EP3551947B1 - Regenerator for a cryo-cooler with helium as a working gas, a method for producing such a regenerator, and a cryo-cooler comprising such a regenerator - Google Patents

Regenerator for a cryo-cooler with helium as a working gas, a method for producing such a regenerator, and a cryo-cooler comprising such a regenerator Download PDF

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Publication number
EP3551947B1
EP3551947B1 EP17832047.9A EP17832047A EP3551947B1 EP 3551947 B1 EP3551947 B1 EP 3551947B1 EP 17832047 A EP17832047 A EP 17832047A EP 3551947 B1 EP3551947 B1 EP 3551947B1
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EP
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Prior art keywords
regenerator
cell
cells
working gas
cavities
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EP17832047.9A
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German (de)
French (fr)
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EP3551947A1 (en
Inventor
Jens Dr. Höhne
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Pressure Wave Systems GmbH
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Pressure Wave Systems GmbH
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    • 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
    • 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
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/002Gas cycle refrigeration machines with parallel working cold producing expansion devices in one circuit
    • 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 
    • F25B2309/1408Pulse-tube cycles with pulse tube having U-turn or L-turn type 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 
    • F25B2309/1415Pulse-tube cycles characterised by regenerator details

Definitions

  • the invention relates to a regenerator for cryocoolers with helium as the working gas according to claim 1, a method for producing such a regenerator according to claims 13 and 14 and a cryocooler provided with such a regenerator according to claim 15.
  • cryo-coolers e.g. B. Stirling, Gifford-McMahon and pulse tube coolers are operated regeneratively. i.e. the thermal capacity of a material is used to store the cold or to pre-cool warm gas as it enters the expansion chamber.
  • a problem here is that at temperatures in the 2K to 20K range, the heat capacity of almost all materials decreases sharply. It is therefore very difficult to find materials that have a sufficiently high heat capacity in the range between 2K and 20K.
  • 12 shows the typical structure of a two-stage pulse tube cooler with a first cold stage of 20 to approx. 30K and a second cold stage of 22 to approx. 2K.
  • the first cold stage 220 includes a first pulse tube 224 and a first regenerator 226.
  • the second cold stage 222 includes a second pulse tube 228 and a second regenerator 230 in accordance with the present invention. With the first cold stage 220 approx. 30K and with the second cold stage 222 approx. 4K are achieved.
  • the first pulse tube 224, the first regenerator 226 and the second pulse tube 228 terminate in a connecting means 232 which separates the environment from the area to be cooled.
  • Working gas is supplied and discharged in a pulsating manner by a pump (not shown) via working gas lines 234 .
  • the working gas lines 234 open into the first regenerator 226 and via valves 236 there is a connection to the first pulse tube 224 and the second pulse tube 228 as well as to ballast volume 238.
  • the second regenerator 230 in the second cold stage 222 consists of a first regenerator section 240 and a low-temperature - Regenerator section 242.
  • the first regenerator section 240 consists of superimposed metal screens 244 - see figure 13 .
  • the cryogenic regenerator section 242 contains rare earth connections, e.g. B. ErNi, HoCu 2 and the like.
  • the structure of the second regenerator 230 is shown schematically in 11 shown. Rare earth compounds are relatively expensive. Furthermore, these materials are used in the form of beads 46 (100 to several 100 micrometers in diameter).
  • a problem here is the fixation of the balls in the oscillating flow of the working gas, since any kind of movement leads to abrasion and thus dust, which drastically reduces the service life of the cryocooler.
  • ball beds according to 13 a significant dead volume that does not contribute to heat exchange or cooling capacity.
  • Helium is often used as a working gas in cryogenic coolers. In the temperature range from 2K to 20K, helium has a comparatively high heat capacity, which is equal to the heat capacity of rare earth compounds in this temperature range. It has therefore been proposed to use helium as the regenerator material. From the U.S. 2012/0304668 A1 , the, DE 10319510 A1 , the DE 102005007627 A1 , CN 104197591A , DE 19924184 A1 and the US4359872A closed hollow bodies made of glass or metal and filled with helium are known as regenerator structures. This basic idea has not yet resulted in a finished product.
  • regenerator which is inexpensive in comparison to regenerators with rare earth compounds and which uses helium as the heat storage material and nevertheless has a simple structure.
  • the regenerator consists of a hollow cell with heat-conducting cell walls.
  • the outside of the cell walls at least partially delimits a flow channel for the working gas helium.
  • the cavity is filled with helium as a heat storage material and is connected to the outside of the cell via a pressure equalization opening.
  • the working gas, helium flows around the can-shaped cell, as a result of which heat transfer takes place via the cell walls between the working gas helium outside the cavity and the helium inside the cavity.
  • the size of the cell(s) in relation to the size of the flow channel of the working gas is selected in such a way that the desired pressure differences are set between the high-pressure side and the low-pressure side of the regenerator with the smallest possible dead volume.
  • the cell walls of the cell are very thin, so that the desired heat exchange can take place.
  • the ratio of the volume of the cavity or cavities to the opening area or outflow resistance of the pressure equalization opening is chosen so that the pressure in the cavity or cavities in the working frequency range of cooler operation (approx. 1 to 60 Hz) hardly changes, or at least only slightly.
  • This mode of operation can be compared to a capacitor at high frequencies - it is virtually unaware of the change in voltage if the capacity is high enough and the voltage change is small.
  • the pressure in the cell would always fluctuate around the medium pressure of the cooling system, typically around 16 bar.
  • the stable pressure is important because otherwise the volume of the cavity or cavities would be a large contributor to the "dead volume" if its pressure was between e.g.
  • the opening area or the outflow resistance of the pressure compensation opening is selected in such a way that before the regenerator is put into operation and during the start-up phase, helium penetrates into the cavity or cavities due to the prevailing pressure conditions.
  • the high outflow resistance of the pressure equalization opening results in the "condenser effect" explained above during the Pressure fluctuations in the area of the regenerator with the working frequency of a cooler.
  • the temperature of the working gas helium and also of the helium in the regenerator cavities decreases. As a result, the volume of helium is reduced and helium continues to flow into the regenerator cavities via the pressure equalization opening. i.e.
  • the pressure equalization opening has the form of a capillary.
  • the cell is penetrated by flow channels that are delimited by cell walls. This results in an enlarged heat exchange surface and thus improved heat transfer between the helium in the cavities and the working gas outside.
  • the flow channels are preferably designed as slots. The slits end short of the edge of the cell, preventing the cell from falling apart.
  • the flow channels are formed as a plurality of slots that are straight and parallel to each other and terminate short of the edge of the cell so that the cell cannot fall apart.
  • a circumferential channel is formed at the edge of the cell into which the multiple interconnected cavities open.
  • the slit-shaped flow channels for working gas preferably run in a straight line and parallel to one another, on the one hand to minimize the flow resistance and on the other hand to uniformly close the tubular cavities between the shape. Due to the straightness and the parallelism, an equal distance is obtained in a simple manner between two flow channels.
  • a single cell optionally with a plurality of tubular structures, can have the shape of a disc. Alternatively, multiple cells can be assembled into a disk shape. - Claim2.
  • the arrangement in a row according to claim 3 increases the heat storage capacity of the regenerator.
  • Thermal insulation between cells arranged one behind the other in the direction of flow of the working gas - claim 4 - prevents heat from being exchanged between the cavities in the direction of flow of the working gas.
  • Such a heat exchange in the flow direction of the working gas would mean a short circuit of the regenerator; a heat exchange in the flow direction of the working gas does not contribute to the function of the regenerator.
  • the thickness of the thermally insulating layer is preferably between 0.1 mm and 0.5 mm.
  • the alignment elements according to claim 5 to 7 simplify the alignment of the flow channels of cells lying one on top of the other.
  • the alignment elements are z.
  • the shape of a capillary means that the cross-sectional area of the opening is very small compared to the surface area of the hollow body.
  • the pressure equalization opening can also be provided by leaks that occur during the manufacture of the cells - claim 8.
  • the size and thus the permeability of the pressure equalization opening are chosen so that during a working cycle of the regenerator, the pressure change in the cell is a maximum of 20% and preferably a maximum of 10%. This is an optimization process.
  • the larger the capillary the greater the unwanted mass transfer, the greater the pressure fluctuations in the cell cavity and the faster the helium penetrates into the cavities when the regenerator is started up.
  • the smaller the capillary the less compression work has to be done, but the longer it takes for the helium to penetrate the cavities when the regenerator is started up.
  • the surfaces of the hollow bodies are provided with turbulence structures - claim 9
  • the cross-sectional shapes of the tubular cavities according to claim 10 enable the manufacture of the regenerator by means of 3D printing (claim 14).
  • the cuboid or rectangular shape of the cross sections of the cavities is optimal for heat exchange.
  • Cells with tubular cavities with at least one sloping cell wall or with a triangular cross-section can be easily created using 3D printing.
  • structures with vertical or sloping cell walls slopes of 45° or more
  • a diamond-shaped cross-section, a pentagonal cross-section or a house-shaped cross-section is also suitable - claim 10.
  • flow channels are arranged between the tubular cavities - claim 11.
  • the disk-shaped regenerator in which the disk-shaped regenerator consists of one or more disk-shaped cells and each cell comprises two half-cells, means that both half-cells can be produced by means of 3D printing.
  • the proportion of the volume of the cavities—and thus of the helium in the cavities—in the total volume of the regenerator increases compared to regenerators that only have one-piece cells. This increases the Heat storage capacity of the regenerator or the regenerator can be made more compact with the same heat capacity.
  • cuboid cavities or elliptical cavities can be produced from two components as a whole or in two steps - claim 13 or 14.
  • a first component with "open cavities” or with pot-shaped depressions is first produced.
  • these depressions are then covered by second components.
  • the first and second components are permanently joined together, e.g. B. by gluing or welding.
  • regenerators according to the present invention are particularly suitable for Stirling, Gifford-McMahon or pulse tube coolers in particular - claim 15.
  • the hollow bodies are made of metal and/or and can be made very thin compared to the prior art due to the pressure equalization opening, which reduces the heat transfer resistance between the helium inside the cavities and the helium working gas outside the cavities.
  • the cell walls of the cavities preferably have a constant thickness, at least along the flow channels, and are in the range between 0.1 mm and 0.5 mm. Due to the constant wall thickness of the cell walls, a uniform heat transfer is achieved between the working gas helium in the flow channels and the helium in the cavities.
  • the entire regenerator preferably has a thickness of 5 mm to 100 mm in the flow direction of the working gas.
  • the Figures 1 and 2 show a first embodiment of the regenerator 1 according to the invention in its simplest form.
  • the regenerator 1 consists of a cell 2 with cell walls 4 which enclose a cavity 6 .
  • the cell walls 4 have an outside 4a and an inside 4i.
  • a pressure equalization opening in the form of a capillary 8 passes through the cell walls 4 .
  • the regenerator 1 has a circular cross-section and is arranged in a tubular flow channel 10 for the working gas helium.
  • the interior of the cavity 6 is filled with helium as a regenerator medium or a heat-accumulating medium.
  • the regenerator 1 or the cell 2 is dimensioned in such a way that an annular gap 12 remains between the tubular flow channel 10 for the working gas and the outside 4a of the cell wall 4 .
  • the working gas helium can thus flow around the regenerator 1 and exchange heat with the helium in the cavity 6 via the heat-conducting cell walls 4 .
  • Figures 3a and 3b show a second embodiment of the invention with a disc-shaped cell 2.
  • the cell 2 differs from the cell 2 by Figure 1 and 2 in that the cell 2 according to the second embodiment is penetrated by a plurality of slots 20 running in a straight line in one plane as flow channels for the working gas.
  • the slit-shaped flow channels 20 run parallel to one another, but end in front of the edge of the cell 2, so that the cell 2 cannot fall apart.
  • tubular cavities 6 with a rectangular cross section. All the cavities 6 open into a peripheral channel 24 provided at the edge of the disc-shaped cell 2, so that the cavities 6 and the peripheral channel 24 form a single cavity.
  • one or two larger openings 22 initially remain through which the loose 3D printing material can be blown out before the 3D printing. These openings are then closed so that only one or more pressure equalization openings 8 remain in the form of capillaries. It is also possible to arrange several cells 2 one behind the other in the flow direction of the working gas, resulting in a regenerator with a higher output.
  • FIG. 4 1 shows a third embodiment of the invention, in which a plurality of cells 2-1, 2-2, 2-3 are stacked one on top of the other.
  • the three disk-shaped cells 2-i with a circular cross-section have an identical structure.
  • the cells 2-i are similar to the cell 2 of the second embodiment and differ from the cell by Figure 1 and 2 in that the cells 2-i are penetrated by a plurality of slots 20 running in a straight line in one plane as flow channels for the working gas.
  • the slit-shaped flow channels 20 run parallel to one another, but end in front of the edge of the cells 2-i, so that the cell 2 cannot fall apart.
  • tubular cavities 6-i which have a cross-section in the form of an equilateral triangle with a right angle.
  • the apex of the right-angled triangle points upwards, so that the two sides of the equilateral triangle extend upwards at a 45° angle.
  • Cavities 6-i with a triangular cross-section can be easily produced using 3D printing.
  • the cavities 6-i are connected to one another at the edge of the disc-shaped cells 2-i.
  • a pressure equalization opening 8 connects the cavities 6-i with the area outside the cells 2-i.
  • the cells 2-i have a plurality of alignment pins 30 on their upper side and corresponding alignment depressions 32 are arranged on the opposite side. Through these alignment elements 30, 32 is achieved that the slit-shaped flow channels 20 of the cells 6-i lying one above the other are aligned with one another, so that continuous flow channels result through the regenerator.
  • a thermally insulating layer 34 is arranged between the individual cells 6 - i, through which the alignment pin 30 passes, so that the alignment pins can engage in the alignment openings 32 located above.
  • FIG 5 shows schematically a fourth embodiment of the regenerator in the form of a disk-shaped cell 2, which differs from the cells 2-i according to 4 differs in that instead of a tubular cavity with a triangular cross section, two tubular cavities 6a and 6b are provided.
  • the cross section of the tubular cavities 6a and 6b is also in the shape of a right-angled equilateral triangle. The right angle begins on the inside of the partition wall 4, which delimits the slit-shaped flow channels. This results in a partition 4 with a constant wall thickness between the flow channels 20 and the cavities 6-i. This leads to an improved heat transfer between the working gas in the flow channel 20 and the helium in the cavities 6a and 6b.
  • the pressure equalization opening 8 connects the cavities 6a, 6b with the area outside the cell 2.
  • FIG. 6 shows a fifth embodiment of the invention, which differs from the embodiment according to FIG figure 4 differs only in that the tubular cavities 6a, 6b are arranged with triangular cross section with the base of the right triangle towards the flow channels 20. Since the base is the length of the side of the equilateral triangle, this improves heat transfer.
  • FIG. 1 shows a regenerator 101 with a large number of cells 102 which are arranged in the form of a 3-dimensional matrix 103 with two layers of cells 102.
  • FIG. The cells 102 are cubic and basically identical in construction. However, since the regenerator 101 fills a pipe cross section, the cells 102 inevitably have a different shape in the edge area.
  • the individual cells 102 each comprise a cube-shaped cavity 106 with a heat-conducting shell 104 and a pressure equalization opening 108 in the form of a capillary. How out 8 can be seen, the individual cells are 102 arranged offset one behind the other in the direction of flow 112 of the working gas.
  • the cells 102 lying next to one another are connected to one another by means of thermally conductive connecting elements 114 .
  • the cells 102 lying one behind the other in the direction of flow 112 are connected to one another with thermally insulating or poorly conducting connecting elements 116 and form a flow channel 120.
  • FIG 7 only two tiers of cells 102 are shown, while in 8 three layers of cells 102 are shown.
  • the gas volume of the individual cavities 106 is approximately 1 mm 2
  • the wall thickness of the shell 104 is approximately 0.2 mm.
  • the distance between the individual cells 102 is approximately 0.2 mm.
  • the total space requirement of a cell 102 is approximately 8 mm 3 .
  • the regenerator 101 according to the invention is preferably used as a low-temperature regenerator section 242 in the coldest cold stage of a cryocooler.
  • FIG 11 shows an eighth embodiment of the invention in the form of a disc-shaped cell 2, which is composed of a first and a second half-cell 50, 52, so that a cell 2 results analogously to the embodiments according to FIG figure 5 and 6 between the slit-shaped flow channels 20 has cuboid structures in cross-section.
  • Both half-cells 50, 52 each have a plurality of first and second cavities 54 and 56 having a cross section of an isosceles triangle.
  • the two half-cells 50, 52 can be produced using 3D printing.
  • the two half-cells each have a flat side 58 and an uneven side 60 .
  • the two uneven sides 60 have a complementary shape and when the two half-cells 50, 52 are assembled, the complementary uneven sides 60 of the two half-cells lie on top of each other.
  • the regenerators with cells 2, each having two half-cells 50, 52 increases in the regenerators with cells 2, each having two half-cells 50, 52, the proportion of the cavity volume in the total volume of the regenerator. This makes the regenerator more efficient.
  • the pressure equalization opening 8 is in the Figures 2 to 6 and 9 to 11 not marked but available. Since the cavities 6-i; 6′, 6a, 6b are connected to one another, the pressure equalization opening 8 can be provided at any point in the cells 2.
  • Figures 12a, 12b and 12c show possible further cross-sectional shapes of the cavities 6 in the disk-shaped regenerators according to FIG Figures 3 to 6 and 11 that can be easily produced using 3D printing.

