US3406526A - Double walled cryogenic vessel - Google Patents

Double walled cryogenic vessel Download PDF

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Publication number
US3406526A
US3406526A US571565A US57156566A US3406526A US 3406526 A US3406526 A US 3406526A US 571565 A US571565 A US 571565A US 57156566 A US57156566 A US 57156566A US 3406526 A US3406526 A US 3406526A
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United States
Prior art keywords
pressure
sphere
annulus
ullage
space
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US571565A
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English (en)
Inventor
Dudley T Lusk
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Chicago Bridge and Iron Co
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Chicago Bridge and Iron Co
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Filing date
Publication date
Priority to NL132688D priority Critical patent/NL132688C/xx
Application filed by Chicago Bridge and Iron Co filed Critical Chicago Bridge and Iron Co
Priority to US571565A priority patent/US3406526A/en
Priority to GB04623/67A priority patent/GB1180094A/en
Priority to DE19671551573 priority patent/DE1551573A1/de
Priority to NL6705800A priority patent/NL6705800A/xx
Priority to FR116594A priority patent/FR1533092A/fr
Priority to BE702402D priority patent/BE702402A/xx
Application granted granted Critical
Publication of US3406526A publication Critical patent/US3406526A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C3/00—Vessels not under pressure
    • F17C3/02—Vessels not under pressure with provision for thermal insulation
    • F17C3/022—Land-based bulk storage containers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • 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
    • 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
    • F17C2201/0128—Shape spherical or elliptical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/01—Reinforcing or suspension means
    • F17C2203/014—Suspension means
    • F17C2203/015—Bars
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/03—Thermal insulations
    • F17C2203/0304—Thermal insulations by solid means
    • F17C2203/0337—Granular
    • F17C2203/0341—Perlite
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602—Wall structures; Special features thereof
    • F17C2203/0612—Wall structures
    • F17C2203/0626—Multiple walls
    • F17C2203/0629—Two walls
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0636—Metals
    • F17C2203/0639—Steels
    • F17C2203/0643—Stainless steels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01—Mounting arrangements
    • F17C2205/0153—Details of mounting arrangements
    • F17C2205/018—Supporting feet
    • 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
    • F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0341—Filters
    • F17C2205/0344—Sinter type
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146—Two-phase
    • F17C2223/0153—Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • 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
    • 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
    • F17C2227/01—Propulsion of the fluid
    • F17C2227/0107—Propulsion of the fluid by pressurising the ullage

