GB2454571A

GB2454571A - A method of constructing a thermal radiation shield in a cryostat

Info

Publication number: GB2454571A
Application number: GB0819639A
Authority: GB
Inventors: Richard Gowland; Edgar Charles Malcolm Rayner; Nicholas John Clayton
Original assignee: Siemens Magnet Technology Ltd
Current assignee: Siemens Magnet Technology Ltd
Priority date: 2007-10-16
Filing date: 2007-10-16
Publication date: 2009-05-13
Anticipated expiration: 2027-10-16
Also published as: CN101413735B; CN101413735A; GB2457422B; GB0720191D0; US20090107151A1; GB2454571B; US9212782B2; GB0819639D0; GB2457422A

Abstract

A method of constructing a thermal radiation shield in a cryostat comprising a cryogen vessel 12 retained within an outer vacuum container (OVC) 14, comprising the steps of: axially dividing an outer cylindrical surface 44 into two sections 48; axially dividing an inner cylindrical surface 42 into two sections; joining each of two substantially planar end walls 46 to a respective one section 48 of the outer cylindrical surface and a respective one section of the inner cylindrical surface, thereby to produce two half-shields; mounting the half-shields onto the cryogen vessel; and joining the two half-shields at the outer cylindrical surface 44 by a joining conduit comprising at least two flanges 54; 84, respective first and second sections of the outer cylindrical surface being attached to respective flanges of said joining conduit; and joining the two half-shields at the inner cylindrical surface 42 by a joining conduit comprising at least two flanges 54; 84, respective first and second sections of the inner cylindrical surface being attached to respective flanges of said joining conduit, such that the joining conduits form integral parts of the thermal radiation shield.

Description

A METHOD OF CONSTRUCTING A THERMAL RADIATION SHIELD

IN A CRYOSTAT

The present invention relates to cryostats including cryogen vessels for retaining cooled equipment such as superconductive magnet coils. In particular, the present invention relates to radiation shields provided for reducing thermal radiation reaching a cryogen vessel from cryostat components which are at a higher temperature, and to venting arrangements allowing cryogen gas to escape from the cryogen vessel.

Fig. 1 shows a conventional arrangement of a cryostat including a cryogen vessel 12. A cooled superconducting magnet 10 is provided within cryogen vessel 12, itself retained within an outer vacuum chamber (OVC) 14. One or more thermal radiation shields 16 are provided in the vacuum space between the cryogen vessel 12 and the outer vacuum chamber 14. In some known arrangements, a refrigerator 17 is mounted in a refrigerator sock 15 located in a turret 18 provided for the purpose, towards the side of the cryostat. Alternatively, a refrigerator 17 may be located within access turret 19, which retains access neck (vent tube) 20 mounted at the top of the cryostat. The refrigerator 17 provides active refrigeration to cool cryogen gas within the cryogen vessel 12, in some arrangements by recondensing it into a liquid. The refrigerator 17 may also serve to cool the radiation shield 16. As illustrated in Fig. 1, the refrigerator 17 may be a two-stage refrigerator. A first cooling stage is thermally linked to the radiation shield 16, and provides cooling to a first temperature. In a cryostat with a single shield, the first stage typically cools the shield to about 50K. In cryostats with two shields, they are typically cooled to temperatures of about 80K and 20K. A second cooling stage provides cooling of the cryogen gas to a much lower temperature, typically in the region of 4-10K.

A negative electrical connection 21a is usually provided to the magnet 10 through the body of the cryostat. A positive electrical connection 21 is usually provided by a conductor passing through the vent tube 20.

For fixed current lead (FCL) designs, a separate vent path (auxiliary vent) (not shown in Fig.1) is provided as a fail-safe vent in case of blockage of the vent tube.

The present invention addresses the consumption of cryogen during transportation of the cryostat, or at any time that the refrigerator 17 is inoperative. When the refrigerator 17 is inoperative, heat from the OVC 14, which is at approximately ambient temperature (250-315K), will flow towards the cryogen vessel 12 by any available mechanism. This may be by conduction through support structures (not illustrated) which retain the cryogen vessel and the radiation shield 16 in position within the OVC; by convection using of gases, typically hydrogen, which may be present in the volume between the cryogen vessel 12 and the OVC 14; or by radiation from the inner surface of the OVC. Much attention is typically paid to reducing all of these possible mechanisms for thermal influx. Support structures are made as long and thin as mechanically practicable, and are constructed from materials of low thermal conductiviy, to reduce thermal influx by conduction. Care is taken to remove as much gas as possthle from the volume between the cryogen vessel and the OVC, although many gases will freeze as a frost on the surface of a cryogen vessel if a very cold cryogen such as helium is in use. There are some measurements of hydrogen gas being released from the steel which makes up the cryostat.

