EP0803687B1 - Kryostat für Tiefsttemperatur-Kälteanlage und Kälteanlagen mit einem solchen Kryostat - Google Patents

Kryostat für Tiefsttemperatur-Kälteanlage und Kälteanlagen mit einem solchen Kryostat Download PDF

Info

Publication number
EP0803687B1
EP0803687B1 EP19970400898 EP97400898A EP0803687B1 EP 0803687 B1 EP0803687 B1 EP 0803687B1 EP 19970400898 EP19970400898 EP 19970400898 EP 97400898 A EP97400898 A EP 97400898A EP 0803687 B1 EP0803687 B1 EP 0803687B1
Authority
EP
European Patent Office
Prior art keywords
cryostat
gas
cooler
piston
regenerator
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 - Lifetime
Application number
EP19970400898
Other languages
English (en)
French (fr)
Other versions
EP0803687A1 (de
Inventor
Patrick Curlier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales Cryogenie SA
Original Assignee
Thales Cryogenie SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Thales Cryogenie SA filed Critical Thales Cryogenie SA
Publication of EP0803687A1 publication Critical patent/EP0803687A1/de
Application granted granted Critical
Publication of EP0803687B1 publication Critical patent/EP0803687B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/14Compression 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
    • F25B9/145Compression 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/14Compression 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/003Gas cycle refrigeration machines characterised by construction or composition of the regenerator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/14Compression machines, plants or systems characterised by the cycle used 
    • F25B2309/1406Pulse-tube cycles with pulse tube in co-axial or concentric geometrical arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/14Compression machines, plants or systems characterised by the cycle used 
    • F25B2309/1407Pulse-tube cycles with pulse tube having in-line geometrical arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/14Compression machines, plants or systems characterised by the cycle used 
    • F25B2309/1421Pulse-tube cycles characterised by details not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/14Compression machines, plants or systems characterised by the cycle used 
    • F25B2309/1424Pulse tubes with basic schematic including an orifice and a reservoir
    • F25B2309/14241Pulse tubes with basic schematic including an orifice reservoir multiple inlet pulse tube

