CA1103143A - Cryostat with refrigerator for superconduction nmr spectrometer - Google Patents
Cryostat with refrigerator for superconduction nmr spectrometerInfo
- Publication number
- CA1103143A CA1103143A CA321,936A CA321936A CA1103143A CA 1103143 A CA1103143 A CA 1103143A CA 321936 A CA321936 A CA 321936A CA 1103143 A CA1103143 A CA 1103143A
- Authority
- CA
- Canada
- Prior art keywords
- radiation shield
- reservoir
- cryostat
- temperature
- liquid nitrogen
- 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.)
- Expired
Links
- 230000005855 radiation Effects 0.000 claims abstract description 55
- 238000012546 transfer Methods 0.000 claims description 9
- 238000009835 boiling Methods 0.000 claims description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 abstract description 56
- 239000007788 liquid Substances 0.000 abstract description 54
- 239000001307 helium Substances 0.000 abstract description 36
- 229910052734 helium Inorganic materials 0.000 abstract description 36
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 abstract description 36
- 229910052757 nitrogen Inorganic materials 0.000 abstract description 28
- 229920000728 polyester Polymers 0.000 abstract description 9
- 238000005057 refrigeration Methods 0.000 abstract description 4
- 239000002826 coolant Substances 0.000 description 22
- 229910052782 aluminium Inorganic materials 0.000 description 13
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 12
- 239000007789 gas Substances 0.000 description 11
- 238000001816 cooling Methods 0.000 description 10
- 239000000543 intermediate Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 239000010935 stainless steel Substances 0.000 description 7
- 229910001220 stainless steel Inorganic materials 0.000 description 7
- 238000002955 isolation Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 238000009987 spinning Methods 0.000 description 3
- 238000004804 winding Methods 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 230000002688 persistence Effects 0.000 description 2
- 239000000523 sample Substances 0.000 description 2
- IKOKHHBZFDFMJW-UHFFFAOYSA-N 2-[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]-3-(2-morpholin-4-ylethoxy)pyrazol-1-yl]-1-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethanone Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C=1C(=NN(C=1)CC(=O)N1CC2=C(CC1)NN=N2)OCCN1CCOCC1 IKOKHHBZFDFMJW-UHFFFAOYSA-N 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001369 Brass Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229920004934 Dacron® Polymers 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- UODXCYZDMHPIJE-UHFFFAOYSA-N menthanol Chemical compound CC1CCC(C(C)(C)O)CC1 UODXCYZDMHPIJE-UHFFFAOYSA-N 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000002085 persistent effect Effects 0.000 description 1
- 239000005020 polyethylene terephthalate Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000003507 refrigerant Substances 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R33/00—Arrangements or instruments for measuring magnetic variables
- G01R33/20—Arrangements or instruments for measuring magnetic variables involving magnetic resonance
- G01R33/28—Details of apparatus provided for in groups G01R33/44 - G01R33/64
- G01R33/30—Sample handling arrangements, e.g. sample cells, spinning mechanisms
- G01R33/31—Temperature control thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/08—Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
- F17C3/085—Cryostats
-
- 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
- F25D3/00—Devices using other cold materials; Devices using cold-storage bodies
- F25D3/10—Devices using other cold materials; Devices using cold-storage bodies using liquefied gases, e.g. liquid air
-
- 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
- F17C2270/00—Applications
- F17C2270/05—Applications for industrial use
- F17C2270/0527—Superconductors
- F17C2270/0536—Magnetic resonance imaging
-
- 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
- F25D19/006—Thermal coupling structure or interface
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)
- Condensed Matter Physics & Semiconductors (AREA)
- General Physics & Mathematics (AREA)
- Containers, Films, And Cooling For Superconductive Devices (AREA)
- Devices That Are Associated With Refrigeration Equipment (AREA)
Abstract
PATENT APPLICATION
of GEORGE D. KNEIP, JR. AND MARVIN H. ANDERSON
for IMPROVED CRYOSTAT WITH EXTERNAL REFRIGERATOR
FOR SUPERCONDUCTING NMR SPECTROMETER
Abstract of Disclosure An improved cryostat for the superconducting magnet of an NMR spectrometer comprises a nested structure of isothermal shells surrounding a thermally conductive central reservoir of substantially spherical shape containing liquid helium in which the superconducting solenoid remains operational when only partially immersed. A radiation shield surrounding the central reservoir is cooled by the boil-off of escaping helium vapor. The radiation shield is enclosed within an isothermal shell maintained at the temperature of liquid nitrogen by thermal contact with a liquid nitrogen reservoir disposed above the region of the central reservoir and shielded therefrom by a wall of the isothermal shell. An outer radiation shield surround the liquid nitrogen reservoir and associated isothermal shell and the outer radiation shield is maintained at a temperature of the order of 180° K by an external refrigeration facility. A hermitically sealed containment vessel forms the outer wall of the cryostat and provides a port for evacuating to a vary low common pressure all the interior spaces between adjacent nested structures. The spacing between adjacent nested surfaces is maintained by a novel internal mechanical bracing system of low thermal conductivity comprising polyester cords disposed under tension between adjacent shells.
of GEORGE D. KNEIP, JR. AND MARVIN H. ANDERSON
for IMPROVED CRYOSTAT WITH EXTERNAL REFRIGERATOR
FOR SUPERCONDUCTING NMR SPECTROMETER
Abstract of Disclosure An improved cryostat for the superconducting magnet of an NMR spectrometer comprises a nested structure of isothermal shells surrounding a thermally conductive central reservoir of substantially spherical shape containing liquid helium in which the superconducting solenoid remains operational when only partially immersed. A radiation shield surrounding the central reservoir is cooled by the boil-off of escaping helium vapor. The radiation shield is enclosed within an isothermal shell maintained at the temperature of liquid nitrogen by thermal contact with a liquid nitrogen reservoir disposed above the region of the central reservoir and shielded therefrom by a wall of the isothermal shell. An outer radiation shield surround the liquid nitrogen reservoir and associated isothermal shell and the outer radiation shield is maintained at a temperature of the order of 180° K by an external refrigeration facility. A hermitically sealed containment vessel forms the outer wall of the cryostat and provides a port for evacuating to a vary low common pressure all the interior spaces between adjacent nested structures. The spacing between adjacent nested surfaces is maintained by a novel internal mechanical bracing system of low thermal conductivity comprising polyester cords disposed under tension between adjacent shells.
Description
Back~round of the Invention This invention relates to cryostats for the contain-ment of very low temperature liquids such as liquid helium and in particular to cryostats housing superconducting apparatus such as NMR spectrometer magnets.