Any such released hydrogen will degrade the OVC vacuum. However, in the case of a helium cryogen, the hydrogen is solid during normal operation and will only be released as a gas if the cryogen vessel heats up to above about 20K.

One or more thermal radiation shields 16 are provided to intercept thermal radiation from the OVC. Any resultant heating of the thermal radiation shield is removed by the refrigerator 17. Further thermal insulation may be provided, such as the well-known "superinsulation": multilayered insulation of aluminised polyester sheet, typically aluminised polyethylene terephthalate sheet, played in a layer between the cryogen vessel and the thermal shield 16; or between the thermal shield 16 and the OVC; or both.

In operation, cryogen liquid in cryogen vessel 12 boils, keeping the cooled equipment 10 at a constant temperature, being the boiling point of the cryogen. Refrigerator 17 removes heat from the cryogen gas and the thermal shield 16. Provided that the cooling power of the refrigerator is sufficient to remove any heat generated by the cooled equipment and any heat influx reaching the cryogen vessel, the cooled equipment 10 will remain at its steady temperature, and cryogen will not be consumed.

A difficulty arises during transportation of the cryostat, when the refrigerator is switched off; or at any other time that the refrigerator 17 is inoperative. With the refrigerator inoperative, any heat influx reaching the cryogen vessel, and any heat generated within the cryogen vessel, will cause cryogen liquid to boil. As the refrigerator is inoperative, the boiled-off cryogen cannot be recondensed into liquid, and will vent to atmosphere through vent tube 20 or the auxiliary vent. In the case of superconducting magnets, for example as used in Magnetic Resonance Imaging (MRI) systems, liquid helium is typically used as the cryogen. Liquid helium is expensive, and difficult to obtain in some parts of the world. It is also a finite resource. For these reasons, it is desired to reduce the consumption of helium cryogen during transport or at other times that the refrigerator 17 is not operating.

It is of course possible to transport the cryostat and the equipment at ambient temperature, empty of cryogen. This will avoid the problem of cryogen consumption during transport. However, the equipment 10 and indeed the cryostat itself will need to be cooled on arrival at its destination. Such cooling is a skilled process, and on-site cooling has been found to be very expensive. Furthermore, the quantity of cryogen required to cool the equipment and cryostat from ambient temperature on arrival at an installation site has been found to far exceed current consumption rates over a reasonable transport time. Typical current systems are able to travel for at least 30 days without the refrigerator operating, and without the liquid cryogen boiling dry.

Current known solutions consume approximately 2.53.O% of cryogen inventory per day of transit time. On current systems, this may equate to a consumption of 50 litres of liquid helium per day. The present invention aims to reduce this level of consumption, and so increase the maximum transport time, simplifying the logistics of delivering a cooled equipment to a destination and/or reducing the consumption of cryogen.

Known attempts to address this problem have met with difficulties.

Some of the known attempts to address this problem will be briefly discussed.

A second thermal radiation shield, concentric with first thermal shield 16 may be provided. This has been found somewhat effective in reducing thermal influx to the cryogen vessel, but has required increased size of OVC, and caused increased manufacturing costs.

A thermally conductive pipe has been run around the thermal shield, carrying escaping cryogen gas. As the gas is at a temperature little above its boiling point, which is about 4K, such arrangements serve to cool the thermal shield. This has been somewhat effective at reducing thermal influx to the cryogen vessel. Such an arrangement is described, for example, in US patent 7,170,377 and UK patent application GB 2 414 536, but has also required increased size of OVC to accommodate the thickness of the conductive pipe. Increased manufacturing costs also resulted from the additional assembly effort, and the material and labour costs of increasing the size of the OVC.

The present invention accordingly aims to provide an improved cryostat which reduces consumption of cryogen during transportation, or at any time when active refrigeration is not present, and does not suffer

from the problems of the prior art.