Definitions

  • the present invention relates to the design and production of cryogenic coolers which works a working gas following a thermodynamic cycle in closed circuit between a compression chamber and a expansion chamber, through a thermal accumulator said regenerator, which ensures a recovery exchange between compressed hot gas and expanded cold gas.
  • coolers conventionally include a pressure oscillator controlled to vary the volume of the compression chamber, and a cold finger ending with the expansion chamber, in thermal contact with an element to be cooled, placed at the bottom of an envelope thermal insulation.
  • the element to be cooled is commonly an electronic component that must be kept in operation at temperatures between 60 ° K and 200 ° K, in particular to improve the signal to noise.
  • cryogenic coolers of the type in question are successful each growing day, mainly when they are designed to be manufactured at low cost in forms incorporating the pressure oscillator with the cold finger in one mechanical assembly no longer needing external pipes to close the working gas circuit.
  • the present invention is mainly offers to make available to users a cryostat which is not limited to an envelope insulating capable of receiving the cold finger from the cooler, but which incorporates part of its essential organs, in a form allowing their interchangeable adaptation to different configurations.
  • a cooler cryostat cryogenic produced according to the invention adapts easily, in accordance with its interchangeable character, both at a pulsed gas tube configuration than a Stirling cycle, and that driving the oscillator of pressure goes through a rotary type drive to crankshaft or linear type, according to the expressions used by those skilled in the art, as they are repeated in particular in the article already cited.
  • the invention allows also to make significant improvements to the construction chillers incorporating such a cryostat and their driving style.
  • the resulting benefits relate in particular to the combination of the cryostat with a pressure oscillator in a relevant embodiment of a pulsed gas tube configuration.
  • cryostats have the advantage of being particularly suitable well to the respective operating modes of two types of coolers and improve their clean performance.
  • This is particularly the case with the provisions recommended for the regenerator, which is responsible to absorb and release heat, alternatively, by compared to the gas passing through it.
  • This is also the case an exchanger advantageously provided in a cold zone, at level of the relaxation room, to favor the transfer towards the component to be cooled, as well as for a exchanger located in hot zone and under pressure which is especially useful in gas type coolers pulsed, to favor a heat loss towards outside.
  • the invention more specifically relates to a cryostat for cryogenic cooler using a closed working gas circuit between a compression located in a pressure oscillator housing associated and a relaxation room located at the bottom of the cryostat, in heat exchange situation with a component to be cooled, comprising inside an envelope thermal insulation, integral with a mounting base on said housing, a thermal regenerator interposed on the working gas circuit.
  • This regenerator is in annular arrangement around an extending axial volume between a cold exchanger which is in thermal contact with the component to be cooled and makes the regenerator communicate with said axial volume at the bottom of the cryostat.
  • the cryostat also has a gas distribution ring in said regenerator, at the head of the cryostat, from a conduit drilled through the base for connection to the chamber compression.
  • the timing ring is formed by a central piece mounting through said base axially at its center. Said central part is mounted removably in said base, in particular by tight screwing.
  • At least one channel is advantageously provided passage of gas under controlled flow between a tank gas buffer formed inside the oscillator housing pressure, and the internal axial volume of the cryostat which works in gas tube. It is also advantageous to add one or more other flow-controlled channels allowing hot gas to be drawn directly at the outlet compression, at the timing ring to the regenerator.
  • the internal volume is at the contrary occupied by the displacer piston, which is preferably solid, made of a weak material thermal conductivity, and which leaves only the volume of the expansion chamber at the bottom of the cryostat.
  • the central piece is made integral with a central tube limiting said axial volume.
  • This tube is then advantageously of the same internal diameter as the axial bore of the model intended for connection of the cryostat to a cooler Stirling cycle. It can therefore constitute either the tube containing the pulsed gas in the first model, namely the guide tube of the cooler displacement piston in the second case.
  • the cryostat is associated with the cryostat a hot exchanger, positioning in the internal volume at the top of the cryostat. Its role is located in the evacuation of calories which takes place by heat loss to the outside through the base and the casing of the compressor part of the cooler, made for this purpose of thermally conductive material. It is especially useful in the cooler variant with pulsed gas tube, taking into account the heat to be evacuated in gas tube outlet, which adds to the stored heat by the gas back from the regenerator.