Prior art cryostats for containment of superconduct-ing apparatus, for example, superconducting magnets, have employPd a helium vessel shaped to exhibit a relatively small cylindrical volume surrounding the superconducting magnet, in open communication with a larger volume dispos-ed immediately above the solanoid. In this geometry the solenoid is maintained completely submerged in the liquid helium bath. A sufficient hold time for the liquid heli-um is provided by the head of liquid helium in the large volume. This form of helium reservoir exhibits a surface area to volume ratio substantially higher than the mini-mum achievable; consequently additional radiation losses ' are introduced which contribute to a higher rate of I helium boil-off.
Prior axt cryostats have taken the form of nested ¦ chambers which have been internally braced, as for ex-ample with stainless steel spokes, to withstand mechanical shock and to maintain minimum clearances between adjacent nested walls. Stainless steel has been a popular mater-ial of choice because of its relatively low thermal , conductivity and its high strength. However, the thermal i conductivity of such bracing places a limit upon the thermal isolation which can be achieved between adjacent surfaces of nested structures.
' 30 Cryostats of the prior art have employed a second-ary temperature bath to shield the lowest temperature coolant from ambient temperature. Ordinarily, the
Prior art cryostats for containment of superconduct-ing apparatus, for example, superconducting magnets, have employPd a helium vessel shaped to exhibit a relatively small cylindrical volume surrounding the superconducting magnet, in open communication with a larger volume dispos-ed immediately above the solanoid. In this geometry the solenoid is maintained completely submerged in the liquid helium bath. A sufficient hold time for the liquid heli-um is provided by the head of liquid helium in the large volume. This form of helium reservoir exhibits a surface area to volume ratio substantially higher than the mini-mum achievable; consequently additional radiation losses ' are introduced which contribute to a higher rate of I helium boil-off.
Prior axt cryostats have taken the form of nested ¦ chambers which have been internally braced, as for ex-ample with stainless steel spokes, to withstand mechanical shock and to maintain minimum clearances between adjacent nested walls. Stainless steel has been a popular mater-ial of choice because of its relatively low thermal , conductivity and its high strength. However, the thermal i conductivity of such bracing places a limit upon the thermal isolation which can be achieved between adjacent surfaces of nested structures.
' 30 Cryostats of the prior art have employed a second-ary temperature bath to shield the lowest temperature coolant from ambient temperature. Ordinarily, the
-2 li~3143 secondary coolant reservoir is itself insulated from an~ient temperature~ as for example with layers of an insulating material. In a superconducting magnet with room temperature access, a relatively large magnet bore is required by prior art cryostat structures to provide sufficient space for this insulation. As a result, the inside diameter of such prior art solenoid is constrained to span a proportionately larger diameter to accommodate the additional insulation, whereby a much greater length of superconducting wire is required for fabrication of the solenoid.
It is an object of the present invention to achieve an improved cryostat for the containment of a liquified gas whereby the loss of such liquified gas from a cryostat due to the boiling of such liquified gas is minimized.
Accordingly, the present invention provides-in a cryostat wherein a first liquified gas is contained in a central vessel and said central vessel is surrounded by shielding means maintained at the temperature of another liquified gas of higher boiling point, said cryostat further comprising a containment vessel at ambient tempera-ture, said containment vessel comprising a wall portion having an interior surface spaced from the outer surface of said shielding means, the improvement comprising: a radiation shield disposed between the interior surface of said containment vessel and the outer surface of said shielding means; mechanical refrigerating means for main-taining said radiation shield at a temperature substantially ¦ intermediate said shielding means and am~ient temperature ¦ 30 during operation.
In a described embodiment the amount of liquid helium required for operation of~ a superconducting magnet is minimized and the interval between replenishments of the liquid helium is maximized.
In one embodiment of this invention a substantially spherical central vessel is provided to contain the liquified gas forming a primary coolant, whereby the ratio of surface area to volume of such vessel is minimized. The central vessel may be constructed of aluminum of such thickness that the thermal gradient introduced by the finite thermal conductivity of the necessary fill and vent tubes leading from the central vessel, and still be small enough to permit operation of superconducting apparatus only partly submerged in the liquified gas.
The central coolant reservoir may be surrounded by a radiation shield spaced from the central reservoir and maintained at a first intermediate temperature through vapor cooling provided by the boil-off from the liquified gas contained in the central reservoir.
In a described embodiment, the central'reservoir and its ~urround'ing radiation shield are enclosed by an isothermal surface defined by a second surrounding chamber j and a second reservoir is provided externally above the second surrounding chamber, and in thermal contact with the outer surface of the second chamber, whereby the second chamber and reservoir form an isothermal body maintained at i the temperature of a second liquified gas comprising the secondary coolant filling the second reservoir. An outer radiation shield is provided, enclosing the isothermal i body comprising the second reservoir and the second chamber I in contact therewith, such outer radiation shield maintained ¦ 30 at a temperature intermediate the second coolant and ambient temperature. The outer radiation shield is maintained at the desired temperature by an auxiliary refrigeration ~ 3~43 facility.
In a described embodiment the primary coolant (hereafter, liquid helium) is contained in a central reservoir having a substantially spherical shape. The central reservoir is formed of aluminum and has a kore through its centre defined by an aluminum cylindrical wall welded to the quasi-spherical reservoir. A superconducting solenoid is disposed within the central reservoir coaxial with the bore. In the embodiment the surface to volume ratio is minimized, reducing the area of the central reservoir for absorption of heat by radiation and permitting operation of the solenoid to continue when the level of liquid helium falls substantially below the top of the solenoid.
A radiation shield surrounding the helium reservoir is provided to establish a first isothermal surface inter-mediate the central reservoir and a surrounding second iso-thermal surface, the latter maintained at the temperature of a secondary coolant (hereinafter, liquid nitrogen). me radiation shield is maintained at about 50K through vapor cooling affected by the helium boil-off escaping up the fill and vent tubes with which the radiation shield is in therMal contact.
Surrounding the radiation shield and partially surrounding the fill and vent tubes, there is provided a secondary isothermal shell cooled by thermal contact with a liquid nitrogen reservoir disposed external the shell, above the region of the central reservoir. In this geometry the vent and fill tube from the central reservoir (partially surrounded by a cylindrical portion of the secondary iso-thermal shell) passes through a greater length of the secondary coolant reservoir as compared to prior art ~1~ 31~3 cryostats with conse~uently improved thermal isolation for the liquid helium reservoir.
The thermal isolation from ambient temperature of the secondary coolant reservoir and associated secondary iso-thermal shell is further improved in the embodiment by provision of an outer radiation shield surrounding the secondary coolant reservoir and associated isothermal chamber. This outer radiation shield is maintained at a temperature intermediate the secondary coolant and ambient temperature by means of an auxiliary refrigeration facility.
