US20070051116A1 - Device for loss-free cryogen cooling of a cryostat configuration - Google Patents
Device for loss-free cryogen cooling of a cryostat configuration Download PDFInfo
- Publication number
- US20070051116A1 US20070051116A1 US11/171,429 US17142905A US2007051116A1 US 20070051116 A1 US20070051116 A1 US 20070051116A1 US 17142905 A US17142905 A US 17142905A US 2007051116 A1 US2007051116 A1 US 2007051116A1
- Authority
- US
- United States
- Prior art keywords
- cooling device
- heat
- cryostat
- cold
- tube
- 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.)
- Abandoned
Links
- 238000001816 cooling Methods 0.000 title claims abstract description 89
- 239000007788 liquid Substances 0.000 claims abstract description 55
- 239000000725 suspension Substances 0.000 claims abstract description 37
- 230000005855 radiation Effects 0.000 claims abstract description 22
- 239000007789 gas Substances 0.000 claims abstract description 18
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 38
- 239000001307 helium Substances 0.000 claims description 30
- 229910052734 helium Inorganic materials 0.000 claims description 30
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 30
- 229910052757 nitrogen Inorganic materials 0.000 claims description 19
- 238000005481 NMR spectroscopy Methods 0.000 claims description 17
- 238000009835 boiling Methods 0.000 claims description 4
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 238000002595 magnetic resonance imaging Methods 0.000 claims description 3
- 238000004611 spectroscopical analysis Methods 0.000 claims description 2
- 230000037431 insertion Effects 0.000 claims 1
- 238000003780 insertion Methods 0.000 claims 1
- 238000001704 evaporation Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 230000002349 favourable effect Effects 0.000 description 3
- 230000001771 impaired effect Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000009413 insulation Methods 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 238000010668 complexation reaction Methods 0.000 description 1
- 230000005493 condensed matter Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000009420 retrofitting Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D19/00—Arrangement or mounting of refrigeration units with respect to devices or objects to be refrigerated, e.g. infrared detectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
- F25B9/14—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the cycle used, e.g. Stirling cycle
- F25B9/145—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the cycle used, e.g. Stirling cycle pulse-tube cycle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2309/00—Gas cycle refrigeration machines
- F25B2309/14—Compression machines, plants or systems characterised by the cycle used
- F25B2309/1408—Pulse-tube cycles with pulse tube having U-turn or L-turn type geometrical arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2400/00—General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
- F25B2400/17—Re-condensers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
- F25B9/10—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point with several cooling stages
Definitions
- the invention concerns a cooling device for re-liquefying cryogenic gases, comprising an outer jacket which delimits a vacuum chamber, and a cryocooler cold head installed therein, which has at least two cold stages and is at least partially surrounded by a radiation shield.
- a cooling device for re-liquefying cryogenic gases, comprising an outer jacket which delimits a vacuum chamber, and a cryocooler cold head installed therein, which has at least two cold stages and is at least partially surrounded by a radiation shield.
- EP0905436, EP0905524, WO03036207, WO03036190 U.S. Pat. No. 5,966,944, U.S. Pat. No. 5,563,566, U.S. Pat. No. 5,613,367, U.S. Pat. No. 5,782,095, U.S. Pat. No. 2002/000283, US2003/230089 e.g. describe cooling of a superconducting magnet system with no or little cryogen loss using a cryocool
- the e.g. two-stage cold head of the cryocooler is usually installed in a separate sleeve assembly which is under vacuum (described e.g. in U.S. Pat. No. 5,613,367) or directly in the vacuum chamber of a cryostat (described e.g. in U.S. Pat. No. 5,563,566) such that the first cold stage of the cold head is rigidly connected to a radiation shield and the second cold stage is connected in a heat-conducting manner to the helium container either directly, or via a fixed thermal bridge, wherein the helium container holds the superconducting magnet in liquid helium.
- the cold head can be inserted into a neck tube which connects the outer vacuum sleeve of the cryostat to the helium container and is correspondingly filled with helium gas as described e.g. in US2002/0002830A1.
- the first cold stage of the two-stage cold head is in fixed thermal contact with a radiation shield and the second cold stage is freely suspended in the helium atmosphere to directly liquefy evaporating helium.
- magnetic regenerator materials are usually used in the regenerator of the second stage of the cold head of cryocoolers such as pulse tube coolers or Gifford-McMahon coolers, and the regenerator may be relatively close to the magnetic center of the NMR magnet system. In consequence thereof, the regenerator must generally be shielded to prevent disturbance of the magnetic field at the location of the NMR sample and to prevent the function of the regenerator from being impaired.
- an unstable state occurs when the cryocooler fails, and the temperatures of cryostat components such as e.g. the radiation shield continuously change until a new balanced state is reached. In a magnet system for high-resolution nuclear magnetic resonance (NMR) spectroscopy, this can preclude NMR measurements, since the shim state of the magnet constantly changes or, in the worst case, the magnet runs dry and quenches.
- NMR nuclear magnetic resonance
- One method for preventing some of these disadvantages while still realizing a partially loss-free cryogen system entails use of a device cooled by a cryocooler which can be used for re-liquefying one single evaporated cryogen.
- the magnet In a hitherto common cryostat arrangement for e.g. a superconducting magnet system, the magnet is usually installed into a container filled with liquid helium at 4.2 K.
- the helium container is generally surrounded by a boil-off-gas-cooled radiation shield and a further shield cooled with liquid nitrogen, such that the external heat input onto the helium container is minimized. Due to passive cooling by the evaporating cryogens, liquid helium and nitrogen must be refilled at certain intervals.
- JP11257770 and JP2000283578 propose inserting a heat-transferring device in the form of a heat tube into the existing neck or suspension tubes of a nitrogen container of a cryostat configuration, the heat tube being connected to the cold head of a cryocooler to re-liquefy evaporating nitrogen (see also Advances of Cryogenic Engineering, 45, 41-48).
- the liquefier is thereby directly flanged onto the cold head of the one-stage pulse tube cooler and consists of a thin tube in which the nitrogen vapor rises, is liquefied on a cold surface which is in contact with the cold head, and runs downwards along the tube wall.
- This very thin tube is surrounded by a vacuum sleeve in its upper region and can be directly inserted into a nitrogen neck tube or suspension tube to prevent or reduce evaporation of the nitrogen and nitrogen losses.
- the helium losses are not addressed, since only the nitrogen is re-liquefied.
- the cold head of the cryocooler is in an outer jacket which delimits a vacuum chamber.
- parts of the cold head are usually surrounded by a radiation shield which is in contact with a cold stage (not the coldest stage) to ensure good insulation of the cold head against thermal radiation in the low temperature region.
- cryostat configurations which are used, in particular, for magnet systems in high-resolution nuclear magnetic resonance (NMR) spectroscopy have more than one cryogen.
- an additional radiation shield is e.g. provided which is cooled with liquid nitrogen.
- this object is achieved in that at least two cold stages of the cold head of the cryocooler are each individually connected in a heat-conducting manner to a heat-transferring device which can be inserted into the neck or suspension tubes of a cryostat for keeping at least two different cryogenic liquids.
- a cooling device of this type offers the following advantages: Existing cryostat configurations, and in particular those which contain superconducting magnets can be retrofitted without (or with only minor) adjustments, to permit operation with no or little cryogen loss requiring only little extra hardware even if several cryogens are used.
- the cryostat must not be re-engineered.
- the additional heat input into the cryostat produced by the device is small and can be predicted quite precisely when properly engineered.
- the heat-transferring devices in which the cryogens are liquefied are designed such that they can be introduced in a contact-free manner into the neck or suspension tubes of the cryostat configuration.
- the evaporating gas is liquefied in a thermodynamically effective manner, since the vapor is not overheated and therefore need not be cooled down to the liquefying temperature.
- the cryocooler cold head is placed at such a distance from the magnetic center of a superconducting magnet arrangement in the cryostat that disturbances on the magnet arrangement caused by the magnetic regenerator material are less severe than if the cold head were directly integrated into the cryostat.
- the function of the cryocooler is also less impaired by the magnetic field of the magnet arrangement. If the cryocooler fails or must be switched off for maintenance work, the cryostat configuration still functions, e.g. for cooling a superconducting magnet arrangement. This ensures high operational reliability.
- the user can freely select the mode of operation (conventional or without cryogen loss).
- At least one of the heat-transferring devices has a cavity which is connected to an open line, in particular a conduit.
- the cryogen which evaporates from the liquid tank of the cryostat is guided through the conduit to the cavity at the cold stage, where it is liquefied.
- the condensed matter then flows back through the conduit into the liquid tank of the cryostat.
- This heat-transferring device functions like conventional heat engineering heat pipes.
- At least one of the heat-transferring devices comprises a metallic connection with excellent heat transferring properties, at the end of which the cryogen evaporated from the liquid tank of the cryostat is liquefied and subsequently flows back into the liquid bath of the liquid tank of the cryostat.
- the other end of this connection is flanged to a cold stage of the cold head of the cryocooler.
- a metallic connection with excellent heat conducting properties may e.g. be flanged to the first cold stage of a two-stage cold head, while the second cold stage is connected to a conduit.
- the cryocooler is advantageously a pulse tube cooler, since pulse tube coolers operate with extremely low vibration. Moreover, pulse tube coolers also provide reliable operation and require little maintenance.
- the cooling device may also be operated with a Gifford McMahon cooler.