  • the invention foresees, according to a secondary characteristic, that one can apply advantageously with others in any operating combination, to use a geometry structure of revolution, alternating around the axis of the cryostat, in a daisy arrangement, massive areas in material good thermal conductor and void areas open to the passage of gas. As a result, these areas are in particular on horseback, on both sides, in relation to a centering shoulder at the end of the central tube.
  • piloting means comprising a crankshaft actuating a transmission mechanism of movement by movable ball bearing in a groove formed transversely outside said piston.
  • the arrangement ring of the regenerator lends itself particularly well to a manufacture from a sheet wound on itself.
  • the invention makes it possible to significantly improve the efficiency of the heat exchanges sought, compared to stacks of conventional grids or balls, in using for this a sheet of suitable material, which has been previously machined, in particular by photolithographic process, so as to form longitudinal strips with smooth surfaces and transverse bars in extra thickness occasionally joining the strips successive.
  • the different bands are succeed the length of the regenerator. They form annular smooth surface layers intersected by intervals between bands and bars inserted between the layers help to distribute the flow in all directions at each cross section level.
  • the cryostat of the figure 1 is used in combination with a pressure oscillator either to constitute a cryogenic cooler of the pulsed gas according to Figure 6, or alternatively to constitute a Stirling cycle type cooler as shown in Figure 5.
  • a pressure oscillator either to constitute a cryogenic cooler of the pulsed gas according to Figure 6, or alternatively to constitute a Stirling cycle type cooler as shown in Figure 5.
  • the cooler thus constituted is of compact construction, the cryostat and pressure oscillator being integrated in one same mechanical assembly.
  • cryostat is not limited, as in the embodiments known, to a thermal insulation envelope intended to receive a cold finger previously formed in all its functional organs necessary for the implementation work of the thermodynamic cycle of the working gas.
  • the passive functional organs which are not subject to displacement during operation, are permanently installed in the cryostat, the latter being constructed so that it can be connected alternately at the user's choice, at the housing of an oscillator pressure either from a specific cooler for implementation of a Stirling cycle, ie of a cooler of the pulsed gas tube type.
  • regenerator 5 with its own envelopes, including an outer envelope which is then separate from the inner wall 2 of the thermal insulation envelope and / or an internal envelope which is then added against the tube central 3.
  • this exchanger 8 which constitutes in operation the cold exchanger of the cooler.
  • this exchanger is designed and arranged to facilitate the transfer of cooling capacity resulting from the expansion of the work towards a component to be cooled 21, while ensuring pneumatic communication allowing the passage of gas of work between the bottom of the axial volume 6 and the space ring occupied by the regenerator 5.
  • the intermediate shell of the cryostat of the invention constituted by the wall 2, is closed at its end lower, at the bottom of the cryostat, by a transverse plate 22 against which the cold exchanger 8 is affixed.
  • the component 21 On its opposite side to this exchanger is mounted the component 21, generally by simple bonding.
  • an electronic component 21 for example a optoelectronic detector
  • an electrical distribution ring 23 of which the conductive parts pass through watertight bushings through the outer wall of the insulation jacket thermal 1, as well as conductive wires 24 which then connect to component 21.
  • the envelope 1 as a whole has the function of limit heat losses by radiation or convection to level of organs involved in the thermodynamic cycle of the complete cooler in the cold zone thereof.
  • a quality of stainless steel corresponding to a alloy with low thermal conductivity adapted to be compatible with the working gas used, which is preferably helium in the case of the regenerator at metallic foil rolled up as described below.
  • the outer wall of the envelope 1 is produced also in stainless steel, or possibly in one appropriate quality of glass, for economic reasons.
  • the base 4 At the head of the cryostat, at the upper end of the thermally insulating envelope 1 and of the regenerator 5, the base 4 is on the contrary in the hot zone of the cooler in operation, where there is also pressure working gas dynamics, subjected to pulsations of periodic pressures, printed by the moving parts of the cooler when the cryostat is connected to the housing 50 an associated pressure oscillator.
  • the base 4 there is a collar circular 16, pierced with holes for the passage of screws 48 fixing to the casing 50 of the cooler, which is connected by pressing on the upper face of the flange 16, opposite the thermal envelope 1.
  • a ring 17, forming part of the base 4 which ensures the centering of the two elements one inside the other.
  • the tight connection of these two elements (cryostat and pressure oscillator) vis-à-vis the outside is ensured by a seal 19, housed in an annular groove on the face upper part of the collar 16.
  • the base 4 delivers passage, in the axis of the system, to a central part 10, tightly screwed into the ring 17, which is internally threaded.
  • a throat hexagonal 41 formed in its upper planar face, serves to handling during assembly.