The present invention provides apparatus andlor methods as set out in the appended claims.

The above, and further, objects, advantages and characteristics of the present invention will become more apparent from consideration of the following description of certain embodiments thereof, given by way of non-limiting examples only, in conjunction with the accompanying drawings wherein: Fig. I shows a conventional arrangement of a cryostat containing a superconducting magnet; Fig. 2 shows a cross-section of a portion of a thermal radiation shield S of the present invention, comprising a joining conduit; Figs. 3-3B show cross-sections of a portion of thermal radiation shields according to further embodiments of the present invention, each comprising a joining conduit; Fig. 4 shows a perspective view of a thermal radiation shield according to an embodiment of the present invention; Fig. 5 shows a cross-section of a portion of a thermal radiation shield of the present invention, comprising a joining conduit; Fig. 6 shows a perspective view of a thermal radiation shield according to an embodiment of the present invention; Figs. 7A-7B show cross-sections of a portion of thermal radiation shields according to further embodiments of the present invention, each comprising a joining conduit; and Fig. 8 shows summarised results of simulations of the effect of a thermal radiation shield according to the present invention.

The present invention improves upon the cooled thermal radiation shield, as proposed in US patent 7,170,377 and UK patent application GB 2 414 536. These prior art documents propose a cryogen gas carrying, thermally conductive tube wrapped around the outside of a thermal radiation shield. The thickness of the thermal radiation shield is effectively increased by the thickness of the tube, plus any fittings used to attach the tube to the thermal radiation shield. The increased effective thickness of the shield leads to increased overall dimension of the cryostat, including a larger OVC. In turn, this means a more costly system.

Assembly is also complicated by the need to mount the cryogen gas carrying tube. The present invention aims to provide similar functionality but without increasing the thickness of the thermal radiation shield to such an extent; and to provide a simplified method of assembling a thermal radiation shield, by providing a thermally conductive conduit for carrying boiled off cryogen gas from the cryostat, as an integral part of the thermal shield.

Fig. 4 shows a perspective view of a thermal radiation shield according to the present invention, and Fig. 2 shows an enlarged cross-section of a part of the radiation shield of Fig. 4. As shown in Fig. 4, the thermal radiation shield 40 is typically a closed, dual-cylinder having an inner cylindrical surface 42, an outer cylindrical surface 44 and substantially planar end walls 46 joining inner and outer cylindrical surfaces. It is typically constructed of aluminium, joints 49 between end walls 46 and respective cylindrical surfaces 42, 44 are made by any convenient method, typically by welding. In the illustrated embodiment, the outer cylindrical surface 44 is axially divided into two or more sections 48. The sections 48 are joined together using a joining conduit 50 which extends around the thermal radiation shield 44 in a manner which will now be described with reference to Fig. 2.

Fig. 2 shows a cross-section of a joining conduit 50 according to an aspect of the present invention. The conduit 50 includes a substantially central bore 52 for carrying cryogen gas and pairs of retaining flanges 54 on opposing sides for retaining sections 48 of thermal radiation shield.

Joining conduit 50 is preferably provided as a linear extrusion, flexible enough to be bent to the radius of the sections 48 of the thermal radiation shield. Edges of respective sections 48 of the thermal radiation shield are placed into slots defined by respective pairs of retaining flanges 54. The edges may be retained by an interference fit, or at least one of each pair of retaining flanges may be mechanically deformed onto the corresponding section 48 of the thermal radiation shield. Other acceptable arrangements for attaching the retaining flanges onto the corresponding section 48 of the thermal radiation shield include welding, soldering, braising, clips, clamps, through-hole tabs, push-to-fit retaining features, such as complementary cavities and protrusions provided in the material of the thermal radiation shield and the material of the conduit, the provision of barbs or gripping textures in the material of the shield and/or the material of the conduit. At least one of the flanges may have a chamfer to assist with assembly of the thermal radiation shield. It is believed that the joint between the retaining flanges and the thermal radiation shield needs structural and thermal integrity.

Any combination of interference fit, mechanical deformation or any other arrangement may alternatively be used as desired. It is necessary to ensure that sufficient thermal contact is made between the joining conduit and the sections 48 of thermal radiation shield that the gas escaping through the bore(s) cools the shield effectively.