- a Gifford McMahon cooler One disadvantage of this cryocooler compared to a pulse tube cooler are increased vibrations. This disadvantage can be overcome if soft sealing elements are provided between the cryocooler and the cryostat configuration, as is described below.
- At least one connecting line which is open at both sides, is provided to connect the cold head of the cryocooler to at least one neck or suspension tube of the liquid tank containing the cryogen of lowest-boiling temperature and into which no heat-transferring device is inserted, wherein the line is in thermal contact with at least two cold stages of the cold head and may also contact a regenerator tube above the coldest cold stage, wherein the line terminates in the cavity mounted to the cold head after thermal contact with the coldest cold stage, or is guided along the metallic connection into the liquid tank.
- the gas in the line is cooled at the cold head of the cryocooler and liquefied at the coldest cold stage such that a flow is generated in the line through the neck or suspension tubes to the cooling device due to the resulting suction.
- the gas flow cools the neck or suspension tubes thereby ideally completely compensating for the heat input via the neck or suspension tubes. This circulating flow for the cooling neck or suspension tubes further reduces heat input into the cryostat.
- a valve and/or a pump is provided in the connecting line between the neck or suspension tubes and the cold head to control the gas flow.
- the gas flow can be reduced or the optimum gas flow can be adjusted as required if e.g. the suction effect at the cold head is so large that the gas flow becomes greater than required for optimum cooling of the suspension or neck tubes.
- helium can be liquefied at the coldest cold stage of the cold head at a temperature of 4.2 K or less to provide a plurality of possible applications in the region of low temperature.
- the helium loss and the refilling processes can be reduced or loss-free operation can be obtained if the cooling capacity of the cryocooler is sufficiently large.
- nitrogen can be liquefied at 77 K or less at a cold stage of the cryocooler cold head.
- the nitrogen loss can be reduced or eliminated during operation if the cooling capacity of the cryocooler is sufficiently large.
- a cold stage of the cold head which is not the coldest, is connected in a heat-conducting manner to the radiation shield which, at least partially, surrounds the cold head. In this manner, the radiative heat input onto the colder components of the cold head is substantially reduced.
- the heat-transferring device comes to rest at least partially within the outer jacket of the cooling device, i.e. within the vacuum chamber. This is relevant in particular for that part of the heat-transferring device which is connected to the cold head of the cryocooler. This part of the heat-transferring device is thereby excellently insulated against heat conduction towards the outside.
- the heat-transferring device is surrounded at least partially by a first tube in the region outside of the outer jacket.
- This tube thermally insulates the heat-transferring device. It may but must not have a constant diameter along its entire length. It may be more favorable in view of construction to select the smallest possible diameter for one part of the tube, and a larger diameter for the rest.
- the first tube which surrounds the heat-transferring device is open at one end, and that end is connected to the vacuum chamber of the outer jacket, while the other end is connected to the conduit or the metallic connection of the heat-transferring device in a gas-tight manner. If the vacuum chamber of the cooling device of this embodiment is evacuated, the part of the heat-transferring device surrounded by the first tube is also under vacuum. The heat-transferring device is then excellently insulated in this region against thermal conduction towards the outside.
- the first tube surrounding the heat-transferring device is connected at both ends to the conduit or the metallic connection of the heat-transferring device in a gas-tight manner, and evacuated via a separate connection.
- the interior of the tube can thereby be evacuated and the part of the heat-transferring device, which is surrounded by the tube can be excellently insulated against thermal conduction towards the outside.
- the conduit or the metallic connection of the heat-transferring device can advantageously at least partially surround a further second tube which is connected in a heat-conducting manner to the radiation shield.
- This tube is disposed within the first tube to provide vacuum insulation, as described above. In this manner, the part of the heat-transferring device surrounded by the second tube is excellently insulated against thermal radiation towards the outside.
- the above-described tubes surrounding the heat-transferring device are flexible, at least in sections, and are preferably designed as a bellows.
- the heat-transferring device is designed to be flexible, at least in sections, in particular as a bellows or in the form of wires plaited into strands.
- the heat-transferring device and the surrounding tubes are flexible to considerably facilitate installation thereof into the neck or suspension tubes of a cryostat configuration.
- the heat-transferring device and the surrounding tubes can be connected to and disconnected from each other at at least one location using a gas-tight coupling.
- the coupling is designed such that the functionality of the heat-transferring device and the surrounding tubes is not impaired. This substantially, facilitates mounting of the cooling device to a cryostat configuration.
- the cooling device can be mounted to the cryostat for keeping cryogenic liquids either at the neck, at the suspension tubes, or on the outer jacket of the cryostat configuration.
- the cooling device may be mounted outside of the cryostat e.g. on the room ceiling or on a separate stand. In this case, the cryostat configuration does not have to bear the weight of the cooling device. This can increase the mechanical stability of the cryostat configuration.
- a soft connecting element which does not transmit vibrations is advantageously provided as a seal between the cooling device and the cryostat. This ensures that—in particular for high-resolution NMR methods—none or only little disturbing vibrations of the cooling device are transferred to the cryostat configuration.
- Another possibility is mounting electric heaters to the cold stages of the cold head of the cryocooler.
- the heaters can be adjusted such that the cryocooler exactly compensates for the heat input into the different containers of the cryostat configuration.
- the cooling device serves to cool a superconducting magnet arrangement, in particular, a superconducting magnet arrangement which is part of a nuclear magnetic resonance apparatus, in particular, a magnetic resonance imaging (MRI) or nuclear magnetic resonance spectroscopy (NMR) apparatus.
- MRI magnetic resonance imaging
- NMR nuclear magnetic resonance spectroscopy
- An electric heater can also be introduced into the liquid tank of a cryostat configuration provided with the inventive cooling device via a neck or suspension tube of at least one liquid tank.
- the pressure in the liquid containers can thereby be kept at a constant level above the surrounding pressure. It is, however, also feasible to control the power of the cryocooler via its operating frequency and/or the fill amount of working gas in the cryocooler.
- FIG. 1 shows a cryostat configuration with two liquid tanks for cryogenic liquids
- FIG. 2 a shows an inventive cooling device with heat-transferring devices having a cavity
- FIG. 2 b shows an inventive cooling device with heat-transferring devices comprising a metallic connection with excellent heat-transferring properties
- FIG. 3 shows a cooling device installed in a cryostat according to FIG. 2 a;
- FIG. 4 shows a cooling device according to the present invention which is installed in a cryostat, with a connecting line which connects the cold head of the cryocooler to a suspension tube of a liquid tank;
- FIG. 5 a shows a cooling device in accordance with the present invention, which is mounted on the cryostat;
- FIG. 5 b shows a cooling device in accordance with the present invention which is mounted to the room ceiling
- FIG. 5 c shows a cooling device in accordance with the invention which is mounted to a stand.
- FIG. 1 is a schematic illustration of a cryostat 1 with a magnet arrangement 5 as commonly used for MR applications.
- the cryostat 1 comprises a liquid tank 2 a filled with helium which is connected via suspension tubes 3 a to an outer jacket 4 of the cryostat 1 and contains a magnet arrangement 5 .
- a further liquid tank 2 b is disposed about the liquid tank 2 a, which contains nitrogen and is connected via the suspension tubes 3 b to the outer jacket 4 of the cryostat 1 .
- the liquid tank 2 b with nitrogen is in thermal contact with the suspension tubes 3 a.
- a boil-off-gas-cooled radiation shield 6 is disposed between the two liquid tanks 2 a, 2 b and is also in thermal contact with the suspension tubes 3 a.
- FIG. 2 a shows an embodiment of an inventive cooling device 7 .
- the cooling device comprises an outer jacket 8 which delimits a vacuum chamber 9 , and a cold head 10 of a cryocooler disposed therein which comprises at least two cold stages 11 , 12 and is at least partially surrounded by a radiation shield 13 .
- the cold stages 11 , 12 of the cold head 10 are each connected in a heat-conducting manner to a heat-transferring device 14 a, 14 b.
- the heat-transferring devices 14 a, 14 b each have a cavity 15 a, 15 b, wherein each cavity 15 a, 15 b is connected to a respective conduit 16 a, 16 b.
- FIG. 2 b shows an alternative embodiment of the inventive cooling device 7 , wherein the heat-transferring devices 14 a, 14 b comprise connections 17 a, 17 b with excellent heat conducting properties.
- These connections may be e.g. in the form of cold fingers which are generally designed as metal rods.
- Such a metal rod should have a maximum cross-sectional surface to ensure minimum temperature differences along the rod.
- the conduits 16 a, 16 b can be inserted into the suspension tubes 3 a, 3 b of the liquid tanks 2 a, 2 b of a cryostat 1 .
- FIG. 3 shows an inventive cooling device 7 in the installed state.
- the conduits 16 a, 16 b are located in the cryogen vapor above the liquid surface of the cryogens 18 a, 18 b disposed in the liquid tanks 2 a, 2 b.
- the heat-transferring devices 14 a, 14 b are each connected in a heat-conducting manner to a cold stage 11 , 12 of the cryocooler ( FIGS. 2 a, 2 b and 3 ).
- the cryogens 18 a, 18 b evaporated from the liquid tanks 2 a, 2 b of the cryostat 1 are guided through the conduits 16 a, 16 b into the cavity 15 a, 15 b on the respective cold stage 12 , 11 where the cryogens 18 a, 18 b are condensed and are thereby liquefied and subsequently flow back through the conduits 16 a, 16 b into the liquid tanks 2 a, 2 b of the cryostat 1 .