  • this central piece of the cryostat is designed in two different models which, by their external geometry, their dimensioning, and their functional design, are interchangeable in one same construction of cryostat. Both models are illustrated by FIG. 1 and by FIG. 2, depending on whether the cryostat 30 is mounted to be coupled with housings 50 or 60 from either of the two pressure oscillators in the two cooler variants shown on the Figures 6 and 5 respectively.
  • this central part therefore in in particular that bearing the reference 10 in FIG. 1, here consists of a single piece with the inner tube 3 cryostat.
  • this crown forms a distribution crown 71, for the annular distribution of the gas at the top of the regenerator 5. Consequently, this crown is placed above of it (in the vertical arrangement shown, cryostat under the casing 50), and more precisely at center of the base 4 in its main part formed by the flange 16.
  • the crown of distribution 71 has a circular groove 45, hollowed out in its underside, which abuts the regenerator 5. This groove communicates through orifices 46 with an annular chamber 43, extended upwards at 42, which is arranged externally in the part of the room central 10 located at the flange 16, between this part and the face opposite the base 4.
  • the central part 10 is shown in Figure 1 in the model suitable for a cooler TGP type illustrated in Figure 6.
  • the second model of central part of the cryostat, intended for a Stirling cycle cooler, is shown on the schematic representation in exploded layout of Figure 2.
  • the central part 20 is identical to the previous one externally, but internally, it simply comprises an axial bore 72, formed all along through it, at the same diameter as the tube 3 of which it extends the central volume.
  • the calibrated orifices of channels 11-12 are working, in a conventional manner in itself, like valves introducing pneumatic impedances.
  • Main channel 11 as well equipped in operation provides the useful phase shift between the pressure wave generated by the pressure oscillator and the resulting flow variations in the container tube pulsed gas.
  • Secondary impedance (channel 12) allows to bring a fraction of the periodic feed rate of the tube by taking it directly out of compression, by diversion of the circulation passing to through the regenerator and the tube. This decreases the load thermal on the regenerator and helps to improve the efficiency of the chiller, in the case of a gas cycle pulsed.
  • FIG. 1 finally shows an exchanger 9, located at hot zone in the central volume, at the crown distribution 71.
  • This hot exchanger can possibly be performed analogously to what will be described more far for the cold exchanger, the main thing being that in this variant embodiment of the cryostat of the invention, it complete the removal of excess calories from the thermodynamic cycle by completing, starting from the zone hot of the pulsed gas tube, heat losses outwardly occurring through the base 4, and incidentally from the associated pressure oscillator housing.
  • the thermal regenerator 5 is advantageously constituted, as it appears from Figures 1 and 3, so to fully play its role of thermal accumulator for the recovery taking place, in a conventional manner, between the working gas passing from the compression phase to the expansion phase and the working gas passing from the expansion during the compression phase.
  • regenerator comes in the form of a leaf continuous which is wound in a series of turns around the central tube 3 which limits the internal volume 6 of the regenerator, so as to fill, as completely as it is possible in industrial practice, the annular space between this tube 3, which forms its envelope ferrule internal, and its associated external envelope shell, constituted by the internal wall 2 of the insulating envelope 1.
  • Machining processes by photolithography which are known in themselves, are particularly interesting in this sense, insofar as they represent means particularly simple to implement for a limited cost price, when it comes to driving to the configuration illustrated by the detail in FIG. 3.
  • the sheet which is thus wound in contiguous consecutive turns forms a succession of separate longitudinal bands 27, which are oriented perpendicular to the axis of the cryostat and which are separated from each other by intervals 28.
  • Bars 26 are formed in excess thickness of the strips and across them in a perpendicular direction. They are evenly distributed over the entire length and leaf height and staggered, each joining two successive bands over the interval that separates them.
  • a regenerator thus constructed, we can cite as an example the case of a sheet 100 to 200 microns thick, hollowed out halfway through each side, for a regenerator from 2 to 3 millimeters in radial thickness.
  • the tapes and intervals between them can, for example, be of a same width, of the order of 50 to 100 microns.
  • the length transverse of the bars 26 can correspond, here again for example, at 1.5 times the repetition step of longitudinal strips 27, with a width of about half lesser and a distance between two successive bars offset, equivalent to about three times the width of each.
  • the invention thus makes it possible to take advantage of a relationship between local convective exchange and losses of longitudinal loads which, in the case of plates parallel to the axis of the cold finger, would be greater than the value that can be obtained by the usual stacks of grids or balls, however that in this form of practical realization, it ensures better distribution of the gas flow between the parallel layers of smooth surfaces.