An outer hermetically sealed vessel encloses the outer radiation shield and the interior of the cryostat permitting the spaces between adjacent nested surfaces to be evacuated to a pressure of the order of 10 6 torr. In this way gas conduction and convection mechanisms are minimized for heat transport to the central reservoir.
The described embodiments virtually eliminate direct conduction losses between nested structures due to the mechanical support and internal bracing by replacing the bracing spokes of the prior art with bracing formed of polyester cord.
All of the walls forming the nested structure of the cryostat are constructed of aluminum, save for the fill and ven-t tubes of both the liquid nitrogen and helium reservoirs.
The aluminum surfaces are subject to a treatment which reduces radiant emissivity. Consequently, heat transport by radiation is further reduced between adjacent surfaces.
Embodiments of the invention will now be described, by way of example, with reference to the accompanying drawings in which:-Figure 1 is a schematic of an NMR spectrometer system.
Figure 2 is a top view of the cryostat of the '~ ' preferred embodiment.
Figure 3 i5 a section through the cryostat of Figure 2.
Figure 4 is a detail of the section of Figure 2.
Figure 5 is a detail in section of the cryostat of Figure 2.
Figure 6 shows the cold head for thermal linkage to the refrigerator.
A superconducting NMR spectrometer system employs a cryostat l having room temperature access to the magnetic field created within the cryostat 1 in a manner more explicitly depicted belo~. A probe 5 containing a sample 7 is introduced through bore 3 for analysis. A transmitter 9, receiver 11 and control unit 13, data processing unit 15 and display means 17 form the complete spectrometer (exclusi~e of power supplying systems for initiating persistent currents for the magnet).
¦ Figure 2 is a top view of the preferred embodiment of the cryostat 1 of this invention. A bore 3 provides room temperature access to the magnetic field created by ¦ apparatus within cryostat l as described below.
Turning now to Figure 3, the cryostat 1 contains a superconducting solenoid assembly 50 within a central reservoir llO. Reservoir llO contains a primary coolant, preferably liquid helium, to maintain the superconducting state of the windings comprising solenoid assembly 50.
Leads from the solenoid windings, collectively denoted 52 terminate in a connector 54 for access to external current sources introduced in a manner to be described. Additional circuits comprising persistence switches for controlling transitions between the normal and superconducting state for selected windings are not shown. These circuits and _ 7 _ ` 3~
preferred persistence switche~ are further described in, and form the subject matter of respective United States Patents Nos. 4,164,777, and 4,173,775 assigned to the assignees of the present invention. The solenoid assembly 50 is not within the scope of the present invention and is ~urther described in United States Patent No. 4,180,779 assigned to the assignee of the present invention.
Central coolant reservoir 110 is formed from 0.125"
10 - aluminum to a substantially spherical shape as shown, by spinning techniques well known in the art. In the preferred embodiment, reservoir 110 has a coolant capacity of about 25 litres. Reservoir 110 is further characterized by a bore formed by cylindrical wall 111, welded-to reservoir 110. Room temperature access is thereby afforded to the magnetic field of solenoid assembly 50. Reservoir 110 is isolated from ambient temperature by means of a plurality of consecutively nested surrounding chambers 112, 114, 116, and 118 having coaxial bores defined by cylindrical tubes 113, 115, 117, and 119, respectively. The wall thickness of each of the respective cylindrical coaxial tubes is determined by the heat load on each and varies from 0.02"
to 0.049". The spaces between chambers 112, 114, 116, and 118 are mutually communicating in a manner described below and evacuated through pump-out port 120 in exterior chamber 118 to achieve a very low pressure, as for example 10 6 torr to minimize thermal conduction between adjacent nested surfaces through gas conductivity and convection.
A secondary coolant reservoir 114', is disposed above central reservoir 110 and in thermal contact with chamber 114 whereby chamber 114, preferably formed of nominal 0.190" aluminum, comprises a shell at the temperature of - B -. . :) -~1~ 3:1~`3 the secondary coolant, preferably liquid nitrogen.
Returning to Figure 2, two vent and fill tubes 130 and 130' are required for access to the central reservoir.
These are constructed of 5/8" I.D. stainless steel having a wall thickness of 0.005". Two such vent and fill tubes 130 and 130' appear in Figure 1 and one such structure is disclosed in greater detail in Figure 3. These vent and fill structures differ only in that electrical connector 54 is required only for tube 130. Tube 130 (and 130') is preferably of stainless steel in order to minimize thermal conductivity from the liquid helium reservoir to the exterior of the cryostat. Tube 130 is shielded by coaxial tubes 132, 134, 136, and 138, each of which form part of the respective nested chambers 112, 114, 116, and 118.
Thermal transfer collar 133 ~and 133', not shown), preferably of aluminum, serves to transfer heat to the boil-off helium vapor ~assing through tube 130 (and 130'), thereby to maintain isothermal shell 112 at a fixed temperature.
Radiation shield 112 is preferably constructed of aluminum by conventional spinning techniques and defines an isothermal shell of temperature intermediate the secondary coolant (liquid nitrogen at 77.4K) and the primary coolant (liquid helium at 4.2K). For liquid nitrogen-liquid helium combinations the temperature of the I radiation shield 112 is optimized at about 50K. Heat is transferred to the radiation shield principally by radiation (and by conduction through mechanical bracing means described below) from the interior of surrounding shell 114 and heat is transferred from the radiation shield 112 to the helium vapor in the fill and vent tubes 130 and 130'-through aluminum contact collars 133 and 133' respectively, welded to fill and vent tubes 130 and 130' _ g _ ., . ,. .. ,.. ., . - , i 13i43 and to radiation shield 112. Thermal contact between tubes ~ 130 and 1~0' and their respective collars 133 and 133' occurs at a point where approximately 10 mw. of thermal power is supplied to the escaping helium vapor from radiation shield 112.
Radiation shield 112 is nested within surrounding isothermal shell 114 which is maintained at liquid nitrogen temperature by welded contact with liquid nitrogen reservoir 114'. The outer surface of isothermal body 114-114' is itself shielded by outer radiation shield 116 which is maintained at a temperature intermediate that of liquid nitrogen and room temperature in a manner described more fully below.
Hermetically sealed external vessel 118 encloses the cryostat structure and provides external mechanical and vacuum integrity.
Baffled apertures 135 and 137 are provided in radiation shields 112 and 116 as shown. A similar baffled aperture in shell 114, not visible in the section of Figure 2, provides communication between all interior spaces of the nested structure whereby these interior spaces are main-tained at a common pressure by evacuation through port 120.