During assembly of the cryostat, the thermal radiation shield may be constructed, with the sections 48 of thermal radiation shield 44 being assembled together using the joining conduit 50, followed by mounting of the end walls 46, typically by welding. The conduit 50 does not form a closed loop, but ends of the conduit are arranged (not shown) to direct escaping cryogen gas from the vent tube 20 andior the auxiliary vent into one end of the bore 52, around the thermal radiation shield, and out of the other end of the bore to atmosphere.

During transport of the cryostat, or at other times that no active refrigeration is provided, thermal influx and/or heat generation within the cryostat cause some of the liquid cryogen to boil off. The resulting cryogen gas, at a temperature near to its boiling point, escapes from the cryogen vessel through vent tube 20 or an auxiliary vent. According to the present invention, at least some of this escaping cryogen gas is routed through the bore 52 of joining conduit 50. As the escaping cryogen gas circulates through the bore, it draws heat from the conduit, which in turn cools the thermal radiation shield. Since the thermal radiation shield is then at a lower temperature than would have been the case had the gas simply been allowed to vent to atmosphere, the temperature differential between the shield and the cryogen vessel is reduced, which in turn reduces the heat influx to the cryogen vessel. It is known that radiated power scales as T4, where T is the temperature differential between source and destination of the thermal radiation. Any reduction in the temperature differential will therefore lead to a significant reduction in energy transferred by thermal radiation. Such reduction in heat influx leads to a corresponding reduction in cryogen consumption, or an increased autonomy for transport, or both.

Fig. 3 illustrates an improvement to the embodiment shown in Fig. 2. In Fig. 3, the joining conduit 60 includes a channel 62 which is preferably partially closed, or is able to be partially closed, for example by deformation of a wall. According to this embodiment, auxiliary equipment 63 such as electrical wires and cables, temperature sensors, or pipes may be housed within the channel 62. As shown in Fig. 3, the channel 62 may -lo-be embodied as a U-shaped channel with an overhang 64, which overhang may be deformed onto retained auxiliary equipment to secure it into place within the channel, as illustrated in Fig. 3A. In one particular embodiment, a perforated pipe may be provided and used to improve evacuation of the volume between the cryogen vessel and the OVC, known as pumpdown.

Fig. 3B shows a further embodiment of the present invention. In this embodiment, joining conduit 66 is provided with two bores 68, 70.

Such an arrangement may provide improved cooling of the thermal radiation shield by causing cryogen gas escaping from the cryogen vessel to pass twice through the joining conduit. This may be arranged by providing one end of the joining conduit 66 with a U-shaped return connector, which joins corresponding ends of the two bores 68, 70 together, with ingress and egress fittings at opposite ends of bores 68, 70.

The gas flow in the two conduits will be in opposing directions.

Alternatively, the gas flows in the two conduits may be directed in a same direction by connecting a first end of one bore to a second end of the other bore, with ingress and egress fittings connected to remaining bore endings. It is believed that gas flowing from the cryogen vessel may provide useful cooling to the thermal radiation shield through more than one circuit of the thermal radiation shield. As such, further embodiments, similar to that of Fig. 3B, may be provided with three or more bores, suitably connected, to provide an extended path for escaping cryogen gas.

Embodiments such as shown in Fig. 3B may be provided with one or more channels, such as shown in Fig. 3A for retaining auxiliary equipment.

-11 -Fig. 5 shows another embodiment of a joining conduit 80 according to the present invention, and Fig. 6 shows a perspective view of a thermal radiation shield constructed using the joining conduit of Fig. 5.

As illustrated in Fig. 5, joining conduit 80 provides at least one bore 82 with flanges 84 on opposing sides. Since no slots are provided for retaining the edges of the sections 48 of thermal radiation shield, the joining conduit must be attached by means such as rivets 86, welding, soldering, braising, clips, clamps, through-hole tabs and so on. It is necessary to ensure that sufficient thermal contact is made between the joining conduit 80 and the sections 48 of thermal radiation shield that the cryogen gas escaping through the bore(s) 82 cools the shield effectively.

Fig. 6 illustrates a perspective view of a thermal radiation shield according to the present invention, using a joining conduit 80 as illustrated in Fig. 5. The thermal radiation shield is similar to that illustrated in Fig. 4, other than having cylindrical wall sections 48 attached to the joining conduit 80 by rivets 86. Joints 49 between end walls 46 and respective cylindrical surfaces 42, 44 are made by any convenient method, typically by welding.