  • barriers 26 which remain low dimensions compared to the length and thickness of the regenerative, also allows the introduction of an interrupt of the longitudinal flow between the strip layers successive from one end to the other of the regenerator, and thereby to stabilize the overall gas flow. Simultaneously, like these bars adjoin two adjacent layers of bands, we thanks to them a reduction in energy losses thermal by conduction in the longitudinal direction. Simultaneously, this ensures a reduction in energy losses thermal by conduction in the longitudinal direction.
  • regenerator 5 allows, particularly advantageously in the context of the present invention to obtain a relationship between the exchange local convective and longitudinal pressure drop very advantageous, while improving the flow distribution of gas between the parallel layers oriented longitudinally, up to recovery performance thermal at least equivalent, if not greater than those that we know get in known achievements by regenerators with stacked transverse grids or balls.
  • This cold exchanger is produced in accordance with this which emerges from Figures 1, 2 and 4, in a form called Daisy. It is constituted by a structure with geometry of revolution, which is made of a material strongly conductor such as copper or aluminum.
  • This structure alternates in a star around a central core 31, empty areas 32 hollowed out through its longitudinal thickness and massive zones 33 ensuring the thermal conduction. Both extend radially astride the shoulder 34, in part and from the end of the central tube 3. They leave therefore the gas circulate freely between the central volume 6 of the cryostat (or at least the expansion chamber remaining at the bottom of the cryostat in the case of a cooler according to the figure 5 applying a Stirling cycle), bypassing the lower end of the central tube 3 received in shoulder 34.
  • Such a miniature exchanger for example under 5 mm diameter and 3 mm thick, can be manufactured easily by electrochemical machining of a cylindrical bar, which is then cut into sections.
  • the core 31 can also be pierced with a empty passage in its center, and there is no need to leave a peripheral crown of material, contiguous continuously with the central tube 3.
  • FIG. 5 illustrates the combination of the cryostat of the previous figures, using the central part 20 of the Figure 2, with a pressure oscillator corresponding to the configuration of a Stirling cycle cooler, in which the piloting is with rotary motor.
  • the displacement piston 55 is axially movable in the internal volume 6 of the cryostat 30. It occupies almost everything volume, leaving no room at the bottom of the tube 3 which constitutes his guide, that the thickness of the expansion chamber, considerably enlarged in the figure compared to the practical reality.
  • Figure 6 uses an oscillator of pressure designed for a TGP type cooler including the casing 50 is connected to the cryostat around the central part 10 of the model in FIG. 1.
  • the mode of piloting is of rotary type.
  • the motor shaft is perpendicular to the axis of the system and, by an axis crankshaft off center 66, it involves an oscillating movement, a single piston 74.
  • the piston 74 is movable, vertically on the figure, in the axis of the cryostat, in a jacket formed at inside the housing 50.
  • the internal cage 68 On the offset axis 66 is mounted the internal cage 68 a ball bearing, the outer cage 67 of which is trapped in a rectilinear groove 75 dug laterally in the peripheral surface of the piston 74, perpendicular to its axis and to the plane of the figure. This provision ensures the reciprocating movement of the piston while immobilizing it in rotation.
  • the compression chamber 63 is formed between the upper end face of the piston and the casing 60. It is connected, as in the previous case, by a hole 62 and a conduit 61 to channel 39 opening into the chamber distribution of the cryostat.
  • the exchanger 8 here consists of lobes 77 of massive material in radiating arrangement around a core central 34. Between these lobes 77 are the passages of gases 78 which connect the lower end of the regenerator with the axial volume of the tube 3.
  • the gas flow tranquilization laminate which has already been discussed, is represented by a stack of perforated grids 81 mounted in section transverse of the tube 3 at this lower end. These grids can be retained by legs of tube 3, as shown, or just stuck between the end of the tube and the exchanger 8 in its central part limited by a tube centering shoulder 79 3. In all cases, the gas passing between the exchanger lobes is found to have cross the stack of grids.
  • This circulation is indicated by arrows in FIG. 8, which relates to another embodiment particularly advantageous especially since it facilitates a tranquilization of the gas flow as close as possible to the cold plate 22.
  • the cold exchanger is produced there in two parts 83 and 84 concentrically embossed one in the other; Each has its own material lobes heat exchange alternating with empty areas free to gas circulation. In other words, functionally the exchanger is therefore pierced with channels dividing into two crowns, one under regenerator 5, the other at the end of the tube 3.
  • the internal part 83 of the exchanger is shorter than the external part 84 which surrounds it and so that the end of the tube 3 comes center in the part 84 in abutment on the part 83.
  • a stack of grids 82 constitutes the laminated to calm the gas flow. These grids are interposed directly against the cold plate 22 between this and the two parts 83 and 84 of the exchanger. In case if necessary, they could be blocked in the exchanger on the outskirts, providing for this purpose a shoulder in the part 84 forming the annular ring of this exchanger.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Containers, Films, And Cooling For Superconductive Devices (AREA)

