EP0014250A1 - Dispositif de suspension pour récipient basse-température - Google Patents

Dispositif de suspension pour récipient basse-température Download PDF

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Publication number
EP0014250A1
EP0014250A1 EP79105087A EP79105087A EP0014250A1 EP 0014250 A1 EP0014250 A1 EP 0014250A1 EP 79105087 A EP79105087 A EP 79105087A EP 79105087 A EP79105087 A EP 79105087A EP 0014250 A1 EP0014250 A1 EP 0014250A1
Authority
EP
European Patent Office
Prior art keywords
tank
suspension device
individual elements
low
fastening
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP79105087A
Other languages
German (de)
English (en)
Other versions
EP0014250B1 (fr
Inventor
Wolfgang Buchs
Martin Müller
Werner Malburg
Albert Seidel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of EP0014250A1 publication Critical patent/EP0014250A1/fr
Application granted granted Critical
Publication of EP0014250B1 publication Critical patent/EP0014250B1/fr
Expired 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
    • F17C13/00—Details of vessels or of the filling or discharging of vessels
    • F17C13/08—Mounting arrangements for vessels
    • F17C13/086—Mounting arrangements for vessels for Dewar vessels or cryostats
    • 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
    • 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
    • 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
    • F17C2203/016—Cords
    • 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
    • F17C2203/0308—Radiation shield
    • F17C2203/0316—Radiation shield cooled by vaporised gas from the interior
    • 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
    • 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
    • F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01—Mounting arrangements
    • F17C2205/0153—Details of mounting arrangements
    • F17C2205/0196—Details of mounting arrangements with shock absorbing means
    • 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
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/22—Assembling processes
    • F17C2209/228—Assembling processes by screws, bolts or rivets
    • 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
    • F17C2221/016—Noble gases (Ar, Kr, Xe)
    • F17C2221/017—Helium
    • 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