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  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
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Description

Die Erfindung betrifft einen Regenerator für Kryo-Kühler mit Helium als Arbeitsgas gemäß Anspruch 1, ein Verfahren zur Herstellung eines solchen Regenerators nach Anspruch13 und 14 sowie einen mit einem solchen Regenerator versehenen KryoKühler nach Anspruch 15.The invention relates to a regenerator for cryocoolers with helium as the working gas according to claim 1, a method for producing such a regenerator according to claims 13 and 14 and a cryocooler provided with such a regenerator according to claim 15.

Periodisch betriebene Kryo-Kühler, wie z. B. Stirling-, Gifford-McMahon- und Pulsrohr-Kühler werden regeneratorisch betrieben. D. h. man nutzt die Wärmekapazität eines Materials aus, um die Kälte zu speichern bzw. um warmes Gas beim Eintritt in die Expansionskammer vor zu kühlen. Ein Problem hierbei ist, dass bei Temperaturen im Bereich 2K bis 20K die Wärmekapazität fast aller Materialien stark abnimmt. Damit ist es sehr schwer, Materialien zu finden, die im Bereich zwischen 2K und 20K eine ausreichend hohe Wärmekapazität aufweisen. Fig. 12 zeigt den typischen Aufbau eines zweistufigen Pulsröhrenkühlers mit einer ersten Kaltstufe 20 bis ca. 30K und einer zweiten Kaltstufe 22 bis ca. 2K. Die erste Kaltstufe 220 umfasst ein erstes Pulsrohr 224 einen ersten Regenerator 226. Die zweite Kaltstufe 222 umfasst ein zweites Pulsrohr 228 und einen zweiten Regenerator 230 gemäß der vorliegenden Erfindung. Mit der ersten Kaltstufe 220 werden ca. 30K und mit der zweiten Kaltstufe 222 werden ca. 4K erreicht. Das erste Pulsrohr 224, der erste Regenerator 226 und das zweite Pulsrohr 228 enden in einem Verbindungsmittel 232, der die Umgebung von dem zu kühlenden Bereich trennt. Über Arbeitsgasleitungen 234 wird von einer nicht dargestellten Pumpe pulsierend Arbeitsgas zu- und abgeführt. Die Arbeitsgasleitungen 234 münden in den ersten Regenerator 226 und über Ventile 236 besteht eine Verbindung mit dem ersten Pulsrohr 224 und dem zweiten Pulsrohr 228 sowie mit Balastvolumen 238. Der zweite Regenerator 230 in der zweiten Kaltstufe 222 besteht aus einem ersten Regeneratorabschnitt 240 und aus einem Tieftemperatur-Regeneratorabschnitt 242. Der erste Regeneratorabschnitt 240 besteht aus übereinanderliegenden Metallsieben 244 - siehe Fig. 13. Der Tieftemperatur-Regeneratorabschnitt 242 enthält seltene Erdverbindungen, z. B. ErNi, HoCu2 und dergleichen. Der Aufbau des zweiten Regenerators 230 ist schematisch in Fig. 11 dargestellt. Seltene Erdverbindungen sind relativ teuer. Weiterhin werden diese Materialen in Form von Kügelchen 46 (100 bis mehrere 100 Mikrometer Durchmesser) eingesetzt. Ein Problem hierbei ist die Fixierung der Kugeln im oszillierenden Fluss des Arbeitsgases, da jede Art von Bewegung zum Abrieb und damit Staub führt, welche die Lebensdauer der Kryo-Kühler drastisch reduziert. Darüber hinaus bedingen Kugelschüttungen gemäß Fig. 13 ein erhebliches Totvolumen, das nicht zum Wärmetausch und auch nicht zur Kühlleistung beiträgt.Intermittently operated cryo-coolers, e.g. B. Stirling, Gifford-McMahon and pulse tube coolers are operated regeneratively. i.e. the thermal capacity of a material is used to store the cold or to pre-cool warm gas as it enters the expansion chamber. A problem here is that at temperatures in the 2K to 20K range, the heat capacity of almost all materials decreases sharply. It is therefore very difficult to find materials that have a sufficiently high heat capacity in the range between 2K and 20K. 12 shows the typical structure of a two-stage pulse tube cooler with a first cold stage of 20 to approx. 30K and a second cold stage of 22 to approx. 2K. The first cold stage 220 includes a first pulse tube 224 and a first regenerator 226. The second cold stage 222 includes a second pulse tube 228 and a second regenerator 230 in accordance with the present invention. With the first cold stage 220 approx. 30K and with the second cold stage 222 approx. 4K are achieved. The first pulse tube 224, the first regenerator 226 and the second pulse tube 228 terminate in a connecting means 232 which separates the environment from the area to be cooled. Working gas is supplied and discharged in a pulsating manner by a pump (not shown) via working gas lines 234 . The working gas lines 234 open into the first regenerator 226 and via valves 236 there is a connection to the first pulse tube 224 and the second pulse tube 228 as well as to ballast volume 238. The second regenerator 230 in the second cold stage 222 consists of a first regenerator section 240 and a low-temperature - Regenerator section 242. The first regenerator section 240 consists of superimposed metal screens 244 - see figure 13 . The cryogenic regenerator section 242 contains rare earth connections, e.g. B. ErNi, HoCu 2 and the like. The structure of the second regenerator 230 is shown schematically in 11 shown. Rare earth compounds are relatively expensive. Furthermore, these materials are used in the form of beads 46 (100 to several 100 micrometers in diameter). A problem here is the fixation of the balls in the oscillating flow of the working gas, since any kind of movement leads to abrasion and thus dust, which drastically reduces the service life of the cryocooler. In addition, ball beds according to 13 a significant dead volume that does not contribute to heat exchange or cooling capacity.