Claims (15)

  1. Kryostat für Tiefsttemperatur-Kühleinrichtung, der zwischen einer Verdichtungskammer, die sich in einem zugeordneten Druckoszillatorgehäuse befindet, und einer Entspannungskammer, die sich am Boden des Kryostaten befindet und mit einer zu kühlenden Komponente in Wärmeaustausch steht, einen geschlossenen Arbeitsgaskreis verwendet und innerhalb einer Wärmeisolierhülle (1), die mit einer Grundplatte (4) für die Anbringung am Gehäuse (50, 60) fest verbunden ist, einen in den Arbeitsgaskreis eingesetzten Wärmespeicher (5) umfaßt, der ringförmig um ein axiales Volumen (6) angeordnet ist, das sich zwischen einem Kältetauscher (8) erstreckt, der mit der zu kühlenden Komponente (21) in thermischem Kontakt steht und am Boden des Kryostaten (30) eine Verbindung zwischen dem Wärmespeicher (5) und dem axialen Volumen herstellt, dadurch gekennzeichnet, daß er einen Kranz (71) umfaßt, der im Wärmespeicher (5) am oberen Ende des Kryostaten Gas von einer durch die Grundplatte (4) verlaufenden Leitung (39), die eine Verbindung mit der Verdichtungskammer herstellt, verteilt, wobei der Verteilungskranz (71) durch ein Mittelteil (10, 20) gebildet ist, das über der Grundplatte (4) abnehmbar angebracht ist und axial durch deren Zentrum verläuft, und zwischen einem Modell, das geeignet ist für eine Kühleinrichtung des Typs mit pulsierendem Gas, in dem das axiale Volumen (6) als Gaskolben arbeitet, und einem Modell, das geeignet ist für eine Kühleinrichtung des Typs mit Stirling-Zyklus, in dem sich ein Verdrängerkolben in dem axialen Volumen verschiebt, austauschbar ist.
  2. Kryostat nach Anspruch 1, dadurch gekennzeichnet, daß das Mittelteil, das den Verteilungskranz (71) aufweist, mit einem das axiale Volumen (6) begrenzenden Rohr (3) einteilig verbunden ist.
  3. Kryostat nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, daß das Mittelteil in dem für eine Kühleinrichtung des Typs mit Stirling-Zyklus geeigneten Modell eine axiale Bohrung aufweist, durch die ein Verdrängerkolben der Kühleinrichtung verlaufen kann, der in das axiale Volumen (6) dicht gleitend eingesetzt ist.
  4. Kryostat nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß der Kältetauscher (8) eine Struktur mit rotationssymmetrischer Geometrie aufweist, in der sich um die Mittelachse des Kryostaten massive Zonen (33) aus einem gut wärmeleitenden Material und Leerzonen (32), die für den Gasdurchlaß offen sind, abwechseln.
  5. Kryostat nach Anspruch 4, dadurch gekennzeichnet, daß sich die Leerzonen (33) beiderseits einer Schulter (34) für die Zentrierung eines das axiale Volumen begrenzenden Mittelrohrs (3) erstrecken.
  6. Kryostat nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß die Wärmeisolierhülle (1) eine an den Wärmespeicher angrenzende röhrenförmige Innenwand (2) aufweist, die durch eine Platte (22) für die Aufnahme der zu kühlenden Komponente verschlossen ist, an der der Kältetauscher (8) anliegt.
  7. Kryostat nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß der Wärmespeicher aus einer aufgewickelten Folie in dem ringförmigen Raum zwischen einer Innenwand (2) der Hülle (1) und einem das axiale Volumen begrenzenden Mittelrohr (3) in der Verlängerung des Verteilungskranzes gebildet ist, wobei die Folie insbesondere durch ein photolithographisches Verfahren in der Weise bearbeitet ist, daß getrennte Stege (27) mit glatten Oberflächen parallel zur Mittelachse des Kryostaten und transversale, überdicke Spangen (26), die die aufeinanderfolgenden Stege punktförmig miteinander verbinden, ausgebildet sind.
  8. Kryostat nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, daß der Verteilungskranz eine untere Fläche aufweist, mit der er am Wärmespeicher anliegt und in der eine kreisförmige Nut (45) ausgespart ist, die durch regelmäßig verteilte Öffnungen mit einer ringförmigen Kammer (42, 43) in Verbindung steht, die auf Höhe der Grundplatte (4) des Kryostaten außen um das Mittelteil ausgebildet ist und mit dem Kanal (39) in Verbindung steht.
  9. Kryostat nach einem der Ansprüche 1 bis 8, gekennzeichnet durch einen Verbund aus übereinander angeordneten Gasströmungs-Beruhigungsgittern, der am Boden des axialen Volumens gegenüber dem Kältetauscher angeordnet ist.
  10. Kryostat nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, daß die Grundplatte (4) einen Ring (17) für die Anbringung des Mittelteils (10, 20) in der Verlängerung des axialen Volumens (6) bildet.
  11. Kühleinrichtung, dadurch gekennzeichnet, daß sie einen Kryostaten nach einem der Ansprüche 1 bis 10 enthält und, wenn sie dem für eine Kühleinrichtung mit Stirling-Zyklus geeignetem Modell entspricht, mit dem Gehäuse (60) eines Druckoszillators verbunden ist, der einen Verdrängerkolben umfaßt, der phasenverschoben zu einem Verdichtungskolben synchronisiert vorgesteuert wird, und daß der Verdrängerkolben (55) in dem inneren Volumen (6) des Kryostaten (30) axial beweglich ist und sich dicht gleitend in einer axialen Bohrung (72) bewegt, die hierzu in dem in der Grundplatte des Kryostaten angebrachten Mittelteil (20) vorgesehen ist.
  12. Kühleinrichtung, dadurch gekennzeichnet, daß sie einen Kryostaten nach einem der Ansprüche 1 bis 10 enthält und, wenn sie dem für eine Kühleinrichtung mit pulsierendem Gas geeignetem Modell entspricht, mit dem Gehäuse (50) eines Druckoszillators verbunden ist, das Mittel zur periodischen Vorsteuerung eines Gasverdichtungskolbens, der das Volumen der Verdichtungskammer verändert, und einen Pufferspeicher für Gas mit konstantem Druck umfaßt, und daß das in der Grundplatte (4) des Kryostaten angebrachte Mittelteil (10) Mittel für eine Druckluftverbindung mit gesteuertem Durchsatz mit dem Speicher (65) umfaßt.
  13. Kühleinrichtung nach Anspruch 12; dadurch gekennzeichnet, daß das Mittelteil zusätzlich zu einem Gasdurchlaßkanal (11) mit gesteuertem Durchsatz zwischen dem Pufferspeicher für Gas mit konstantem Druck, der in dem Gehäuse (50) des Druckoszillators ausgebildet ist, und dem inneren axialen Volumen (6) des Kryostaten, das sich im Betrieb mit Gas füllt, um einen Gaskolben mit Phasenverschiebung in bezug auf die periodische Verdichtung zu bilden, wenigstens einen weiteren Kanal (12) mit gesteuertem Durchsatz umfaßt, der in eine ringförmige Kammer (42, 43) mündet, die durch das gemäß Anspruch 8 verwirklichte Mittelteil gebildet ist.
  14. Kühleinrichtung nach Anspruch 12 oder 13, dadurch gekennzeichnet, daß das Gaspuffervolumen in einem Verdichtungskolben ausgebildet ist, der durch die Vorsteuermittel gesteuert wird und hierzu in einem Führungsmantel des Kolbens direkt in das Mittelteil (10) des Kryostaten mündet.
  15. Kühleinrichtung nach einem der Ansprüche 12 bis 14, dadurch gekennzeichnet, daß die Vorsteuermittel in einer Konfiguration des Typs mit rotierendem Motor eine Kurbelwelle enthalten, die einen Bewegungsübertragungsmechanismus über ein Kugellager betätigen, das in einer Nut, die transversal zur Außenseite des Kolbens ausgespart ist, beweglich ist.
EP19970400898 1996-04-23 1997-04-22 Kryostat für Tiefsttemperatur-Kälteanlage und Kälteanlagen mit einem solchen Kryostat Expired - Lifetime EP0803687B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9605086 1996-04-23
FR9605086A FR2747767B1 (fr) 1996-04-23 1996-04-23 Cryostat pour refroidisseur cryogenique et refroidisseurs comportant un tel cryostat