- the helium vapor can also be liquefied at the end of a metallic connection 17 a, 17 b which is in contact with the cold head 10 and has excellent heat conducting properties ( FIG. 2 b ).
- the cryogen 18 b with higher boiling temperature from the liquid tank 2 b is thereby liquefied on the first cold stage 11 of the cold head 10 while the cryogen 18 a with a lower boiling temperature is liquefied at the second, colder cold stage 12 of the cold head 10 .
- the invention also comprises cooling devices with a multi-stage cold head 10 such that, in principle, any number of cryogens, corresponding to the number of the cold stages of the cold head 10 , can be liquefied.
- the heat-transferring devices 14 a, 14 b are surrounded by a first tube 19 a, 19 b to insulate them from thermal input, the first tube being connected to the vacuum chamber 9 of the outer jacket 8 of the cooling device 7 and can be evacuated together with the vacuum chamber 9 ( FIGS. 2 a, 2 b ).
- a second tube 20 is disposed within the first tube 19 a which is connected in a heat-conducting manner to the radiation shield 13 .
- the diameter of the first tube 19 b varies along its length in FIGS. 2 a, 2 b and FIG. 3 .
- a bellows provides a flexible connection between the first tube 19 b and the outer jacket 8 of the cooling device 7 .
- a bellows may also be interposed between the first tube 19 a and the outer jacket 8 and in a section of the second tube 20 .
- the metallic connection 17 a, 17 b shown in FIG. 2 b can be made flexible through flexible connecting elements 21 a, 21 b (such as e.g. wire plaited into strands).
- additional heaters can be mounted to the cold stages 11 , 12 of the cold head 10 of the cryocooler.
- the pressure in the liquid tanks 2 a, 2 b for the cryogens 18 a, 18 b can be kept constant using heaters 22 a, 22 b which are disposed in the liquid tanks 2 a, 2 b and which are e.g. inserted via remaining free neck or suspension tubes 3 c, 3 d.
- FIG. 4 shows an advantageous variant of the inventive cooling device, wherein a free neck or suspension tube 3 c of the cryostat 1 is connected, via a line 23 which is open on both sides, after thermal contact with the cold stages 11 , 12 of the cold head 10 , to the cavity 15 a and therefore also to the liquid tank 2 a.
- a connection of this type can also be realized with several free neck or suspension tubes 3 c.
- the lines from the suspension tubes 3 c are initially combined into one line 23 .
- This line 23 is then guided through the outer jacket 8 of the cooling device 7 which contains the cold head 10 and is thermally contacted using the heat exchanger 24 b, 24 a with at least two cold stages 11 , 12 of the cold head 10 and possibly also with the regenerator tube 25 above the coldest cold stage 12 e.g. by wrapping it around the regenerator tube 25 .
- the line 23 terminates in the cavity 15 a mounted to the cold head 10 or is guided along the metallic connection 17 a into the liquid tank 2 a for the cryogen 18 a (helium).
- the gas in the line 23 is cooled by the cold head 10 and liquefied at the coldest cold stage 12 , thereby generating a flow in the line 23 through the suspension tube 3 c towards the cooling device 7 due to the resulting suction.
- the heated gas flow cools the suspension tube 3 c, whereby in the ideal case, the heat input is completely compensated or at least reduced via the suspension tube 3 c.
- the overall cooling capacity of the cryocooler slightly decreases due to the additional load.
- the gain due to the reduced heat input is larger than the loss in cooling power. In particular for systems with massive neck or suspension tubes 3 c, a cryocooler with lower power can thereby be used.
- the heat-transferring devices 14 a, 14 b may be made from two or more parts, which permits separation thereof using gas-tight couplings (not shown). This facilitates installation and-disassembly.
- the line 23 has a valve 26 and a pump 27 to control the gas flow through the line 23 and thereby adjust an optimum gas flow.
- the line 23 may be provided with such a device (valve 26 or pump 27 ) or such devices can be completely omitted.
- heaters 22 a, 22 b are provided in the liquid tank 2 a, 2 b. For reasons of clarity, the connections are omitted in FIG. 4 .
- FIGS. 5 a through 5 c show various possibilities for fixing the cooling device 7 .
- the vacuum container which contains the cold head 10 of the cryocooler can either be directly mounted on the outer jacket 4 of the cryostat 1 as shown in FIG. 5 a or externally e.g. on the room ceiling 28 ( FIG. 5 b ) or on a separate-stand 29 ( FIG. 5 c ).
- a seal 30 must be used for mounting onto the cryostat 1 .
- further sealing elements 31 a, 31 b are used between the vacuum chamber 9 and the outer jacket 4 of the cryostat 1 with the consequence that no or only minimum vibrations of the cryocooler are transferred to the cryostat 1 .
- the cooling device 7 is used for cooling a cryostat configuration which contains a superconducting magnet arrangement 5 , in particular, if the superconducting magnet arrangement 5 is part of a nuclear magnetic resonance apparatus, in particular magnetic resonance imaging (MRI) or magnetic resonance spectroscopy (Nuclear Magnetic Resonance, NMR).
- MRI magnetic resonance imaging
- NMR Magnetic resonance spectroscopy
- a cooling device which permits retrofitting to existing cryostat configurations, and in particular such configurations which contain superconducting magnets without (or with only minor) adjustments to permit, in a straightforward manner, operation with no or little cryogen loss even if several cryogens are used.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Containers, Films, And Cooling For Superconductive Devices (AREA)
Abstract
A cooling device (7) for re-liquefying cryogenic gases, comprising an outer jacket (8) which delimits a vacuum chamber (9), and a cryocooler cold head (10) installed therein, which has at least two cold stages (11, 12) and is at least partially surrounded by a radiation shield (13) is characterized in that at least two cold stages (11, 12) of the cold head (10) are separately individually connected in a heat-conducting manner to a heat-transferring device (14 a, 14 b) which can be inserted into the neck or suspension tubes (3 a, 3 b) of a cryostat (1) for keeping at least two different cryogenic liquids (18 a, 18 b). The cooling device can be easily retrofitted into existing cryostat configurations, in particular, those containing superconducting magnets and without (or with minimum) adjustment to permit operation with no or little cryogen loss, even if several cryogens are used.
Description
- This application claims Paris Convention priority of DE 10 2004 037 173.3 filed Jul. 30, 2004 the complete disclosure of which is hereby incorporated by reference.
- The invention concerns a cooling device for re-liquefying cryogenic gases, comprising an outer jacket which delimits a vacuum chamber, and a cryocooler cold head installed therein, which has at least two cold stages and is at least partially surrounded by a radiation shield. EP0905436, EP0905524, WO03036207, WO03036190, U.S. Pat. No. 5,966,944, U.S. Pat. No. 5,563,566, U.S. Pat. No. 5,613,367, U.S. Pat. No. 5,782,095, U.S. Pat. No. 2002/000283, US2003/230089 e.g. describe cooling of a superconducting magnet system with no or little cryogen loss using a cryocooler.
- The e.g. two-stage cold head of the cryocooler is usually installed in a separate sleeve assembly which is under vacuum (described e.g. in U.S. Pat. No. 5,613,367) or directly in the vacuum chamber of a cryostat (described e.g. in U.S. Pat. No. 5,563,566) such that the first cold stage of the cold head is rigidly connected to a radiation shield and the second cold stage is connected in a heat-conducting manner to the helium container either directly, or via a fixed thermal bridge, wherein the helium container holds the superconducting magnet in liquid helium. Through recondensation of the helium, which evaporates due to external heat input, on the cold contact surface in the helium container, the overall heat input into the helium container can be compensated for, thereby providing operation with no or little cryogen loss of the system. In an alternative manner, the cold head can be inserted into a neck tube which connects the outer vacuum sleeve of the cryostat to the helium container and is correspondingly filled with helium gas as described e.g. in US2002/0002830A1. The first cold stage of the two-stage cold head is in fixed thermal contact with a radiation shield and the second cold stage is freely suspended in the helium atmosphere to directly liquefy evaporating helium.
- These variants have certain disadvantages. The design and construction of the cryostat becomes more demanding and complex and installation of the additional sleeve which receives the cryocooler cold head generates additional heat input into the cold head. If an additional neck tube is used for the cold head, further heat is transferred into the helium container or cooler cold head due to thermal conduction in the helium gas column and in the tube wall and through possible convection flow in the helium gas. Moreover, fixed, rigid or even flexible thermal elements connected between the cold head and the cryostat can transfer cold head vibrations to the cryostat. Furthermore, in a temperature range below 10K, magnetic regenerator materials are usually used in the regenerator of the second stage of the cold head of cryocoolers such as pulse tube coolers or Gifford-McMahon coolers, and the regenerator may be relatively close to the magnetic center of the NMR magnet system. In consequence thereof, the regenerator must generally be shielded to prevent disturbance of the magnetic field at the location of the NMR sample and to prevent the function of the regenerator from being impaired. Finally, an unstable state occurs when the cryocooler fails, and the temperatures of cryostat components such as e.g. the radiation shield continuously change until a new balanced state is reached. In a magnet system for high-resolution nuclear magnetic resonance (NMR) spectroscopy, this can preclude NMR measurements, since the shim state of the magnet constantly changes or, in the worst case, the magnet runs dry and quenches.