The liquid nitrogen reservoir 114' and associated shell 114 are effectively insulated by cooling outer radiation shield 116 to a temperature intermediate that of liquid nitrogen and ambient temperature. Maintaining radiation shield 116 at preferably 173-183K is accomplished by providing a heat exchanger discussed below in tube 145 to afect thermal exchange between outer radiation shield ¦ 30 116 and an auxiliary refrigeration facility 140. An ¦ external mechanical refrigerator~ such as the Neslab ¦ Instruments, Inc., Crvocool CC-100, has been found 1~33 43 convenient for this purpose although similar equipment will undoubtedly serve ~s well. Turning now to Figure 5 the means by which the external refrigerati~s facility is coupled to the cryostat appears in greater detail.
An access port 142 (Fig. 2) in the top of containment vessel 118 is hermetically sealed by tube 143 which carries a well assembly for thermal access to outer radiation shield 116. An outer wall 144 and an inner conducting tube 144' for the well is formed of a tubing of low thermal conductivity, as for example stainless steel, and an inner contact tube 145 is constrùcted of thermally conductive tubing which is joined to outer radiation shield 116 in a one turn coil welded along the periphery of shield 116.
Inner and outer walls 144' and 144 are hermetically sealed to end plug 144'. Thermal linkage of the refrigerator i 140 to radiation shield 116 is accomplished by insertioninto cooling tube 145 of cold head 147 shown in greater detail in ~igure 6.
Cold head 147 comprises a single ended flexible bellows 148 of nickel plated brass or copper tubing having j a mounting flange 149 and a coaxial capillary tube 150.
Cold refrigerant from the refrigerator 140 flows through capillary 150 and returns along-the outside of capillary 150 through aperture in flange 149. The bellows serrations provide a large cooling area and the void between the bellows serrations and the inner wall of cooling tube 146 is filled with a 90%
menthanol,lO% water mixture to facilitate heat transfer between cooling tube 146 and cold head 147.
I Figure 4 is a section through the liquid nitrogen vent ¦ 30 and fill tube assembly 152. A thermally non-conductive ¦ central fill tube 153, preferably of stainless steel tubing, 0.005 inches in wall thickness, supports a thermal gradient '
It is an object of the present invention to achieve an improved cryostat for the containment of a liquified gas whereby the loss of such liquified gas from a cryostat due to the boiling of such liquified gas is minimized.
Accordingly, the present invention provides-in a cryostat wherein a first liquified gas is contained in a central vessel and said central vessel is surrounded by shielding means maintained at the temperature of another liquified gas of higher boiling point, said cryostat further comprising a containment vessel at ambient tempera-ture, said containment vessel comprising a wall portion having an interior surface spaced from the outer surface of said shielding means, the improvement comprising: a radiation shield disposed between the interior surface of said containment vessel and the outer surface of said shielding means; mechanical refrigerating means for main-taining said radiation shield at a temperature substantially ¦ intermediate said shielding means and am~ient temperature ¦ 30 during operation.
In a described embodiment the amount of liquid helium required for operation of~ a superconducting magnet is minimized and the interval between replenishments of the liquid helium is maximized.
In one embodiment of this invention a substantially spherical central vessel is provided to contain the liquified gas forming a primary coolant, whereby the ratio of surface area to volume of such vessel is minimized. The central vessel may be constructed of aluminum of such thickness that the thermal gradient introduced by the finite thermal conductivity of the necessary fill and vent tubes leading from the central vessel, and still be small enough to permit operation of superconducting apparatus only partly submerged in the liquified gas.
The central coolant reservoir may be surrounded by a radiation shield spaced from the central reservoir and maintained at a first intermediate temperature through vapor cooling provided by the boil-off from the liquified gas contained in the central reservoir.
In a described embodiment, the central'reservoir and its ~urround'ing radiation shield are enclosed by an isothermal surface defined by a second surrounding chamber j and a second reservoir is provided externally above the second surrounding chamber, and in thermal contact with the outer surface of the second chamber, whereby the second chamber and reservoir form an isothermal body maintained at i the temperature of a second liquified gas comprising the secondary coolant filling the second reservoir. An outer radiation shield is provided, enclosing the isothermal i body comprising the second reservoir and the second chamber I in contact therewith, such outer radiation shield maintained ¦ 30 at a temperature intermediate the second coolant and ambient temperature. The outer radiation shield is maintained at the desired temperature by an auxiliary refrigeration ~ 3~43 facility.
In a described embodiment the primary coolant (hereafter, liquid helium) is contained in a central reservoir having a substantially spherical shape. The central reservoir is formed of aluminum and has a kore through its centre defined by an aluminum cylindrical wall welded to the quasi-spherical reservoir. A superconducting solenoid is disposed within the central reservoir coaxial with the bore. In the embodiment the surface to volume ratio is minimized, reducing the area of the central reservoir for absorption of heat by radiation and permitting operation of the solenoid to continue when the level of liquid helium falls substantially below the top of the solenoid.
A radiation shield surrounding the helium reservoir is provided to establish a first isothermal surface inter-mediate the central reservoir and a surrounding second iso-thermal surface, the latter maintained at the temperature of a secondary coolant (hereinafter, liquid nitrogen). me radiation shield is maintained at about 50K through vapor cooling affected by the helium boil-off escaping up the fill and vent tubes with which the radiation shield is in therMal contact.
Surrounding the radiation shield and partially surrounding the fill and vent tubes, there is provided a secondary isothermal shell cooled by thermal contact with a liquid nitrogen reservoir disposed external the shell, above the region of the central reservoir. In this geometry the vent and fill tube from the central reservoir (partially surrounded by a cylindrical portion of the secondary iso-thermal shell) passes through a greater length of the secondary coolant reservoir as compared to prior art ~1~ 31~3 cryostats with conse~uently improved thermal isolation for the liquid helium reservoir.
The thermal isolation from ambient temperature of the secondary coolant reservoir and associated secondary iso-thermal shell is further improved in the embodiment by provision of an outer radiation shield surrounding the secondary coolant reservoir and associated isothermal chamber. This outer radiation shield is maintained at a temperature intermediate the secondary coolant and ambient temperature by means of an auxiliary refrigeration facility.
An outer hermetically sealed vessel encloses the outer radiation shield and the interior of the cryostat permitting the spaces between adjacent nested surfaces to be evacuated to a pressure of the order of 10 6 torr. In this way gas conduction and convection mechanisms are minimized for heat transport to the central reservoir.
The described embodiments virtually eliminate direct conduction losses between nested structures due to the mechanical support and internal bracing by replacing the bracing spokes of the prior art with bracing formed of polyester cord.
All of the walls forming the nested structure of the cryostat are constructed of aluminum, save for the fill and ven-t tubes of both the liquid nitrogen and helium reservoirs.
The aluminum surfaces are subject to a treatment which reduces radiant emissivity. Consequently, heat transport by radiation is further reduced between adjacent surfaces.
Embodiments of the invention will now be described, by way of example, with reference to the accompanying drawings in which:-Figure 1 is a schematic of an NMR spectrometer system.