In alternate embodiments, joining conduits may be used to join the end walls 46 to the respective cylindrical surfaces 42, 44. Figs. 7A and 7B illustrate joining conduits suitable for this purpose, based on the embodiments of Figs. 2, 5 respectively. Variations on these conduits may be provided, containing multiple bores, as in Fig. 3B or containing a channel for retaining auxiliary equipment, as in Fig. 3A. In further embodiments, the end walls 46 of the thermal radiation shield may be -12-made up of several sections, with joining conduits according to the present invention being provided to join the sections together.

According to the present invention, escaping cryogen gas is directed through a conduit which forms an integral part of a thermal radiation shield.

The inventor has performed certain simulations on an embodiment of the invention, to demonstrate its effectiveness. Various lengths of single 8.8 mm diameter bore extruded aluminium conduit were simulated, carrying escaping cryogen gas to cool the thermal radiation shield of a typical cryostat. Fig. 8 shows summarised results. The temperature Tout represents the temperature of cryogen gas venting to atmosphere from the downstream end of the joining conduit. As shown, with a conduit length of more than 2m, the thermal shield temperature equals the temperature Tout of the escaping cryogen gas. No further cooling effect is found by extending the length of the joining conduit beyond 2m. This length will be referred to herein as the 100% heat transfer length. Different results would have been obtained with different cryostats, different boil-off rates and different sizes or different numbers of bores in the conduit. Table 1 below shows calculated results of the 100% heat transfer length for different shield temperatures -and so also temperatures of gas venting to atmosphere, and for different gas flow rates (expressed in equivalent litres of liquid helium per day). The results show that, for the cryostat considered in the simulation, a length of 2m is sufficient to provide all available shield cooling. As the inner cylindrical surface 42 of a thermal radiation shield used in a cryostat housing a superconducting MRI magnet typically has a diameter of slightly less than 1m, a single bore conduit around the circumference of the inner cylindrical surface may prove -13 -sufficient to cool the thermal radiation shield. The outer cylindrical surface 44 of such a thermal radiation shield typically has a diameter of about I.8m, so a single bore conduit around the circumference of the inner cylindrical surface may well prove sufficient to cool the thermal radiation shield.

Shield Temperature Flow rate Length of joining conduit needed (K) (litreslday) for 100% heat transfer (m) 50 2 25 1.3 50 1.9 25 1.4

Table 1

In a preferred embodiment of the present invention, the thermal radiation shield is constructed as follows. The outer cylindrical surface 44 is axially divided into two sections 48. Similarly, the inner cylindrical surface is axially divided into two sections. Each substantially planar end wall 46 is joined at joints 49 to one section 48 of the outer cylindrical surface and one section of the inner cylindrical surface, typically by welding, although other means such as braising, soldering or adhesive bonding could be used provided that the resulting joint is sufficiently thermally conductive. This will produce two half-shields. These half-shields may then be mounted onto the cryogen vessel, by means known in themselves to those skilled in the art, the two half-shields being joined at outer cylindrical surface 44 and inner cylindrical surface by a joining conduit as described. Arrangements must be made to direct at least some of cryogen gas escaping from the cryogen vessel through a bore in at least one of the joining conduits. it may be found sufficient to direct escaping -14-gas through only one of the joining conduits. It may be simplest to direct the escaping gas through only the conduit provided as an integral part of the outer cylindrical surface 44, since provision will in any case be made for a vent tube to pass through this surface. The joining conduit provided as an integral part of the inner cylindrical surface 42 may have an unused bore, or the bore may be absent. The joining conduit provided as an integral part of the inner cylindrical surface may be joined into a closed loop by welding, soldering or any suitable method.

Any of the conduits described may be used in this assembly process.

Conduits such as shown in Fig. 2 may retain edges of the sections of inner and outer cylindrical surfaces by any suitable arrangement. Examples include interference fit, by having flanges deformed into mechanical engagement with the edges, by use of push-to-fit retaining features, such as complementary cavities and protrusions provided in the material of the thermal radiation shield and the material of the conduit, soldering, welding, the provision of barbs or gripping textures in the material of the shield andJor the material of the conduit.