Helium wird häufig als Arbeitsgas bei Kryo-Kühler eingesetzt. Helium besitzt in dem Temperaturbereich von 2K bis 20K eine vergleichsweise hohe Wärmekapazität, die der Wärmekapazität von seltenen Erdverbindungen in diesem Temperaturbereich gleich kommt. Daher ist vorgeschlagen worden Helium als Regenerator-Material einzusetzen. Aus der US 2012/0304668 A1 , der, DE 10319510 A1 , der DE 102005007627 A1 , CN 104197591 A , DE 19924184 A1 und der US 4359872 A sind mit Helium gefüllte geschlossene Hohlkörper aus Glas oder Metall als Regeneratorstrukturen bekannt. Diese Grundidee hat bis jetzt zu keinem fertigen Produkt geführt. Darüber hinaus führen mit Helium gefüllte Kügelchen wieder zu Abrieb, was die Einsatzdauer des Kryo-Kühlers verringert. Das Grundproblem dieser bekannten geschlossenen Hohlkörper mit Helium besteht in der aufwendigen Befüllung der Hohlkörper mit Helium unter Überdruck. Aufgrund des Überdrucks muss die Wandstärke der Hohlkörper erhöht werden, was zu einer Verschlechterung der Wärmeübergangswiderstände führt.Helium is often used as a working gas in cryogenic coolers. In the temperature range from 2K to 20K, helium has a comparatively high heat capacity, which is equal to the heat capacity of rare earth compounds in this temperature range. It has therefore been proposed to use helium as the regenerator material. From the U.S. 2012/0304668 A1 , the, DE 10319510 A1 , the DE 102005007627 A1 , CN 104197591A , DE 19924184 A1 and the US4359872A closed hollow bodies made of glass or metal and filled with helium are known as regenerator structures. This basic idea has not yet resulted in a finished product. In addition, helium-filled beads again cause attrition, reducing the service life of the cryocooler. The basic problem of these known closed hollow bodies with helium consists in the complex filling of the hollow bodies with helium under overpressure. Due to the overpressure, the wall thickness of the hollow body has to be increased, which leads to a deterioration in the heat transfer resistance.

In dem Artikel " Heat Capacity Characterization of a 4K Regenerator with Non-Rare Earth Material" in Cryocoolers 19, International Cryocooler Conference, Inc., Boulder, CO, 2016 wird eine Struktur mit Adsorbermaterial, das Helium absorbieren kann, als Regenerator für Kryo-Kühler vorgeschlagen. Der Aufbau des Regenerators ist kompliziert und aufwendig und es besteht die Gefahr, dass Teile des Adsorbermaterials durch den Arbeitsgasstrom mitgerissen werden. Durch die mitgerissenen Adsorberpartikel würde die Lebensdauer eines Kryo-Kühlers mit einem solchen Regenerator drastisch reduziert.In the article " Heat Capacity Characterization of a 4K Regenerator with Non-Rare Earth Material" in Cryocoolers 19, International Cryocooler Conference, Inc., Boulder, CO, 2016 a structure using adsorbent material capable of absorbing helium is proposed as a regenerator for cryocoolers. The structure of the regenerator is complicated and expensive, and there is a risk that parts of the adsorber material will be entrained by the working gas flow. The service life of a cryocooler with such a regenerator would be drastically reduced by the adsorber particles carried along.

Es ist daher Aufgabe der vorliegenden Erfindung einen im Vergleich zu Regeneratoren mit seltenen Erdverbindungen kostengünstigen Regenerator anzugeben, der Helium als Wärmespeichermaterial nutzt und dennoch einen einfachen Aufbau aufweist.It is therefore the object of the present invention to specify a regenerator which is inexpensive in comparison to regenerators with rare earth compounds and which uses helium as the heat storage material and nevertheless has a simple structure.

Die Lösung dieser Aufgabe erfolgt durch die Merkmale des Anspruch 1.This problem is solved by the features of claim 1.

Der Regenerator besteht im einfachsten Fall aus einer hohlen Zelle mit Wärme leitenden Zellwänden. Die Außenseite der Zellwände begrenzt wenigstens zum Teil einen Strömungskanal für das Arbeitsgas Helium. Der Hohlraum ist mit Helium als Wärmespeichermaterial gefüllt und ist über eine Druckausgleichsöffnung mit Außenseite der Zelle verbunden. Das Arbeitsgas Helium, umströmt die dosenförmige Zelle, wodurch über die Zellwände ein Wärmeübergang zwischen dem Arbeitsgas Helium außerhalb des Hohlraums und dem Helium innerhalb des Hohlraums stattfindet. Die Größe der Zelle(n) in Relation zu der Größe des Strömungskanals des Arbeitsgases ist so gewählt, dass sich zwischen der Hochdruckseite und der Niederdruckseite des Regenerators die gewünschten Druckdifferenzen bei einem möglichst geringen Totvolumen einstellen. Die Zellwände der Zelle weisen eine sehr geringe Wandstärke auf, sodass der gewünschte Wärmeaustausch erfolgen kann. Das Verhältnis von Volumen des oder der Hohlräume zu Öffnungsfläche bzw. Ausströmwiderstand der Druckausgleichsöffnung ist so gewählt, dass sich der Druck im Hohlraum oder in den Hohlräumen im Arbeitsfrequenzbereich des Kühlerbetriebs (ca. 1 bis 60 Hz) kaum oder zumindest nur wenig ändert. Diese Funktionsweise ist vergleichbar mit einem Kondensator bei hohen Frequenzen - dieser bekommt von der Änderung der Spannung quasi nichts mit, wenn die Kapazität hoch genug ist und die Spannungsänderung gering. Im typischen Anwendungsfall würde der Druck in der Zelle immer um den Mitteldruck des Kühlsystems, typischer Weise ca. 16 bar, schwanken. Der stabile Druck ist deshalb wichtig, da ansonsten das Volumen des oder der Hohlräume einen großen Beitrag zum "Totvolumen" wäre, wenn dessen Druck bei jeder Periode zwischen z. B. 8 und 24 bar schwanken würde, ohne dass es zur Kühlung beiträgt. Die Öffnungsfläche bzw. der Ausströmwiderstand der Druckausgleichsöffnung ist so gewählt, dass vor Inbetriebnahme des Regenerators und während der Anlaufphase aufgrund der herrschenden Druckverhältnisse Helium in den oder die Hohlräume eindringt. Durch den hohen Ausströmwiderstand der Druckausgleichsöffnung ergibt sich der vorstehend erläuterte "Kondensator-Effekt" während der Druckschwankungen im Bereich des Regenerators mit der Arbeitsfrequenz eines Kühlers. In der Anlaufphase sinkt die Temperatur des Arbeitsgases Helium und auch des Heliums in den Regeneratorhohlräumen. Folglich verringert sich das Volumen des Heliums und über die Druckausgleichsöffnung strömt weiter Helium in die Regeneratorhohlräume nach. D. h. während der Anlaufphase muss Helium nachgefüllt werden, bis sich die Arbeitstemperaturen und -drücke eingestellt haben. Ohne Druckausgleichsöffnung müssten die Hohlräume in der Zelle vorab mit Helium befüllt werden, was aufgrund der Drücke im Bereich von 16 bar im Arbeitsbereich des Kryo-Kühlers erheblich dickere Zellwände bedingen würde. Werden die Hohlkörper bei Umgebungstemperatur mit Helium befüllt, müssen aufgrund der geringeren Dichte von Helium bei Umgebungstemperatur noch wesentlich höhere Drücke für die Befüllung gewählt werden. Dies führt zu dickeren Zellwänden mit erheblich höheren Wärmedurchgangswiderstand. Durch die dickeren Zellwände würde einen Wärmedurchgangswiderstand der Zellwände so hoch, dass im Arbeitsfrequenzbereich von Kryo-Kühlern kaum mehr zu einem Wärmeaustausch zwischen dem Arbeitsgas Helium und dem Helium im Inneren des oder der Hohlräume kommen würde. Dies dürfte auch der Grund sein, dass kein Kryo-Kühler auf dem Markt ist, der einen Regenerator mit Helium in geschlossenen Hohlräumen einsetzt. Die Druckausgleichsöffnung hat erfindungsgemäß die Form einer Kapillare.In the simplest case, the regenerator consists of a hollow cell with heat-conducting cell walls. The outside of the cell walls at least partially delimits a flow channel for the working gas helium. The cavity is filled with helium as a heat storage material and is connected to the outside of the cell via a pressure equalization opening. The working gas, helium, flows around the can-shaped cell, as a result of which heat transfer takes place via the cell walls between the working gas helium outside the cavity and the helium inside the cavity. The size of the cell(s) in relation to the size of the flow channel of the working gas is selected in such a way that the desired pressure differences are set between the high-pressure side and the low-pressure side of the regenerator with the smallest possible dead volume. The cell walls of the cell are very thin, so that the desired heat exchange can take place. The ratio of the volume of the cavity or cavities to the opening area or outflow resistance of the pressure equalization opening is chosen so that the pressure in the cavity or cavities in the working frequency range of cooler operation (approx. 1 to 60 Hz) hardly changes, or at least only slightly. This mode of operation can be compared to a capacitor at high frequencies - it is virtually unaware of the change in voltage if the capacity is high enough and the voltage change is small. In a typical application, the pressure in the cell would always fluctuate around the medium pressure of the cooling system, typically around 16 bar. The stable pressure is important because otherwise the volume of the cavity or cavities would be a large contributor to the "dead volume" if its pressure was between e.g. B. 8 and 24 bar would fluctuate without it contributing to the cooling. The opening area or the outflow resistance of the pressure compensation opening is selected in such a way that before the regenerator is put into operation and during the start-up phase, helium penetrates into the cavity or cavities due to the prevailing pressure conditions. The high outflow resistance of the pressure equalization opening results in the "condenser effect" explained above during the Pressure fluctuations in the area of the regenerator with the working frequency of a cooler. During the start-up phase, the temperature of the working gas helium and also of the helium in the regenerator cavities decreases. As a result, the volume of helium is reduced and helium continues to flow into the regenerator cavities via the pressure equalization opening. i.e. During the start-up phase, helium must be refilled until the working temperatures and pressures have settled. Without a pressure equalization opening, the cavities in the cell would have to be filled with helium in advance, which would require significantly thicker cell walls due to the pressures in the range of 16 bar in the working area of the cryocooler. If the hollow bodies are filled with helium at ambient temperature, significantly higher pressures must be chosen for the filling due to the lower density of helium at ambient temperature. This leads to thicker cell walls with significantly higher thermal resistance. Due to the thicker cell walls, a heat transfer resistance of the cell walls would be so high that in the working frequency range of cryogenic coolers there would hardly be any heat exchange between the working gas helium and the helium inside the cavity or cavities. This may also be the reason that there is no cryo-cooler on the market that uses a regenerator with helium in closed cavities. According to the invention, the pressure equalization opening has the form of a capillary.