Figure 2 is a top view of the cryostat of the '~ ' preferred embodiment.
Figure 3 i5 a section through the cryostat of Figure 2.
Figure 4 is a detail of the section of Figure 2.
Figure 5 is a detail in section of the cryostat of Figure 2.
Figure 6 shows the cold head for thermal linkage to the refrigerator.
A superconducting NMR spectrometer system employs a cryostat l having room temperature access to the magnetic field created within the cryostat 1 in a manner more explicitly depicted belo~. A probe 5 containing a sample 7 is introduced through bore 3 for analysis. A transmitter 9, receiver 11 and control unit 13, data processing unit 15 and display means 17 form the complete spectrometer (exclusi~e of power supplying systems for initiating persistent currents for the magnet).
¦ Figure 2 is a top view of the preferred embodiment of the cryostat 1 of this invention. A bore 3 provides room temperature access to the magnetic field created by ¦ apparatus within cryostat l as described below.
Turning now to Figure 3, the cryostat 1 contains a superconducting solenoid assembly 50 within a central reservoir llO. Reservoir llO contains a primary coolant, preferably liquid helium, to maintain the superconducting state of the windings comprising solenoid assembly 50.
Leads from the solenoid windings, collectively denoted 52 terminate in a connector 54 for access to external current sources introduced in a manner to be described. Additional circuits comprising persistence switches for controlling transitions between the normal and superconducting state for selected windings are not shown. These circuits and _ 7 _ ` 3~
preferred persistence switche~ are further described in, and form the subject matter of respective United States Patents Nos. 4,164,777, and 4,173,775 assigned to the assignees of the present invention. The solenoid assembly 50 is not within the scope of the present invention and is ~urther described in United States Patent No. 4,180,779 assigned to the assignee of the present invention.
Central coolant reservoir 110 is formed from 0.125"
10 - aluminum to a substantially spherical shape as shown, by spinning techniques well known in the art. In the preferred embodiment, reservoir 110 has a coolant capacity of about 25 litres. Reservoir 110 is further characterized by a bore formed by cylindrical wall 111, welded-to reservoir 110. Room temperature access is thereby afforded to the magnetic field of solenoid assembly 50. Reservoir 110 is isolated from ambient temperature by means of a plurality of consecutively nested surrounding chambers 112, 114, 116, and 118 having coaxial bores defined by cylindrical tubes 113, 115, 117, and 119, respectively. The wall thickness of each of the respective cylindrical coaxial tubes is determined by the heat load on each and varies from 0.02"
to 0.049". The spaces between chambers 112, 114, 116, and 118 are mutually communicating in a manner described below and evacuated through pump-out port 120 in exterior chamber 118 to achieve a very low pressure, as for example 10 6 torr to minimize thermal conduction between adjacent nested surfaces through gas conductivity and convection.
A secondary coolant reservoir 114', is disposed above central reservoir 110 and in thermal contact with chamber 114 whereby chamber 114, preferably formed of nominal 0.190" aluminum, comprises a shell at the temperature of - B -. . :) -~1~ 3:1~`3 the secondary coolant, preferably liquid nitrogen.
Returning to Figure 2, two vent and fill tubes 130 and 130' are required for access to the central reservoir.
These are constructed of 5/8" I.D. stainless steel having a wall thickness of 0.005". Two such vent and fill tubes 130 and 130' appear in Figure 1 and one such structure is disclosed in greater detail in Figure 3. These vent and fill structures differ only in that electrical connector 54 is required only for tube 130. Tube 130 (and 130') is preferably of stainless steel in order to minimize thermal conductivity from the liquid helium reservoir to the exterior of the cryostat. Tube 130 is shielded by coaxial tubes 132, 134, 136, and 138, each of which form part of the respective nested chambers 112, 114, 116, and 118.
Thermal transfer collar 133 ~and 133', not shown), preferably of aluminum, serves to transfer heat to the boil-off helium vapor ~assing through tube 130 (and 130'), thereby to maintain isothermal shell 112 at a fixed temperature.
Radiation shield 112 is preferably constructed of aluminum by conventional spinning techniques and defines an isothermal shell of temperature intermediate the secondary coolant (liquid nitrogen at 77.4K) and the primary coolant (liquid helium at 4.2K). For liquid nitrogen-liquid helium combinations the temperature of the I radiation shield 112 is optimized at about 50K. Heat is transferred to the radiation shield principally by radiation (and by conduction through mechanical bracing means described below) from the interior of surrounding shell 114 and heat is transferred from the radiation shield 112 to the helium vapor in the fill and vent tubes 130 and 130'-through aluminum contact collars 133 and 133' respectively, welded to fill and vent tubes 130 and 130' _ g _ ., . ,. .. ,.. ., . - , i 13i43 and to radiation shield 112. Thermal contact between tubes ~ 130 and 1~0' and their respective collars 133 and 133' occurs at a point where approximately 10 mw. of thermal power is supplied to the escaping helium vapor from radiation shield 112.
Radiation shield 112 is nested within surrounding isothermal shell 114 which is maintained at liquid nitrogen temperature by welded contact with liquid nitrogen reservoir 114'. The outer surface of isothermal body 114-114' is itself shielded by outer radiation shield 116 which is maintained at a temperature intermediate that of liquid nitrogen and room temperature in a manner described more fully below.
Hermetically sealed external vessel 118 encloses the cryostat structure and provides external mechanical and vacuum integrity.
Baffled apertures 135 and 137 are provided in radiation shields 112 and 116 as shown. A similar baffled aperture in shell 114, not visible in the section of Figure 2, provides communication between all interior spaces of the nested structure whereby these interior spaces are main-tained at a common pressure by evacuation through port 120.
The liquid nitrogen reservoir 114' and associated shell 114 are effectively insulated by cooling outer radiation shield 116 to a temperature intermediate that of liquid nitrogen and ambient temperature. Maintaining radiation shield 116 at preferably 173-183K is accomplished by providing a heat exchanger discussed below in tube 145 to afect thermal exchange between outer radiation shield ¦ 30 116 and an auxiliary refrigeration facility 140. An ¦ external mechanical refrigerator~ such as the Neslab ¦ Instruments, Inc., Crvocool CC-100, has been found 1~33 43 convenient for this purpose although similar equipment will undoubtedly serve ~s well. Turning now to Figure 5 the means by which the external refrigerati~s facility is coupled to the cryostat appears in greater detail.
An access port 142 (Fig. 2) in the top of containment vessel 118 is hermetically sealed by tube 143 which carries a well assembly for thermal access to outer radiation shield 116. An outer wall 144 and an inner conducting tube 144' for the well is formed of a tubing of low thermal conductivity, as for example stainless steel, and an inner contact tube 145 is constrùcted of thermally conductive tubing which is joined to outer radiation shield 116 in a one turn coil welded along the periphery of shield 116.
