under"-1 stood that the only heat transferred bo the lowtempera; ture liquid in the inner container will be from these ambient vgases in the passages 18 and the insulating nierny bers 16 and 19 resist such heat transfer.
- various types o'f passage constructions can be provided between the' outer skin and inner container and the shape and sizeof the tankcan be varied in accordance with the use of the tank.
- Various other modifications are contemplated 4by those skilled in the art without departing from the spirit and scope of the invention as hereinafter defined by the appended claims.
- An apparatus for storing gas material in the forni of a low temperature liquid comprising a tank having inner container forhousing said liquid and an outer skin, a uniform layer of insulation covering said inner eontainer, an insulation member positionedbetween said uni; form layer and said outer skin and having a plurality of inner passages on its inner surface and aplurality of outer passages formed on its outer, surface adjacent said outer skin, separate header means formed at each end of said tank for said inner passages and for said outer passages, means for passing the gas evaporating from said liquid to said inner passages, means for circulating said gas from one header means to the other header means for said inner passages and through said inner passages, heat exchanger means for cooling said circulated gas in said inner passages with the low temperature liquid with-l drawn from said inner container, means for supplying evaporated gas to said outer passages from said inner passages and containing a pressure relief vals'ie tocontrol the pressure in said inner passagesgand ineans for heat'- ing the gascirc
- heating means receives a high temperature gas supply as the heating medium, said heating means being exhausted to atmosphere through a conduit containing a release valve for maintaining the desired pressure within said heating means.
- An apparatus for storing gas material in the form ot' a low temperature liquid comprising a tank having an inner container and an outer skin, iirst passage means surrounding said inner container of said tank and connected with the gas evaporating from said liquid, means for recirculating evaporated gas through said first passage means to thereby insulate said liquid, second passage means surrounding the outer skin of said tank and connected with gases evaporating from said tank, heat exchange means connected with said second passage means for raising the temperature of the gas in the said second passage means, and means for recirculating evaporated gas through said second passage means and said heat exchanger means to maintain said outer skin at about ambient temperature.
- An apparatus as deiined in claim 4 having means for removing the low temperature liquid from said tank, a heat exchanger connected with said first passage means and with said removing means for cooling the gas recirculated through said iirst passage means with the liquid removed from the tank.
- An apparatus as deiined in claim 4 having means connecting said iirst passage means with said second passage means for supplying evaporated gas to said second passage means.
- An apparatus for storing gas material in the form of low temperature liquid comprising a tank, first means for collecting cold gas evaporating from said liquid and recirculating said gas around said low temperature liquid in said tank to insulate said liquid, second means for circulating a heating medium around the outer surface of said tank to heat said surface and prevent the formation of frost thereon, said evaporated gas being combustible, combustion means supplied with said gas and an oxidant for maintaining combustion therein and producing heat, and heat exchanger means connected with said combustion means and with said second means for raising the temperature of said heating medium.
- An apparatus for storing gas material in the form of a low temperature liquid comprising a tank having an inner container for housing said liquid and an outer skin separated from said inner container, first passage means positioned adjacent said inner container, means for connecting said rst passage means with gas evaporated from Said liquid in order to insulate said liquid, second passage means positioned adjacent said outer skin, means for connecting said second passage means with a heating medium, means for heating said medium in said second passage means to maintain said outer skin at about ambient temperature and prevent the formation of frost, said evaporated gas being combustible, said heating means comprising combustion means supplied with evaporated gas and an oxidant for maintaining combustion therein and producing heat and heat exchanger means connected with said combustion means and with said second passage means for raising the temperature of said heating medium.
- An apparatus for storing gas material in the form of a low temperature liquid comprising a tank having an inner container for housing said liquid and an outer skin Separated from said inner container, first passage means positioned adjacent said inner container, means for connecting said iirst passage means with gas evaporated from said liquid in order to insulate said liquid, second passage means positioned adjacent saidzouter skin, means for connecting said second passage means with a heating medium, means for heating said medium in said second passage means to maintain said outer skin at about ambient temperature and prevent the formation of frost, said heating medium comprising evaporated gas, and means for supplying said evaporated gas to said second passage means from said vfirst passage means.
- heating means comprises a heat exchanger connected with said second passage means, and combustion means for combusting gas received from said second passage means to supply heat for said heat exchanger.