Die Zelle wird von Strömungskanälen durchsetzt, die von Zellwänden begrenzt sind. Hierdurch ergibt sich eine vergrößerte Wärmeaustauschfläche und somit ein verbesserter Wärmübergang zwischen dem Helium in den Hohlräumen und dem Arbeitsgas außen. Die Strömungskanäle sind vorzugsweise als Schlitze ausgebildet. Die Schlitze enden vor dem Rand der Zelle, sodass die Zelle nicht auseinanderfallen kann. Die Strömungskanäle sind als eine Mehrzahl von Schlitzen ausgebildet, die geradlinig und parallel zueinander verlaufen und vor dem Rand der Zelle enden, sodass die Zelle nicht auseinanderfallen kann. Ein umlaufender Kanal ist an dem Rand der Zelle ausgebildet, in den die mehrere miteinander verbundenen Hohlräume münden.The cell is penetrated by flow channels that are delimited by cell walls. This results in an enlarged heat exchange surface and thus improved heat transfer between the helium in the cavities and the working gas outside. The flow channels are preferably designed as slots. The slits end short of the edge of the cell, preventing the cell from falling apart. The flow channels are formed as a plurality of slots that are straight and parallel to each other and terminate short of the edge of the cell so that the cell cannot fall apart. A circumferential channel is formed at the edge of the cell into which the multiple interconnected cavities open.

Die schlitzförmigen Strömungskanäle für Arbeitsgas verlaufen vorzugsweise geradlinig und parallel zueinander, um zum einen den Strömungswiderstand zu minimieren und zum anderen, um die rohrförmigen Hohlräume zwischen den gleichförmig zu gestalten. Durch die Geradlinigkeit und die Parallelität ergibt sich auf einfache Weise zwischen zwei Strömungskanälen ein gleicher Abstand.The slit-shaped flow channels for working gas preferably run in a straight line and parallel to one another, on the one hand to minimize the flow resistance and on the other hand to uniformly close the tubular cavities between the shape. Due to the straightness and the parallelism, an equal distance is obtained in a simple manner between two flow channels.

Durch die runde Außenform des Regenerators lassen sie sich auf einfache Weise in die üblicherweise runden Querschnitte der Kryokühler einfügen. Dabei kann eine einzige Zelle, gegebenenfalls mit mehreren rohrförmigen Strukturen, die Form einer Scheibe haben. Alternativ können mehrere Zellen zu einer Scheibenform zusammengefügt werden. - Anspruch2.Due to the round outer shape of the regenerator, they can easily be inserted into the usually round cross-sections of cryocoolers. A single cell, optionally with a plurality of tubular structures, can have the shape of a disc. Alternatively, multiple cells can be assembled into a disk shape. - Claim2.

Durch die Hintereinanderanordnung nach Anspruch 3 erhöht sich die Wärmespeicherkapazität des Regenerators.The arrangement in a row according to claim 3 increases the heat storage capacity of the regenerator.

Durch eine thermische Isolierung zwischen in Strömungsrichtung des Arbeitsgases hintereinander angeordneten Zellen - Anspruch 4 - wird verhindert, dass zwischen den Hohlräumen in Strömungsrichtung des Arbeitsgases Wärme ausgetauscht wird. Ein solcher Wärmeaustausch in Strömungsrichtung des Arbeitsgases würde einen Kurzschluss des Regenerators bedeuten; ein Wärmeaustausch in Strömungsrichtung des Arbeitsgases trägt nicht zur Funktion des Regenerators bei. Die Dicke der thermisch isolierenden Schicht beträgt vorzugsweise zwischen 0,1mm und 0,5mm.Thermal insulation between cells arranged one behind the other in the direction of flow of the working gas - claim 4 - prevents heat from being exchanged between the cavities in the direction of flow of the working gas. Such a heat exchange in the flow direction of the working gas would mean a short circuit of the regenerator; a heat exchange in the flow direction of the working gas does not contribute to the function of the regenerator. The thickness of the thermally insulating layer is preferably between 0.1 mm and 0.5 mm.

Durch die Ausrichtelemente nach Anspruch 5 bis 7 wird die fluchtende Ausrichtung der Strömungskanäle aufeinander liegender Zellen vereinfacht. Die Ausrichtelemente sind z. B. Ausrichtzapfen, die eine konische oder pyramidenförmige Spitze aufweisen.The alignment elements according to claim 5 to 7 simplify the alignment of the flow channels of cells lying one on top of the other. The alignment elements are z. B. Alignment pins having a conical or pyramidal tip.

Die Form einer Kapillare bedeuted, dass die Querschnittsfläche der Öffnung im Vergleich zur Oberfläche des Hohlkörpers sehr klein ist.The shape of a capillary means that the cross-sectional area of the opening is very small compared to the surface area of the hollow body.

Die Druckausgleichsöffnung kann auch durch Undichtigkeiten bereitgestellt sein, die bei der Herstellung der Zellen auftreten - Anspruch 8.The pressure equalization opening can also be provided by leaks that occur during the manufacture of the cells - claim 8.

Die Größe und damit die Durchlässigkeit der Druckausgleichsöffnung werden so gewählt, dass während eines Arbeitszyklus des Regenerators die Druckänderung in der Zelle maximal 20% und vorzugsweise maximal 10% beträgt. Es handelt sich hier um einen Optimierungsprozess. Je größer die Kapillare, desto größer ist der unerwünschte Stoffaustausch, desto größer sind die Druckschwankungen im Hohlraum der Zelle und umso schneller erfolgt das Eindringen des Heliums in die Hohlräume bei Inbetriebnahme des Regenerators. Je kleiner die Kapillare desto weniger Kompressionsarbeit muss verrichtet werden, aber desto länger dauert das Eindringen des Heliums in die Hohlräume bei Inbetriebnahme des Regenerators..The size and thus the permeability of the pressure equalization opening are chosen so that during a working cycle of the regenerator, the pressure change in the cell is a maximum of 20% and preferably a maximum of 10%. This is an optimization process. The larger the capillary, the greater the unwanted mass transfer, the greater the pressure fluctuations in the cell cavity and the faster the helium penetrates into the cavities when the regenerator is started up. The smaller the capillary, the less compression work has to be done, but the longer it takes for the helium to penetrate the cavities when the regenerator is started up.

Um den Wärmeaustausch zwischen dem Arbeitsgas Helium und dem in dem Hohlkörper befindlichen, Wärme speichernden Helium zu verbessern, sind die Oberflächen der Hohlkörper mit Verwirbelungsstrukturen versehen - Anspruch 9In order to improve the heat exchange between the working gas helium and the heat-storing helium located in the hollow body, the surfaces of the hollow bodies are provided with turbulence structures - claim 9

Die Querschnittsformen der rohrförmigen Hohlräume nach Anspruch 10 ermöglichen die Herstellung des Regenerators mittels 3D-Druck (Anspruch 14). Die Quaderoder Rechteckform der Querschnitte der Hohlräume ist für den Wärmeaustausch optimal. Zellen mit rohrförmigen Hohlräumen mit wenigstens einer schrägen Zellwand oder mit Dreiecksquerschnitt lassen sich leicht mittels 3D-Druck erzeugen. Mittels 3D-Druck können Strukturen mit vertikalen oder schrägen Zellwänden (Schrägen von 45° oder mehr) leicht hergestellt werden. Dies ist am einfachsten gewährleistet, wenn der Dreiecksquerschnitt der Hohlräume einen rechten Winkel aufweist. Auch geeignet ist ein rautenförmiger Querschnitt, ein fünfeckiger Querschnitt oder ein hausförmiger Querschnitt - Anspruch 10.The cross-sectional shapes of the tubular cavities according to claim 10 enable the manufacture of the regenerator by means of 3D printing (claim 14). The cuboid or rectangular shape of the cross sections of the cavities is optimal for heat exchange. Cells with tubular cavities with at least one sloping cell wall or with a triangular cross-section can be easily created using 3D printing. Using 3D printing, structures with vertical or sloping cell walls (slopes of 45° or more) can easily be produced. This is most easily ensured when the triangular cross section of the cavities has a right angle. A diamond-shaped cross-section, a pentagonal cross-section or a house-shaped cross-section is also suitable - claim 10.