Inner and outer walls 144' and 144 are hermetically sealed to end plug 144'. Thermal linkage of the refrigerator i 140 to radiation shield 116 is accomplished by insertioninto cooling tube 145 of cold head 147 shown in greater detail in ~igure 6.
Cold head 147 comprises a single ended flexible bellows 148 of nickel plated brass or copper tubing having j a mounting flange 149 and a coaxial capillary tube 150.
Cold refrigerant from the refrigerator 140 flows through capillary 150 and returns along-the outside of capillary 150 through aperture in flange 149. The bellows serrations provide a large cooling area and the void between the bellows serrations and the inner wall of cooling tube 146 is filled with a 90%
menthanol,lO% water mixture to facilitate heat transfer between cooling tube 146 and cold head 147.
I Figure 4 is a section through the liquid nitrogen vent ¦ 30 and fill tube assembly 152. A thermally non-conductive ¦ central fill tube 153, preferably of stainless steel tubing, 0.005 inches in wall thickness, supports a thermal gradient '
3~'~3 between the 77K temperature of liquid nitrogen reservoir 114' and ambient temperature over a distance of about
4 1/4". This tube is shielded by concentric tubes 154 and 155, respectively the nitrogen fill tube shield portions of outer radiation shield 116 and containment vessel 118. Aluminum end contact tubes 156, brazed to central fill tube 153 provide strength and a surface for welding ~urther to reservoir 114' and outside shield tube 155. A thermally conductive collar 157 contacts the central nitrogen fill tube 153 at a point along the thermal gradient where the heat transfer from outer radiation shield 116 to liquid nitrogen escaping up the central fill tube 153 is sufficient to maintain the outer radiation shield 116 at a desired temperature intermediate the temperature of liquid nitrogen and ambient temperature.
In similar fashion, helium fill and vent tube 130 (see . Figure 3) is thermally joined to liquid nitrogen reservoir 114' through heat transfer collar 158 and at a point along the thermal gradient of tube 130 another thermal - 20 collar 159 provides a heat transfer path from outer radiation shield 116 to the vapor escaping up tube 130.
The temperature of the thermal contact point of collar 159 .is selected to be substantially equal to that of collar 157 on the nitrogen fill and vent tube 153. A second helium fill and vent tube 130' not shown provides another thermal contact point, the details of which do not differ from that shown and described above. Thus, in addition to the cooling provided by refrigerator 140, outer radiation shield 116 is vapor cooled in exact analogy to the cooling 1 30 of radiation shield 112 as described previously.
¦ The central reservoir 110, radiation shield 112, liquid nitrogcn reservoir 114 ' and shel l 114, oute r radiation - , . .. .. ...
shield 116 and containment vessel 118 are fabricated from an aluminum alloy, preferably alloy 1100-0. This alloy is well-~nown and commercially available from several manufacturers. After the above-listed bodies have been formed by spinning, the interior adjacent facing surfaces of the respective bodies are polished and subject to a surface treatment technique which lowers the emissivity of these surfaces by 35%. In this manner, heat transport by radiation to the liquid helium central reservoir is drastically reduced.
The nested structure of a cryostat such as exhibited by the present invention requires an internal mechanical support to maintain the centering of the various shells, and the coaxial alignments and close tolerances therebetween.
It is important that the coaxial tubes 111, 113, 115, 117 and 119 forming the bore for room temperature access be ; precisely located. It is equally important to constrain the nested structure during shipment of the apparatus because the thermal-mechanical specifications of certain components result in a measure of mechanical fragility. It is clear that any mechanical constraint linking adjacent I structures must per~orce result in a conductive path for ¦ heat transport; consequently, a very low thermal conductivity is essential. Moreover, high strength is essential to provide i the required mechanical constraints. Braided polyester cord has been found to be an ideal material for this purpose, not-withstanding the precision required for alignment of the ~ components of the cryostat.
¦ Returning to Figure 3, it will be perceived that adjacent members of the nested structures 110, 112, 114 and 114', 116 and 118 are subject to constraints through polyester cord centering spokes. In the interest of clarity 11~3~4~
only a representative spoke 160 is described in detail.
- The spoke itself is formed of polyester cord, preferably of braided Dacron. The strength and thermal conductivity parameter of this material are known and exhibit the highest known ratio of strength to thermal conductivity.
The polyester material which has been employed in the preferred embodiment is supplied as #2 Corsair DB by Rocky Mount Cord Company of Rocky Mount, No. Carolina.
A loop is formed at each end secured to the running length of the cord by aluminum sleeves 162. One of the loops formed thereby is affixed to an eye-bolt 164 secured to one of the adjacent pairs of shells and the other loop engages a snubbing post 1~6 welded to the other ad~acent shell. These polyester spokes are disposed at regular intervals for example 120 about the axis of bore 3.
The representative spacing between adjacent coaxial bore tubes 111-113, 113-115, 115-117, and 117-119 range from 0.178" to 0.16" for the widest and most narrowly-spaced Of the aforementioned bore tube pairs; it is 20 - desired to maintain these bore tubes mounted coaxial with one another and with solenoid assembly 50 to a precision substantially better than 0.03". This has been accomplished with the aforementioned polyester spokes with resulting additional improvement in the shipping properties of the;
apparatus at room temperature. Stainless steel spokes properly dimensioned for operating conditions in the liquid helium-liquid nitrogen temperature range are under substantial tensile stresses at room temperature. Such rigid spokes which would exhibit thermal conductance comparable to the spokes of the present invention are known to be highly susceptible to failure due to shock and vibration. In contrast, the polyester tensile loaded 11~314~
spokes of the present invention exhibit a degree of stretch at room temperature during shipment. The bore tubes are thereby permitted to touch when subject to lateral shock and vibration. For shipment purposes, a mandrel slip fit to the central bore, prevents permanent deformation of the several coaxial bore tubes in collision.
Precise location of the components is facilitated by the behaviour of the coefficient of expansion of the spoke material of the present invention in the temperature range from liquid helium to am~ient. As a result of the present invention, it has been found that the coefficient of expansion of the subject material which is normal in behaviour to about -25C anomalously changes sign and the material expands as the temperature is further reduced.
A very low net thermal expansion is thereby obtained for this material.
The cryostat of the preferred embodiment achieves very substantial improvement over the prior art in consumption of the coolants. For example, the liquid helium boil-off rate measured for one prior art cryostat amounts to 30 cc/hr whereas the preferred embodiment of the instant invention exhibits a measured boil-off rate of about 6 cc/hr. m e low boil-off rate conjoined with ; the geometry of the central reservoir 110 yields an extended mean time between replenishment of liquid helium of about 120 days, wherein about 20.5 liters of liquid helium are consumed. A superconducting NMR spectrometer having a magnet of comparable characteristics requires ~ liquid helium replenishment at intervals of 8 days and i 30 consumes about 86.4 liters of liquid helium in the same 120 day period.