Conduits such as shown in Fig. 5 may be mechanically connected to the edges of the sections of inner and outer cylindrical surfaces by any suitable arrangement. Examples include flanges deformed into mechanical engagement with the edges, by use of push-to-fit retaining features, such as complementary cavities and protrusions provided in the material of the shield and the material of the conduit, soldering, welding, riveting or the provision of barbs or gripping textures in the material of the shield andlor the material of the conduit. As illustrated in Fig. 5, one of the flanges may have a chamfer 88 to assist with assembly of the thermal radiation shield.

-15 -Further embodiments of the present invention are provided by spirally winding a flanged conduit to form at least part of a cylindrical surface of the thermal radiation shield. Flanges of adjacent turns of the conduit should be joined by a suitable method such as interference fit, welding, soldering or adhesive bonding. In such arrangements, thermal conductivity of the joins is not as important as in other embodiments, since the entire surface is in direct thermal contact with a part of the bore of the conduit. End faces and the other cylindrical surface may be of similar or conventional construction as required by a particular apparatus.

Typically, the joining conduit provided by the present invention will have a constant cross-section, and may conveniently be provided by extrusion of aluminium. A thermally-conductive surface passivation, such as hard anodising, may be applied to the aluminium extrusion. The joining conduit may be extruded from any other suitable, thermally conductive material, such as copper. Embodiments may employ more than one type of joining conduit, for example a double-bore conduit as part of the outer cylindrical surface, with a cable-carrying joining conduit as shown in Fig. 3A as a part of the inner cylindrical surface.

While the present invention has been described with specific reference to a limited number of particular embodiments, many modifications and variations will be apparent to those skilled in the art, and fall within the scope of the present invention. For example, thermal radiation shields according to the present invention may be provided in cryostats holding cooled equipment other than magnets for MRI systems, being useful in any cryogenic storage Dewar. Similarly, thermal radiation shields according to the present invention are useful for cryostats containing any liquid cryogen, and the present invention is not limited to helium-cooled cryostats.

Claims

CLAIMS: 1. A method of constructing a thermal radiation shield in a cryostat comprising a cryogen vessel (12) retained within an outer vacuum container (OVC) (14), comprising the steps of: -axially dividing an outer cylindrical surface (44) into two sections (48); -axially dividing an inner cylindrical surface (42) into two sections; -joining each of two substantially planar end walls (46) to a respective one section (48) of the outer cylindrical surface and a respective one section of the inner cylindncaj surface, thereby to produce two half-shields; -mounting the half-shields onto the cryogen vessel; and -joining the two half-shields at the outer cylindrical surface (44) by a joining conduit comprising at least two flanges (54; 84), respective first and second sections of the outer cylindrical surface being attached to respective flanges of said joining Conduit; and -joining the two half-shields at the inner cylindrical surface (42) by a joining conduit comprising at least two flanges (54; 84), respective first and second sections of the inner cylindrical surface being attached to respective flanges of said joining conduit, such that the joining conduits form integral parts of the thermal radiation shield.
2. A cryostat comprising a cryogen vessel (12) retained within an outer vacuum container (OVC) (14), the cryogen vessel being provided with a vent path (20) allowing cryogen gas to escape from the cryogen vessel, the cryostat further comprising a thermal radiation shield (16) interposed between the cryogen vessel and the OVC, characterised in that the vent path is arranged such that escaping cryogen gas is directed through a conduit (50; 80; 60; 66) which forms an integral part of a thermal radiation shield.
3. A method according to claim 1 or claim 2, wherein the end walls are made lip of several sections, with joining conduits joining the sections together. C) c'J

3. A cryostat according to claim 2 wherein the conduit is a joining conduit comprising a bore (52; 82) and at least two flanges (54; 84).

4. A cryostat according to claim 3 wherein the thermal radiation shield is composed of at least two sections (48), respective first and second sections being attached to respective flanges of said joining conduit.

5. A cryostat according to claim 4 wherein the respective sections are attached to the respective flanges by any of the following means: welding, soldering, braising, clips, clamps, through-hole tabs, push-to-fit retaining features, complementary cavities and protrusions provided in the material of the thermal radiation shield and the material of the conduit, barbs or gripping textures in the material of the shield and/or the material of the conduit, riveting 6. A cryostat according to claim 4 or claim 5 wherein one of the flanges is provided with a chamfer (88).