Für den optimalen Wärmetausch zwischen dem Helium in den rohrförmigen Hohlräumen und dem Arbeitsgas Helium außerhalb der Hohlräume sind zwischen den rohrförmigen Hohlräumen Strömungskanäle angeordnet - Anspruch 11.For the optimal heat exchange between the helium in the tubular cavities and the working gas helium outside of the cavities, flow channels are arranged between the tubular cavities - claim 11.

Durch die vorteilhafte Ausgestaltung nach Anspruch 12, bei der der scheibenförmige Regenerator aus einer oder mehreren scheibenförmigen Zellen besteht und jede Zelle jeweils zwei Halbzellen umfasst, wird erreicht, dass beide Halbzellen mittels 3D-Druck herstellbar sind. Gleichzeitig erhöht sich der Anteil des Volumens der Hohlräume - und damit des Heliums in den Hohlräumen - am Gesamtvolumen des Regenerators im Vergleich zu Regeneratoren, die nur einteilige Zellen aufweisen. Dies erhöht die Wärmespeicherfähigkeit des Regenerators oder der Regenerator kann bei gleicher Wärmekapazität kompakter ausgeführt werden.The advantageous embodiment according to claim 12, in which the disk-shaped regenerator consists of one or more disk-shaped cells and each cell comprises two half-cells, means that both half-cells can be produced by means of 3D printing. At the same time, the proportion of the volume of the cavities—and thus of the helium in the cavities—in the total volume of the regenerator increases compared to regenerators that only have one-piece cells. This increases the Heat storage capacity of the regenerator or the regenerator can be made more compact with the same heat capacity.

Bei 3D-Druck-Verfahren können quaderförmige Hohlräume oder ellipsoidförmige Hohlräume als Ganzes oder in zwei Schritten aus zwei Komponenten hergestellt werden - Anspruch 13 oder 14. Nach Anspruch 14 wird zunächst eine erste Komponente mit "offenen Hohlräumen" bzw. mit topfförmigen Vertiefungen erzeugt. Diese Vertiefungen werden dann in einem zweiten Schritt durch zweite Komponenten abgedeckt. Die ersten und zweiten Komponenten werden dauerhaft miteinander verbunden, z. B. durch Verklebung oder Verschweißung.In 3D printing processes, cuboid cavities or elliptical cavities can be produced from two components as a whole or in two steps - claim 13 or 14. According to claim 14, a first component with "open cavities" or with pot-shaped depressions is first produced. In a second step, these depressions are then covered by second components. The first and second components are permanently joined together, e.g. B. by gluing or welding.

Die Regeneratoren gemäß der vorliegenden Erfindung sind besonders für insbesondere für Stirling-, Gifford-McMahon- oder Pulsrohr-Kühler geeignet - Anspruch 15.The regenerators according to the present invention are particularly suitable for Stirling, Gifford-McMahon or pulse tube coolers in particular - claim 15.

Die Hohlkörper bestehen aus Metall und/oder und können aufgrund der Druckausgleichsöffnung gegenüber dem Stand der Technik sehr dünn ausgebildet werden, wodurch der Wärmeübergangswiderstand zwischen dem Helium im Inneren der Hohlräume und dem Arbeitsgas Helium außerhalb Hohlräume sinkt. Die Zellwände der Hohlräume weisen zumindest entlang der Strömungskanäle vorzugsweise eine konstante Dicke auf und liegen im Bereich zwischen 0,1mm und 0,5mm. Durch die konstante Wandstärke der Zellwände wird zwischen dem Arbeitsgas Helium in den Strömungskanälen und dem Helium in den Hohlräumen ein gleichmäßiger Wärmeübergang erreicht.The hollow bodies are made of metal and/or and can be made very thin compared to the prior art due to the pressure equalization opening, which reduces the heat transfer resistance between the helium inside the cavities and the helium working gas outside the cavities. The cell walls of the cavities preferably have a constant thickness, at least along the flow channels, and are in the range between 0.1 mm and 0.5 mm. Due to the constant wall thickness of the cell walls, a uniform heat transfer is achieved between the working gas helium in the flow channels and the helium in the cavities.

Der gesamte Regenerator weist in Strömungsrichtung des Arbeitsgases vorzugsweise eine Dicke von 5mm bis 100mm auf.The entire regenerator preferably has a thickness of 5 mm to 100 mm in the flow direction of the working gas.

Die übrigen Ansprüche beziehen sich auf weitere vorteilhafte Ausgestaltungen der Erfindung.The remaining claims relate to further advantageous configurations of the invention.

Nachfolgend werden bevorzugte Ausführungsformen der Erfindung anhand der Zeichnung beschrieben.Preferred embodiments of the invention are described below with reference to the drawing.

Es zeigt:

  • Fig. 1 eine Schnittdarstellung einer ersten Ausführungsform des Regenerators in einem Strömungskanal für Arbeitsgas,
  • Fig. 2 eine Schnittdarstellung der ersten Ausführungsform entlang II - II in Fig. 1,
  • Fig. 3a und 3b eine schematische Darstellung einer zweiten Ausführungsform,
  • Fig. 4 eine schematische Darstellung einer dritten Ausführungsform,
  • Fig. 5 eine schematische Darstellung einer vierten Ausführungsform,
  • Fig. 6 eine schematische Darstellung einer fünften Ausführungsform,
  • Fig. 7 eine sechste Ausführungsform, die nicht durch die beanspruchte Erfindung abgedeckt ist, in Form einer dreidimensionalen Matrixanordnung mit zwei Lagen von Zellen mit einem kreisringförmigen Außendurchmesser,
  • Fig. 8, die nicht durch die beanspruchte Erfindung abgedeckt ist, eine Detaildarstellung der Matrixanordnung mit drei Lagen von Zellen senkrecht zur Strömungsrichtung des Arbeitsgases betrachtet,
  • Fig. 9 und 10 schematische Darstellungen zur Herstellung des Regenerators aus einer Schalenstruktur und einer Abdeckung gemäß einer siebten Ausführungsform,
  • Fig. 11 eine achte Ausführungsform der Erfindung, die aus zwei mittels 3D-Druck hergestellten Strukturen besteht,
  • Fig. 12a, 12b und 12c Beispiele für Querschnitte der Hohlräume mit dem wärmespeichernden Helium, die sich ohne weiteres mittels 3D-Druck herstellen lassen,
  • Fig. 13 den typischen Aufbau eines Kryo-Kühlers in Form einer Pulsrohrkühlers mit zwei Kaltstufen, wobei die zweite Kaltstufe einen Tieftemperatur-Regenerator aufweist, und
  • Fig. 14 den schematischen Aufbau eines Tieftemperatur-Regenerators nach dem Stand der Technik mit seltenen Erden in Form von Kügelchen.
It shows:
  • 1 a sectional view of a first embodiment of the regenerator in a flow channel for working gas,
  • 2 a sectional view of the first embodiment along II - II in 1 ,
  • Figures 3a and 3b a schematic representation of a second embodiment,
  • 4 a schematic representation of a third embodiment,
  • figure 5 a schematic representation of a fourth embodiment,
  • 6 a schematic representation of a fifth embodiment,
  • 7 a sixth embodiment, which is not covered by the claimed invention, in the form of a three-dimensional matrix arrangement with two layers of cells with a circular outer diameter,
  • 8 , which is not covered by the claimed invention, a detailed view of the matrix arrangement with three layers of cells perpendicular to the direction of flow of the working gas,
  • Figures 9 and 10 schematic representations for the production of the regenerator from a shell structure and a cover according to a seventh embodiment,
  • 11 an eighth embodiment of the invention consisting of two structures produced by means of 3D printing,
  • Figures 12a, 12b and 12c Examples of cross-sections of the cavities with the heat-storing helium, which can be easily produced using 3D printing,
  • 13 the typical structure of a cryocooler in the form of a pulse tube cooler with two cold stages, the second cold stage having a low-temperature regenerator, and
  • 14 the schematic structure of a low-temperature regenerator according to the prior art with rare earths in the form of small beads.

Die Figuren 1 und 2 zeigen eine erste Ausgestaltung des erfindungsgemäßen Regenerators 1 in seiner einfachsten Form. Der Regenerator 1 besteht aus einer Zelle 2 mit Zellwänden 4, die einen Hohlraum 6 umschließen. Die Zellwände 4 weisen eine Außenseite 4a und einen Innenseite 4i auf. Die Zellwände 4 werden von einer Druckausgleichsöffnung in Form einer Kapillare 8 durchsetzt. Der Regenerator 1 weist einen kreisringförmigen Querschnitt auf und ist in einem rohrförmigen Strömungskanal 10 für Arbeitsgas Helium angeordnet. Das Innere des Hohlraums 6 ist mit Helium als Regeneratormedium oder als Wärme speicherndes Medium gefüllt. Der Regenerator 1 bzw. die Zelle 2 ist so dimensioniert, dass zwischen dem rohrförmigen Strömungskanal 10 für Arbeitsgas und der Außenseite 4a der Zellwand 4 ein Ringspalt 12 verbleibt. Damit kann das Arbeitsgas Helium den Regenerator 1 umströmen und über die Wärme leitenden Zellwände 4 mit dem Helium im Hohlraum 6 Wärme austauschen.the Figures 1 and 2 show a first embodiment of the regenerator 1 according to the invention in its simplest form. The regenerator 1 consists of a cell 2 with cell walls 4 which enclose a cavity 6 . The cell walls 4 have an outside 4a and an inside 4i. A pressure equalization opening in the form of a capillary 8 passes through the cell walls 4 . The regenerator 1 has a circular cross-section and is arranged in a tubular flow channel 10 for the working gas helium. The interior of the cavity 6 is filled with helium as a regenerator medium or a heat-accumulating medium. The regenerator 1 or the cell 2 is dimensioned in such a way that an annular gap 12 remains between the tubular flow channel 10 for the working gas and the outside 4a of the cell wall 4 . The working gas helium can thus flow around the regenerator 1 and exchange heat with the helium in the cavity 6 via the heat-conducting cell walls 4 .