Publications (2)

Publication Number Publication Date
EP0803687A1 EP0803687A1 (de) 1997-10-29
EP0803687B1 true EP0803687B1 (de) 2002-06-26

Family

ID=9491490

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19970400898 Expired - Lifetime EP0803687B1 (de) 1996-04-23 1997-04-22 Kryostat für Tiefsttemperatur-Kälteanlage und Kälteanlagen mit einem solchen Kryostat

Country Status (3)

Country Link
EP (1) EP0803687B1 (de)
DE (1) DE69713547T2 (de)
FR (1) FR2747767B1 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3751175B2 (ja) * 1999-12-21 2006-03-01 シャープ株式会社 スターリング冷凍機
FR2815700B1 (fr) * 2000-10-19 2004-10-22 Sagem Dispositif cryogenique a cycle ferme
KR100393792B1 (ko) * 2001-02-17 2003-08-02 엘지전자 주식회사 맥동관 냉동기
US8910486B2 (en) * 2010-07-22 2014-12-16 Flir Systems, Inc. Expander for stirling engines and cryogenic coolers
GB2510912B (en) * 2013-02-19 2018-09-26 The Hymatic Engineering Company Ltd A pulse tube refrigerator / cryocooler apparatus
CN118129389B (zh) * 2024-05-07 2024-07-02 上海量羲技术有限公司 一种稀释制冷装置