7. A cryostat according to claim 3 or claim 4 wherein the at least two flanges are positioned on opposite sides of the bore.

8. A cryostat according to claim 3 wherein the joining conduit (50) comprises two pairs of flanges (54), each pair of flanges defining a slot such that respective first and second sections (48) are retained within respective slots.

9. A cryostat according to claim 8 wherein the respective sections are retained within respective slots by any of the following means: welding, soldering, braising, clips, clamps, through-hole tabs, interference fit, flanges deformed into mechanical engagement, push-to- fit retaining features, complementary cavities and protrusions provided in the material of the sections and the material of the conduit, barbs or gripping textures in the material of the sections andior the material of the conduit.

10. A cryostat according to claim 8 or claim 9 wherein the pairs of flanges are positioned on opposite sides of the bore.

11. A cryostat according to any preceding claim wherein the conduit comprises at least two bores (68, 70; 82) and the vent path is arranged such that escaping cryogen gas is directed through at least two of said bores.

12. A cryostat according to any preceding claim, wherein the conduit is provided with a channel (62) for retaining auxiliary equipment (63).

13. A cryostat according to any preceding claim, wherein the channel is partially closed by an overhang (64).

14. A cryostat according to claim 10, wherein the overhang is deformable, whereby auxiliary equipment (63) may be retained within the channel.

15. A cryostat according to claim 2 wherein at least part of a cylindrical surface of the thermal radiation shield is formed by a spirally wound flanged conduit, wherein flanges of adjacent turns of the conduit are joined.

16. A cryostat according to claim 15 wherein flanges of adjacent turns of the conduit are joined by one of the following methods: interference fit; welding; soldering; and adhesive bonding.

17. A joining conduit for forming an integral part of a thermal radiation shield for a cryostat, the joining conduit comprising at least one substantially central bore (52) for carrying cryogen gas and at least two retaining flanges (54) directed in respective directions generally away from the central bore, for retaining sections (48) of a thermal radiation shield.

18. A joining conduit according to claim 17, wherein respective pairs of retaining flanges (54) are provided, said pairs defining respective slots between the members of each pair, said slots being directed in respective directions generally away from the central bore, such that sections (48) of a thermal radiation shield may be retained within said slots.

-21 - 19. A joining conduit according to claim 17 or claim 18, wherein at least one of the flanges has a chamfer to assist with assembly of a thermal radiation shield.

20. A joining conduit according to any of claims 17-19, wherein the joining conduit includes at least one channel (62) for housing auxiliary equipment (63).

21. A joining conduit according to claim 20 wherein the channel is partially closed.

22. A joining conduit according to claim 21 wherein the channel is U-shaped in cross-section and is provided with an overhang (64), which overhang is deformable onto any retained auxiliary equipment, thereby to secure such auxiliary equipment into place within the channel.

23. A joining conduit according to any of claims 17-22, comprising at least two bores, thereby enabling gas to pass at least twice through the joining conduit.

Amendments to the claims have been filed as follows 1. A method of constructing a thermal radiation shield in a cryostat comprising a cryogen vessel (12) retained within an outer vacuum container (OVC) (14), comprising the steps of: -axially dividing an outer cylindrical surface (44) into two sections (48); -axially dividing an inner cylindrical surface (42) into two sections; -joining each of two substantially planar end walls (46) to a respective one section (48) of the outer cylindrical surface and a respective one section (42) of the inner cylindrical surface, thereby to produce two half-shields; -mounting the half-shields onto the cryogen vessel; and 0) -joining the two half-shields at the outer cylindrical surface (44) by a joining conduit comprising at least two flanges (54; 84), respective first and second sections of the outer cylindrical surface being attached to respective flanges of said joining Conduit; and -joining the two half-shields at the inner cylindrical surface (42) by a joining conduit comprising at least two flanges (54; 84), respective first and second sections of the inner cylindrical surface being attached to respective flanges of said joining conduit, such that the joining conduits form integral parts of the thermal radiation shield.

2. A method according to claim 1, wherein the step of joining the substantially planar end walls to the section of the outer cylindrical surface and the inner cylindrical surface is performed by a joining conduit comprising at least two flanges.