Definitions

  • the invention relates to a suspension device for a low-temperature tank according to the preamble of claim 1.
  • the fastening tapes are also exposed to enormous thermal requirements: on the one hand, they must have a high thermal conductivity so that they do not have a thermal bridge between the outer container when the low-temperature tank is cold and the tank, and on the other hand, despite the strong temperature fluctuations of the inner tank - between room temperature in the unfilled state and extremely low temperature level when the tank is full - remain as uniform as possible under all operating conditions and guarantee an exact fixation of the low-temperature tank, and these thermal loads are the known suspension devices with sufficient strength and rigidity of the one-piece fastening tapes not grown.
  • the one-piece fastening tapes are made of carbon fibers
  • the thermally induced changes in the tension of the fastening tapes between the room and the low-temperature condition of the inner tank can be kept low, but due to the comparatively high thermal conductivity of this fiber material, there is an excessive heat inflow lengthwise in the low-temperature condition of the inner tank the fastening straps.
  • a gradation of the thermal material properties in the longitudinal direction of the tape is effected in such a way that the thermal expansion coefficient of the individual elements gradually decreases and at the tank-side band end, that is, at the narrow point of the fastening band, where the greatest temperature difference between the filled, cold and unfilled; when the inner tank is warmed to room temperature, is the smallest, while the individual elements closer to the outer container, in which the temperature fluctuations relevant for thermal expansion become increasingly smaller, are made from fiber material with a comparatively higher thermal expansion coefficient, but also a lower coefficient of thermal conductivity.
  • each fastening tape according to claim 2 preferably consists of at least three individual elements made of different fiber materials with a gradually decreasing coefficient of thermal expansion from the outer container to the low-temperature tank and accordingly increasing coefficient of thermal conductivity, and according to claim 3 are in a particularly useful manner as pas material for the tank element next to carbon fibers and glass fibers for the single element attacking the outer container.
  • the insulation pieces result in a strong local throttling of the heat flow, while by appropriate selection of the fiber material for the individual elements one of the occurring temperature fluctuations between the room temperature and the low temperature level of the inner tank is possible constant tape tension is achieved, so that it is possible despite the high strength and rigidity of the fastening tapes, the thermal conductivity in relation to that between the minimum and maximum operating temperature of the interior ntanks to significantly increase the tension changes in the fastening straps caused by thermal expansion.
  • At least one individual element of each fastening tape is cooled in the heat flow direction in front of the insulation piece, the cooling in front of the insulation piece having the additional advantage of simple heat dissipation with a relatively high level Has cooling temperature level.
  • successive individual elements in a structurally simple, thermally and mechanically particularly advantageous embodiment of the invention are preferably connected to each other in a tensile manner by a multi-part end connection according to claim 6, the second connection part of the end connection according to claim 7 expediently having a thermal barrier layer to further increase the insulation effect is occupied.
  • the preferred inclined arrangement of the fastening tapes ensures, on the one hand, that the recesses kept free for the fastening tapes are arranged offset in successive radiation shields, so that no radiation holes aligned in the main radiation direction between the outer container and the inner tank arise, and at the same time this geometric arrangement allows of the fastening tapes at least partially compensate for their thermal changes in length by a corresponding thermal displacement of the strap fastening points on the outer container and on the inner tank.
  • the latter according to claim 11 are advantageously each designed as a double loop having a unidirectional fiber direction, and the incident on the inner container heat radiation to further reduce, according to claim 12 elschlaufe p in the space between the longitudinal legs each Dop preferably a filler acting as a radiation shield is used.
  • the suspension device 2 via which the low-temperature tank 4 is suspended coaxially in the outer container 6, contains an upper and a lower row 8, 10 of six fastening straps 12 in each case.
  • Each of these fastening straps runs under pretension between an anchoring point on the outer container side Form of a securing bolt 14 on the one hand (FIG. 2) and a tank-side anchoring point in the form of a tension screw 16 on the other hand.
  • the fastening tapes 12 are inclined so that the distance between the upper and lower row of belts 8, 10 increases from the outer container 6 to the low-temperature tank 4.
  • the thermal length contraction of the low-temperature tank 4 leads to a reduction in the axial distance between the upper and lower anchoring points 16 on the tank side, as a result of which the thermal radial contraction of the tank 4 and the thermal length change of the fastening straps 12 are partially compensated.
  • the tank-side anchorage points 16 are arranged in pairs in such a way that they are mutual The circumferential distance is smaller than the circumferential distance to the immediately adjacent, tank-side anchorage points (FIG. 1b), while the anchorage points 14 on the outer container side are uniformly distributed in the circumferential direction, so that the fastening tapes 12 of each row 8 or 10 from the outer container 6 converge in pairs to the inner tank 4.
  • This geometric arrangement of the fastening straps 12 also reduces the angle of inclination of the fastening straps 12 with respect to a radial beam in the event of a thermal contraction of the inner tank 4, so that the thermal changes in length are at least partially compensated for.
  • an extremely stable fixation of the inner tank 4 in the outer container 6 is achieved in the axial, radial and rotational directions.
  • the structure of the fastening tapes 12 is of crucial importance. These are each composed of several, approximately four individual elements 18.1, 18.2, 18.3 and 18.4 connected in series from fiber composite material, each individual element 18 consisting of one or more parallel, endlessly wound double loops 20 with a unidirectional fiber direction in the longitudinal direction of the loop, as shown in FIG. 4 by the Double arrows is indicated.
  • a filler 24 acts as a radiation shield, for example made of aluminum-coated polyphthalate films.
  • the individual elements 18 are made of different types of fibers with a coefficient of thermal expansion decreasing from the outer container 6 to the inner tank 4 and consequently increasing the coefficient of thermal conductivity due to the material.
  • the space between the outer container 6 and the z. B. with helium fillable inner tank 4 is evacuated for better heat insulation in the usual way and equipped with the inner tank 4 shell-shaped enclosing radiation shields 26, 28, which also consist of aluminum-coated polyphthalate films and are cooled with the help of cooling coils 30, about which the approximately during the experiment resulting helium vapor is passed from the inner tank 4 to the outside.
  • the radiation shields 26, 28 are suspended near the pipe coils 30 via heat-conducting intermediate plates 32 at the end connections 34 which connect the ends of adjacent individual elements with one another in a tensile manner, the construction of which is explained using the right end connection 34, which is effective between the individual elements 18.2 and 18.3, according to FIG. 3 .
  • the end connection 34 consists of a plurality of socket-shaped connecting parts 36.1 and 36.2, which are clamped together by a central screw bolt 38 at a material which is a good heat conductor and to which the intermediate plates 32 are also fastened.
  • the connecting part 36.1 to which the inner ("colder"), loop-shaped end of the individual element 18.2 closer to the outer container 6 is connected, also consists of a thermally highly conductive material, for. B. copper beryllium, so that a large part of the heat flowing in via the individual element is dissipated via the connecting part 36.1, the screw bolt 38, the intermediate plates 32 and the cooling coils 30.
  • the connecting parts 36.2 form thermal insulation pieces and are made of a thermally poorly conductive material, e.g. B. titanium, and in addition to their adjacent to the connecting part 36.1 or the remote tank element 18.2 surfaces with a thermal barrier layer 40 z. B. again in the form of aluminum-coated polyphthalate film.
  • adjacent individual elements 18 are connected to one another in a tensile manner with the interposition of thermal insulation pieces 36.2, 40, and the individual element remote from the tank is at its inner end facing the tank 4 in the heat flow direction in front of the insulation pieces cooled via thermally highly conductive intermediate pieces 36.1, 38, 32.
  • the left end connection 34 in the sense of FIG. 3 contains a central connecting part 36.2 made of titanium for the loop area of the individual element 18.2 on the outer container side and two outer connecting parts 36.1 made of copper-beryllium for the loop areas of the band element 18.1 anchored to the outer container 6 near the tank.
  • the openings 42 in the radiation shields 26, 28 which are kept free in the region of the end connections 34 are offset in the main radiation direction, so that the formation of radiation holes in the space between the outer container 6 and the low-temperature tank 4 is prevented.
  • the thermal conductivity and expansion behavior of the fastening tapes 12 can be varied and adapted to the respectively required mechanical and thermal stresses.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
EP79105087A 1979-02-01 1979-12-11 Dispositif de suspension pour récipient basse-température Expired EP0014250B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE2903787 1979-02-01
DE2903787A DE2903787C2 (de) 1979-02-01 1979-02-01 Aufhängevorrichtung für einen in einem Außenbehälter thermisch isoliert angeordneten Tieftemperaturtank