Fig. 3a und 3b zeigen eine zweite Ausführungsform der Erfindung mit einer scheibenförmigen Zelle 2. Die Zelle 2 unterscheidet sich von der Zelle 2 nach Figur 1 und 2 dadurch, dass die Zelle 2 gemäß der zweiten Ausführungsform von einer Mehrzahl von geradlinig in einer Ebene verlaufenden Schlitzen 20 als Strömungskanäle für Arbeitsgas durchsetzt ist. Die schlitzförmigen Strömungskanäle 20 verlaufen parallel zueinander, enden jedoch vor dem Rand der Zelle 2, so dass die die Zelle 2 nicht auseinander fallen kann. In den durch Zellwände 4 umschlossenen quaderförmigen Bereichen zwischen den schlitzförmigen Strömungskanälen 20 befinden sich rohrförmige Hohlräume 6 mit einem rechteckigen Querschnitt. Alle Hohlräume 6 münden in einen am Rand der scheibenförmigen Zelle 2 vorgesehenen umlaufenden Kanal 24, so dass die Hohlräume 6 und der umlaufende Kanal 24 einen einzigen Hohlraum bilden. Figures 3a and 3b show a second embodiment of the invention with a disc-shaped cell 2. The cell 2 differs from the cell 2 by Figure 1 and 2 in that the cell 2 according to the second embodiment is penetrated by a plurality of slots 20 running in a straight line in one plane as flow channels for the working gas. The slit-shaped flow channels 20 run parallel to one another, but end in front of the edge of the cell 2, so that the cell 2 cannot fall apart. In the cuboid areas enclosed by cell walls 4 between the slit-shaped flow channels 20 there are tubular cavities 6 with a rectangular cross section. All the cavities 6 open into a peripheral channel 24 provided at the edge of the disc-shaped cell 2, so that the cavities 6 and the peripheral channel 24 form a single cavity.

Bei der Herstellung der scheibenförmigen Zelle 2 mittels 3D-Druck verbleiben zunächst eine oder zwei größere Öffnungen 22 durch die das lose 3D-Druck-Material noch dem 3D-Druck ausgeblasen werden kann. Diese Öffnungen werden anschließend verschlossen, so das lediglich eine oder mehrere Druckausgleichsöffnungen 8 in Form von Kapillaren verbleiben. Es lassen sich auch mehrere Zellen 2 in Strömungsrichtung des Arbeitsgases hintereinander anordnen, wodurch sich ein Regenerator mit höherer Leistung ergibt.When the disc-shaped cell 2 is produced by means of 3D printing, one or two larger openings 22 initially remain through which the loose 3D printing material can be blown out before the 3D printing. These openings are then closed so that only one or more pressure equalization openings 8 remain in the form of capillaries. It is also possible to arrange several cells 2 one behind the other in the flow direction of the working gas, resulting in a regenerator with a higher output.

Fig. 4 zeigt eine dritte Ausführungsform der Erfindung, bei der eine Mehrzahl von Zellen 2-1, 2-2, 2-3 übereinander gestapelt sind. Die drei scheibenförmigen Zellen 2-i mit kreisförmigem Querschnitt weisen einen identischen Aufbau auf. Die Zellen 2-i ähneln der Zelle 2 der zweiten Ausführungsform und unterscheiden sich von der Zelle nach Figur 1 und 2 dadurch, dass die Zellen 2-i von einer Mehrzahl von geradlinig in einer Ebene verlaufenden Schlitzen 20 als Strömungskanäle für Arbeitsgas durchsetzt sind. Die schlitzförmigen Strömungskanäle 20 verlaufen parallel zueinander, enden jedoch vor dem Rand der Zellen 2-i, sodass die die Zelle 2 nicht auseinander fallen kann. In den durch Zellwände 4 umschlossenen quaderförmigen Bereichen zwischen den schlitzförmigen Strömungskanälen 20 befinden sich rohrförmige Hohlräume 6-i, die einen Querschnitt in Form eines gleichseitigen Dreiecks mit rechtem Winkel aufweisen. Die Spitze des Dreiecks mit dem rechten Winkel zeigt nach oben, so dass sich die beiden Seiten des gleichseitigen Dreiecks in einem Winkel von 45° nach oben erstrecken. Hohlräume 6-i mit dreieckigem Querschnitt lassen sich leicht mittels 3D-Druck herstellen. Bei der Herstellung der scheibenförmigen Zellen 2 mittels 3D-Druck verbleibt zunächst eine oder zwei größere Öffnungen 22 durch die das lose 3D-Druck-Material noch dem 3D-Druck ausgeblasen werden kann. Diese Öffnungen werden anschließend verschlossen, so das lediglich eine oder mehrere Druckausgleichsöffnungen 8 in Form von Kapillaren verbleiben. 4 1 shows a third embodiment of the invention, in which a plurality of cells 2-1, 2-2, 2-3 are stacked one on top of the other. The three disk-shaped cells 2-i with a circular cross-section have an identical structure. The cells 2-i are similar to the cell 2 of the second embodiment and differ from the cell by Figure 1 and 2 in that the cells 2-i are penetrated by a plurality of slots 20 running in a straight line in one plane as flow channels for the working gas. The slit-shaped flow channels 20 run parallel to one another, but end in front of the edge of the cells 2-i, so that the cell 2 cannot fall apart. In the cuboid areas enclosed by cell walls 4 between the slit-shaped flow channels 20 there are tubular cavities 6-i, which have a cross-section in the form of an equilateral triangle with a right angle. The apex of the right-angled triangle points upwards, so that the two sides of the equilateral triangle extend upwards at a 45° angle. Cavities 6-i with a triangular cross-section can be easily produced using 3D printing. When the disc-shaped cells 2 are produced by means of 3D printing, one or two larger openings 22 initially remain through which the loose 3D printing material can still be blown out for the 3D printing. These openings are then closed so that only one or more pressure equalization openings 8 remain in the form of capillaries.

Die Hohlräume 6-i sind am Rand der scheibenförmigen Zellen 2-i miteinander verbunden. Eine Druckausgleichsöffnung 8 verbindet die Hohlräume 6-i mit dem Bereich außerhalb der Zellen 2-i. Die Zellen 2-i weisen auf ihrer Oberseite eine Mehrzahl von Ausrichtzapfen 30 auf und an der gegenüberliegenden Seite sind entsprechende Ausrichtvertiefungen 32 angeordnet. Durch diese Ausrichtelemente 30, 32 wird erreicht, dass die schlitzförmigen Strömungskanäle 20 der übereinander liegenden Zellen 6-i zueinander fluchten, sodass sich durch den Regenerator durchgehende Strömungskanäle ergeben. Zwischen den einzelnen Zellen 6-i ist jeweils eine thermisch-isolierende Schicht 34 angeordnet, die von dem Ausrichtzapfen 30 durchsetzt wird, sodass die Ausrichtzapfen in die darüber liegenden Ausrichtöffnungen 32 eingreifen können.The cavities 6-i are connected to one another at the edge of the disc-shaped cells 2-i. A pressure equalization opening 8 connects the cavities 6-i with the area outside the cells 2-i. The cells 2-i have a plurality of alignment pins 30 on their upper side and corresponding alignment depressions 32 are arranged on the opposite side. Through these alignment elements 30, 32 is achieved that the slit-shaped flow channels 20 of the cells 6-i lying one above the other are aligned with one another, so that continuous flow channels result through the regenerator. A thermally insulating layer 34 is arranged between the individual cells 6 - i, through which the alignment pin 30 passes, so that the alignment pins can engage in the alignment openings 32 located above.

Fig. 5 zeigt schematisch eine vierte Ausführungsform des Regenerators in Form einer scheibenförmigen Zelle 2, die sich von den Zellen 2-i nach Fig. 4 dadurch unterscheidet, dass statt einem rohrförmigem Hohlraum mit Dreiecksquerschnitt jeweils zwei rohrförmige Hohlräume 6a und 6b vorgesehen sind. Der Querschnitt der rohrförmigen Hohlräume 6a und 6b weist ebenfalls die Form eines gleichseitigen Dreiecks mit rechtem Winkel auf. Der rechte Winkel setzt an der Innenseite der Trennwand 4 an, die die schlitzförmigen Strömungskanäle begrenzt. Hierdurch ergibt sich eine Trennwand 4 mit konstanter Wandstärke zwischen den Strömungskanälen 20 und den Hohlräumen 6-i. Dies führt zu einem verbesserten Wärmeübergang zwischen dem Arbeitsgas im Strömungskanal 20 und dem Helium in den Hohlräumen 6a und 6b. Die Druckausgleichsöffnung 8 verbindet die Hohlräume 6a, 6b mit dem Bereich außerhalb der Zelle 2. figure 5 shows schematically a fourth embodiment of the regenerator in the form of a disk-shaped cell 2, which differs from the cells 2-i according to 4 differs in that instead of a tubular cavity with a triangular cross section, two tubular cavities 6a and 6b are provided. The cross section of the tubular cavities 6a and 6b is also in the shape of a right-angled equilateral triangle. The right angle begins on the inside of the partition wall 4, which delimits the slit-shaped flow channels. This results in a partition 4 with a constant wall thickness between the flow channels 20 and the cavities 6-i. This leads to an improved heat transfer between the working gas in the flow channel 20 and the helium in the cavities 6a and 6b. The pressure equalization opening 8 connects the cavities 6a, 6b with the area outside the cell 2.

Fig. 6 zeigt eine fünfte Ausführungsform der Erfindung, die sich von der Ausführungsform nach Figur 4 lediglich dadurch unterscheidet, dass die rohrförmigen Hohlräume 6a, 6b mit Dreiecksquerschnitt mit der Basis des rechtwinkligen Dreiecks zu den Strömungskanälen 20 hin angeordnet sind. Da die Basis die Länge der Seite des gleichseitigen Dreiecks ist, wird hierdurch der Wärmeübergang verbessert. 6 shows a fifth embodiment of the invention, which differs from the embodiment according to FIG figure 4 differs only in that the tubular cavities 6a, 6b are arranged with triangular cross section with the base of the right triangle towards the flow channels 20. Since the base is the length of the side of the equilateral triangle, this improves heat transfer.