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3220201A (en) * 1965-01-25 1965-11-30 Little Inc A Cryogenic refrigerator operating on the stirling cycle
US3851173A (en) * 1973-06-25 1974-11-26 Texas Instruments Inc Thermal energy receiver
US4425764A (en) * 1982-03-16 1984-01-17 Kryovacs Scientific Corporation Micro-cryogenic system with pseudo two stage cold finger, stationary regenerative material, and pre-cooling of the working fluid
US4550571A (en) * 1983-12-28 1985-11-05 Helix Technology Corporation Balanced integral Stirling cryogenic refrigerator
US4569203A (en) * 1984-10-29 1986-02-11 Texas Instruments Incorporated Cryogenic cooler
DE3812427A1 (de) * 1988-04-14 1989-10-26 Leybold Ag Verfahren zur herstellung eines regenerators fuer eine tieftemperatur-kaeltemaschine und nach diesem verfahren hergestellter regenerator
US4858442A (en) * 1988-04-29 1989-08-22 Inframetrics, Incorporated Miniature integral stirling cryocooler
US5293748A (en) * 1990-07-10 1994-03-15 Carrier Corporation Piston cylinder arrangement for an integral Stirling cryocooler
US5435136A (en) * 1991-10-15 1995-07-25 Aisin Seiki Kabushiki Kaisha Pulse tube heat engine
GB9213350D0 (en) * 1992-06-24 1992-08-05 Marconi Gec Ltd Refrigerator
FR2702269B1 (fr) * 1993-03-02 1995-04-07 Cryotechnologies Refroidisseur muni d'un doigt froid du type tube pulsé.
US5613365A (en) * 1994-12-12 1997-03-25 Hughes Electronics Concentric pulse tube expander

Also Published As

Publication number Publication date
DE69713547D1 (de) 2002-08-01
DE69713547T2 (de) 2003-01-16
EP0803687A1 (de) 1997-10-29
FR2747767B1 (fr) 1998-08-28
FR2747767A1 (fr) 1997-10-24

Similar Documents

Publication Publication Date Title
EP0119502B1 (de) Thermoelektrische Anlage
EP2223022B1 (de) Magnetokalorischer generator
EP1969294A2 (de) Vorrichtung zur kälte- und wärmeerzeugung durch einen magnetokalorischen effekt
FR2505035A1 (fr) Compresseur hermetique de refrigeration equipe d'un silencieux, notamment pour refrigerateurs menagers
EP1581774A1 (de) Verfahren und vorrichtung zur kontinuierlichen kälte-und wärmeerzeugung durch magneto-kalorischen effekt
WO2010061064A1 (fr) Generateur thermioue a materiau magnetocalorioue
WO2010037980A1 (fr) Structure d'echangeur thermique et chambre de compression ou de detente isotherme
EP1040274A1 (de) Verdrängungspumpe
FR2942305A1 (fr) Generateur thermique magnetocalorique
EP0803687B1 (de) Kryostat für Tiefsttemperatur-Kälteanlage und Kälteanlagen mit einem solchen Kryostat
EP2480777A1 (de) Thermodynamische maschine mit stirlingkreisprozess
CA2595360A1 (fr) Pompe a vide a cycle de translation circulaire a plusieurs arbres
EP0114781B1 (de) Wärmemaschine mit internem oder externem Energiebrunnen, mit Zylinder des Verdichtertyps oder Stirling-Zyklustyps
EP2603747B1 (de) Wärmegenerator mit magnetokalorischem material
EP2399088A1 (de) Magnetokalorischer wärmeerzeuger
WO2020127300A1 (fr) Regenerateur et procede de fabrication d'un tel regenerateur
FR2821150A1 (fr) Refregirateur a tube pulse
FR2566886A1 (fr) Refrigerateur cryogenique a soupape poussee par la force elastique d'un gaz
FR2566887A1 (fr) Refrigerateurs cryogeniques a etages multiples, capables d'obtenir une refrigeration a une temperature se situant entre 4,5 et 10o kelvin
FR2741940A1 (fr) Refroidisseur a moteur lineaire
FR2742215A1 (fr) Refroidisseur stirling a pilotage rotatif
EP0258093B1 (de) Joule-Thomson-Kühler und mit diesem Kühler versehener Kryostat
FR3024768A1 (fr) Machine thermique a materiau magnetocalorique du genre machine frigorifique ou pompe a chaleur
FR2760075A1 (fr) Systeme de conditionnement de composants fonctionnant a temperature cryogenique
FR2754593A1 (fr) Procede et dispositif de refroidissement cryogenique de composants par detente de joule-thomson

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB NL

17P Request for examination filed

Effective date: 19980417

17Q First examination report despatched

Effective date: 20001115

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: THALES CRYOGENIE S.A.

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB NL

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REF Corresponds to:

Ref document number: 69713547

Country of ref document: DE

Date of ref document: 20020801

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20020906

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20030327

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20160323

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20160411

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20160419

Year of fee payment: 20

Ref country code: GB

Payment date: 20160420

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 69713547

Country of ref document: DE

REG Reference to a national code

Ref country code: NL

Ref legal event code: MK

Effective date: 20170421

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20170421

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20170421