- One method for preventing some of these disadvantages while still realizing a partially loss-free cryogen system entails use of a device cooled by a cryocooler which can be used for re-liquefying one single evaporated cryogen. In a hitherto common cryostat arrangement for e.g. a superconducting magnet system, the magnet is usually installed into a container filled with liquid helium at 4.2 K. The helium container is generally surrounded by a boil-off-gas-cooled radiation shield and a further shield cooled with liquid nitrogen, such that the external heat input onto the helium container is minimized. Due to passive cooling by the evaporating cryogens, liquid helium and nitrogen must be refilled at certain intervals.
- JP11257770 and JP2000283578 propose inserting a heat-transferring device in the form of a heat tube into the existing neck or suspension tubes of a nitrogen container of a cryostat configuration, the heat tube being connected to the cold head of a cryocooler to re-liquefy evaporating nitrogen (see also Advances of Cryogenic Engineering, 45, 41-48). The liquefier is thereby directly flanged onto the cold head of the one-stage pulse tube cooler and consists of a thin tube in which the nitrogen vapor rises, is liquefied on a cold surface which is in contact with the cold head, and runs downwards along the tube wall. This very thin tube is surrounded by a vacuum sleeve in its upper region and can be directly inserted into a nitrogen neck tube or suspension tube to prevent or reduce evaporation of the nitrogen and nitrogen losses. The helium losses are not addressed, since only the nitrogen is re-liquefied.
- In a similar manner, re-liquefaction of helium only has also been carried out in a helium storage container using a two-stage cryocooler cold head.
- In both cases (nitrogen or helium liquefier), the cold head of the cryocooler is in an outer jacket which delimits a vacuum chamber. When multi-stage cryocoolers are used, parts of the cold head are usually surrounded by a radiation shield which is in contact with a cold stage (not the coldest stage) to ensure good insulation of the cold head against thermal radiation in the low temperature region.
- As already mentioned above, different conventional cryostat configurations which are used, in particular, for magnet systems in high-resolution nuclear magnetic resonance (NMR) spectroscopy have more than one cryogen. In addition to a container filled with liquid helium and holding the magnet, an additional radiation shield is e.g. provided which is cooled with liquid nitrogen. In this manner, one would have to use a separate helium liquefier and a separate nitrogen liquefier to reduce both the helium and nitrogen losses or to obtain loss-free operation. This would considerably increase the number of devices, the investment, and the operating costs.
- It is therefore the object of the present invention to provide a cooling device which, in an advantageous and straightforward manner, can be retrofitted to an existing cryostat configuration containing at least two cryogenic liquids, in particular, a cryostat configuration which comprises a superconducting magnet arrangement, to eliminate or strongly reduce loss of some or all existing cryogenic liquids relative to conventional devices.
- Departing from prior art and in accordance with the invention, this object is achieved in that at least two cold stages of the cold head of the cryocooler are each individually connected in a heat-conducting manner to a heat-transferring device which can be inserted into the neck or suspension tubes of a cryostat for keeping at least two different cryogenic liquids.
- A cooling device of this type offers the following advantages: Existing cryostat configurations, and in particular those which contain superconducting magnets can be retrofitted without (or with only minor) adjustments, to permit operation with no or little cryogen loss requiring only little extra hardware even if several cryogens are used. The cryostat must not be re-engineered. The additional heat input into the cryostat produced by the device is small and can be predicted quite precisely when properly engineered. The heat-transferring devices in which the cryogens are liquefied are designed such that they can be introduced in a contact-free manner into the neck or suspension tubes of the cryostat configuration. The evaporating gas is liquefied in a thermodynamically effective manner, since the vapor is not overheated and therefore need not be cooled down to the liquefying temperature. The cryocooler cold head is placed at such a distance from the magnetic center of a superconducting magnet arrangement in the cryostat that disturbances on the magnet arrangement caused by the magnetic regenerator material are less severe than if the cold head were directly integrated into the cryostat. Conversely, the function of the cryocooler is also less impaired by the magnetic field of the magnet arrangement. If the cryocooler fails or must be switched off for maintenance work, the cryostat configuration still functions, e.g. for cooling a superconducting magnet arrangement. This ensures high operational reliability. Moreover, the user can freely select the mode of operation (conventional or without cryogen loss).
- In a particularly preferred embodiment of the inventive cooling device, at least one of the heat-transferring devices has a cavity which is connected to an open line, in particular a conduit. The cryogen which evaporates from the liquid tank of the cryostat is guided through the conduit to the cavity at the cold stage, where it is liquefied. The condensed matter then flows back through the conduit into the liquid tank of the cryostat. This heat-transferring device functions like conventional heat engineering heat pipes.
- In a further preferred embodiment of the invention, at least one of the heat-transferring devices comprises a metallic connection with excellent heat transferring properties, at the end of which the cryogen evaporated from the liquid tank of the cryostat is liquefied and subsequently flows back into the liquid bath of the liquid tank of the cryostat. The other end of this connection is flanged to a cold stage of the cold head of the cryocooler. Various combinations of the heat-transferring devices are possible. A metallic connection with excellent heat conducting properties may e.g. be flanged to the first cold stage of a two-stage cold head, while the second cold stage is connected to a conduit.
- In particular for high-resolution NMR methods, the cryocooler is advantageously a pulse tube cooler, since pulse tube coolers operate with extremely low vibration. Moreover, pulse tube coolers also provide reliable operation and require little maintenance.
- The cooling device may also be operated with a Gifford McMahon cooler. One disadvantage of this cryocooler compared to a pulse tube cooler are increased vibrations. This disadvantage can be overcome if soft sealing elements are provided between the cryocooler and the cryostat configuration, as is described below.
- In a particularly advantageous manner, at least one connecting line, which is open at both sides, is provided to connect the cold head of the cryocooler to at least one neck or suspension tube of the liquid tank containing the cryogen of lowest-boiling temperature and into which no heat-transferring device is inserted, wherein the line is in thermal contact with at least two cold stages of the cold head and may also contact a regenerator tube above the coldest cold stage, wherein the line terminates in the cavity mounted to the cold head after thermal contact with the coldest cold stage, or is guided along the metallic connection into the liquid tank. The gas in the line is cooled at the cold head of the cryocooler and liquefied at the coldest cold stage such that a flow is generated in the line through the neck or suspension tubes to the cooling device due to the resulting suction. The gas flow cools the neck or suspension tubes thereby ideally completely compensating for the heat input via the neck or suspension tubes. This circulating flow for the cooling neck or suspension tubes further reduces heat input into the cryostat.
- In a further development of this embodiment, a valve and/or a pump is provided in the connecting line between the neck or suspension tubes and the cold head to control the gas flow. The gas flow can be reduced or the optimum gas flow can be adjusted as required if e.g. the suction effect at the cold head is so large that the gas flow becomes greater than required for optimum cooling of the suspension or neck tubes.
- In an advantageous manner, helium can be liquefied at the coldest cold stage of the cold head at a temperature of 4.2 K or less to provide a plurality of possible applications in the region of low temperature. The helium loss and the refilling processes can be reduced or loss-free operation can be obtained if the cooling capacity of the cryocooler is sufficiently large.
- According to a further advantageous aspect, nitrogen can be liquefied at 77 K or less at a cold stage of the cryocooler cold head. With the use of the heat-transferring devices in a cryostat configuration having a container with liquid nitrogen, the nitrogen loss can be reduced or eliminated during operation if the cooling capacity of the cryocooler is sufficiently large.
- In an advantageous embodiment, a cold stage of the cold head, which is not the coldest, is connected in a heat-conducting manner to the radiation shield which, at least partially, surrounds the cold head. In this manner, the radiative heat input onto the colder components of the cold head is substantially reduced.
- It is moreover advantageous if the heat-transferring device comes to rest at least partially within the outer jacket of the cooling device, i.e. within the vacuum chamber. This is relevant in particular for that part of the heat-transferring device which is connected to the cold head of the cryocooler. This part of the heat-transferring device is thereby excellently insulated against heat conduction towards the outside.
- It is also very advantageous if the heat-transferring device is surrounded at least partially by a first tube in the region outside of the outer jacket. This tube thermally insulates the heat-transferring device. It may but must not have a constant diameter along its entire length. It may be more favorable in view of construction to select the smallest possible diameter for one part of the tube, and a larger diameter for the rest.
- In a preferred embodiment, the first tube which surrounds the heat-transferring device is open at one end, and that end is connected to the vacuum chamber of the outer jacket, while the other end is connected to the conduit or the metallic connection of the heat-transferring device in a gas-tight manner. If the vacuum chamber of the cooling device of this embodiment is evacuated, the part of the heat-transferring device surrounded by the first tube is also under vacuum. The heat-transferring device is then excellently insulated in this region against thermal conduction towards the outside.
- In another advantageous embodiment, the first tube surrounding the heat-transferring device is connected at both ends to the conduit or the metallic connection of the heat-transferring device in a gas-tight manner, and evacuated via a separate connection. The interior of the tube can thereby be evacuated and the part of the heat-transferring device, which is surrounded by the tube can be excellently insulated against thermal conduction towards the outside.
- The conduit or the metallic connection of the heat-transferring device can advantageously at least partially surround a further second tube which is connected in a heat-conducting manner to the radiation shield. This tube is disposed within the first tube to provide vacuum insulation, as described above. In this manner, the part of the heat-transferring device surrounded by the second tube is excellently insulated against thermal radiation towards the outside.
- With particular preference, the above-described tubes surrounding the heat-transferring device are flexible, at least in sections, and are preferably designed as a bellows.