- said supply means comprises a conduit means containing a relief valve for controlling the pressure in said rst passage means and the flow of gas from said rst passage means to said second passage means.
- An apparatus for storing gas in the form of a low temperature liquid comprising an inner container for housing said liquid, an outer skin separated from said inner container, substantially the entire space between said container and skin containing only rst and second passage means separated by insulation means, said insulation means enclosing said inner container, said rst passage means being located at one side of and inwardly of said insulation means and positioned adjacent said inner container, means for connecting said rst passage means with gas evaporated from said liquid in order to insulate said liquid, said second passage means being located at the other side of and outwardly of said insulation means and adjacent said outer skin, means for connecting said second passage means with a heating medium, and means for heating said medium in said second passage means to maintain said outer skin at about ambient temperature to prevent the formation of frost.
- An apparatus as dened in claim 13 having heat exchange means connected with said tirst passage means and with said low temperature liquid in said inner container, and means for recirculating the evaporated gas in said rst passage means through said heat exchange means to cool the gas in said rst passage means with the liquid withdrawn from the inner container.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
March 8, 1960 R. s, RAE 2,927,437
TANK FOR sToRING Low TEMPERATURE LIQUIDS IN AMBIENT sURRoUNDINGs Filed sept. 2o, 1954 Arran/VEY :United States Patent TANK FOR STORING LOW TEMPERATURE LIQUIDS IN AMBIENT SURROUNDINGS Randolph Samuel Rae, Santa Monica, Calif., assignor to The Garrett Corporation, Los Angeles, Calif., a corporation of California Application September 20, 1954, Serial No. 457,174
14 Claims. (Cl. 62-53) This invention relates to a tank for storing low temperature liquids in ambient surroundings and more particularly to the storage tank which includes both means for cooling the low temperature liquid and means for maintaining the outside surface of said tank at about ambient temperature in order to prevent the formation of excessive frost on the exterior of the tank.
When a low temperature liquid, such as liquid hydrogen, is utilized as fuel for a non-air breathing engine or in other processes, it is necessary to store the low temperature liquid .without excessive evaporation. Also, when the liquid is utilized in ambient surroundings, a considerable amount of frost will normally form on the exterior surface of the container because of the low temperature of the liquid. In the liquid storage tank disclosed in pending U.S. application Serial No. 417,- 658 tiled March 22, 1954 by Randolph Samuel Rae, the cold evaportaed gases are recirculated around the low temperature liquid container in order to maintain the liquid at about the liquitication temperature. Also, as disclosed in pending U.S. application Serial No. 457,173 filed September 20, 1954 by Randolph Samuel Rae, it is possible to utilize arseparate refrigerant of lower temperature than the liquid being stored in order to prevent excessive evaporation of the liquid. By the present invention, two separate passage means are provided around the container for the low temperature liquids. The tirst passage `means is for vthe recirculation of the evaporated gases in order to continually cool the liquid within the tank and these recirculated gases are cooled to a low temperature by passing through a heat exchanger connected to the low temperature liquid supply. In the second passage means, a quantity of the evaporated gas is circulated around the outer shell of the tank and is heated to about ambient temperature in order to maintain the outer skin of the tank at about ambient ternperature and thereby eliminate the formation of frost on the exterior of the tank. The gas circulated in this passage means can be heated by the engine exhaust or by burning a portion of this circulate gas in a combustion chamber. Also, provision is made to supply gas to the second passage means from the rst passage means when the pressure in the iirst passage means exceeds a predetermined value. The tank of this inventionis particularly suitable for storage of liquid hydrogen which, in gas form, can be combusted to heat the outer skin of the tank.
. It is therefore an object of the present invention to provide a storage tank for low temperature liquids which has its outer skin continually maintained at about ambient temperature in order to prevent the formation of frost on the outer skin. c
Another object of the invention is to provide a tank for storing low temperature liquids in which the evaporated liquid is recirculated around the inner container to prevent excessive evaporation and a portion of the evaporated liquid is supplied to a heating cycle which c discharge f rorn the outer chamber is connected with;-
ice
maintains the outer skin of the tank at about ambient temperature.
Another object of the invention is to provide a liquid storage tank having inner passage means associated with the inner container to maintain the low temperature liquid with minimum evaporation and having an outer passage means containing evaporated gas at about ambient temperature in order to prevent formation of frost 0n the exterior of the tank.