Figuren 7 und 8 zeigen schematisch den Aufbau einer sechsten Ausführungsform, die nicht durch die beanspruchte Erfindung abgedeckt ist. Fig. 7 zeigt einen Regenerator 101 mit einer Vielzahl von Zellen 102, die in Form einer 3-dimensionalen Matrix 103 mit zwei Lagen von Zellen 102 angeordnet sind. Die Zellen 102 sind würfelförmig und grundsätzlich in ihrem Aufbau identisch. Da jedoch der Regenerator 101 einen Rohrquerschnitt ausfüllt, weisen die Zellen 102 im Randbereich zwangsweise eine abweichende Form auf. Die einzelnen Zellen 102 umfassen jeweils einen würfelförmigen Hohlraum 106 mit einer Wärme leitenden Hülle 104 und einer Druckausgleichsöffnung 108 in Form einer Kapillare. Wie aus Fig. 8 zu ersehen ist, sind die einzelnen Zellen 102 in Strömungsrichtung 112 des Arbeitsgases hintereinander versetzt angeordnet. Die nebeneinander liegenden Zellen 102 sind mittels thermisch leitender Verbindungselemente 114 miteinander verbunden. Die in Strömungsrichtung 112 hintereinander liegenden Zellen 102 sind mit thermisch isolierenden bzw. schlecht leitenden Verbindungselementen 116 miteinander verbunden und bilden einen Strömungskanal 120. Auf diese Weise ergibt sich die mechanisch feste Matrixanordnung 103 aus Zellen 102. In Fig. 7 sind lediglich zwei Lagen von Zellen 102 gezeigt, während in Fig. 8 drei Schichten bzw. Lagen von Zellen 102 gezeigt sind. Das Gasvolumen der einzelnen Hohlräume 106 beträgt ca. 1mm2, die Wandstärke der Hülle 104 beträgt ca. 0,2 mm. Der Abstand zwischen den einzelnen Zellen 102 beträgt ca. 0,2 mm. Der gesamte Platzbedarf einer Zelle 102 beträgt ca. 8mm3. figures 7 and 8th Fig. 12 schematically show the structure of a sixth embodiment not covered by the claimed invention. 7 FIG. 1 shows a regenerator 101 with a large number of cells 102 which are arranged in the form of a 3-dimensional matrix 103 with two layers of cells 102. FIG. The cells 102 are cubic and basically identical in construction. However, since the regenerator 101 fills a pipe cross section, the cells 102 inevitably have a different shape in the edge area. The individual cells 102 each comprise a cube-shaped cavity 106 with a heat-conducting shell 104 and a pressure equalization opening 108 in the form of a capillary. How out 8 can be seen, the individual cells are 102 arranged offset one behind the other in the direction of flow 112 of the working gas. The cells 102 lying next to one another are connected to one another by means of thermally conductive connecting elements 114 . The cells 102 lying one behind the other in the direction of flow 112 are connected to one another with thermally insulating or poorly conducting connecting elements 116 and form a flow channel 120. This results in the mechanically strong matrix arrangement 103 of cells 102. In Figure 7 only two tiers of cells 102 are shown, while in 8 three layers of cells 102 are shown. The gas volume of the individual cavities 106 is approximately 1 mm 2 , the wall thickness of the shell 104 is approximately 0.2 mm. The distance between the individual cells 102 is approximately 0.2 mm. The total space requirement of a cell 102 is approximately 8 mm 3 .

Der erfindungsgemäße Regenerator 101 wird vorzugsweise in der kältesten Kaltstufe eines Kryo-Kühlers als Tieftemperatur-Regeneratorabschnitt 242 eingesetzt.The regenerator 101 according to the invention is preferably used as a low-temperature regenerator section 242 in the coldest cold stage of a cryocooler.

Figuren 9 und 10 zeigen siebte Ausführungsform der Erfindung, bei der die Zelle 2 mit schlitzförmigen Strömungskanälen 20 entsprechend den Ausführungsformen nach den Figuren 3 bis 6. Der Unterschied zu den Ausführungsformen nach den Figuren 4 bis 6 besteht in der Form der rohrförmigen Hohlräume 6'. Die Hohlräume 6' sind wie bei der zweiten Ausführungsform nach Fig. 3a und 3b im Querschnitt rechteckig. Die Herstellung erfolgt - im Gegensatz zu der zweiten Ausführungsform in zwei Schritten mit wenigstens zwei Komponenten. Zunächst wird eine erste Komponente 40 mit "offenen Hohlräumen" bzw. mit topfförmigen Vertiefungen 42 erzeugt, z. B. mittels 3D-Druck. Loses 3D-Druck-Material wird in einem zweiten Schritt aus den topfförmigen Vertiefungen entfernt. Dann werden die Vertiefungen 42 in einem dritten Schritt durch zweite Komponenten 44 abgedeckt. Die ersten und zweiten Komponenten 40, 44 werden dauerhaft miteinander verbunden, z. B. durch Verklebung oder Verschweißung. Figures 9 and 10 show seventh embodiment of the invention, in which the cell 2 with slit-shaped flow channels 20 according to the embodiments according to Figures 3 to 6 . The difference from the embodiments according to the Figures 4 to 6 consists in the form of the tubular cavities 6'. The cavities 6' are as in the second embodiment Figures 3a and 3b rectangular in cross section. In contrast to the second embodiment, production takes place in two steps with at least two components. First, a first component 40 with “open cavities” or with cup-shaped depressions 42 is produced, e.g. B. by means of 3D printing. In a second step, loose 3D printing material is removed from the cup-shaped indentations. Then, in a third step, the depressions 42 are covered by second components 44 . The first and second components 40, 44 are permanently joined together, e.g. B. by gluing or welding.

Fig. 11 zeigt eine achte Ausführungsform der Erfindung in Form einer scheibenförmigen Zelle 2, die aus einer ersten und einer zweiten Halbzelle 50, 52 zusammengesetzt ist, so dass sich eine Zelle 2 ergibt die analog den Ausführungsformen nach Fig. 5 und 6 zwischen den schlitzförmigen Strömungskanälen 20 Strukturen im Querschnitt quaderförmige Strukturen aufweist. Beide Halbzellen 50, 52 weisen jeweils eine Mehrzahl von ersten und zweiten Hohlräumen 54 und 56 mit einem Querschnitt eines gleichschenkeligen Dreiecks auf. Die beiden Halbzellen 50, 52 lassen sich mittels 3D-Druck herstellen. Die beiden Halbzellen weisen jeweils eine plane Seite 58 und eine unebene Seite 60 auf. Die beiden unebenen Seiten 60 weisen eine komplementäre Form auf und wenn die beiden Halbzellen 50, 52 zusammengesetzt sind, liegen die komplementären unebenen Seiten 60 der beiden Halbzellen aufeinander. Im Vergleich zu den Ausführungsformen nach Fig. 4 bis 6 vergrößert sich bei den Regeneratoren mit Zellen 2, die jeweils zwei Halbzellen 50, 52 aufweisen der Anteil des Hohlraumvolumens am Gesamtvolumen des Regenerators. Der Regenerator wird dadurch leistungsfähiger. 11 shows an eighth embodiment of the invention in the form of a disc-shaped cell 2, which is composed of a first and a second half-cell 50, 52, so that a cell 2 results analogously to the embodiments according to FIG figure 5 and 6 between the slit-shaped flow channels 20 has cuboid structures in cross-section. Both half-cells 50, 52 each have a plurality of first and second cavities 54 and 56 having a cross section of an isosceles triangle. The two half-cells 50, 52 can be produced using 3D printing. The two half-cells each have a flat side 58 and an uneven side 60 . The two uneven sides 60 have a complementary shape and when the two half-cells 50, 52 are assembled, the complementary uneven sides 60 of the two half-cells lie on top of each other. Compared to the embodiments according to Figures 4 to 6 increases in the regenerators with cells 2, each having two half-cells 50, 52, the proportion of the cavity volume in the total volume of the regenerator. This makes the regenerator more efficient.

Analog der zweiten Ausführungsform nach Fig. 3a und 3b weisen auch die Ausführungsformen nach Fig. 4 bis 6 und 9 bis 11 einen umlaufenden Kanal 24 auf.Analogous to the second embodiment Figures 3a and 3b also show the embodiments Figures 4 to 6 and 9 to 11 a circumferential channel 24 on.

Die Druckausgleichsöffnung 8 ist in den Figuren 2 bis 6 und 9 bis 11 nicht eingezeichnet aber vorhanden. Da die Hohlräume 6-i; 6', 6a, 6b miteinander verbunden sind, kann die Druckausgleichsöffnung 8 an beliebiger Stelle der Zellen 2 vorgesehen sein.The pressure equalization opening 8 is in the Figures 2 to 6 and 9 to 11 not marked but available. Since the cavities 6-i; 6′, 6a, 6b are connected to one another, the pressure equalization opening 8 can be provided at any point in the cells 2.

Die Figuren 12a, 12b und 12c zeigen mögliche weitere Querschnittsformen der Hohlräume 6 in den scheibenförmigen Regeneratoren nach den Figuren 3 bis 6 und 11, die sich einfach mittels 3D-Druck herstellen lassen.the Figures 12a, 12b and 12c show possible further cross-sectional shapes of the cavities 6 in the disk-shaped regenerators according to FIG Figures 3 to 6 and 11 that can be easily produced using 3D printing.

Bezugszeichenliste:Reference list:

11
Regeneratorregenerator
22
Zellecell
44
Zellwandcell wall
4i4i
Innenseite der Zellwand 4Inside of the cell wall 4
4a4a
Außenseite der Zellwand 4Outside of the cell wall 4
6, 6-i, 6a, 6b6, 6-i, 6a, 6b
Hohlraumcavity
88th
Druckausgleichsöffnungpressure equalization opening
1010
Strömungskanal für ArbeitsgasFlow channel for working gas
1212
Ringspalt zwischen 2 und 10Annular gap between 2 and 10
2020
schlitzförmige Strömungskanäle für Arbeitsgasslit-shaped flow channels for working gas
2222
Ausblasöffnungenexhaust openings
2424
umlaufender Verbindungskanalperipheral connecting channel
3030
Ausrichtzapfenalignment pin
3232
Ausrichtvertiefungenalignment dimples
3434
thermisch isolierende Schichtthermally insulating layer
4040
erste Komponente mit topfförmigen Vertiefungenfirst component with cup-shaped indentations
4242
topfförmige Vertiefungenpot-shaped indentations
4444
Abdeckungencovers
5050
erste Halbzellefirst half cell
5252
zweite Halbzellesecond half cell
5454
erste Hohlräumefirst cavities
5656
zweite Hohlräumesecond cavities
5858
plane Seite von 50, 52flat side of 50, 52
6060
uneben Seite von 50, 52uneven side of 50, 52
101101
Regeneratorregenerator
102102
Zellencells
103103
Matrixanordnungmatrix arrangement
104104
Hülle bzw. Zellwändeshell or cell walls
106106
Hohlraumcavity
108108
Druckausgleichsöffnungpressure equalization opening
112112
Strömungsrichtung des ArbeitsgasesFlow direction of the working gas
114114
thermisch leitende Verbindungselementethermally conductive fasteners
116116
thermisch isolierende Verbindungselementethermally insulating fasteners
120120
Strömungskanalflow channel
220220
erste Kaltstufefirst cold stage
222222
zweite Kaltstufesecond cold stage
224224
erstes Pulsrohrfirst pulse tube
226226
erster Regeneratorfirst regenerator
228228
zweites Pulsrohrsecond pulse tube
230230
zweiter Regeneratorsecond regenerator
232232
Verbindungsmittellanyard
234234
Arbeitsgasleitungenworking gas lines
236236
Ventilevalves
238238
Balastvolumenballast volume
240240
erster Regeneratorabschnitt von 230first regenerator section of 230
242242
Tieftemperatur-Regeneratorabschnitt von 230Cryogenic regenerator section of 230
244244
Metallsiebe in 230Metal screens in 230
246246
Kügelchen aus seltenen ErdverbindungenRare earth compound globules

Claims (15)

  1. Regenerator for cryo-coolers with helium as a working gas, comprising
    at least one cell (2) with cell walls (4) including an exterior (4a) and an inner side (4i);
    wherein the cell walls (4) are at least partly heat conductive,
    the at least one cell (2) has a plurality of cavities (6; 6-i; 6a, 6b) connected with each other, which are surrounded by cell walls (4),
    the exterior (4a) of the cell walls (4) at least partly delimits a flow channel for the helium working gas;
    the at least one cell (2) has a pressure-equalizing opening (8), and
    the at least one cell (2) includes flow channels (20) for the working gas, which are delimited by cell walls (4; 104), and
    the cavities (6; 6-I; 6a, 6b) are filled with helium gas as a heat storage material,
    characterized in that
    the pressure-equalizing opening (8) is formed as a capillary, and
    the flow channels (20) are formed as a plurality of slots extending rectilinearly and parallel to each other and end before the rim of the cell (2) so that the cell (2) cannot fall apart,
    a circumferential channel (24) is formed at the rim of the cell (2) into which the plurality of cavities (6; 6-i; 6a, 6b) connected with each other open.
  2. Regenerator according to one of the preceding claims, characterized in that the at least one cell (2) is formed as a disk with a round cross-section.
  3. Regenerator according to one of the preceding claims, characterized in that a plurality of cells (2) is arranged one behind the other in a flow direction of the working gas.
  4. Regenerator according to claim 3, characterized in that cells (2) arranged one behind the other in a flow direction of the working gas are separated from each other by a thermally insulating layer (34) including flow channels (20) for the working gas.
  5. Regenerator according to claim 4, characterized in that the cells (2) and the thermally insulating layer (34) each have alignment elements (30, 32), so that the flow channels (20) of the cells (2) and the thermally insulating layer or layers (34) are in alignment with each other.
  6. Regenerator according to claim 5, characterized in that the alignment elements include a plurality of alignment pins (30) on one side of the cells (2) and complementarily formed aligning recesses (32) on the other side of the cells.
  7. Regenerator according to claim 6, characterized in that the thermally insulating layer (34) includes alignment openings that are permeated by the alignment pins (30), so that the flow channels (20) for the working gas in the cells (2) and in the thermally insulating layer (34) are in alignment with each other.
  8. Regenerator according to one of the preceding claims, characterized in that the pressure-equalizing opening (8) results on account of leaks occurring during production of the regenerator.
  9. Regenerator according to one of the preceding claims, characterized in that the exterior of the cell walls (4) has turbulence structures in the flow channels (20) for the working gas.
  10. Regenerator according to one of the preceding claims, characterized in that the cavities (6-i; 6', 6a, 6b) have the shape of a tube and a cross-section in form of a triangle, a cross-section in form of a rectangle, or a cross-section with at least one slanting cell wall.
  11. Regenerator according to claim 10, characterized in that in a plurality of tube-shaped cavities (6-i, 6', 6a, 6b), flow channels (20) for the working gas are arranged per cell (2) between the tube-shaped cavities (6-i, 6', 6a, 6b).
  12. Regenerator according to one of the preceding claims, characterized in that
    the cells (2) are composed of two half cells (51, 50), each including a plurality of cavities with a cross-section in form of a triangle,
    that the tube-shaped cavities (6-i; 6'; 6a, 6b) are arranged between the flow channels (20) for the working gas,
    that each of the half cells has a flat side and an uneven side,
    that the uneven sides of the two half cells are formed complementarily to each other, and
    that the two complementary uneven sides of the two half cells contact each other.
  13. Method for producing a regenerator according to one of the preceding claims, characterized in that the cell (2) is produced by 3D printing.
  14. Method for producing a regenerator according to one of claims 1 to 12, characterized in that the cell (2) is produced from at least two components (40, 44), which, after manufacture of the two components (40, 44), are connected to each other, and that at least one component (40) has a recess (42) forming at least part of the cavity/cavities (6').
  15. Cryo-cooler in form of a Stirling cooler, a Gifford-McMahon cooler or a pulse tube cooler including at least one regenerator (1), characterized in that the at least one regenerator (1) is a regenerator according to one of the preceding claims 1 to 12.
EP17832047.9A 2016-12-08 2017-12-06 Regenerator for a cryo-cooler with helium as a working gas, a method for producing such a regenerator, and a cryo-cooler comprising such a regenerator Active EP3551947B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE202016106860.6U DE202016106860U1 (en) 2016-12-08 2016-12-08 Regenerator for cryocooler with helium as working gas
DE102017203506.4A DE102017203506A1 (en) 2016-12-08 2017-03-03 Regenerator for cryocooler with helium as working gas, a method for producing such a regenerator and a cryocooler with such a regenerator
PCT/EP2017/081750 WO2018104410A1 (en) 2016-12-08 2017-12-06 Regenerator for a cryo-cooler with helium as a working gas, a method for producing such a regenerator, and a cryo-cooler comprising such a regenerator

Publications (2)

Publication Number Publication Date
EP3551947A1 EP3551947A1 (en) 2019-10-16
EP3551947B1 true EP3551947B1 (en) 2022-09-14

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EP17832047.9A Active EP3551947B1 (en) 2016-12-08 2017-12-06 Regenerator for a cryo-cooler with helium as a working gas, a method for producing such a regenerator, and a cryo-cooler comprising such a regenerator

Country Status (6)

Country Link
US (1) US11333406B2 (en)
EP (1) EP3551947B1 (en)
JP (2) JP2019536972A (en)
CN (1) CN110050161B (en)
DE (2) DE202016106860U1 (en)
WO (1) WO2018104410A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10041747B2 (en) * 2010-09-22 2018-08-07 Raytheon Company Heat exchanger with a glass body
FR3090840B1 (en) * 2018-12-20 2021-01-08 Univ Franche Comte Regenerator and method of manufacturing such a regenerator
DE202021100084U1 (en) 2021-01-11 2022-04-12 Pressure Wave Systems Gmbh Regenerator for cryo-cooler with helium as working gas and as heat storage material and a cryo-cooler with such a regenerator

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4359872A (en) * 1981-09-15 1982-11-23 North American Philips Corporation Low temperature regenerators for cryogenic coolers
JPS62233688A (en) * 1986-03-31 1987-10-14 Aisin Seiki Co Ltd Heat accumulator
JP2558810B2 (en) * 1988-05-14 1996-11-27 住友電気工業株式会社 Manufacturing method of sintered hollow parts
JP2697470B2 (en) * 1992-04-08 1998-01-14 ダイキン工業株式会社 Regenerator and manufacturing method thereof
EP0637727A3 (en) * 1993-08-05 1997-11-26 Corning Incorporated Cross-flow heat exchanger and method of forming
DE4401246A1 (en) * 1994-01-18 1995-07-20 Bosch Gmbh Robert regenerator
JPH07318181A (en) * 1994-05-20 1995-12-08 Daikin Ind Ltd Very low temperature freezer
US6131644A (en) * 1998-03-31 2000-10-17 Advanced Mobile Telecommunication Technology Inc. Heat exchanger and method of producing the same
DE19924184A1 (en) 1999-05-27 2000-11-30 Christoph Heiden Arrangement for using specific heat of helium gas in regenerators for low temperature gas refrigeration machines uses one of two types of helium gas regenerators with refrigeration machine
DE10318510A1 (en) * 2003-04-24 2004-11-11 Leybold Vakuum Gmbh Heat storage medium
DE10319510B4 (en) 2003-04-30 2016-12-29 Zumtobel Lighting Gmbh Busbar system for luminaires and locking element for use in a busbar system
DE102005007627A1 (en) * 2004-02-19 2005-09-15 Siemens Ag A cryogenic refrigeration regenerator is filled with a higher thermal capacity material than the system gas pulsed through it
JP5468424B2 (en) * 2010-03-12 2014-04-09 住友重機械工業株式会社 Regenerator, regenerative refrigerator, cryopump, and refrigeration system
CN102812311B (en) * 2010-03-19 2015-05-20 住友重机械工业株式会社 Cold storage apparatus, gifford-mcmahon cooler, and pulse tube refrigerator
JP2014501868A (en) * 2010-11-18 2014-01-23 エタリム インコーポレイテッド Stirling cycle converter device
JP5790989B2 (en) * 2011-05-10 2015-10-07 独立行政法人国立高等専門学校機構 Regenerator
CN104197591B (en) * 2014-08-29 2016-11-30 浙江大学 Use helium as the deep hypothermia regenerator of backheat medium and vascular refrigerator thereof
JP6185954B2 (en) * 2015-03-31 2017-08-23 ミネベアミツミ株式会社 Spherical plain bearing and manufacturing method thereof

Also Published As

Publication number Publication date
WO2018104410A1 (en) 2018-06-14
US20190323737A1 (en) 2019-10-24
CN110050161B (en) 2021-06-04
DE202016106860U1 (en) 2018-03-09
EP3551947A1 (en) 2019-10-16
US11333406B2 (en) 2022-05-17
JP2019536972A (en) 2019-12-19
CN110050161A (en) 2019-07-23
DE102017203506A1 (en) 2018-06-14
US20220057114A9 (en) 2022-02-24
JP2022084912A (en) 2022-06-07

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