- In a further favorable manner, the heat-transferring device is designed to be flexible, at least in sections, in particular as a bellows or in the form of wires plaited into strands. In this embodiment of the inventive cooling device, the heat-transferring device and the surrounding tubes are flexible to considerably facilitate installation thereof into the neck or suspension tubes of a cryostat configuration.
- In this connection, it is also advantageous if the heat-transferring device and the surrounding tubes can be connected to and disconnected from each other at at least one location using a gas-tight coupling. The coupling is designed such that the functionality of the heat-transferring device and the surrounding tubes is not impaired. This substantially, facilitates mounting of the cooling device to a cryostat configuration.
- In a further embodiment of the invention, the cooling device can be mounted to the cryostat for keeping cryogenic liquids either at the neck, at the suspension tubes, or on the outer jacket of the cryostat configuration.
- In an alternative and preferred manner, the cooling device may be mounted outside of the cryostat e.g. on the room ceiling or on a separate stand. In this case, the cryostat configuration does not have to bear the weight of the cooling device. This can increase the mechanical stability of the cryostat configuration.
- In this connection, a soft connecting element which does not transmit vibrations is advantageously provided as a seal between the cooling device and the cryostat. This ensures that—in particular for high-resolution NMR methods—none or only little disturbing vibrations of the cooling device are transferred to the cryostat configuration.
- Another possibility is mounting electric heaters to the cold stages of the cold head of the cryocooler. In case of surplus cooling capacity of the cryocooler, the heaters can be adjusted such that the cryocooler exactly compensates for the heat input into the different containers of the cryostat configuration.
- The advantages of the inventive cooling device are particularly well utilized if they are part of a cryostat configuration.
- In a particularly advantageous manner, the cooling device serves to cool a superconducting magnet arrangement, in particular, a superconducting magnet arrangement which is part of a nuclear magnetic resonance apparatus, in particular, a magnetic resonance imaging (MRI) or nuclear magnetic resonance spectroscopy (NMR) apparatus.
- An electric heater can also be introduced into the liquid tank of a cryostat configuration provided with the inventive cooling device via a neck or suspension tube of at least one liquid tank. In case of surplus cooling capacity of the cryocooler cold head which is integrated in the cooling device, the pressure in the liquid containers can thereby be kept at a constant level above the surrounding pressure. It is, however, also feasible to control the power of the cryocooler via its operating frequency and/or the fill amount of working gas in the cryocooler.
- Further advantages of the invention can be extracted from the description and the drawings. The features mentioned above and below may be used individually or collectively in arbitrary combination. The embodiments shown and described are not to be understood as exhaustive enumeration but have exemplary character for illustrating the invention.
-
FIG. 1 shows a cryostat configuration with two liquid tanks for cryogenic liquids; -
FIG. 2 a shows an inventive cooling device with heat-transferring devices having a cavity; -
FIG. 2 b shows an inventive cooling device with heat-transferring devices comprising a metallic connection with excellent heat-transferring properties; -
FIG. 3 shows a cooling device installed in a cryostat according toFIG. 2 a; -
FIG. 4 shows a cooling device according to the present invention which is installed in a cryostat, with a connecting line which connects the cold head of the cryocooler to a suspension tube of a liquid tank; -
FIG. 5 a shows a cooling device in accordance with the present invention, which is mounted on the cryostat; -
FIG. 5 b shows a cooling device in accordance with the present invention which is mounted to the room ceiling; and -
FIG. 5 c shows a cooling device in accordance with the invention which is mounted to a stand. -
FIG. 1 is a schematic illustration of acryostat 1 with amagnet arrangement 5 as commonly used for MR applications. Thecryostat 1 comprises aliquid tank 2 a filled with helium which is connected viasuspension tubes 3 a to anouter jacket 4 of thecryostat 1 and contains amagnet arrangement 5. Afurther liquid tank 2 b is disposed about theliquid tank 2 a, which contains nitrogen and is connected via thesuspension tubes 3 b to theouter jacket 4 of thecryostat 1. Theliquid tank 2 b with nitrogen is in thermal contact with thesuspension tubes 3 a. A boil-off-gas-cooledradiation shield 6 is disposed between the two 2 a, 2 b and is also in thermal contact with theliquid tanks suspension tubes 3 a. -
FIG. 2 a shows an embodiment of aninventive cooling device 7. The cooling device comprises anouter jacket 8 which delimits avacuum chamber 9, and acold head 10 of a cryocooler disposed therein which comprises at least two 11, 12 and is at least partially surrounded by acold stages radiation shield 13. The cold stages 11, 12 of thecold head 10 are each connected in a heat-conducting manner to a heat-transferring 14 a, 14 b. The heat-transferringdevice 14 a, 14 b each have adevices 15 a, 15 b, wherein eachcavity 15 a, 15 b is connected to acavity 16 a, 16 b.respective conduit -
FIG. 2 b shows an alternative embodiment of theinventive cooling device 7, wherein the heat-transferring 14 a, 14 b comprisedevices 17 a, 17 b with excellent heat conducting properties. These connections may be e.g. in the form of cold fingers which are generally designed as metal rods. Such a metal rod should have a maximum cross-sectional surface to ensure minimum temperature differences along the rod.connections - The
16 a, 16 b can be inserted into theconduits 3 a, 3 b of thesuspension tubes 2 a, 2 b of aliquid tanks cryostat 1.FIG. 3 shows aninventive cooling device 7 in the installed state. The 16 a, 16 b are located in the cryogen vapor above the liquid surface of theconduits cryogens 18 a, 18 b disposed in the 2 a, 2 b. The heat-transferringliquid tanks 14 a, 14 b are each connected in a heat-conducting manner to adevices 11, 12 of the cryocooler (cold stage FIGS. 2 a, 2 b and 3). Thecryogens 18 a, 18 b evaporated from the 2 a, 2 b of theliquid tanks cryostat 1 are guided through the 16 a, 16 b into theconduits 15 a, 15 b on the respectivecavity 12, 11 where thecold stage cryogens 18 a, 18 b are condensed and are thereby liquefied and subsequently flow back through the 16 a, 16 b into theconduits 2 a, 2 b of theliquid tanks cryostat 1. The helium vapor can also be liquefied at the end of a 17 a, 17 b which is in contact with themetallic connection cold head 10 and has excellent heat conducting properties (FIG. 2 b). - The cryogen 18 b with higher boiling temperature from the
liquid tank 2 b is thereby liquefied on the firstcold stage 11 of thecold head 10 while thecryogen 18 a with a lower boiling temperature is liquefied at the second, coldercold stage 12 of thecold head 10. The invention also comprises cooling devices with a multi-stagecold head 10 such that, in principle, any number of cryogens, corresponding to the number of the cold stages of thecold head 10, can be liquefied. - The heat-transferring
14 a, 14 b are surrounded by adevices 19 a, 19 b to insulate them from thermal input, the first tube being connected to thefirst tube vacuum chamber 9 of theouter jacket 8 of thecooling device 7 and can be evacuated together with the vacuum chamber 9 (FIGS. 2 a, 2 b). To improve thermal insulation from the external heat radiation, asecond tube 20 is disposed within thefirst tube 19 a which is connected in a heat-conducting manner to theradiation shield 13. The diameter of thefirst tube 19 b varies along its length inFIGS. 2 a, 2 b andFIG. 3 . It may be necessary to reduce the diameter of the tube at the closed end such that it can be inserted into thesuspension tube 3 b of theliquid tank 2 b in a contact-free manner. A bellows provides a flexible connection between thefirst tube 19 b and theouter jacket 8 of thecooling device 7. A bellows may also be interposed between thefirst tube 19 a and theouter jacket 8 and in a section of thesecond tube 20. The 17 a, 17 b shown inmetallic connection FIG. 2 b can be made flexible through flexible connecting 21 a, 21 b (such as e.g. wire plaited into strands). In case of surplus cooling capacity of the cryocooler, additional heaters (not shown) can be mounted to theelements 11, 12 of thecold stages cold head 10 of the cryocooler. Alternatively or additionally, in case of surplus cooling capacity of the cryocooler, the pressure in the 2 a, 2 b for theliquid tanks cryogens 18 a, 18 b can be kept constant using 22 a, 22 b which are disposed in theheaters 2 a, 2 b and which are e.g. inserted via remaining free neck orliquid tanks 3 c, 3 d.suspension tubes -
FIG. 4 shows an advantageous variant of the inventive cooling device, wherein a free neck orsuspension tube 3 c of thecryostat 1 is connected, via aline 23 which is open on both sides, after thermal contact with the 11, 12 of thecold stages cold head 10, to thecavity 15 a and therefore also to theliquid tank 2 a. A connection of this type can also be realized with several free neck orsuspension tubes 3 c. The lines from thesuspension tubes 3 c are initially combined into oneline 23. Thisline 23 is then guided through theouter jacket 8 of thecooling device 7 which contains thecold head 10 and is thermally contacted using the 24 b, 24 a with at least twoheat exchanger 11, 12 of thecold stages cold head 10 and possibly also with theregenerator tube 25 above the coldestcold stage 12 e.g. by wrapping it around theregenerator tube 25. After contact with the coldestcold stage 12, theline 23 terminates in thecavity 15 a mounted to thecold head 10 or is guided along themetallic connection 17 a into theliquid tank 2 a for thecryogen 18 a (helium). The gas in theline 23 is cooled by thecold head 10 and liquefied at the coldestcold stage 12, thereby generating a flow in theline 23 through thesuspension tube 3 c towards the coolingdevice 7 due to the resulting suction. The heated gas flow cools thesuspension tube 3 c, whereby in the ideal case, the heat input is completely compensated or at least reduced via thesuspension tube 3 c. The overall cooling capacity of the cryocooler slightly decreases due to the additional load. The gain due to the reduced heat input is larger than the loss in cooling power. In particular for systems with massive neck orsuspension tubes 3 c, a cryocooler with lower power can thereby be used. The heat-transferring 14 a, 14 b (heat tubes or cold fingers) may be made from two or more parts, which permits separation thereof using gas-tight couplings (not shown). This facilitates installation and-disassembly. Thedevices line 23 has avalve 26 and apump 27 to control the gas flow through theline 23 and thereby adjust an optimum gas flow. Theline 23 may be provided with such a device (valve 26 or pump 27) or such devices can be completely omitted. In the embodiment ofFIG. 4 and also in the embodiment ofFIG. 3 , 22 a, 22 b are provided in theheaters 2 a, 2 b. For reasons of clarity, the connections are omitted inliquid tank FIG. 4 . -
FIGS. 5 a through 5 c show various possibilities for fixing thecooling device 7. The vacuum container which contains thecold head 10 of the cryocooler can either be directly mounted on theouter jacket 4 of thecryostat 1 as shown inFIG. 5 a or externally e.g. on the room ceiling 28 (FIG. 5 b) or on a separate-stand 29 (FIG. 5 c). Aseal 30 must be used for mounting onto thecryostat 1. In case of external suspension only further sealing 31 a, 31 b are used between theelements vacuum chamber 9 and theouter jacket 4 of thecryostat 1 with the consequence that no or only minimum vibrations of the cryocooler are transferred to thecryostat 1. This is particularly favorable if thecooling device 7 is used for cooling a cryostat configuration which contains asuperconducting magnet arrangement 5, in particular, if thesuperconducting magnet arrangement 5 is part of a nuclear magnetic resonance apparatus, in particular magnetic resonance imaging (MRI) or magnetic resonance spectroscopy (Nuclear Magnetic Resonance, NMR). The inventive cooling device therefore allows high-resolution NMR methods. - In summary, a cooling device is provided which permits retrofitting to existing cryostat configurations, and in particular such configurations which contain superconducting magnets without (or with only minor) adjustments to permit, in a straightforward manner, operation with no or little cryogen loss even if several cryogens are used.