These and other objects of the invention not specilically set forth above will become readily apparent from the accompanying description and drawings in which,
Figure 1 is a perspective view of the storage tank of the present invention illustrating the shape of the tank.
Figure 2 is -a transverse vertical section along line 2-2 of Figure 1 illustrating the inner and outer passages for the tank and the baffles for the tank.
Figure 3 is a vertical section along line 3--3 of Figure 2 illustrating the apparatus associated with the tank for cooling the low temperature liquid and for heating the outside skin of the tank.
Referring to Figure l, the tank is illustrated as having a cylindrical center section with dome shaped ends. The tank is formed of an inner container 5 which can be constructed ofany suitable material, such as steel or plastic, and an outer skin 6 which can likewise be constructed of any suitable material. The inner container supports a pair of vertical baies 7 and 8 which have openings 9 and 10, respectively, in order to permit some movement of the liquid within the tank. Also, a horizontal bafe 11 is supported by the inner container and has openings 12 for permitting some vertical movement of the liquid within the tank. An inlet passage 13 passes through the outer skin and the inner container and is secured to a fitting 14. The inlet passage discharges near the bottom of the tank and has a cap 15 to seal the passage when not in use. The outer shell and inner container are separated by an insulating member 16 in which is formed a plurality of inner passages 17 and a plurality of outer passages 18. The outer passages 18 are closed by the outer skin 6 of the tank while the inner passages 17 are in contact with an insulating layer 19 of uniform thickness which surrounds the inner container 5. Each of the passages 17 and 18 pass completely around the tank and are separated from one another by projections 20 and 21, respectively, of member 16. The passages 17 all communicate with a header space 22 at one end of the tank and with a header space 23 at the other end of the tank and these header spaces are closed by circular enlargements 24 and 25, respectively, formed at each end of the member 16. The outer skin 6 has circular extensions 26 and 27 at opposite dome ends of the tank and these circular members are larger in diameter than the enlargements 24 and 25, respectively, in order to form header spaces 28 and 29 at the end of the tank with which the passages `18 connect.
Referring now to the cooling system including passages 17, the gases evaporating from the level 30 of the low temperature liquid are led through passage 31 to the center passage 17. Passage 31 is protected by a plate 32 secured to the underside of the inner container 5 and by bafes 33. These evaporated gases pass to header space 23 where they are intermingled with previously evaporated gases received from all of the passages y17. A passage 34 extends through enlargement member 2'5 and connects with header space 23 and is also connected to a passage 35 through a litting 36. Passage 35 connectsv with the outer chamber 37 of heat exchanger 38 and the Y3 hesiter ze -thgh pss'gess and brewer 4o. 'n1 e blower 40 serves to continually recirculte the cooled evaporated gases through the heat exchanger 38 and through the passages 17. The 4lowu temperature liquid within the nner container -sV is withdrawn atraiga pas: sage-41 containing a pump 42 and the passage 41. leads" to the inner chamber '43 of heat exchanger 38 which in tutti is connected by passage 44 to the point of use, such as non-air breathing engine or other process. The low temperature liquid will be evaporated in inner cham# ber 43 by the heat absorbed from the recirculated Vgases in chamber 37 and the recirculated gas in passage 39 will be at about the liquilication temperatureof the low temperature liquid. By recirculating the cooled evaporated gases around the inner container of the tank by blower 40, the amount of gas which will evaporate from the liquid will be substantially reduced.
Since the liquid will continuato evaporateto form incre gas, it is necessary to permit a portion of the gas from the cooling passages-17 to escape. For this 'purpose, a passage 45 connects with fitting 36 and has an enlarged portion 46 which contains apacking 47, the enlarged portion being connected with a passage 48 through a tting `49. The packing 47 acts as aresistant to the flow of evaporated gas throughpassage 4S to' passage 48 and permits flow only when the pressure of the gas in passage 45 exceeds a predetermined value. Therefore, the packing serves as a release valve to prevent the pressure in the cooling passages 17 from exceeding a set va 1ue.
The heating system which serves tomaintain the outer skin of the tank at about ambient temperature, will now be described. The passage 48 connects with the diseharge header 29 and with the outer chamber 50 of heat exchanger 51. The outer chamber 50 is also conneeted with the inlet header 28 through passage 52 which contains blower 53 to maintain circulation of the gases through passages 18. The inner chamber 54 of heat exchanger 51 is connected to iitting 55 through passage 56 and. two alternate passages are connected with fitting 55 in order to supply heating gases through passage 6 to chamber 54. In the event the low ltemperature liquid, such as hydrogen, is utilized as a fuel fora nonair breathing engine, the exhaust of the engine can be con-Y nected Vto fitting 55 through passage 57 which contains avalve 58 for regulating the amount of exhaust supplied to the chamber 54. Also, a combustion chamber '59 is connected to fitting 55 and is supplied with oxygen gas or other oxidant through passage r60 which contains a' valve 61 for regulating the supply. The fuel supplied to the combustion chamber is withdrawn from passage 52 through passage 62 which also contains a valve 63 for regulating the fuel supply to the combustion chamber.
When the valve 58 is closed and the valves 61 and 61'y are regulated, a portion of, the evaporated gas in the heating cycle is continually withdrawn and combusted in combustion chamber 59, and the combustion products are discharged to atmosphere through a passage 64, which contains a release valve 65 in order to prevent the pressure in the combustion chamber from exceeding a predetermined value. By continually combusting a portion of the evaporated gases in the heating system, the pressure in this system including passages 1'8 will be continually relieved.
When it is desired to heat the gases in the heating system by engine exhaust only, the valves 61 and 63 are closed and the valve yS8 is regulated to supply the desired amount of heat to heat exchanger 51, and theex# haust gases are exhausted to atmosphere through passage 6 4 and the pressure of the exhaust is rnaintained a t `the desired value by release valve 6 5. When both valves 61 and `6.?) are closed, there willbe Vno evaporated gas withf drawn from the heating system and therefre a release Valve' 66 is placed in passage 48 in'order td prevent the pressure in the heating system; from exceeding a preselected value. In operati-on of the heating system, a portion of the evaporated gas is supplied 4to this system through passage 45 to passage 48 and the gases are heated in heat exchanger 51 to about ambient temperature. The circulation of these heated gases through passages 18 serve to maintain the outer skin 6 of the tank at about ambient temperature so that frost will not form on the outer skin of the tank. It is understood that the heated gases entering header 28 will be at somewhat higher temperature than the gases leaving header 29 and that the heat exchanger 51 can be regulated to rnaiiitaintli average temperature of the outer skin at about ambient temperature. The formationof frost, of course, is un desirable since it adds weight to the tank and *makes it difficult to utilize the tank in eonnectionwith other structure. The oxygen supply passage 60 can connect with any available oxygen supply and the heat exchangers can beof any desired construction, 0f course, both engine exhaust and the combustionchamber 59, `c an he used at the vsante time by proper regulation of valves 58, 61 and 6 While the tankhas been describedas containinv4 a low temperature liquid, it is apparent that this low temper Vture substance must be in the form of a fuel, lsuch as liquid hydrogen, if combustion vchamber y59 is to' be utilized. By the present invention, a storage tank for a low temperature liquid has been provided in which the inner container of thetank is continually cooled byold gases evaporating from the liquid and these gases are' further cooled by the low-temperature liquid itself. `Iii addition, the tank is supplied with aheating system "cli warms the outer skin of the tank to about ambient 'ternl perature and prevents the formation of frost on the tank.' This heatingcycle can utilize either the exhaust'frofrnf an engine or can continually utilize a portion 4ofthe evaporated gases in a combustion chamber.l Itis under"-1 stood that the only heat transferred bo the lowtempera; ture liquid in the inner container will be from these ambient vgases in the passages 18 and the insulating nierny bers 16 and 19 resist such heat transfer. ,Various types o'f passage constructions can be provided between the' outer skin and inner container and the shape and sizeof the tankcan be varied in accordance with the use of the tank. Various other modifications are contemplated 4by those skilled in the art without departing from the spirit and scope of the invention as hereinafter defined by the appended claims.
What is claimeds:
l. An apparatus for storing gas material in the forni of a low temperature liquid comprising a tank having inner container forhousing said liquid and an outer skin, a uniform layer of insulation covering said inner eontainer, an insulation member positionedbetween said uni; form layer and said outer skin and having a plurality of inner passages on its inner surface and aplurality of outer passages formed on its outer, surface adjacent said outer skin, separate header means formed at each end of said tank for said inner passages and for said outer passages, means for passing the gas evaporating from said liquid to said inner passages, means for circulating said gas from one header means to the other header means for said inner passages and through said inner passages, heat exchanger means for cooling said circulated gas in said inner passages with the low temperature liquid with-l drawn from said inner container, means for supplying evaporated gas to said outer passages from said inner passages and containing a pressure relief vals'ie tocontrol the pressure in said inner passagesgand ineans for heat'- ing the gascirculated in said outer passages to maintain said outer skin at about ambient temperature.
2. An apparatus as defined in claim 1 havingeonibus` aan 'chamber' 'means utilizing s tiefstenf the gas Ain snit- A este Passages as f eh and' Sepat nia'frrffirrrvi-ssf an' oxidant to said combustion' chamber means, said comav bustion chamber means supplying high temperature heating medium to said heating means.
3. An apparatus as defined in claim 1 wherein said heating means receives a high temperature gas supply as the heating medium, said heating means being exhausted to atmosphere through a conduit containing a release valve for maintaining the desired pressure within said heating means.
4. An apparatus for storing gas material in the form ot' a low temperature liquid comprising a tank having an inner container and an outer skin, iirst passage means surrounding said inner container of said tank and connected with the gas evaporating from said liquid, means for recirculating evaporated gas through said first passage means to thereby insulate said liquid, second passage means surrounding the outer skin of said tank and connected with gases evaporating from said tank, heat exchange means connected with said second passage means for raising the temperature of the gas in the said second passage means, and means for recirculating evaporated gas through said second passage means and said heat exchanger means to maintain said outer skin at about ambient temperature.
5. An apparatus as deiined in claim 4 having means for removing the low temperature liquid from said tank, a heat exchanger connected with said first passage means and with said removing means for cooling the gas recirculated through said iirst passage means with the liquid removed from the tank.
6. An apparatus as deiined in claim 4 having means connecting said iirst passage means with said second passage means for supplying evaporated gas to said second passage means.
7. An apparatus for storing gas material in the form of low temperature liquid, comprising a tank, first means for collecting cold gas evaporating from said liquid and recirculating said gas around said low temperature liquid in said tank to insulate said liquid, second means for circulating a heating medium around the outer surface of said tank to heat said surface and prevent the formation of frost thereon, said evaporated gas being combustible, combustion means supplied with said gas and an oxidant for maintaining combustion therein and producing heat, and heat exchanger means connected with said combustion means and with said second means for raising the temperature of said heating medium.
8. An apparatus as defined in claim 7 wherein said liquid and evaporated gas is hydrogen.
9. An apparatus for storing gas material in the form of a low temperature liquid comprising a tank having an inner container for housing said liquid and an outer skin separated from said inner container, first passage means positioned adjacent said inner container, means for connecting said rst passage means with gas evaporated from Said liquid in order to insulate said liquid, second passage means positioned adjacent said outer skin, means for connecting said second passage means with a heating medium, means for heating said medium in said second passage means to maintain said outer skin at about ambient temperature and prevent the formation of frost, said evaporated gas being combustible, said heating means comprising combustion means supplied with evaporated gas and an oxidant for maintaining combustion therein and producing heat and heat exchanger means connected with said combustion means and with said second passage means for raising the temperature of said heating medium.
10. An apparatus for storing gas material in the form of a low temperature liquid comprising a tank having an inner container for housing said liquid and an outer skin Separated from said inner container, first passage means positioned adjacent said inner container, means for connecting said iirst passage means with gas evaporated from said liquid in order to insulate said liquid, second passage means positioned adjacent saidzouter skin, means for connecting said second passage means with a heating medium, means for heating said medium in said second passage means to maintain said outer skin at about ambient temperature and prevent the formation of frost, said heating medium comprising evaporated gas, and means for supplying said evaporated gas to said second passage means from said vfirst passage means.
l1. An apparatus as dened in claim 10 wherein said heating means comprises a heat exchanger connected with said second passage means, and combustion means for combusting gas received from said second passage means to supply heat for said heat exchanger.
12. An apparatus as defined in claim 10 wherein said supply means comprises a conduit means containing a relief valve for controlling the pressure in said rst passage means and the flow of gas from said rst passage means to said second passage means.