The extended mean time between filling of the central ~
'~ - 15 -~1~3~3 reservoir 110 is achieved in part because the central reservoir 110 has a substantially spherical shape. In the present invention the central reservoir 110 is fabricated of aluminum of sufficiently heavy gauge that the thermal gradient from top to bottom of the central reservoir ~due to heat conducted down fill and vent tubes 130 and 130' and radiation from shield 112) is so xeduced that the reservoir 110 is isothermal independent of the level of liquid helium contained therein. It has been found that in this reservoir the liquid helium level can be allowed to drop well below the top of the superconducting solenoid without adverse effect upon the operation of the solenoid. The solenoid assembly 50, having a length of about 10 inches, has been operated satisfactorily with liquid helium level reduced to about 3 inches in the reservoir 110 exposing about 7 inches of the solenoid assembly 50.
For the liquid nitrogen coolant the rate of - consumption is also reduced and the mean interval between replenishment extended. The liquid nitrogen boil-off rate is measured at about 20 cc/hour with the outer radiation shield cooled to 173-183K. With the liquid nitrogen reservoir insulated from ambient temperature without benefit of cooling of the radiation shield, the liquid nitrogen boil-off rate increases to 80 cc/hr and would increase to 160 cc/hr without any shield. The outer radiation shield cooled to the above preferred temperature reduces the thermal transfer by radiation to the liquid nitrogen reservoir 114' by approximately 88% in comparison with an unshielded reservoir. This is a consequence of the Stefan-Boltzmann radiation law which states that the energy radiated (or absorbed) in~unit time by an emissive ~3143 body is proportional to the difference in the fourth powers of the absolute temperatures of the radiating (absorbing~ body and that o its surroundings.
The cryostat of the present invention has been described particularly in terms of a liquid nitrogen shielded liquid helium cooled superconducting magnet for an NMR spectrometer. The inventive contributions to cryostat design disclosed herein transcend the specific application and employment of particular coolants. These inventive contributions may be directed to cryostats housing apparatus used for applying a variety of low temperature phenomena and to other superconductive devices.
Since many changes can be made in the above construction and many apparently widely differing embodiments of this invention could be made without departingfrom the scope thereof, is intended that all matter contained in the above description and shown in the encompanying drawing shall be interpreted as illustrative and not in a limiting sense.
.
!
I
- 17 ~
In similar fashion, helium fill and vent tube 130 (see . Figure 3) is thermally joined to liquid nitrogen reservoir 114' through heat transfer collar 158 and at a point along the thermal gradient of tube 130 another thermal - 20 collar 159 provides a heat transfer path from outer radiation shield 116 to the vapor escaping up tube 130.
The temperature of the thermal contact point of collar 159 .is selected to be substantially equal to that of collar 157 on the nitrogen fill and vent tube 153. A second helium fill and vent tube 130' not shown provides another thermal contact point, the details of which do not differ from that shown and described above. Thus, in addition to the cooling provided by refrigerator 140, outer radiation shield 116 is vapor cooled in exact analogy to the cooling 1 30 of radiation shield 112 as described previously.
¦ The central reservoir 110, radiation shield 112, liquid nitrogcn reservoir 114 ' and shel l 114, oute r radiation - , . .. .. ...
shield 116 and containment vessel 118 are fabricated from an aluminum alloy, preferably alloy 1100-0. This alloy is well-~nown and commercially available from several manufacturers. After the above-listed bodies have been formed by spinning, the interior adjacent facing surfaces of the respective bodies are polished and subject to a surface treatment technique which lowers the emissivity of these surfaces by 35%. In this manner, heat transport by radiation to the liquid helium central reservoir is drastically reduced.
The nested structure of a cryostat such as exhibited by the present invention requires an internal mechanical support to maintain the centering of the various shells, and the coaxial alignments and close tolerances therebetween.
It is important that the coaxial tubes 111, 113, 115, 117 and 119 forming the bore for room temperature access be ; precisely located. It is equally important to constrain the nested structure during shipment of the apparatus because the thermal-mechanical specifications of certain components result in a measure of mechanical fragility. It is clear that any mechanical constraint linking adjacent I structures must per~orce result in a conductive path for ¦ heat transport; consequently, a very low thermal conductivity is essential. Moreover, high strength is essential to provide i the required mechanical constraints. Braided polyester cord has been found to be an ideal material for this purpose, not-withstanding the precision required for alignment of the ~ components of the cryostat.
¦ Returning to Figure 3, it will be perceived that adjacent members of the nested structures 110, 112, 114 and 114', 116 and 118 are subject to constraints through polyester cord centering spokes. In the interest of clarity 11~3~4~
only a representative spoke 160 is described in detail.
- The spoke itself is formed of polyester cord, preferably of braided Dacron. The strength and thermal conductivity parameter of this material are known and exhibit the highest known ratio of strength to thermal conductivity.
The polyester material which has been employed in the preferred embodiment is supplied as #2 Corsair DB by Rocky Mount Cord Company of Rocky Mount, No. Carolina.
A loop is formed at each end secured to the running length of the cord by aluminum sleeves 162. One of the loops formed thereby is affixed to an eye-bolt 164 secured to one of the adjacent pairs of shells and the other loop engages a snubbing post 1~6 welded to the other ad~acent shell. These polyester spokes are disposed at regular intervals for example 120 about the axis of bore 3.
The representative spacing between adjacent coaxial bore tubes 111-113, 113-115, 115-117, and 117-119 range from 0.178" to 0.16" for the widest and most narrowly-spaced Of the aforementioned bore tube pairs; it is 20 - desired to maintain these bore tubes mounted coaxial with one another and with solenoid assembly 50 to a precision substantially better than 0.03". This has been accomplished with the aforementioned polyester spokes with resulting additional improvement in the shipping properties of the;
apparatus at room temperature. Stainless steel spokes properly dimensioned for operating conditions in the liquid helium-liquid nitrogen temperature range are under substantial tensile stresses at room temperature. Such rigid spokes which would exhibit thermal conductance comparable to the spokes of the present invention are known to be highly susceptible to failure due to shock and vibration. In contrast, the polyester tensile loaded 11~314~
spokes of the present invention exhibit a degree of stretch at room temperature during shipment. The bore tubes are thereby permitted to touch when subject to lateral shock and vibration. For shipment purposes, a mandrel slip fit to the central bore, prevents permanent deformation of the several coaxial bore tubes in collision.