-
- 1 cryostat
- 2 a, 2 b liquid tanks
- 3 a,b,c,d suspension tubes
- 4 outer jacket
- 5 magnet arrangement
- 6 radiation shield of the cryostat
- 7 cooling device
- 8 outer jacket of the cooling device
- 9 vacuum chamber
- 10 cold head
- 11 first cold stage
- 12 second cold stage
- 13 radiation shield of the cooling device
- 14 a,b heat-transferring device
- 15 a,b cavity
- 16 a,b conduit
- 17 a,b connection
- 18 a,b cryogen
- 19 a,b first tube
- 20 second tube
- 21 a,b connecting element
- 22 a,b heater
- 23 open line
- 24 a,b heat exchanger
- 25 regenerator tube
- 26 valve
- 27 pump
- 28 room ceiling
- 29 stand
- 30 seal
- 31 a,b sealing elements
Claims (27)
1. A cooling device for re-liquefying cryogenic gases emanating from a cryostat, the cryostat keeping at least two different cryogenic liquids, the cryostat having neck and suspension tubes, the cooling device comprising:
a first cryocooler cold head stage;
a second cryocooler cold head stage;
a radiation shield surrounding at least portions of said first and said second stages;
an outer jacket delimiting a vacuum chamber, said jacket surrounding said radiation shield and said first and said second stages;
a first heat transferring device in heat-conducting connection with said first cold head stage; and
a second heat transferring device in heat-conducting connection with said second cold head stage, said first and said second heat transferring devices structured and dimensioned for insertion into the neck or the suspension tubes of the cryostat.
2. The cooling device of claim 1 , wherein at least one of said first and said second heat-transferring devices has a cavity disposed in heat-conducting contact with said first or said second cold stage, said cavity connected to an open line or conduit feeding into a liquid tank of the cryostat, wherein cryogen is evaporated from the liquid tank and enters into said cavity where it is liquefied to subsequently flow back through said open line or conduit into the liquid tank.
3. The cooling device of claim 1 , wherein at least one of said first and said second heat-transferring devices has a metallic connection with excellent heat conducting properties at the end of which cryogen evaporated from a liquid tank of the cryostat is liquefied and subsequently returned into a liquid bath of the liquid tank.
4. The cooling device of claim 1 , wherein said cryocooler is a pulse tube cooler.
5. The cooling device of claim 1 , wherein said cryocooler is a Gifford-McMahon cooler.
6. The cooling device of claim 1 , further comprising at least one connecting line, which is open at both ends, to connect said cold head of said cryocooler to at least one neck or suspension tube, in which no heat-transferring device is inserted, of a liquid tank containing a cryogen having a lowest boiling temperature, wherein said line is in thermal contact with said first and said second cold stages of said cold head.
7. The cooling device of claim 6 , wherein said line is in thermal contact with a regenerator tube disposed above a coldest cold stage and said line terminates in said cavity or is guided along a metallic connection into the liquid tank after thermal contact with said coldest cold stage.
8. The cooling device of claim 6 , further comprising a valve and/or a pump inserted into said connecting line between the neck or suspension tube and said cold head.
9. The cooling device of claim 1 , wherein helium can be liquefied at a temperature of 4.2 K or less at a coldest stage of said cryocooler.
10. The cooling device of claim 1 , wherein liquid nitrogen can be generated at 77K or less at a cold stage of said cold head of said cryocooler.
11. The cooling device of claim 1 , wherein a cold stage of said cold head of said cryocooler, which is not a coldest cold stage, is connected in a heat-conducting manner to said radiation shield which at least partially surrounds said cold head.
12. The cooling device of claim 1 , wherein at least one of said first and said second heat-transferring device is at least partially disposed within said outer jacket.
13. The cooling device of claim 2 , wherein at least one of said first and said second the heat-transferring device is at least partially surrounded by a first tube in a region outside of said outer jacket.
14. The cooling device of claim 13 , wherein said first tube is open at one end, that end being connected to a vacuum chamber of said outer jacket while an other end is connected in a gas-tight manner to one of said first and said second heat-transferring devices.
15. The cooling device of claim 13 , wherein said first tube is connected at both ends in a gas-tight manner to one of said first and said second heat-transferring devices and is provided with a separate connection for evacuation.
16. The cooling device of claim 13 , wherein said conduit or a metallic connection of said first or said second heat-transferring device is at least partially surrounded by a second tube which is connected in a heat-conducting manner to said radiation shield, wherein said second tube is disposed within said first tube.
17. The cooling device of claim 16 , wherein said first and said second tubes are flexible or are designed as bellows.
18. The cooling device of claim 2 , wherein said conduit or a metallic connection comprises a flexible section, a bellows, or wires which are plaited into strands.
19. The cooling device of claim 16 , wherein in at least one of said first and said second heat-transferring devices and a least one of said first and said second tubes can be connected and disconnected at at least one point using a gas-tight coupling.
20. The cooling device of claim 1 , wherein the cooling device can be mounted in a gas-tight manner to the cryostat for keeping cryogenic liquids.
21. The cooling device of claim 1 , wherein the cooling device can be mounted outside of the cryostat.
22. The cooling device of claim 21 , further comprising a soft connecting element which does not transmit vibrations and which is sealingly disposed between the cooling device and the cryostat.
23. The cooling device of claim 1 , further comprising electric heaters mounted to at least one of said first and said second cold stages of said cryocooler.
24. A cryostat configuration characterized by the cooling device of claim 1 .
25. The cryostat configuration of claim 24 , further comprising a superconducting magnet arrangement, wherein said cooling device serves to cool said superconducting magnet arrangement.
26. The cryostat configuration of claim 25 , wherein said superconducting magnet arrangement is part of an apparatus for nuclear magnetic resonance, magnetic resonance imaging (MRI), or magnetic resonance spectroscopy (nuclear magnetic resonance NMR).