13. An apparatus for storing gas in the form of a low temperature liquid comprising an inner container for housing said liquid, an outer skin separated from said inner container, substantially the entire space between said container and skin containing only rst and second passage means separated by insulation means, said insulation means enclosing said inner container, said rst passage means being located at one side of and inwardly of said insulation means and positioned adjacent said inner container, means for connecting said rst passage means with gas evaporated from said liquid in order to insulate said liquid, said second passage means being located at the other side of and outwardly of said insulation means and adjacent said outer skin, means for connecting said second passage means with a heating medium, and means for heating said medium in said second passage means to maintain said outer skin at about ambient temperature to prevent the formation of frost.
14. An apparatus as dened in claim 13 having heat exchange means connected with said tirst passage means and with said low temperature liquid in said inner container, and means for recirculating the evaporated gas in said rst passage means through said heat exchange means to cool the gas in said rst passage means with the liquid withdrawn from the inner container.
References Cited in the le of this patent UNITED STATES PATENTS 1,088,052 Aumont Feb. 24, 1914 2,356,778 Morrison Aug. 29, 1944 2,444,667 Philipp July 6, 1948 2,509,612 Philipp May 30, 1950 2,682,154 Wilkinson .Tune 29, 1954 FOREIGN PATENTS 668,602 Germany Dec. 7, 1938
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US457174A US2927437A (en) | 1954-09-20 | 1954-09-20 | Tank for storing low temperature liquids in ambient surroundings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US457174A US2927437A (en) | 1954-09-20 | 1954-09-20 | Tank for storing low temperature liquids in ambient surroundings |
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US2927437A true US2927437A (en) | 1960-03-08 |
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US457174A Expired - Lifetime US2927437A (en) | 1954-09-20 | 1954-09-20 | Tank for storing low temperature liquids in ambient surroundings |
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Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3064451A (en) * | 1960-01-14 | 1962-11-20 | Union Carbide Corp | Cooling head for small chambers |
US3069042A (en) * | 1961-07-06 | 1962-12-18 | Herrick L Johnston Inc | Method and apparatus for storing liquefied gases |
US3122004A (en) * | 1961-03-27 | 1964-02-25 | Union Carbide Corp | Apparatus for cryogenic refrigeration |
US3134237A (en) * | 1960-12-21 | 1964-05-26 | Union Carbide Corp | Container for low-boiling liquefied gases |
US3159005A (en) * | 1962-06-06 | 1964-12-01 | Phillips Petroleum Co | Insulation system for low temperature service |
US3177672A (en) * | 1960-03-31 | 1965-04-13 | Martin Marietta Corp | Space simulating apparatus and method |
US3254498A (en) * | 1963-08-09 | 1966-06-07 | Linde Eismasch Ag | Method of and apparatus for the transportation and storage of liquefiable gases |
US3269137A (en) * | 1964-12-18 | 1966-08-30 | Cryo Vac Inc | Dense gas helium refrigerator |
US3313117A (en) * | 1964-12-18 | 1967-04-11 | Cryo Vac Inc | Dense gas helium refrigerator |
US3349572A (en) * | 1966-05-10 | 1967-10-31 | Minikay A G | Insulation of containers for the storage of liquids which boil at atmospheric or slightly superatmospheric pressure |
US3359745A (en) * | 1966-04-19 | 1967-12-26 | Mcmullen John J | System for protecting non-cryogenic material from low temperatures and controlling liquefied gas boil-off rate |
US3364639A (en) * | 1965-12-28 | 1968-01-23 | Fred J. Davenport | Insulation panel |
US3374639A (en) * | 1966-10-25 | 1968-03-26 | Mcmullen John J | Leak detection and pressure relief system for insulated liquefied gas storage tanks |
US3374638A (en) * | 1966-04-19 | 1968-03-26 | Mcmullen John J | System for cooling, purging and warming liquefied gas storage tanks and for controlling the boil-off rate of cargo therein |
US3406526A (en) * | 1966-08-10 | 1968-10-22 | Chicago Bridge & Iron Co | Double walled cryogenic vessel |
US4269323A (en) * | 1978-02-03 | 1981-05-26 | Nippon Sanso Kabushiki Kaisha | Heat insulated tank |
US4561292A (en) * | 1984-01-19 | 1985-12-31 | Owens-Corning Fiberglas Corporation | Double-wall underground container for storing liquids and leak detecting means therefor |
US4676093A (en) * | 1985-05-28 | 1987-06-30 | Owens-Corning Fiberglas Corporation | Double-wall underground tank |
US5956957A (en) * | 1998-04-13 | 1999-09-28 | Siemens Westinghouse Power Corporation | Cryostat apparatus |
US20130008185A1 (en) * | 2011-07-07 | 2013-01-10 | Newman Michael D | Cryogen cylinder |
NO20220733A1 (en) * | 2022-06-28 | 2023-12-29 | Lattice Int As | Insulation system for tanks feasible for storage of liquid hydrogen |
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US1088052A (en) * | 1911-05-16 | 1914-02-24 | Emmanuel Felix Aumont | Apparatus for the manufacture of oxygen. |
DE668602C (en) * | 1932-07-03 | 1938-12-07 | Hans Niederreither Dipl Ing | Method for operating internal combustion engines used to drive aircraft |
US2356778A (en) * | 1940-01-22 | 1944-08-29 | Willard L Morrison | Evaporator unit construction |
US2509612A (en) * | 1946-02-20 | 1950-05-30 | Nash Kelvinator Corp | Refrigerating apparatus |
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Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3064451A (en) * | 1960-01-14 | 1962-11-20 | Union Carbide Corp | Cooling head for small chambers |
US3177672A (en) * | 1960-03-31 | 1965-04-13 | Martin Marietta Corp | Space simulating apparatus and method |
US3134237A (en) * | 1960-12-21 | 1964-05-26 | Union Carbide Corp | Container for low-boiling liquefied gases |
US3122004A (en) * | 1961-03-27 | 1964-02-25 | Union Carbide Corp | Apparatus for cryogenic refrigeration |
US3069042A (en) * | 1961-07-06 | 1962-12-18 | Herrick L Johnston Inc | Method and apparatus for storing liquefied gases |
US3159005A (en) * | 1962-06-06 | 1964-12-01 | Phillips Petroleum Co | Insulation system for low temperature service |
US3254498A (en) * | 1963-08-09 | 1966-06-07 | Linde Eismasch Ag | Method of and apparatus for the transportation and storage of liquefiable gases |
US3269137A (en) * | 1964-12-18 | 1966-08-30 | Cryo Vac Inc | Dense gas helium refrigerator |
US3313117A (en) * | 1964-12-18 | 1967-04-11 | Cryo Vac Inc | Dense gas helium refrigerator |
US3364639A (en) * | 1965-12-28 | 1968-01-23 | Fred J. Davenport | Insulation panel |
US3359745A (en) * | 1966-04-19 | 1967-12-26 | Mcmullen John J | System for protecting non-cryogenic material from low temperatures and controlling liquefied gas boil-off rate |
US3374638A (en) * | 1966-04-19 | 1968-03-26 | Mcmullen John J | System for cooling, purging and warming liquefied gas storage tanks and for controlling the boil-off rate of cargo therein |
US3349572A (en) * | 1966-05-10 | 1967-10-31 | Minikay A G | Insulation of containers for the storage of liquids which boil at atmospheric or slightly superatmospheric pressure |
US3406526A (en) * | 1966-08-10 | 1968-10-22 | Chicago Bridge & Iron Co | Double walled cryogenic vessel |
US3374639A (en) * | 1966-10-25 | 1968-03-26 | Mcmullen John J | Leak detection and pressure relief system for insulated liquefied gas storage tanks |
US4269323A (en) * | 1978-02-03 | 1981-05-26 | Nippon Sanso Kabushiki Kaisha | Heat insulated tank |
US4561292A (en) * | 1984-01-19 | 1985-12-31 | Owens-Corning Fiberglas Corporation | Double-wall underground container for storing liquids and leak detecting means therefor |
US4676093A (en) * | 1985-05-28 | 1987-06-30 | Owens-Corning Fiberglas Corporation | Double-wall underground tank |
US5956957A (en) * | 1998-04-13 | 1999-09-28 | Siemens Westinghouse Power Corporation | Cryostat apparatus |
US20130008185A1 (en) * | 2011-07-07 | 2013-01-10 | Newman Michael D | Cryogen cylinder |
NO20220733A1 (en) * | 2022-06-28 | 2023-12-29 | Lattice Int As | Insulation system for tanks feasible for storage of liquid hydrogen |
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