Publications (2)

Publication Number Publication Date
EP0014250A1 true EP0014250A1 (fr) 1980-08-20
EP0014250B1 EP0014250B1 (fr) 1982-09-29

Family

ID=6061900

Family Applications (1)

Application Number Title Priority Date Filing Date
EP79105087A Expired EP0014250B1 (fr) 1979-02-01 1979-12-11 Dispositif de suspension pour récipient basse-température

Country Status (3)

Country Link
US (1) US4300354A (fr)
EP (1) EP0014250B1 (fr)
DE (1) DE2903787C2 (fr)

Cited By (9)

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Publication number Priority date Publication date Assignee Title
EP0135185A2 (fr) * 1983-09-19 1985-03-27 General Electric Company Cryostat pour aimant par RMN
EP0260036A2 (fr) * 1986-09-09 1988-03-16 Oxford Medical Limited Assemblage de cryostat
DE4121762C1 (fr) * 1991-07-01 1992-09-10 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
WO2008036991A1 (fr) * 2006-09-27 2008-04-03 Matthias Rebernik récipient de COLLECTe de fluides et/ou d'appareils qui doivent être conservés à basse température
EP1705419A3 (fr) * 2005-03-24 2008-07-16 Bruker BioSpin AG Dispositif de montage pour cryostat avec centrage à compensation de température
CN101595340B (zh) * 2006-09-27 2011-12-07 马赛厄斯·雷伯尼克 用于容纳低温储存介质和/或器具的容器
WO2014161898A2 (fr) 2013-04-05 2014-10-09 Cryoshelter Gmbh Dispositif d'accrochage pour un réservoir intérieur, disposé par isolation thermique dans un réservoir extérieur, et ensemble de réservoirs
EP4310528A1 (fr) * 2022-07-21 2024-01-24 Bruker Switzerland AG Réduction passive de dérive de shim induite par la température dans des systèmes magnétiques rmn
EP4310529A1 (fr) * 2022-07-21 2024-01-24 Bruker Switzerland AG Réduction active de dérive de shim indexée en température dans des systèmes magnétiques rmn