Precise location of the components is facilitated by the behaviour of the coefficient of expansion of the spoke material of the present invention in the temperature range from liquid helium to am~ient. As a result of the present invention, it has been found that the coefficient of expansion of the subject material which is normal in behaviour to about -25C anomalously changes sign and the material expands as the temperature is further reduced.
A very low net thermal expansion is thereby obtained for this material.
The cryostat of the preferred embodiment achieves very substantial improvement over the prior art in consumption of the coolants. For example, the liquid helium boil-off rate measured for one prior art cryostat amounts to 30 cc/hr whereas the preferred embodiment of the instant invention exhibits a measured boil-off rate of about 6 cc/hr. m e low boil-off rate conjoined with ; the geometry of the central reservoir 110 yields an extended mean time between replenishment of liquid helium of about 120 days, wherein about 20.5 liters of liquid helium are consumed. A superconducting NMR spectrometer having a magnet of comparable characteristics requires ~ liquid helium replenishment at intervals of 8 days and i 30 consumes about 86.4 liters of liquid helium in the same 120 day period.
The extended mean time between filling of the central ~
'~ - 15 -~1~3~3 reservoir 110 is achieved in part because the central reservoir 110 has a substantially spherical shape. In the present invention the central reservoir 110 is fabricated of aluminum of sufficiently heavy gauge that the thermal gradient from top to bottom of the central reservoir ~due to heat conducted down fill and vent tubes 130 and 130' and radiation from shield 112) is so xeduced that the reservoir 110 is isothermal independent of the level of liquid helium contained therein. It has been found that in this reservoir the liquid helium level can be allowed to drop well below the top of the superconducting solenoid without adverse effect upon the operation of the solenoid. The solenoid assembly 50, having a length of about 10 inches, has been operated satisfactorily with liquid helium level reduced to about 3 inches in the reservoir 110 exposing about 7 inches of the solenoid assembly 50.
For the liquid nitrogen coolant the rate of - consumption is also reduced and the mean interval between replenishment extended. The liquid nitrogen boil-off rate is measured at about 20 cc/hour with the outer radiation shield cooled to 173-183K. With the liquid nitrogen reservoir insulated from ambient temperature without benefit of cooling of the radiation shield, the liquid nitrogen boil-off rate increases to 80 cc/hr and would increase to 160 cc/hr without any shield. The outer radiation shield cooled to the above preferred temperature reduces the thermal transfer by radiation to the liquid nitrogen reservoir 114' by approximately 88% in comparison with an unshielded reservoir. This is a consequence of the Stefan-Boltzmann radiation law which states that the energy radiated (or absorbed) in~unit time by an emissive ~3143 body is proportional to the difference in the fourth powers of the absolute temperatures of the radiating (absorbing~ body and that o its surroundings.
The cryostat of the present invention has been described particularly in terms of a liquid nitrogen shielded liquid helium cooled superconducting magnet for an NMR spectrometer. The inventive contributions to cryostat design disclosed herein transcend the specific application and employment of particular coolants. These inventive contributions may be directed to cryostats housing apparatus used for applying a variety of low temperature phenomena and to other superconductive devices.
Since many changes can be made in the above construction and many apparently widely differing embodiments of this invention could be made without departingfrom the scope thereof, is intended that all matter contained in the above description and shown in the encompanying drawing shall be interpreted as illustrative and not in a limiting sense.
.
!
I
- 17 ~
Claims (2)
1. In a cryostat wherein a first liquified gas is contained in a central vessel and said central vessel is surrounded by shielding means maintained at the temperature of another liquified gas of higher boiling point, said cryostat further comprising a containment vessel at ambient temperature, said containment vessel comprising a wall portion having an interior surface spaced from the outer surface of said shielding means, the improvement comprising:
a radiation shield disposed between the interior surface of said containment vessel and the outer surface of said shielding means;
mechanical refrigerating means for maintaining said radiation shield at a temperature substantially intermediate said shielding means and ambient temperature during operation.
a radiation shield disposed between the interior surface of said containment vessel and the outer surface of said shielding means;
mechanical refrigerating means for maintaining said radiation shield at a temperature substantially intermediate said shielding means and ambient temperature during operation.
2. The apparatus of claim 1 wherein said mechanical refrigerating means comprises, heat transfer means communicating from said mechanical refrigerating means to said shielding means, and said containment vessel comprises a conduit through which conduit said heat transfer means maintains thermal contact between said radiation shield and said mechanical refrigerating means.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA362,712A CA1107633A (en) | 1978-02-21 | 1980-10-17 | Cryostat with external refrigerator for superconducting nmr spectrometer |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US87928978A | 1978-02-21 | 1978-02-21 | |
US879,289 | 1978-02-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1103143A true CA1103143A (en) | 1981-06-16 |
Family
ID=25373826
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA321,936A Expired CA1103143A (en) | 1978-02-21 | 1979-02-20 | Cryostat with refrigerator for superconduction nmr spectrometer |
Country Status (3)
Country | Link |
---|---|
JP (1) | JPS54126089A (en) |
CA (1) | CA1103143A (en) |
FR (1) | FR2417734A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4212169A (en) * | 1978-02-21 | 1980-07-15 | Varian Associates, Inc. | Cryostat for superconducting NMR spectrometer |
DE3022802C2 (en) * | 1980-06-19 | 1982-11-11 | Deutsche Forschungs- Und Versuchsanstalt Fuer Luft- Und Raumfahrt E.V., 5300 Bonn | Device for storing liquid hydrogen |
US4492090A (en) * | 1983-09-19 | 1985-01-08 | General Electric Company | Cryostat for NMR magnet |
JP4939039B2 (en) * | 2005-11-17 | 2012-05-23 | 株式会社 フジヒラ | Cryostat |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3155265A (en) * | 1964-11-03 | Thermal stress equalizing support system | ||
FR1448147A (en) * | 1965-06-16 | 1966-08-05 | Centre Nat Rech Scient | Cryostat adaptable in particular to a chi-ray diffractometer |
FR2071316A5 (en) * | 1969-12-24 | 1971-09-17 | Air Liquide | |
US3698200A (en) * | 1970-12-16 | 1972-10-17 | Air Prod & Chem | Cryogenic storage dewar |
-
1979
- 1979-02-20 CA CA321,936A patent/CA1103143A/en not_active Expired
- 1979-02-21 JP JP1855879A patent/JPS54126089A/en active Granted
- 1979-02-21 FR FR7904407A patent/FR2417734A1/en active Granted
Also Published As
Publication number | Publication date |
---|---|
FR2417734B1 (en) | 1984-05-25 |
FR2417734A1 (en) | 1979-09-14 |
JPH0122578B2 (en) | 1989-04-27 |
JPS54126089A (en) | 1979-09-29 |
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