Definitions

  • ABSTRACT OF THE DISCLOSURE A double walled tank for the storage of cryogens where the pressure in the ullage space in the inner tank is counteracted by a pressure maintained in the space between the inner tank and the outer tank so that the inner tank can be designed to withstand the forces created by the weight of the stored liquid only without considering the force created by the ullage pressure and designing the outer tank to withstand the forces created by the weight of the inner tank and the pressure in the annulus.
  • This invention relates to vessels for the storage of cryogens such as liquid nitrogen and liquid oxygen.
  • cryogens are commonly stored in high pressure, double walled spherical tanks.
  • such tanks employ an inner spherical vessel of stainless steel, or other material of comparable expense, which will retain the notch toughness, ductility, tensile strength and other properties necessary for the storage of liquefied gases at cryogenic temperatures.
  • the inner vessel is suspended inside an outer spherical shell or vessel thereby creating an annulus between the two vessels.
  • Some such tanks require a superimposed ullage pressure to facilitate the removal of stored material when desired. Consequently, common practice has been to design the inner vessel to have walls of sufiicient thickness to withstand the combined forces of the weight of the stored liquid and the superimposed ullage gas pressure.
  • the inner vessel is necessarily made of either a stainless steel type 304 costing approximately $O.50/lb., an aluminum alloy costing approximately $0.50/lb. or 9% nickel steel at approximately $0.35/lb.
  • the outer tank is usually a mild carbon steel costing approximately $0.07/lb.
  • the inner sphere In the storage of liquid nitrogen with a ullage gas pressure of 325 p.s.i. in a vessel having a 32 diameter inner sphere and using conventional design methods, the inner sphere would have to be approximately 1.75" thick and the outer sphere approximately .25" thick.
  • the ullage space of the inner sphere is allowed to communicate with the annulus between the inner and outer spheres so that as the ullage pressure acting on the inner surface of the inner sphere increases, it will be met by an equal and opposite force acting on the outer surface of the inner sphere.
  • the inner sphere is designed to support the weight of the liquid to be stored.
  • a conduit near the top of the inner sphere connects the ullage space of the inner sphere with the annulus between the inner and outer spheres.
  • conduit means be provided that will not only distribute the vapor from the ullage space evenly throughout the annulus, but will prevent any of the insulation from being carried back into the inner sphere when the cycle is reversed, e.g., when the tank is being emptied. Since it is preferred that the outer sphere not be subjected to temperatures below 20 F., it is also an object of the present invention to provide a heat exchanger, if required due to operating conditions, in the line between the inner sphere and the annulus to warm the vapor to ambient temperature before entry into the annulus.
  • FIGURE 1 is a cross-sectional elevation of a cryogenic storage vessel made in accordance with the present invention.
  • FIGURE 2 is a cross-sectional view of a heat exchanger of the type to be used with the present invention.
  • FIGURE 1 a vessel 10 designed for the storage of liquefied, normally gaseous materials L.
  • the vessel 10 is comprised of an outer sphere 11 supported by columns 12.
  • Inner sphere 13 is shown inside outer sphere 11.
  • Annulus 16 is filled with insulation 22 (only partially shown) which insulation may be of the granular type.
  • Inner sphere 13 is fixed in positionv by means of support rods 14.
  • Above liquid L stored in inner sphere 13 is ullage space U containing the vaporized stored material or other gas under pressure. The pressure in ullage space U is determined by the requirements necessary for eflicient storage and removal of liquid L.
  • the force created by the pressure of the gas in ullage space U is shown as P and the weight or pressure of the liquid is shown as P Emanating from ullage space U is line 17 through which gas from ullage space U ultimately passes to annulus 16.
  • Line 17 extends through annulus 16 and the outer sphere 11 into the ambient atmosphere.
  • Line 17 is encased in an expansion joint 23 located in the wall of outer sphere 11 to allow for the expansion and contraction of line 17.
  • the gas passing through line 18 is warmed through heat exchanger 19 before it passes through filter 21 and into annulus 16.
  • the pressure P is therefore equal on either side of the walls of the inner sphere and consequently the thickness of inner sphere 1.3 is determined with sole regard to P
  • the thickness of outer sphere 12 is designed to withstand pressure P and the weight of inner sphere 13.
  • conduit 18 Connected to the end of line 17 terminating in annulus 16 is conduit 18.
  • Conduit 18 circumscribes the inner sphere 13 and has a sufficient number of orifices to facilitate the distribution of vapor throughout the annulus so that the pressure acting on the outer surface of the 3 inner sphere will be substantially uniform throughout.
  • the orifices in conduit 18 are small enough to prohibit the entrance of insulation 22 into the conduit 18.
  • liquid nitrogen be stored in a tank having a 32' diameter inner sphere at a ullage pressure of 325 psi.
  • the inner sphere is stainless steel having a thickness of A" throughout except for the support course which would be slightly thicker. Approximately 34,000 pounds of stainless steel is required.
  • the outer sphere is A516 Grade 70 type carbon steel of a uniform thickness of 2", there being approximately 400,000 pounds of the material.
  • the annulus is 3 wide and is filled with perlite type insulating material.
  • the conduit through which the vapor is distributed into the annulus consists of a spiral wire encased in a tubular fabric skin which in turn is wrapped with approximately 1" of fiberglass which acts as a filter to prevent the passage of perlite while allowing the vapor to pass to and from the annulus.
  • a similar type conduit is now marketed and is commonly referred to as a spiratube filter. A sufficient amount of said conduit is used to distribute the vapor evenly throughout the annulus.
  • a sintered bronze filter may be installed in the line to prevent contamination of the stored material.
  • the line 27 from ullage space U passes through annulus 28 and outer sphere 29 to heat exchanger 31.
  • Line 32 from the heat exchanger 31 encloses line 27 and extends into the annulus where it joins conduit 33.
  • Line 27 and line 32 pass through expansion joints in outer sphere 29 so that the expansion and contraction of lines 27 and 32 will not damage the outer sphere and create a leak therein.
  • said inner sphere having wall means of a thickness sufficient to support forces less than the resulting force of the weight of the liquid and said ullage pressure;
  • an outer sphere enclosing said inner sphere and defining an annulus therebetween, said outer sphere having wall means of sufficient thickness to support the weight of the inner sphere and a pressure in said annulus exceeding ambient pressure;
  • an inner sphere containing the liquid and a ullage space said inner sphere having wall means of a thickness sufiicient to support forces limited to those created by the weight of the liquid;
  • an outer sphere enclosing said inner sphere, said outer sphere having Wall means of a thickness sufiicient to support the weight of the inner sphere and said superimposed ullage pressure, said inner sphere and said outer sphere defining an annulus therebetwee'n;
  • the vessel described in claim 2 including means 4 for withdrawing and warming vapor from said ullage space and delivering the same to said annulus.
  • an inner sphere containing the liquid and a ullage space said inner sphere having wall means of a thickness sufiicient to support forces limited to those created by the weight of the liquid;
  • an outer sphere enclosing said inner sphere, said outer sphere having wall means of a thickness sufiioient to support the weight of the inner sphere and said superimposed ullage pressure, said inner sphere and said outer sphere defining an annulus therebetween,
  • annulus substantially filled with a granular insulating material
  • conduit extending from said line throughout said annulus, said conduit of sufficient porosity to transmit vapor from said ullage space into said annulus while restricting the entry of said granular insulating material into said inner sphere.
  • a method for storing liquid cryogens having a superimposed ullage pressure thereon comprising:
  • an inner sphere for containing said liquid and a ullage space, said inner sphere having walls of a thickness sufiicient to support forces less than the resulting forces of the weight of the liquid and the ullage pressure;
  • a method for storing liquid cryogens having a superimposed ullage pressure thereon comprising:
  • an inner sphere to contain said liquid and a ullage space said inner sphere having walls of a thickness sufiicient to support forces limited to those created by the weight of said liquid; providing an outer sphere enclosing said inner sphere,
  • said outer sphere having walls of a thickness sufiioient to support the weight of the inner sphere and said superimposed ullage pressure the inner sphere and the outer sphere defining an annulus therebetween; and providing means for maintaining the pressure in said annulus at substantially the same pressure as the ullage pressure.