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US4481778A (en) * 1983-03-21 1984-11-13 Ball Corporation Thermally disconnecting passive parallel orbital supports
EP0122498B1 (fr) * 1983-04-15 1988-06-08 Hitachi, Ltd. Cryostat
US4848103A (en) * 1987-04-02 1989-07-18 General Electric Company Radial cryostat suspension system
DE3724569A1 (de) * 1987-07-24 1989-02-02 Spectrospin Ag Kryostat
US4842139A (en) * 1988-04-05 1989-06-27 Krieg Adrian H Cylinder containment vessel
DE3915578C1 (fr) * 1989-05-12 1990-11-15 Spectrospin Ag, Faellanden, Zuerich, Ch
DE4323510C2 (de) * 1993-07-14 1995-05-11 Eurocopter Deutschland Zug- und/oder Druckstrebe
US7147124B2 (en) * 2002-03-27 2006-12-12 Exxon Mobil Upstream Research Company Containers and methods for containing pressurized fluids using reinforced fibers and methods for making such containers
DE102004060591B4 (de) * 2004-12-16 2016-04-07 Magna Steyr Fahrzeugtechnik Ag & Co. Kg Tank für kryogene Medien sowie Verfahren und Vorrichtung zu dessen Zusammenbau
DE102005014479A1 (de) * 2005-03-30 2006-10-05 Magna Steyr Fahrzeugtechnik Ag & Co. Kg Behälter für tiefkalte Flüssigkeiten
US7757882B2 (en) 2005-09-26 2010-07-20 Gm Global Technology Operations, Inc. Suspended liquid hydrogen storage tank
US7717287B2 (en) * 2005-09-26 2010-05-18 Gm Global Technology Operations, Inc. Liquid hydrogen storage tank with radial stiffening
AT504888B1 (de) * 2007-08-28 2008-09-15 Rebernik Matthias Dr Behälter zur aufnahme von bei tiefen temperaturen, vorzugsweise unter 150 grad kelvin, aufzubewahrenden kryogenen medien und/oder geräten
DE102008054090B4 (de) * 2008-10-31 2010-07-29 Mt Aerospace Ag Behälter zum Aufnehmen und Speichern von Flüssigkeiten und viskosen Stoffen, insbesondere von kryogenen Fluiden, und dessen Verwendung
US8511632B2 (en) * 2011-01-06 2013-08-20 General Electric Company Suspension system and method for suspending an inner vessel inside an outer vessel of a cryostat
CN102778660B (zh) * 2011-05-12 2015-11-04 上海联影医疗科技有限公司 用于磁共振成像系统超导磁体的悬挂部件
GB2517746B (en) * 2013-08-30 2016-09-14 Ubh Int Ltd Storage tank suspension member and storage tank for storage of cryogenic liquid
CN107204226B (zh) * 2016-03-18 2020-06-02 上海联影医疗科技有限公司 一种超导磁体的低温容器
JP7026639B2 (ja) * 2016-05-04 2022-02-28 リンデ ゲゼルシャフト ミット ベシュレンクテル ハフツング 輸送容器
EP3610211B1 (fr) * 2017-04-12 2024-05-29 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Procédé de construction d'un module de boîte froide et appareil obtenu
FR3124243B1 (fr) * 2021-06-22 2024-04-05 Cryolor Dispositif de stockage et de transport de gaz liquéfié.
FR3130927B1 (fr) * 2021-12-22 2023-11-24 Faurecia Systemes Dechappement Unité de stockage de fluide cryogénique
US20230235857A1 (en) * 2022-01-26 2023-07-27 Chart Inc. Dual-Purpose Cryogenic Liquid Tank System and Method
CN114877245A (zh) * 2022-05-10 2022-08-09 华陆工程科技有限责任公司 一种双层球罐用内外罐连接装置
FR3135509B1 (fr) * 2022-05-10 2024-08-16 Air Liquide réservoir de stockage de gaz liquéfié à double parois
EP4349716A1 (fr) * 2022-10-05 2024-04-10 Airbus S.A.S. Aéronef avec réservoir d'hydrogène suspendu

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US2396459A (en) * 1939-12-07 1946-03-12 Linde Air Prod Co Insulated container for liquefied gases and the like
US2926810A (en) * 1956-10-30 1960-03-01 Herrick L Johnston Inc Suspension system for container for storing liquefied gas
GB1326231A (en) * 1969-09-02 1973-08-08 Air Prod & Chem Double-walled containers
FR2410211A1 (fr) * 1977-11-25 1979-06-22 Anvar Cryostat a cryogene liquide muni d'un dispositif monobloc de suspension ultra-rigide compatible avec l'ancrage thermique des ecrans de radiation