27. The cryostat configuration of claim 24 , further comprising an electric heater inserted into a cryogenic liquid tank via the suspension or neck tubes thereof.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102004037173.3 | 2004-07-30 | ||
| DE102004037173A DE102004037173B3 (en) | 2004-07-30 | 2004-07-30 | Cryogenic cooler for workpiece incorporates cold head attached to two-stage cooler with attachments to sealed cryostat and with radiation shield inside vacuum-tight housing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20070051116A1 true US20070051116A1 (en) | 2007-03-08 |
Family
ID=35404600
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/171,429 Abandoned US20070051116A1 (en) | 2004-07-30 | 2005-07-01 | Device for loss-free cryogen cooling of a cryostat configuration |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20070051116A1 (en) |
| EP (1) | EP1628089B1 (en) |
| JP (1) | JP2006046896A (en) |
| DE (1) | DE102004037173B3 (en) |
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090301129A1 (en) * | 2008-06-08 | 2009-12-10 | Wang Nmr Inc. | Helium and nitrogen reliquefying apparatus |
| US20110039707A1 (en) * | 2005-11-18 | 2011-02-17 | Magnex Scientific Limited | Superconducting magnet systems |
| CN102299022A (en) * | 2011-08-16 | 2011-12-28 | 南京丰盛超导技术有限公司 | Mechanical heat switch for refrigerating machine to directly cool superconducting magnet |
| US20120011859A1 (en) * | 2010-06-09 | 2012-01-19 | Quantum Design, Inc. | Gas-flow cryostat for dynamic temperature regulation using a fluid level sensor |
| CN102869933A (en) * | 2010-05-04 | 2013-01-09 | 皇家飞利浦电子股份有限公司 | Improved method and apparatus for shipping and storage of cryogenic devices |
| US8598881B2 (en) | 2011-01-11 | 2013-12-03 | General Electric Company | Magnetic resonance imaging system with thermal reservoir and method for cooling |
| CN103697647A (en) * | 2012-09-28 | 2014-04-02 | 中国科学院物理研究所 | Vacuum low-temperature thermostat |
| US20140123681A1 (en) * | 2007-04-02 | 2014-05-08 | General Electric Company | Method and apparatus to hyperpolarize materials for enhanced mr techniques |
| US20150007586A1 (en) * | 2013-07-03 | 2015-01-08 | Bruker Biospin Ag | Method for reconfiguring a cryostat configuration for recirculation cooling |
| CN104795198A (en) * | 2014-01-21 | 2015-07-22 | 西门子(深圳)磁共振有限公司 | Cooling device and method for magnetic resonance imaging system and magnetic resonance imaging system |
| US20150348689A1 (en) * | 2013-01-06 | 2015-12-03 | Institute Of Electrical Engineering, Chinese Academy Of Sciences | Superconducting Magnet System for Head Imaging |
| CN108657667A (en) * | 2018-07-06 | 2018-10-16 | 宁波健信核磁技术有限公司 | A kind of cold magnet transport container of superconduction |
| US10352501B2 (en) | 2015-07-01 | 2019-07-16 | Bruker Biospin Gmbh | Cryostat with active neck tube cooling by a second cryogen |
| CN112133514A (en) * | 2019-06-25 | 2020-12-25 | 布鲁克瑞士股份公司 | Cryostat assembly with spring-elastic, thermally conductive connecting element |
| US20210293475A1 (en) * | 2020-03-23 | 2021-09-23 | Ricoh Company, Ltd. | Helium circulation system, cryogenic refrigeration method, and biomagnetism measuring apparatus |
| US11327062B2 (en) | 2017-12-20 | 2022-05-10 | Bilfinger Noell Gmbh | Device for examining an atmosphere and use of the device |
| CN114556498A (en) * | 2019-11-01 | 2022-05-27 | 日本超导体技术公司 | Helium recondensing device for cryostat |
| US11913714B2 (en) | 2021-11-02 | 2024-02-27 | Anyon Systems Inc. | Dilution refrigerator with continuous flow helium liquefier |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006116042A (en) * | 2004-10-21 | 2006-05-11 | Iwatani Industrial Gases Corp | Cooling unit in super-conductive magnet system |
| JP4814630B2 (en) * | 2005-12-21 | 2011-11-16 | 三菱電機株式会社 | Superconducting magnet system |
| JP4736047B2 (en) * | 2006-04-04 | 2011-07-27 | 学校法人金沢工業大学 | Cooling system |
| DE102007013350B4 (en) * | 2007-03-16 | 2013-01-31 | Bruker Biospin Ag | Power supply with high-temperature superconductors for superconducting magnets in a cryostat |
| JP4855990B2 (en) * | 2007-03-29 | 2012-01-18 | 株式会社東芝 | Recondensing device, mounting method thereof and superconducting magnet using the same |
| JP5728172B2 (en) * | 2010-06-16 | 2015-06-03 | 株式会社神戸製鋼所 | Recondensing device and NMR analyzer equipped with the same |
| DE102011078608B4 (en) * | 2011-07-04 | 2023-06-22 | Bruker Switzerland Ag | cryostat assembly |
| KR101334321B1 (en) | 2012-05-15 | 2013-11-28 | 현대중공업 주식회사 | Cryocooler with the radiant heat shield |
| KR101447525B1 (en) * | 2013-11-06 | 2014-10-15 | 한국기초과학지원연구원 | Adiabatic collector for recycling gas, liquefier for recycling gas and recovery apparatus for recycling gas |
| JP5839734B2 (en) * | 2013-12-26 | 2016-01-06 | 大陽日酸株式会社 | Evaporative gas reliquefaction equipment for low temperature liquefied gas |
| CN113903541B (en) * | 2021-11-04 | 2022-06-28 | 中国原子能科学研究院 | Large high-temperature superconducting magnetic system based on small refrigerator and temperature control method |
| KR20250026979A (en) * | 2023-08-18 | 2025-02-25 | 한국표준과학연구원 | Low Noise Liquid Helium Reliquifing Circulation Apparatus |
Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3894403A (en) * | 1973-06-08 | 1975-07-15 | Air Prod & Chem | Vibration-free refrigeration transfer |
| US4223540A (en) * | 1979-03-02 | 1980-09-23 | Air Products And Chemicals, Inc. | Dewar and removable refrigerator for maintaining liquefied gas inventory |
| US4502296A (en) * | 1983-04-15 | 1985-03-05 | Hitachi, Ltd. | Cryostat |
| US5327733A (en) * | 1993-03-08 | 1994-07-12 | University Of Cincinnati | Substantially vibration-free shroud and mounting system for sample cooling and low temperature spectroscopy |
| US5563566A (en) * | 1995-11-13 | 1996-10-08 | General Electric Company | Cryogen-cooled open MRI superconductive magnet |
| US5613367A (en) * | 1995-12-28 | 1997-03-25 | General Electric Company | Cryogen recondensing superconducting magnet |
| US5701744A (en) * | 1996-10-31 | 1997-12-30 | General Electric Company | Magnetic resonance imager with helium recondensing |
| US5744959A (en) * | 1995-12-22 | 1998-04-28 | Spectrospin Ag | NMR measurement apparatus with pulse tube cooler |
| US5782095A (en) * | 1997-09-18 | 1998-07-21 | General Electric Company | Cryogen recondensing superconducting magnet |
| US5966944A (en) * | 1997-04-09 | 1999-10-19 | Aisin Seiki Kabushiki Kaisha | Superconducting magnet system outfitted with cooling apparatus |
| US20020000283A1 (en) * | 2000-03-17 | 2002-01-03 | Jun Nakano | Transcribing method |
| US20020002830A1 (en) * | 2000-07-08 | 2002-01-10 | Bruker Analytik Gmbh | Circulating cryostat |
| US6378312B1 (en) * | 2000-05-25 | 2002-04-30 | Cryomech Inc. | Pulse-tube cryorefrigeration apparatus using an integrated buffer volume |
| US20030230089A1 (en) * | 2002-06-14 | 2003-12-18 | Bruker Biospin Gmbh | Cryostat configuration with improved properties |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6138363A (en) * | 1984-07-31 | 1986-02-24 | 株式会社日立製作所 | helium refrigeration equipment |
| JPS6266067A (en) * | 1985-09-18 | 1987-03-25 | 株式会社日立製作所 | helium cooler |
| IT1198238B (en) * | 1986-12-23 | 1988-12-21 | Zambon Spa | COMPOUNDS WITH ANTIBIOTIC ACTIVITY |
| JPS63207958A (en) * | 1987-02-23 | 1988-08-29 | Toshiba Corp | Freezer |
| JPS63210572A (en) * | 1987-02-26 | 1988-09-01 | Toshiba Corp | Cryogenic freezer |
| IT1278167B1 (en) | 1995-01-25 | 1997-11-17 | Matec Srl | CUTTING AND SUCTION UNIT FOR THE YARN FOR MACHINE FOR THE PROCESSING OF SOCKS AND SOCKS WITH MULTIPLE FALLS |
| GB2329701B (en) * | 1997-09-30 | 2001-09-19 | Oxford Magnet Tech | Load bearing means in nmr cryostat systems |
| GB2330194B (en) * | 1997-09-30 | 2002-05-15 | Oxford Magnet Tech | A cryogenic pulse tube refrigerator |
| US5936499A (en) * | 1998-02-18 | 1999-08-10 | General Electric Company | Pressure control system for zero boiloff superconducting magnet |
| JP3358053B2 (en) * | 1998-03-13 | 2002-12-16 | 住友重機械工業株式会社 | Liquid nitrogen recondenser |
| US6038867A (en) * | 1998-07-31 | 2000-03-21 | General Electric Company | Wide multilayer insulating blankets for zero boiloff superconducting magnet |
| JP3416559B2 (en) * | 1999-03-30 | 2003-06-16 | 住友重機械工業株式会社 | Liquefied gas storage device, reliquefaction device, and method for reliquefaction of liquefied nitrogen |
| US20030005095A1 (en) | 2001-06-29 | 2003-01-02 | Fee John A. | Method and system for programmable submarine network configuration plans to enable diverse service level agreements in telecommunication networks |
| GB0125189D0 (en) * | 2001-10-19 | 2001-12-12 | Oxford Magnet Tech | A pulse tube refrigerator |