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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)
US571565A 1966-08-10 1966-08-10 Double walled cryogenic vessel Expired - Lifetime US3406526A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
NL132688D NL132688C (de) 1966-08-10
US571565A US3406526A (en) 1966-08-10 1966-08-10 Double walled cryogenic vessel
GB04623/67A GB1180094A (en) 1966-08-10 1967-03-30 Improvements in or relating to Double Walled Insulated Containers.
DE19671551573 DE1551573A1 (de) 1966-08-10 1967-04-08 Doppelwandiger Kugelbehaelter fuer verfluessigte Gase
NL6705800A NL6705800A (de) 1966-08-10 1967-04-25
FR116594A FR1533092A (fr) 1966-08-10 1967-08-02 Perfectionnement aux réservoirs de stockage de cryogènes
BE702402D BE702402A (de) 1966-08-10 1967-08-07

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US571565A US3406526A (en) 1966-08-10 1966-08-10 Double walled cryogenic vessel

Publications (1)

Publication Number Publication Date
US3406526A true US3406526A (en) 1968-10-22

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US571565A Expired - Lifetime US3406526A (en) 1966-08-10 1966-08-10 Double walled cryogenic vessel

Country Status (5)

Country Link
US (1) US3406526A (de)
BE (1) BE702402A (de)
DE (1) DE1551573A1 (de)
GB (1) GB1180094A (de)
NL (2) NL6705800A (de)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3488972A (en) * 1967-09-06 1970-01-13 Preload Co Inc Cryogenic storage structure
US5412952A (en) * 1992-05-25 1995-05-09 Kabushiki Kaisha Toshiba Pulse tube refrigerator
US20080067178A1 (en) * 2006-09-15 2008-03-20 Polyearn Development Corporation Portable tank and tank container for liquefied gas transportation
US20080307798A1 (en) * 2007-06-12 2008-12-18 Yang Luo Cryogenic liquid tank and method
US20140216066A1 (en) * 2013-02-04 2014-08-07 Hebeler Corporation Dynamic Ullage Control System for a Cryogenic Storage Tank
US8955444B2 (en) 2012-07-31 2015-02-17 Electro-Motive Diesel, Inc. Energy recovery system for a mobile machine
US8960100B2 (en) 2012-07-31 2015-02-24 Electro-Motive Diesel, Inc. Energy recovery system for a mobile machine
US9073556B2 (en) 2012-07-31 2015-07-07 Electro-Motive Diesel, Inc. Fuel distribution system for multi-locomotive consist
US20170009940A1 (en) * 2014-02-11 2017-01-12 L'air Liquide, Societe Anonyme Pour I'etude Et I'exploitation Des Procedes Georges Claude Insulated chamber and method for flushing such a chamber
US9718478B2 (en) 2012-07-31 2017-08-01 Electro-Motive Diesel, Inc. Fuel system for consist having daughter locomotive
CN108361543A (zh) * 2018-04-16 2018-08-03 张家港富瑞深冷科技有限公司 一种新型低温容器结构及其制造方法
US20190316734A1 (en) * 2018-04-11 2019-10-17 United States Department of Transportation, FRA Low Pressure Fuel Management and Delivery System for a Liquefied Natural Gas Rail Locomotive Tender

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2092831B1 (de) * 1970-06-23 1974-11-08 Creusot Loire

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1363313A (en) * 1920-12-28 Method oe handling- and utilizing combustible gases
US1876047A (en) * 1928-07-18 1932-09-06 Commercial Solvents Corp Apparatus and process for preserving liquid carbon dioxide
US2707377A (en) * 1952-02-02 1955-05-03 Union Stock Yards & Transit Co Storage and shipping container for cold liquefied gas
US2927437A (en) * 1954-09-20 1960-03-08 Garrett Corp Tank for storing low temperature liquids in ambient surroundings
US2986891A (en) * 1958-02-10 1961-06-06 Little Inc A Low-temperature vessels
US3159005A (en) * 1962-06-06 1964-12-01 Phillips Petroleum Co Insulation system for low temperature service

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1363313A (en) * 1920-12-28 Method oe handling- and utilizing combustible gases
US1876047A (en) * 1928-07-18 1932-09-06 Commercial Solvents Corp Apparatus and process for preserving liquid carbon dioxide
US2707377A (en) * 1952-02-02 1955-05-03 Union Stock Yards & Transit Co Storage and shipping container for cold liquefied gas
US2927437A (en) * 1954-09-20 1960-03-08 Garrett Corp Tank for storing low temperature liquids in ambient surroundings
US2986891A (en) * 1958-02-10 1961-06-06 Little Inc A Low-temperature vessels
US3159005A (en) * 1962-06-06 1964-12-01 Phillips Petroleum Co Insulation system for low temperature service

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3488972A (en) * 1967-09-06 1970-01-13 Preload Co Inc Cryogenic storage structure
US5412952A (en) * 1992-05-25 1995-05-09 Kabushiki Kaisha Toshiba Pulse tube refrigerator
US20080067178A1 (en) * 2006-09-15 2008-03-20 Polyearn Development Corporation Portable tank and tank container for liquefied gas transportation
US20080307798A1 (en) * 2007-06-12 2008-12-18 Yang Luo Cryogenic liquid tank and method
US8960100B2 (en) 2012-07-31 2015-02-24 Electro-Motive Diesel, Inc. Energy recovery system for a mobile machine
US8955444B2 (en) 2012-07-31 2015-02-17 Electro-Motive Diesel, Inc. Energy recovery system for a mobile machine
US9073556B2 (en) 2012-07-31 2015-07-07 Electro-Motive Diesel, Inc. Fuel distribution system for multi-locomotive consist
US9718478B2 (en) 2012-07-31 2017-08-01 Electro-Motive Diesel, Inc. Fuel system for consist having daughter locomotive
US20140216066A1 (en) * 2013-02-04 2014-08-07 Hebeler Corporation Dynamic Ullage Control System for a Cryogenic Storage Tank
US20170009940A1 (en) * 2014-02-11 2017-01-12 L'air Liquide, Societe Anonyme Pour I'etude Et I'exploitation Des Procedes Georges Claude Insulated chamber and method for flushing such a chamber
US10920935B2 (en) * 2014-02-11 2021-02-16 L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Insulated chamber and method for flushing such a chamber
US20190316734A1 (en) * 2018-04-11 2019-10-17 United States Department of Transportation, FRA Low Pressure Fuel Management and Delivery System for a Liquefied Natural Gas Rail Locomotive Tender
CN108361543A (zh) * 2018-04-16 2018-08-03 张家港富瑞深冷科技有限公司 一种新型低温容器结构及其制造方法
CN108361543B (zh) * 2018-04-16 2023-11-17 张家港富瑞深冷科技有限公司 一种新型低温容器结构及其制造方法

Also Published As

Publication number Publication date
DE1551573A1 (de) 1970-03-19
BE702402A (de) 1968-01-15
NL6705800A (de) 1968-02-12
NL132688C (de)
GB1180094A (en) 1970-02-04

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