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FR1190831A (fr) * 1958-01-28 1959-10-15 Air Liquide Câbles résilients aux très basses températures
US3078755A (en) * 1961-01-27 1963-02-26 Samson Cordage Works Braided cordage
US3069042A (en) * 1961-07-06 1962-12-18 Herrick L Johnston Inc Method and apparatus for storing liquefied gases
DE1551602A1 (de) * 1967-04-26 1970-03-19 Messer Griesheim Gmbh Doppelwandiger Behaelter fuer tiefkalte,verfluessigte Gase
US3698200A (en) * 1970-12-16 1972-10-17 Air Prod & Chem Cryogenic storage dewar
US3817047A (en) * 1971-12-07 1974-06-18 Lox Equip Thermal junction for a cryogenic vessel
JPS5249775Y2 (fr) * 1973-08-30 1977-11-11

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2396459A (en) * 1939-12-07 1946-03-12 Linde Air Prod Co Insulated container for liquefied gases and the like
US2926810A (en) * 1956-10-30 1960-03-01 Herrick L Johnston Inc Suspension system for container for storing liquefied gas
GB1326231A (en) * 1969-09-02 1973-08-08 Air Prod & Chem Double-walled containers
FR2410211A1 (fr) * 1977-11-25 1979-06-22 Anvar Cryostat a cryogene liquide muni d'un dispositif monobloc de suspension ultra-rigide compatible avec l'ancrage thermique des ecrans de radiation

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0135185A3 (en) * 1983-09-19 1986-06-04 General Electric Company Cryostat for nmr magnet
EP0135185A2 (fr) * 1983-09-19 1985-03-27 General Electric Company Cryostat pour aimant par RMN
EP0260036A2 (fr) * 1986-09-09 1988-03-16 Oxford Medical Limited Assemblage de cryostat
EP0260036A3 (en) * 1986-09-09 1988-08-17 Oxford Magnet Technology Limited Cyrostat assembly
DE4121762C1 (fr) * 1991-07-01 1992-09-10 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
EP0531632A1 (fr) * 1991-07-01 1993-03-17 Daimler-Benz Aerospace Aktiengesellschaft Dispositif de suspension pour un réservoir
EP1705419A3 (fr) * 2005-03-24 2008-07-16 Bruker BioSpin AG Dispositif de montage pour cryostat avec centrage à compensation de température
EA014658B1 (ru) * 2006-09-27 2010-12-30 Маттиас Реберник Резервуар для хранения веществ и/или приборов при низких температурах
WO2008036991A1 (fr) * 2006-09-27 2008-04-03 Matthias Rebernik récipient de COLLECTe de fluides et/ou d'appareils qui doivent être conservés à basse température
CN101595340B (zh) * 2006-09-27 2011-12-07 马赛厄斯·雷伯尼克 用于容纳低温储存介质和/或器具的容器
US8272530B2 (en) 2006-09-27 2012-09-25 Matthias Rebernik Container for receiving media and/or devices to be stored at low temperatures
WO2014161898A2 (fr) 2013-04-05 2014-10-09 Cryoshelter Gmbh Dispositif d'accrochage pour un réservoir intérieur, disposé par isolation thermique dans un réservoir extérieur, et ensemble de réservoirs
WO2014161899A1 (fr) 2013-04-05 2014-10-09 Cryoshelter Gmbh Dispositif d'accrochage pour un réservoir intérieur, disposé par isolation thermique dans un réservoir extérieur, et ensemble de réservoirs
US10088105B2 (en) 2013-04-05 2018-10-02 Cryoshelter Gmbh Suspension system for an inner container mounted for thermal insulation in an outer container and container arrangement
US10295120B2 (en) 2013-04-05 2019-05-21 Cryoshelter Gmbh Suspension system for an inner container mounted for thermal insulation in an outer container and container arrangement
US10774990B2 (en) 2013-04-05 2020-09-15 Cryoshelter Gmbh Suspension system for an inner container mounted for thermal insulation in an outer container and container arrangement
US11655941B2 (en) 2013-04-05 2023-05-23 Cryoshelter Gmbh Suspension system for an inner container mounted for thermal insulation in an outer container and container arrangement
EP4310528A1 (fr) * 2022-07-21 2024-01-24 Bruker Switzerland AG Réduction passive de dérive de shim induite par la température dans des systèmes magnétiques rmn
EP4310529A1 (fr) * 2022-07-21 2024-01-24 Bruker Switzerland AG Réduction active de dérive de shim indexée en température dans des systèmes magnétiques rmn

Also Published As

Publication number Publication date
DE2903787A1 (de) 1980-08-14
EP0014250B1 (fr) 1982-09-29
US4300354A (en) 1981-11-17
DE2903787C2 (de) 1983-11-03

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