| GB0125188D0 (en) * | 2001-10-19 | 2001-12-12 | Oxford Magnet Tech | A pulse tube refrigerator sleeve |
-
2004
- 2004-07-30 DE DE102004037173A patent/DE102004037173B3/en not_active Expired - Lifetime
-
2005
- 2005-07-01 US US11/171,429 patent/US20070051116A1/en not_active Abandoned
- 2005-07-26 EP EP05016144A patent/EP1628089B1/en not_active Expired - Lifetime
- 2005-07-29 JP JP2005220785A patent/JP2006046896A/en active Pending
Patent Citations (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3894403A (en) * | 1973-06-08 | 1975-07-15 | Air Prod & Chem | Vibration-free refrigeration transfer |
| US4223540A (en) * | 1979-03-02 | 1980-09-23 | Air Products And Chemicals, Inc. | Dewar and removable refrigerator for maintaining liquefied gas inventory |
| US4502296A (en) * | 1983-04-15 | 1985-03-05 | Hitachi, Ltd. | Cryostat |
| US5327733A (en) * | 1993-03-08 | 1994-07-12 | University Of Cincinnati | Substantially vibration-free shroud and mounting system for sample cooling and low temperature spectroscopy |
| US5563566A (en) * | 1995-11-13 | 1996-10-08 | General Electric Company | Cryogen-cooled open MRI superconductive magnet |
| US5744959A (en) * | 1995-12-22 | 1998-04-28 | Spectrospin Ag | NMR measurement apparatus with pulse tube cooler |
| US5613367A (en) * | 1995-12-28 | 1997-03-25 | General Electric Company | Cryogen recondensing superconducting magnet |
| US5701744A (en) * | 1996-10-31 | 1997-12-30 | General Electric Company | Magnetic resonance imager with helium recondensing |
| US5966944A (en) * | 1997-04-09 | 1999-10-19 | Aisin Seiki Kabushiki Kaisha | Superconducting magnet system outfitted with cooling apparatus |
| US5782095A (en) * | 1997-09-18 | 1998-07-21 | General Electric Company | Cryogen recondensing superconducting magnet |
| US20020000283A1 (en) * | 2000-03-17 | 2002-01-03 | Jun Nakano | Transcribing method |
| US6378312B1 (en) * | 2000-05-25 | 2002-04-30 | Cryomech Inc. | Pulse-tube cryorefrigeration apparatus using an integrated buffer volume |
| US20020002830A1 (en) * | 2000-07-08 | 2002-01-10 | Bruker Analytik Gmbh | Circulating cryostat |
| US20030230089A1 (en) * | 2002-06-14 | 2003-12-18 | Bruker Biospin Gmbh | Cryostat configuration with improved properties |
| US6804968B2 (en) * | 2002-06-14 | 2004-10-19 | Bruker Biospin Gmbh | Cryostat configuration with improved properties |
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110039707A1 (en) * | 2005-11-18 | 2011-02-17 | Magnex Scientific Limited | Superconducting magnet systems |
| US20140123681A1 (en) * | 2007-04-02 | 2014-05-08 | General Electric Company | Method and apparatus to hyperpolarize materials for enhanced mr techniques |
| US20090301129A1 (en) * | 2008-06-08 | 2009-12-10 | Wang Nmr Inc. | Helium and nitrogen reliquefying apparatus |
| CN102869933B (en) * | 2010-05-04 | 2015-08-19 | 皇家飞利浦电子股份有限公司 | For loading and transporting and store improving one's methods and equipment of Cryo Equipment |
| CN102869933A (en) * | 2010-05-04 | 2013-01-09 | 皇家飞利浦电子股份有限公司 | Improved method and apparatus for shipping and storage of cryogenic devices |
| US10577175B2 (en) | 2010-05-04 | 2020-03-03 | Koninklijke Philips N.V. | Method and apparatus for shipping and storage of cryogenic devices |
| US20120011859A1 (en) * | 2010-06-09 | 2012-01-19 | Quantum Design, Inc. | Gas-flow cryostat for dynamic temperature regulation using a fluid level sensor |
| US9618257B2 (en) * | 2010-06-09 | 2017-04-11 | Quantum Design International, Inc. | Gas-flow cryostat for dynamic temperature regulation using a fluid level sensor |
| US8598881B2 (en) | 2011-01-11 | 2013-12-03 | General Electric Company | Magnetic resonance imaging system with thermal reservoir and method for cooling |
| CN102299022A (en) * | 2011-08-16 | 2011-12-28 | 南京丰盛超导技术有限公司 | Mechanical heat switch for refrigerating machine to directly cool superconducting magnet |
| CN103697647A (en) * | 2012-09-28 | 2014-04-02 | 中国科学院物理研究所 | Vacuum low-temperature thermostat |
| US20150348689A1 (en) * | 2013-01-06 | 2015-12-03 | Institute Of Electrical Engineering, Chinese Academy Of Sciences | Superconducting Magnet System for Head Imaging |
| US9666344B2 (en) * | 2013-01-06 | 2017-05-30 | Institute Of Electrical Engineering, Chinese Academy Of Sciences | Superconducting magnet system for head imaging |
| US9494344B2 (en) * | 2013-07-03 | 2016-11-15 | Bruker Biospin Ag | Method for reconfiguring a cryostat configuration for recirculation cooling |
| US20150007586A1 (en) * | 2013-07-03 | 2015-01-08 | Bruker Biospin Ag | Method for reconfiguring a cryostat configuration for recirculation cooling |
| WO2015110389A1 (en) * | 2014-01-21 | 2015-07-30 | Siemens Plc | Cooling device and method for a magnetic resonance imaging system |
| CN104795198A (en) * | 2014-01-21 | 2015-07-22 | 西门子(深圳)磁共振有限公司 | Cooling device and method for magnetic resonance imaging system and magnetic resonance imaging system |
| US10352501B2 (en) | 2015-07-01 | 2019-07-16 | Bruker Biospin Gmbh | Cryostat with active neck tube cooling by a second cryogen |
| US11327062B2 (en) | 2017-12-20 | 2022-05-10 | Bilfinger Noell Gmbh | Device for examining an atmosphere and use of the device |
| CN108657667A (en) * | 2018-07-06 | 2018-10-16 | 宁波健信核磁技术有限公司 | A kind of cold magnet transport container of superconduction |
| CN112133514A (en) * | 2019-06-25 | 2020-12-25 | 布鲁克瑞士股份公司 | Cryostat assembly with spring-elastic, thermally conductive connecting element |
| US11810711B2 (en) | 2019-06-25 | 2023-11-07 | Bruker Switzerland Ag | Cryostat assembly having a resilient, heat-conducting connection element |
| CN114556498A (en) * | 2019-11-01 | 2022-05-27 | 日本超导体技术公司 | Helium recondensing device for cryostat |
| US11828513B2 (en) | 2019-11-01 | 2023-11-28 | Japan Superconductor Technology Inc. | Apparatus for recondensing helium for cryostat |
| US20210293475A1 (en) * | 2020-03-23 | 2021-09-23 | Ricoh Company, Ltd. | Helium circulation system, cryogenic refrigeration method, and biomagnetism measuring apparatus |
| US11913714B2 (en) | 2021-11-02 | 2024-02-27 | Anyon Systems Inc. | Dilution refrigerator with continuous flow helium liquefier |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1628089B1 (en) | 2012-05-23 |
| EP1628089A3 (en) | 2009-03-25 |
| JP2006046896A (en) | 2006-02-16 |
| DE102004037173B3 (en) | 2005-12-15 |
| EP1628089A2 (en) | 2006-02-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20070051116A1 (en) | Device for loss-free cryogen cooling of a cryostat configuration | |
| JP3996935B2 (en) | Cryostat structure | |
| JP4031121B2 (en) | Cryostat equipment | |
| US7474099B2 (en) | NMR apparatus with commonly cooled probe head and cryogenic container and method for the operation thereof | |
| US20070089432A1 (en) | Cryostat configuration with cryocooler | |
| US6389821B2 (en) | Circulating cryostat | |
| US5782095A (en) | Cryogen recondensing superconducting magnet | |
| US7430871B2 (en) | NMR spectrometer with a common refrigerator for cooling an NMR probe head and cryostat | |
| US5744959A (en) | NMR measurement apparatus with pulse tube cooler | |
| US5586437A (en) | MRI cryostat cooled by open and closed cycle refrigeration systems | |
| JP4417247B2 (en) | MRI system with superconducting magnet and refrigeration unit | |
| US20130008187A1 (en) | Cryostat configuration | |
| US20170284725A1 (en) | Cryostat with a first and a second helium tank, which are separated from one another in a liquid-tight manner at least in a lower part | |
| JPH11151225A (en) | Mri system of nmr system | |
| GB2542667A (en) | Method and device for precooling a cryostat | |
| US20070051115A1 (en) | Cryostat configuration with cryocooler and gas gap heat transfer device | |
| US20030230089A1 (en) | Cryostat configuration with improved properties | |
| US20090301129A1 (en) | Helium and nitrogen reliquefying apparatus | |
| US11828513B2 (en) | Apparatus for recondensing helium for cryostat | |
| EP0905435A2 (en) | Load bearing means in cryostat systems | |
| JP2025097294A (en) | Apparatus and method for transferring liquid helium to a practical cryostat - Patents.com | |
| GB2463659A (en) | Method and Apparatus for Improved Cooling of a Cryostat Thermal Shield | |
| US11977139B2 (en) | Accelerated cooldown of low-cryogen magnetic resonance imaging (MRI) magnets |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: BRUKER BIOSPIN AG, SWITZERLAND Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:GLEMOT, AGNES;VOGEL, DIETRICH;ECKERT, DANIEL;REEL/FRAME:016753/0183;SIGNING DATES FROM 20050509 TO 20050517 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |