Cryogenic apparatus for operation with liquid helium and method of operating same - Patents.com

Abstract

A cryogenic storage apparatus for operation with liquid helium includes a primary chamber (2) having a main region (4) and a pot region (6) for containing a reservoir (8) of liquid helium-4, and primary inlet means (12) for introducing liquid helium-4 and primary outlet means (14) for discharging gaseous helium-4, the primary inlet means comprising a transfer line (16) extending into the primary region. The cryogenic storage apparatus is configured for operation at reduced helium-4 pressure under a continuous supply of liquid helium-4, whereby gaseous helium-4 is pumped through the outlet means. The primary chamber includes a baffle structure (18) arranged between the pot region and the main region, the baffle structure defining at least one flow path (20a, 20b) for the flow of gaseous helium-4, each flow path forming a bypass connection between the pot region and the main region.

Description

[Technical field]

[0001] The present invention relates generally to cryostat systems for operation with liquid helium. [Background technology]

[0002] A cryostat is a cooling device that allows for a constant low temperature environment. Generally, there are dry and wet cryostats. Dry systems work through closed gas compression or Peltier element methods. Wet cryostats, in contrast, use liquid cryogens, in particular helium, as the cooling medium. Bath and flow cryostats constitute two different approaches to wet cryogenics. Flow cryostats work by flowing liquid helium through a cold finger. In this manner, a compact cryostat with a constant temperature down to 3 K can be realized. Bath cryostats for helium are typically accompanied by an outer liquid nitrogen jacket to thermally shield the inner helium reservoir. Through a pumpable 1 K-pot connected to the main helium-4 reservoir, temperatures down to about 1.5 K can be reached. Adding an additional 1 K-pot for helium-3 allows for reaching 0.3 K.

[0003] However, these cryostat concepts have several shortcomings. Flow-type cryostats are limited in terms of achievable base temperatures, plus have poor helium consumption efficiency. Bath-type cryostats, in contrast, have slow cool-down times and are bulky due to large reservoirs of cryogens such as liquid helium and nitrogen. Furthermore, their operation requires an internal cryo-needle valve.

[0004] A comprehensive overview of cryostat technology can be found in Jack W. Ekin “Experimental Techniques for Low Temperature Measurements - Cryostat Design, Materials, and Critical-Current Testing” (2016) Oxford University Press ISBN 978-0-19-857054-7. A recent example of a flow cryostat is described in van der Linden et. al, “A compact and versatile dynamic flow cryostat for photon science”, Rev. Sci. Instr. 87, 115103 (2016).

[0005] SU529348A1 discloses a cryostat for a helium-4 bath designed to operate at ambient pressure. To reduce the evaporation rate of the liquid helium, the cryostat has a reduced diameter section formed as a corrugated tube with multiple external tail pins. The design appears to be optimized for a relatively large size since the drawings show a large object immersed in the helium-4 bath and resting on a knife edge type structure at the bottom of the bath container.

[0006] US2015 / 0276129A1 discloses a cryostat, particularly for use in magnetic resonance imaging (MRI) systems, and a method for reducing heat input into such a cryostat. The cryostat is designed to be portable while maintaining cryogenic conditions in its core. During operation, a liquid cryogen, particularly liquid helium-4, provides cooling for the superconducting magnet coils of the MRI system. For this purpose, the liquid helium-4 is cooled by an active refrigeration device having a cooling head that is immersed in a liquid helium-4 bath. For transport, the inactive refrigeration device is removed and the cryogenic conditions are maintained by the liquid helium-4. To minimize evaporative helium loss, a specially constructed insert is introduced into the opening that previously held the active refrigeration device. In particular, the insert defines a gas escape channel that is significantly longer than the length of the insert.

[0007] US5365750A discloses a remote refrigerated probe intended for cooling environments such as aquarium tanks and for certain other applications such as cooling photoprocessing baths. The probe is intended for immersion in the medium to be cooled and is connected to a condenser unit by an umbilical tube. Cooling of the medium surrounding the probe is achieved by thermal contact of the entire probe housing. To improve the cooling effect, refrigerated fluid enters the probe in a central duct and is then directed back to the condenser unit along a spiral path adjacent the inner surface of the probe housing.

[0008] SU1118843A1 discloses a "pipe-in-pipe" heat exchanger for use in steam generators and other high voltage heat exchangers. It contains an inner lower pipe and an outer pipe, covered on one side by a lid, the inner surface of which is provided with a convoluted surface.

[0009] US 4136526 A discloses a portable helium-3 cryostat arranged inside a portable helium-4 cryostat, which is configured in a manner essentially known per se by a dewager for a bath of liquid helium-4. [Prior art documents] [Patent documents]

[0010] [Patent Document 1] US Patent Application Publication No. 2015 / 0276129 [Patent Document 2] U.S. Pat. No. 4,136,526 Summary of the Invention [Means for solving the problem]

[0011] Despite the large number of existing cryostat designs, there is still a need for improved cryostat systems. In particular, it would be desirable to have a cryostat that has a compact and cost-effective design and still allows reaching temperatures in the range of 1.5 K to 1.8 K. This would also open up the possibility of implementing an additional cooling stage using helium-3 in an integrated compact design.

[0012] The above objectives are achieved by the cryogenic system of the present invention.

[0013] A cryogenic maintenance apparatus for operation with liquid helium comprises a primary chamber having a main region and a pot region for containing a bath of liquid helium-4, and further comprises primary inlet means for introducing liquid helium-4 and primary outlet means for discharging gaseous helium-4, the primary inlet means comprising a transfer line extending into the primary chamber. the cryogenic maintenance apparatus is configured for operation under a continuous supply of liquid helium-4; the cryostat is configured for operation at reduced helium-4 pressure, whereby gaseous helium-4 is pumped through the outlet means; the primary chamber comprises a baffle structure arranged between the pot region and the main region, the baffle structure defining at least one flow path for flow of gaseous helium-4; Each flow channel forms a bypass connection between a pot region and a main region.

[0014] The present invention provides a completely new type of wet cryogenics. Essentially, it consists of a pumpable heat exchanger together with a so-called "1K-pot" that is directly connected to an external helium dewar. This construction can be miniaturized down to the size of a fingertip while maintaining the same basic base temperature of a bath-type cryostat. The essential part, the pumpable heat exchanger, is a baffle structure, typically a spiral structure, which can be manufactured by 3D printing techniques.

[0015] Compared to bath-based cryostats, the present invention provides a much simplified concept that allows for miniaturization. It allows for compactness comparable to (or better than) flow-based cryostats, while retaining the basic base temperature of bath-based cryostat technology. The simplified design opens up the possibility for faster and cheaper manufacturing. More importantly, the compactness enables entirely new cryogenic applications. Most notably, it provides a practical solution for in-situ vacuum-operated cryogens.

[0016] Unless expressly defined otherwise, any positional indications such as "upper", "lower", "top", "bottom", "above" and "below" shall be understood with reference to the cryostat disposed in an operational position. It should be noted that depending on the design, the cryostat may be operated vertically, horizontally or in any other position.

[0017] The cryostat of the present invention is designed for operation with a minimized bath of liquid helium-4, which is maintained under reduced pressure, thereby correspondingly allowing the temperature to reach below its 4.2 K boiling point at atmospheric pressure. To this end, the cryostat is configured for operation under a continuous supply of liquid helium-4, leading to the formation of a bath of liquid helium-4 confined by the bottom surface of the primary chamber. The reduced helium-4 pressure is established by pumping gaseous helium-4, which is continuously evaporated from the bath through an outlet means by a pumping system connected to the outlet means of the cryostat. It is envisioned that the principles of the present invention may also be applied to other cryogens, such as liquid hydrogen or liquid nitrogen.

[0018] Generally, the cryostat includes some suitable flanges or other connection means to allow insertion of the primary chamber into the high vacuum environment. The term "continuous" in relation to the supply of liquid helium-4 shall be understood in a broad sense to include also supply over long periods of time, particularly interrupted by short pauses. In other words, continuous supply shall include a controlled flow of medium, which may be a steady flow or a patterned flow. A steady flow of medium is generally preferred, since on-off operation may lead to the ingress of gas in the transport lines, which may cause thermal leakage. "Controlled" shall have the meaning of providing a suitable rate in terms of the filling status of the liquid reservoir and in terms of evaporation rate. The cryostat also generally includes various components known in the art, such as temperature sensors, pressure gauges, resistance heaters, etc.

[0019] According to the present invention, the primary chamber contains a baffle structure positioned between the pot region and the main region. This baffle structure acts both as a heat exchange element and as an element that restricts the flow path of gaseous helium-4. In other words, the baffle acts as an obstacle for a simple linear gas flow. Depending on the design choice, the baffle structure defines at least one flow path for gaseous helium-4. Importantly, any of these flow paths shall form a roundabout connection between the pot region and the main region. In other words, the baffle structure shall prevent a straight line connection from any point in the pot region, in particular starting from any point on the surface of the helium-4 vessel, to the main region located above the baffle structure. Thus, "roundabout" shall be understood as equivalent to "indirect" or "non-linear". In combination, the baffle structure of the present invention provides heat exchange through the contact of gaseous helium-4 with the surface of its heat exchange element. Similarly, the baffle structure creates a flow restriction that allows a substantial pressure differential to be maintained between the gaseous region immediately above the helium vessel and the outlet means in the main region, and the baffle structure effectively blocks undesirable heat ingress from the main region by thermal radiation.

[0020] Flow restriction is important to maintain the low pressures required to keep the liquid helium-4 bath at temperatures well below 4.2 K, while keeping pumping rates and attendant helium consumption within acceptable limits.

[0021] Advantageous embodiments are defined in the dependent claims.

[0022] According to one embodiment (claim 2), the baffle structure has a heat exchange area (A H) of the heat exchange area. The heat exchange area is typically configured as a thin sheet with low thermal conductivity, preferably made of a low thermal conductivity metal, across which helium gas is forced to flow. Typically, the sheet has a thickness of 0.2 to 1 mm. In this context, the term "low thermal conductivity" is to be understood as a thermal conductivity at 4 K in the range of 0.01 to 10 W / (mK), in particular in the range of 0.1 to 1 W / (mK), more particularly in the range of 0.2 to 0.4 W / (mK). The heat exchange efficiency of the baffle structure is a function of the total area (A) of the heat exchange area. H Depending on the construction of the baffle structure, the heat exchange area may include a wall section in thermal contact with the sheet-like element that defines the flow path of the gaseous helium-4.

[0023] According to a preferred embodiment (claim 3), the average liquid / gas surface area A of the pot area S Heat exchange area A H is at least 1, particularly at least 2, more particularly at least 5, and even more particularly at least 10, for any operational cryostat orientation. The term "any operational cryostat orientation" shall be understood to include any orientation that prevents liquid helium from contacting the baffle structure and / or flowing freely out of the primary chamber.

[0024] In the present context, the pot area is to be understood as the part of the primary chamber suitable for containing a bath of liquid helium, i.e., which may be in contact with liquid helium in case of maximum filling. When liquid helium is present in the pot area, the respective liquid / gas surface has an area that generally depends on the orientation of the cryostat, more specifically on the orientation of its pot area, and on the liquid level (i.e., the liquid / gas surface may increase or decrease when the cryostat is tilted and / or the amount of liquid is changed). It should be noted that for any given cryostat orientation in physical space, the average liquid / gas surface area A Scan be clearly defined by taking the average over all possible liquid levels in the pot area, i.e., over the range between the empty and full pot areas for a given shape and orientation of the pot area. The term "average" is to be understood here as the arithmetic mean. The average liquid / gas surface area A S can be calculated analytically for some simple shaped pot regions, while in all other cases it can be calculated numerically. The numerical calculations can be performed using data from a computer-aided design (CAD) plane of the structure of interest.

[0025] According to another embodiment, the average cross-sectional area A of the pot region perpendicular to the direction between the pot region and the main region C Heat exchange area A H is at least 1, in particular at least 2, more particularly at least 5, and even more particularly at least 10. For further explanation, in this embodiment, the average cross-sectional area A C results from taking the average over all cross sections of the pot region, where such cross sections are perpendicular to the direction between the pot region and the main region. For simpler pot region shapes, such as a cylinder or a body with a longitudinal axis between the bottom of the pot region and the top of the pot region, the averaged pot region cross sections may be perpendicular to such axis. The term "average" is to be understood here as the arithmetic mean. The average cross-sectional area A c can be calculated analytically for some simple shaped pot regions, while in all other cases it can be calculated numerically.

[0026] The baffle structure may be configured in many ways, so long as it prevents any straight line connection starting from any point in the pot region to any point in the main region of the primary chamber, so that any connection therebetween is necessarily a roundabout connection. According to a preferred embodiment (claim 4), the baffle structure comprises at least one spiral surface leading from the pot region to the main region of the primary chamber. It is also possible and expedient for the baffle structure to have at least one further angularly offset spiral surface. In such a case, the baffle structure defines two or more roundabout flow paths starting from different locations in the pot region and terminating at different locations in the main region.

[0027] In principle, a transport line for delivering liquid helium-4 into the pot region can be arranged separately from the baffle structure, for example as a tubular channel arranged along the side wall of the primary chamber. According to an advantageous embodiment (claim 5), the baffle structure comprises a longitudinal passage, which receives the transport line therein. The term "receive in" is intended to imply that the transport line can be inserted over the entire length of the longitudinal passage or simply inserted into the topmost section of the longitudinal passage. In some embodiments, the longitudinal passage is arranged substantially in the center of the baffle structure. According to one advantageous embodiment (claim 6), the axial passage is formed as a tubular section integrally connected to the baffle structure.

[0028] According to a preferred embodiment (claim 7), the baffle structure, and optionally any connected structures, are made by 3D-printing technology. This technology, also known as additive manufacturing, makes it possible to form baffle structures of any desired shape, for example with multiple angularly displaced convoluted surfaces and longitudinal passages integrally connected in a single part. In one advantageous version, particularly suitable for achieving very compact cryostat designs, the baffle structure is integrally formed with the primary chamber by 3D-printing technology. Considering that the primary chamber shall be mounted in an ultra-high vacuum (UHV) environment, for example for surface-sensitive applications such as photoelectron spectroscopy, the question of UHV compatibility of such chambers formed by 3D-printing becomes important.

[0029] It is generally recognized that additive manufacturing of metal or plastic structures, which relies on some type of sintering or molding of materials supplied in particulate form, is not directly compatible with UHV conditions. Indeed, many 3D printed structures are not leak-proof in nature, but this does not imply that UHV-compatible 3D printed structures cannot be produced (see, for example, Vovrosh, J., Voulazeris, G., Petrov, PG et al. Additive manufacturing of magnetic shielding and ultra-high vacuum flange for cold atom sensors. Sci Rep 8, 2023 (2018). https: / / doi.org / 10.1038 / s41598-018-20352-x). It has been found that the degree of leak-proofness depends on many different parameters, such as the printing material itself, the grain size of the starting material, and the printing angle. It has also been found that initially leaky 3D printed structures can be made leak-proof through different methods. For metal printing of Permalloy-80, heat treatment has been shown to make 3D printed flanges compatible with conventional flanges, for example, and UHV conditions have been obtained with this method.

[0030] In many applications, it is preferred to arrange heat dissipation shields around a certain area of ​​the cryostat to reduce the radiative heat load from surrounding hot structures. Thus, according to one embodiment (claim 8), the cryostat further comprises a heat dissipation shield arranged to substantially surround at least the pot section of the primary chamber. As is known from cryogenics technology, such a heat dissipation shield can be cooled by thermal contact with an auxiliary cryogenic reservoir, in particular a liquid nitrogen reservoir. However, according to a particularly advantageous embodiment (claim 9), the heat dissipation shield can be cooled by thermal contact with an outer wall portion of the primary chamber. Such thermal contact is advantageously made over a significant portion of the main area so as to ensure a sufficiently large contact area. In this embodiment, the heat dissipation shield is cooled by transferring heat to the helium-4 gas being pumped through the baffle structure. It has been found that this type of heat dissipation shield embodiment, together with the primary chamber formed integrally with the baffle structure, makes it possible to reach the low temperatures of the helium-4 bath without the need for an additional (liquid nitrogen) reservoir, thus contributing to a compact design. For this purpose, the heat dissipation shield is made from a material having good thermal conductivity, such as copper.

[0031] The cryostat according to the invention can be realised with various types of primary chamber geometries, but is particularly advantageous when the primary chamber is substantially cylindrical (claim 10). When operated with its cylindrical axis substantially vertical, the average liquid / gas surface (A S ) and the average cross-sectional area of ​​the pot region (A C ) both correspond to the lower inner cylindrical surface of the baffle structure.

[0032] The practical outer diameter of the primary chamber ranges from 0.001 to 1 m. Typically, the primary chamber has an inner diameter in the range of 2 to 200 mm, in particular 5 to 100 mm, more particularly 10 to 80 mm, and most particularly about 20 to 30 mm. The chamber walls typically have a thickness of 0.2 to 1 mm. A typical cylindrical length, including the heat exchange bypass structure and the pot area, lies in the range of 0.03 to 3 m. The total volume enclosed by the outer cryostat wall is therefore about 2.4×10 -8 ~2.4m 3 This ranges from...

[0033] According to the generally intended mode of operation of the helium-4 cryostat, the external surface of the pot region is provided with a primary attachment means for external attachment of a sample (claim 11). The term "external" shall be understood here to refer to the side of the pot region that is not in contact with the helium-4 contained therein. In many cases, the primary attachment means is arranged at the bottom surface of the pot region, i.e., directly below the pot region, under operating conditions. However, the primary attachment means may also be arranged at some other region in close proximity to the liquid helium-4 bath, e.g., laterally therefrom. Such attachment means are generally known in cryogenics. They may be configured, for example, but not limited to, as brackets, clamps, frames, perforated platelets, or flanges. In many applications, the attachment means are made of metal and / or ceramic components. In contrast to certain applications in which the object to be cooled is immersed in the cryogenic liquid contained within the cryostat, the provision of external attachment means allows for the placement of the sample in an area outside the primary chamber, thereby greatly enhancing its accessibility for manipulation and inspection, including spectroscopic examination. It should be emphasized that the term "sample" is intended to apply to any object of interest that, for some scientific, medical, or material technical reasons, requires cryogenic conditions.

[0034] According to an advantageous embodiment (claim 12), the outlet means comprises coupling means for connecting to a helium pumping device. In a preferred embodiment, the coupling means for connecting the helium to the pumping device shall be gas-tight. The term "gas-tight" shall be understood as not allowing any passage of any gas, including helium, from the inner area of ​​the outlet means to the surrounding area and vice versa.

[0035] According to a particularly advantageous embodiment (claim 13), the cryostat further comprises a secondary chamber for operation with helium-3, secondary inlet means for helium-3 and secondary outlet means for helium-3. In particular (claim 14), such a cryostat may be configured for operation at reduced helium-3 pressure in the secondary chamber, whereby gaseous helium-3 is pumped through the secondary outlet means. As will be appreciated, such a design is generally intended to reach low temperatures, in particular in the range of 0.3 to 0.4 K.

[0036] Advantageously (claim 15), the secondary inlet means comprises a cannulated transport line, the cannulated transport line comprising: i) a curved section shaped to substantially follow the flow path of the baffle structure; and / or ii) a serpentine or spiral segment formed in a cannular transport line, the serpentine or spiral segment being in a region of the cannular transport line that is within a liquid helium-4 bath; The system is configured to pre-cool helium-3 supplied by

[0037] The secondary outlet means may be configured as a substantially straight tube. Alternatively, they may be configured as curved sections shaped to substantially follow the flow path of the baffle structure.

[0038] In accordance with the generally intended mode of operation of the Helium-3 cryostat, the exterior surface of the secondary chamber is provided with secondary attachment means for external attachment of a sample (Claim 16). The type, configuration, location, and use of such secondary attachment means are generally identical to the primary attachment means described above, with the only difference being that "external" refers to the secondary chamber.

[0039] According to a further aspect of the invention, a method for operating a cryogenic maintenance apparatus as defined above comprises a cooling phase followed by a steady-state phase, - in a cooling stage, liquid helium-4 is fed from an external reservoir through the primary inlet means into the pot region, thereby evaporatively cooling the liquid helium-4 until a bath of liquid helium-4 begins to accumulate on a bottom surface of the pot region; During the steady state phase, the liquid helium-4 bath temperature is maintained by adjusting the liquid helium-4 inlet flow rate and / or adjusting the rate at which gaseous helium-4 is pumped through the primary outlet means, and optionally by controlled heating.

[0040] According to an embodiment (claim 18) of the method, the bath temperature of the liquid Helium-4 is maintained within the range of 1.8K to 2.0K.

[0041] One embodiment (claim 19) for operating a cryogenic maintenance apparatus equipped with a secondary chamber for helium-3 comprises the following procedure to be performed during the steady-state phase of the primary system: after adjusting the bath temperature of liquid helium-4 to a suitable, preferably as low as possible, temperature, helium-3 is fed from an external reservoir through the secondary inlet means into the secondary chamber, thereby evaporatively cooling the helium-3 until a secondary bath of liquid helium-3 is formed, and thereafter maintaining the secondary bath temperature by adjusting the inlet flow rate of helium-3 and / or adjusting the rate of pumping of gaseous helium-3 through the secondary outlet means.

[0042] According to yet another aspect of the invention, the cryogenic maintenance apparatus as defined above is used to cool a sample, a detector element, a medical scanning device, a superconducting device, an electronic device, or an internal combustion engine component. The term "sample" shall be understood as any part of a material intended for investigation, characterization, or treatment, including, but not limited to, samples for spectroscopy, samples for microscopy, samples for medical or veterinary diagnostics, and samples for material science. The term "detector element" is not limited to a particular wavelength region, but may apply in particular to devices suitable for detection techniques including infrared, visible, and ultraviolet regions, but also SQUID magnetometers. The term "electronic device" generally refers to electronic circuitry, including classical and quantum computing devices.

[0043] According to a further aspect of the present invention, a cryogenic maintenance apparatus as defined above comprises: Spectroscopy, in particular -Raman spectroscopy -Photoelectron spectroscopy -Infrared Spectroscopy -X-ray absorption spectroscopy -Resonant inelastic X-ray scattering - Inelastic neutron or X-ray scattering -Scanning Tunneling Spectroscopy Diffraction measurements, in particular -X-ray diffraction on powders, single crystals and proteins -Neutron diffraction on powders and single crystals - Transmission electron microscopy on single crystals and proteins Electronic property measurements, in particular -Electrical transport properties such as Hall effect and resistivity - Thermoelectric transport measurements such as the Seebeck effect, the Nernst effect and the thermal Hall effect -Polar Kerr effect measurement -Torque and SQUID magnetization measurements Used for.

[0044] According to a further aspect of the invention there is provided a device configured to be cooled by a cryostat, such a device may include, inter alia, a device for performing spectroscopy, diffraction measurements or electronic property measurements.

[0045] According to another aspect of the invention, a sample holder is provided that is configured to be attached to a cryostat. The term "configured to" is intended to include that the sample holder is compatible with the cryostat dimensions and attachment means with which it is used. Such a sample holder may provide mechanical support for the sample and may provide means for keeping the sample in place. The sample holder may be made of metal and / or ceramic components and may be embodied in a variety of designs, with cylinders, arms, rods, or pylons being typical forms. The sample holder may include electrical / optical wiring or other means for electrical or optical conduction. The means for electrical or optical conduction may allow for the transfer of information, charge, current, heat, electric field to the sample or an area in the vicinity of the sample. The sample holder may include heating means for adjusting the temperature in the vicinity of the sample. The sample holder may further include various sensors in the vicinity of the sample to measure various parameters including, but not limited to, temperature, optical response, optical parameters, pressure, which may be adjusted to the needs of a particular application. The sample holder may be embodied in one, two or more parts. For example, in a two-part embodiment, there may be a tip part, which actually holds the sample, and is releasably connected to a base part, which in turn is attachable to a correspondingly configured attachment means of the cryostat. The tip part and base part of the sample holder may be connected by a simple plug-in mechanism, allowing for fast replacement of the first part.

[0046] According to one embodiment (claim 24), the sample holder comprises: Spectroscopy, in particular -Raman spectroscopy -Photoelectron spectroscopy -Infrared Spectroscopy -X-ray absorption spectroscopy -Resonant inelastic X-ray scattering - Inelastic neutron or X-ray scattering -Scanning Tunneling Spectroscopy Diffraction measurements, in particular -X-ray diffraction on powders, single crystals and proteins -Neutron diffraction on powders and single crystals - Transmission electron microscopy on single crystals and proteins Electronic property measurements, in particular -Electrical transport properties such as Hall effect and resistivity - Thermoelectric transport measurements such as the Seebeck effect, the Nernst effect and the thermal Hall effect -Polar Kerr effect measurement -Torque and SQUID magnetization measurements It is adapted for use in

[0047] According to a further embodiment (claim 25) the sample holder is adapted for use for cooling a sample, a detector device, a medical scanning device, a superconducting device, an electronic device, or an internal combustion engine component.

[0048] The general challenge in constructing a cryostat is to shield the cold finger, which is cooled by liquid helium, from the room temperature environment. Essentially, the task is to protect the cryogenic component (the cold finger) from the ambient temperature. The standard approach is to construct the cryostat skeleton from a poor thermally conductive material. In this way, heat transfer from the external environment is minimized. Between this skeleton and the cold finger, a heat exchanger is placed to counter the heat load arising from the ambient environment. This heat exchanger is cooled by gaseous helium evaporating from a liquid helium bath, and to be efficient, a material with good thermal conductivity is used and the surface area between the liquid and the heat exchanger is optimized.

[0049] The present invention uses a completely different approach. As in conventional cryostats, the framework is made of poorly conductive materials (stainless steel, CoCr, or polymer plastics). To minimize the heat load from the surrounding environment, it is preferable to reduce the cross-sectional area of ​​the framework structure. The key difference underlying the present invention is that the framework surface area is optimized. In this way, the framework, although poorly conductive, acts as a heat exchanger between the cold exhaust gas and the heat load from the surrounding environment. Thus, the full cooling power of the liquid helium can be used to directly cool the coldest part of the cryostat to which the sample is connected. In this way, the full cooling power from the liquid can be used to cool the sample, and only the return gas is used to cool the framework of the cryostat. This makes the cryostat more efficient and counters the heat load from the entire room temperature environment. Only the parts to which the sample is connected are made of excellent thermally conductive materials (oxygen-free copper, sapphire, etc.). To make the cryostat more efficient and to eliminate the liquid nitrogen shield, it is possible to connect the cooling shield directly to the framework over a relatively large area to have an efficient heat exchange as well. Thus, the shield is connected to a heat exchange structure with a large area to provide sufficient cooling power to cool the shield down to a temperature below 77K (i.e., liquid nitrogen temperature). All the above new concepts allow the cryostat to be minimized to small diameter and short length.

[0050] The present invention provides a new compact type cryostat, which has numerous advantages over existing concepts and has abundant possibilities for new cryogenic technology applications. The new and simplified design translates directly into less overall construction material, shorter production times, and therefore significantly reduced manufacturing costs. From a functionality standpoint, the cryostat design has a cooling down time that is substantially shorter than all existing designs. It therefore opens up new possibilities for activities with frequent sample changes. This is the case, for example, for neutron powder diffraction and protein structure studies, either with synchrotron radiation or transmission electron microscopy. In fact, with the use of the cryostat according to the invention, it makes sense to connect a sample change robot. The present invention also paves the way for miniature helium-3 and dilute (helium-3 and helium-4 mixture) cryostats. With the advent of quantum computing technology, compact refrigerators are certainly becoming very attractive. Compact cryogenic technology will also foster innovation in low-temperature vacuum operations. Conventional cryostat principles are generally opposed to in-situ vacuum powering. The present invention opens up new solutions to this long-standing problem. Flexible cryostat geometries also offer novel thermal shielding applications. Photon and electron analyzers / detectors could greatly benefit from this technology. Finally, physical property measurement systems in combination with magnetic field instrumentation are obvious applications.

[0051] The cryostat according to the present invention is distinguished by its compatibility with a variety of scientific settings and environments, including, but not limited to, four-circle Euler cradles, xyz and Rz manipulators, robotic sample exchangers, and hot bore magnets. The present invention provides, for example, the following: (Item 1) 1. A cryogenic apparatus for operation with liquid helium, comprising: a primary chamber (2) having a main region (4) and a pot region (6) for containing a bath (8) of liquid helium-4; a primary inlet means (12) for introducing liquid helium-4 and a primary outlet means (14) for discharging gaseous helium-4, said primary inlet means comprising a transfer line (16) extending into said primary chamber; Equipped with the cryostat is configured for operation under a continuous supply of liquid helium-4; the cryostat is configured for operation at reduced helium-4 pressure whereby gaseous helium-4 is pumped through the outlet means; the primary chamber comprises a baffle structure (18) arranged between the pot region and the main region, the baffle structure defining at least one flow passage (20a, 20b) for the flow of gaseous Helium-4; A cryogenic maintenance apparatus, characterized in that each flow passage forms a bypass connection between the pot region and the main region. (Item 2) The baffle structure (18) has a heat exchange area (A H 2. The cryogenic maintenance apparatus according to claim 1, having a heat exchange area having a (Item 3) The average liquid / gas surface area (A S ) to the heat exchange area (A H 3. The cryogenic temperature maintaining apparatus according to claim 2, wherein the ratio of (Item 4) 4. The cryogenic maintenance apparatus of any one of claims 1 to 3, wherein the baffle structure comprises at least one convoluted surface leading from the pot region to the main region of the primary chamber. (Item 5) 5. The cryogenic maintenance apparatus according to any one of claims 1 to 4, wherein the baffle structure (18) comprises an axial passageway, the axial passageway receiving the transport line (16) therein. (Item 6) 6. The cryogenic maintenance apparatus of claim 5, wherein the axial passage is formed as a tubular section integrally connected to the baffle structure (18). (Item 7) 7. The cryogenic maintenance apparatus of any one of claims 1 to 6, wherein the baffle structure, and optionally the primary chamber, are fabricated by 3D-printing technology. (Item 8) 8. The cryogenic maintenance apparatus of any one of claims 1 to 7, further comprising a heat dissipation shield disposed to substantially surround at least the pot region of the primary chamber. (Item 9) 9. The cryogenic maintenance apparatus of claim 8, wherein the heat dissipation shield is coolable by thermal contact with an exterior wall portion of the primary chamber. (Item 10) 10. The cryogenic maintenance apparatus of any one of claims 1 to 9, wherein the primary chamber is substantially cylindrical. (Item 11) 11. The cryogenic apparatus according to any one of claims 1 to 10, wherein the external surface (10) of the pot area is provided with a primary attachment means (17) for the external attachment of a sample. (Item 12) 12. The cryogenic maintenance apparatus according to any one of claims 1 to 11, wherein the outlet means comprises a coupling means for connecting to a helium pumping device. (Item 13) 13. The cryogenic maintenance apparatus according to any one of claims 1 to 12, further comprising a secondary chamber (32) for operation with helium-3, a secondary inlet means (34) for helium-3, and a secondary outlet means (36) for helium-3. (Item 14) Item 14. The cryogenic maintenance apparatus of item 13, configured for operation at reduced helium-3 pressure in the secondary chamber (32), whereby gaseous helium-3 is pumped through the secondary outlet means (36). (Item 15) The secondary inlet means (36) comprises a cannulated transfer line (38), the cannulated transfer line (38) comprising: i) a curved section (40) configured to substantially follow the flow path of the baffle structure (18); and / or ii) a serpentine or spiral section (42) formed in the cannular transport line, the serpentine or spiral section (42) being in a region of the cannular transport line that is within the liquid helium-4 bath; 15. The cryogenic maintenance apparatus of claim 12 or 14, configured for pre-cooling helium-3 provided by (Item 16) 16. The cryogenic maintenance apparatus of any one of claims 13 to 15, wherein the external surface of the secondary chamber (32) is provided with secondary attachment means (44) for external attachment of a sample. (Item 17) A method for operating a cryogenic maintenance apparatus according to any one of claims 1 to 16, comprising a cooling stage followed by a steady-state stage, during said cooling stage, liquid helium-4 is supplied from an external reservoir through said primary inlet means into said pot region, thereby evaporatively cooling the liquid helium-4 until a bath of liquid helium-4 begins to accumulate on a bottom surface of said pot region; wherein during the steady state phase, a bath temperature of liquid helium-4 is maintained by adjusting the inlet flow rate of liquid helium-4 and / or adjusting the rate at which gaseous helium-4 is pumped through the primary outlet means, and optionally by controlled heating. (Item 18) Item 18. The method according to item 17, wherein the liquid helium-4 bath temperature is maintained within a range of 1.4K to 1.5K. (Item 19) Item 18. The method for operating a cryogenic maintenance apparatus according to any one of items 13 to 16, wherein during the steady state phase, helium-3 is supplied from an external reservoir through the secondary inlet means into the secondary chamber region, thereby evaporatively cooling the helium-3 until a secondary bath of liquid helium-3 is formed, and thereafter maintaining the secondary bath temperature by adjusting the inlet flow rate of helium-3 and / or adjusting the rate of pumping of gaseous helium-3 through the secondary outlet means. (Item 20) 17. Use of the cryogenic maintenance apparatus according to any one of items 1 to 16 for cooling a sample, a detector device, a medical scanning device, a superconducting device, an electronic device, or an internal combustion engine component. (Item 21) Spectroscopy, in particular Raman spectroscopy, photoelectron spectroscopy, Infrared spectroscopy, X-ray absorption spectroscopy, Resonant inelastic X-ray scattering, Inelastic neutron or X-ray scattering, Scanning tunneling spectroscopy, Diffraction measurements, in particular X-ray diffraction, Neutron diffraction, Transmission electron microscopy, Electronic property measurements, in particular Electrical transport property measurements, Thermoelectric transport measurements, Polar Kerr effect measurement, Magnetization measurement Use of the cryogenic maintenance apparatus according to any one of items 1 to 16 for the purpose of (Item 22) 17. A device configured to be cooled by the cryogenic temperature maintaining apparatus according to any one of items 1 to 16. (Item 23) A sample holder (46) configured to be attached to a cryogenic maintenance apparatus according to any one of items 1 to 16. (Item 24) Spectroscopy, in particular Raman spectroscopy, photoelectron spectroscopy, Infrared spectroscopy, X-ray absorption spectroscopy, Resonant inelastic X-ray scattering, Inelastic neutron or X-ray scattering, Scanning tunneling spectroscopy, Diffraction measurements, in particular X-ray diffraction, Neutron diffraction, Transmission electron microscopy, Electronic property measurements, in particular Electrical transport property measurements, Thermoelectric transport measurements, Polar Kerr effect measurement, Magnetization measurement 24. The sample holder according to item 23, adapted for use in (Item 25) 24. The sample holder of item 23, adapted for use for cooling a sample, a detector device, a medical scanning device, a superconducting device, an electronic device, or an internal combustion engine component. [Brief description of the drawings]

[0052] The above-mentioned and other features and objects of the present invention and the manner in which they are accomplished will become more apparent, and the invention itself will be better understood, by reference to the following description of various embodiments of the invention, taken in conjunction with the accompanying drawings, in which:

[0053] [Figure 1] FIG. 1 is a first embodiment of a cryostat in a schematic vertical cross-section.

[0054] [Diagram 2] FIG. 2 is a second embodiment of a cryostat in a schematic vertical cross-section.

[0055] [Diagram 3] FIG. 3 is a second embodiment of a cryostat in a schematic vertical cross-section.

[0056] [Figure 4]FIG. 4 is a fourth embodiment of a cryostat in a schematic vertical cross-section.

[0057] [Diagram 5] FIG. 5 is a fifth embodiment of a cryostat in a schematic perspective, partially cut-away view.

[0058] [Figure 6] FIG. 6 is the lower part of the cryostat of FIG. 5 in an enlarged representation.

[0059] [Figure 7] FIG. 7 shows a sixth embodiment of a cryostat in a schematic perspective view. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0060] The cryostat shown in Figure 1 comprises a primary chamber 2 having a main region 4 and a pot region 6 containing a bath 8 of liquid helium-4. The pot region 6 is bounded by a bottom surface 10 of the primary chamber, which in this example has at its bottom an internal diameter d i and configured as a cylindrical tube forming a pot having a constant cylindrical cross-sectional area.

number

[0061] The cryogenic system also uses liquid helium-4 ( 4 He(l)) and an inlet means 12 for introducing gaseous helium-4 ( 41. The pot region 6 includes a liquid helium-4 reservoir 8 and an outlet means 14 for releasing the liquid helium-4 (denoted as He(g)). Typically, liquid helium-4 is provided from an external storage container (not shown) coupled to the inlet means 12. The inlet means 12 includes a transfer line 16 that extends into the main region 4. In the example shown, the transfer line 16 is configured as a thin-walled metal tube that reaches down to the pot region 6 and terminates just above the liquid helium-4 reservoir 8. Also shown in FIG. 1 is a primary attachment means 17 located at the bottom of the pot region 6 for holding a sample (not shown here).

[0062] To enable cryostat operation below 4.2 K at reduced helium-4 pressure under a continuous supply of liquid helium-4, gaseous helium-4 continually evaporating from the reservoir is pumped through outlet means 14 by a suitable pumping system.

[0063] The primary chamber further has a heat exchange area A H 1, the baffle structure 18 defines two separate flow paths 20a and 20b, respectively, which direct the flow of gaseous helium-4. Each flow path includes a convoluted surface leading from the pot region 6 to the main region 4 with a bypassed connection. As clearly shown in FIG. 1, there is no direct connection from the surface of the helium-4 vessel 8 to the main region 4. Note that the narrow space between the cannula-like transport line 16 and the baffle structure 18 is shown with an exaggerated distance merely for illustrative purposes. In practice, such a space does not exist or is so small that no substantial gas flow occurs therethrough. Advantageously, the heat exchange area A H and the average cross-sectional area A C The ratio of A to B is greater than 1. In the example shown in FIG. 1, a baffle structure 18 with a convoluted surface with several turns has a correspondingly large heat exchange area A. H wherein said area ratio is substantially greater than one.

[0064] In an exemplary embodiment, the cryostat main area has an internal diameter of 3 cm and a length of 30-85 cm is used. Thus, the internal volume is approximately 5×10 -4 cubic meters. The length of the heat exchange section typically exceeds the length of the pot section, provided that the surface area of ​​the turn / volute is greater than the average cross-sectional area of ​​the pot section. In the exemplary cryostat, the pot section had a height of 4 cm and an inside diameter of 15 mm.

[0065] In the embodiment of Figure 1, the baffle structure 18 is constructed as a separate piece, which is inserted longitudinally into the primary chamber 2 prior to assembly. In contrast, Figure 2 shows an embodiment in which the baffle structure 18 is integrally formed with the primary chamber 2 by 3-D printing. In other words, all elements 22 forming the convoluted surface are integrally connected with corresponding interior wall regions 24 of the primary chamber 2.

[0066] 3, the cryostat includes a heat dissipation shield 26 disposed to substantially surround the pot region 6 of the primary chamber 2. The heat dissipation shield 26 is cooled by thermal contact with an outer wall portion 28 of the primary chamber that surrounds the baffle structure 18.

[0067] A flange 30 for a vacuum-tight connection with the vacuum chamber is also shown in all figures.

[0068] The bottom surface 10 of the primary chamber is typically used for mounting a sample or other body that is to be cooled.

[0069] FIG. 4 shows a further embodiment, where the cryostat further comprises a secondary chamber 32 for operation with helium-3, secondary inlet means 34 for helium-3, and secondary outlet means 36 for helium-3. In the example shown, the cryostat is configured for operation at reduced helium-3 pressure in the secondary chamber 32, whereby gaseous helium-3 is pumped through the secondary outlet means 36. In particular, the secondary inlet means 34 comprises a cannula-like transfer line 38, which is supplied with gaseous helium-3 ( 3 4. Also shown in FIG. 4 is a secondary mounting means 44 disposed at the bottom of the secondary chamber 32 for holding a sample (not shown here).

[0070] An example of a cryostat construction in accordance with the present invention is shown in Figures 5-7. The same reference numbers are used to indicate features that are the same or functionally equivalent to those discussed in connection with Figures 1-4.

[0071] A cryostat system for use with helium-4 is shown in Figures 5 and 6. As shown in the enlarged view of Figure 6, the bottom surface 10 beneath the pot area 6 includes a sample holder 46 which holds a sample 48. The sample holder 46 is attached to the bottom surface 10 through primary attachment means 17, indicated diagrammatically by an arrow. In the example shown, the sample holder 46 includes a tip piece 50 and a base piece 52 which is pluggable into a correspondingly configured portion of the primary attachment means 17.

[0072] A cryostat system for use with helium-4 and helium-3 is shown in Figure 7. The various components shown in Figure 7 have already been described in relation to Figures 1-4. Figure 7a) shows the entire device, while Figure 7b) shows its lower parts in an enlarged view. To appreciate the degree of miniaturization achieved, Figure 7c) shows in an enlarged view a portion of the primary chamber 2 together with a 2 euro coin, showing that the primary chamber 2 and the complex structure contained therein does not exceed an outer diameter of about 25 mm. [Explanation of symbols]

[0073] 2 Primary Chamber 4 Main areas 6 Pot Area 8 Liquid Helium-4 tank 10 Bottom surface of 2 12 Primary entrance means 14 Primary exit means 16 Transport Line 17 Primary attachment means 18 Baffle structure 20a, b Flow path for gaseous helium-4 22 18 Route Elements 24 2 inner wall area 26 Heat radiation shield 28 Exterior wall of 2 30 Flange 32 Secondary Chamber 34 Secondary entrance means 36 Secondary exit means 38 Transport Line 40 Curved Section 42 Meander or spiral section 44 Secondary attachment means 46 Sample Holder 48 Samples 50 46 tip 52 Base part of 46

Claims

1. 1. A cryostat for operation with liquid helium, the cryostat comprising: a primary chamber (2) having a main region (4) and a pot region (6) for containing liquid helium-4; a primary inlet means (12) for introducing liquid helium-4 and a primary outlet means (14) for discharging gaseous helium-4, said primary inlet means comprising a transfer line (16) extending into said primary chamber and reaching said pot region, said main region being disposed between said pot region and said primary outlet means; Equipped with the cryostat is configured for operation under a continuous supply of liquid helium-4; the cryostat is configured for operation at reduced helium-4 pressure whereby gaseous helium-4 is pumped through the outlet means; the primary chamber comprising a baffle structure (18) disposed between the pot region and the main region, the baffle structure defining at least one flow path (20a, 20b) for flow of gaseous helium-4; Each flow passage forms a bypass connection between the pot region and the main region; The baffle structure (18) has a heat exchange area (A Ｈ ) a heat exchange area having a The heat exchange area of ​​the baffle structure (18) has a thermal conductivity in the range of 0.01 W / (mK) to 10 W / (mK).

2. The average liquid / gas surface area (A Ｓ ) to the heat exchange area (A Ｈ 2. The cryogenic system of claim 1 , wherein the ratio of:

3. The cryogenic maintenance apparatus of any one of claims 1 to 2, wherein the baffle structure comprises at least one convoluted surface leading from the pot region to the main region of the primary chamber.

4. 4. The cryogenic maintenance apparatus of claim 1, wherein the baffle structure (18) comprises an axial passage, the axial passage being for receiving the transportation line (16) therein.

5. The cryogenic maintenance apparatus of claim 4, wherein the axial passage is formed as a tubular section integrally connected to the baffle structure (18).

6. The cryogenic maintenance apparatus of any one of claims 1 to 5, wherein the baffle structure and optionally the primary chamber are fabricated by 3D-printing techniques.

7. The cryogenic maintenance apparatus of any one of claims 1 to 6, further comprising a heat dissipation shield positioned to substantially surround at least the pot region of the primary chamber.

8. The cryogenic maintenance apparatus of claim 7 , wherein the heat dissipation shield is coolable by thermal contact with an exterior wall portion of the primary chamber.

9. A cryostat according to any preceding claim, wherein the primary chamber is substantially cylindrical.

10. A cryostat according to any one of the preceding claims, wherein the external surface (10) of the pot area is provided with primary attachment means (17) for the external attachment of a sample.

11. A cryogenic maintenance apparatus as claimed in any preceding claim, wherein the outlet means comprises coupling means for connection to a helium pumping device.

12. The cryogenic system further comprises a secondary chamber (32) for operation with helium-3, a secondary inlet means (34) for helium-3, and a secondary outlet means (36) for helium-3; the external surface of said secondary chamber (32) is provided with secondary mounting means (44) for the external mounting of a sample to be cooled; The secondary inlet means (34) comprises a cannulated transfer line (38); the cannulated transfer line (38) is configured to pre-cool the supplied helium-3; Pre-cooling the supplied helium-3 includes i) a curved section (40) formed to substantially follow the flow path of the baffle structure (18), the gaseous helium-4 being used to pre-cool the supplied helium-3; and / or ii) a serpentine or spiral section (42) formed in the cannular transport line, the serpentine or spiral section (42) being in a region of the cannular transport line that is within the liquid helium-4, the liquid helium-4 being used to pre-cool the helium-3 supply; It is carried out by 10. The cryogenic temperature maintaining apparatus according to claim 1, wherein the helium-3 and the helium-4 are separated so as not to mix inside the cryogenic temperature maintaining apparatus.

13. 13. The cryogenic system of claim 12, wherein the cryogenic system is configured to operate at reduced helium-3 pressure in the secondary chamber (32), whereby gaseous helium-3 is pumped through the secondary outlet means (36).

14. A method for operating a cryogenic system according to any one of claims 1 to 13, said method comprising a cooling phase followed by a steady-state phase, said cooling step comprising: supplying liquid helium-4 from an external reservoir through said primary inlet means into said pot region and evaporatively cooling the liquid helium-4 until the liquid helium-4 begins to accumulate on a bottom surface of said pot region; wherein during the steady state phase, the temperature of the liquid helium-4 is maintained by adjusting the inlet flow rate of liquid helium-4 and / or adjusting the rate at which gaseous helium-4 is pumped through the primary outlet means, and optionally by controlled heating.

15. 15. The method of claim 14, wherein the temperature of the liquid helium-4 is maintained within the range of 1.4K to 1.5K.

16. 16. A method according to claim 15 for operating a cryogenic system according to any one of claims 12-13, wherein during the steady state phase, helium-3 is supplied from an external reservoir through the secondary inlet means into the secondary chamber region and evaporatively cooled until liquid helium-3 is formed, and thereafter the temperature of the liquid helium-3 is maintained by adjusting the inlet flow rate of helium-3 and / or by adjusting the rate of pumping of gaseous helium-3 through the secondary outlet means.

17. Use of a cryogenic apparatus according to any one of claims 1 to 13 for cooling a sample, a detector device, a medical scanning device, a superconducting device, an electronic device or an internal combustion engine component.

18. Spectroscopy, in particular Raman spectroscopy, photoelectron spectroscopy, Infrared spectroscopy, X-ray absorption spectroscopy, Resonant inelastic X-ray scattering, inelastic neutron or x-ray scattering, Scanning tunneling spectroscopy, Diffraction measurements, in particular X-ray diffraction, Neutron diffraction, Transmission electron microscopy, Electronic property measurements, in particular Electrical transport property measurements, Thermoelectric transport measurements, Polar Kerr effect measurement, Magnetization measurement Use of the cryostat according to any one of claims 1 to 13 for

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