GB2490189A - Superconducting magnet with thermally conductive cooling and methods for its manufacture - Google Patents

Abstract

A superconducting magnet comprises a plurality of axially-aligned annular coils 10 of superconducting wire which are in mechanical contact with a cooled surface 15 of a cooling system transferring thermal energy by conduction. There is a thermal radiation shield 24 located between the inner radial surface of the said coils and their axis. The thermal radiation shield 24 is a metal layer in thermal contact with a cooled surface 15 of the said cooling system. The radiation shield 24 may provide a route of lower thermal resistance to the cooled surface 15 than any passing through a superconductive coil 10. The radiation shield 24 may be provided as at least one metal cylinder which is mechanically and thermally joined to the cooled surface 15 at axial and circumferential intervals. The radiation shield 24 may include metal layers with cladding and/or foil layers allowing a structural support to be provided with high thermal conductive layers. Also disclosed is a method of manufacturing a superconducting magnet comprising providing conductive channel pieces with a layer of electrically insulating material over the inner surfaces of the channel and where a superconducting coil is located within the said channel such that the channel covers the axial and the radial inner surfaces of at least one coil 10.

Description

I

SUPERCONDUCTING MAGNETS WITH THERMAL RADIATION SHIELDS

The present invention provides radiation shields for cylindrical superconducting magnets comprising a plurality of axially aligned coils of superconducting wire. In particular, the present invention relates to superconducting magnets which are not cooled by immersion in a liquid cryogen, but are arranged for cooling by thermal conduction through a cooled surface in mechanical contact with the coils.

Cylindrical superconducting magnets are commonly employed in magnetic resonance imaging (MR1) systems. A strong, homogeneous background magnetic field is provided by the superconducting magnets, and a gradient coil assembly is typically provided inside the bore of the superconducting magnet, and generates rapidly-varying magnetic field gradients in three orthogonal dimensions.

The superconducting magnet is cooled to cryogenic temperatures, and it is conventional for the magnet to be housed inside a hollow cylindrical outer vacuum chamber (OVC), and for one or more hollow cylindrical thermal radiation shields to be positioned between the superconducting magnet and the OVC. Typically, the thermal radiation shield, or the outer thermal radiation shield if there are more than one, is cooled to a temperature of approximately 50K. The assembly therefore comprises at least two closely-stacked cylindrical tubes within the bore of the magnet.

The time-varying currents applied to the gradient coils during an MRI imaging sequence interact with the homogeneous background magnetic field to cause Lorentz forces to act on the gradient coils, resulting in vibration of the gradient coil assembly.

The time-varying magnetic fields generated by the gradient coils induce eddy currents in the material of nearby conductive surfaces, such as bore tubes of the OVC and the thermal radiation shield(s). These eddy currents, flowing through the resistive material of the bore tubes, cause heating which may risk magnet quench due to a rise in coil temperature. Little heat energy is required to cause a quench, due to the very low heat capacity of solid materials at 4K, a typical temperature of operation of cylindrical superconducting magnets.

Furthermore, the eddy currents induced in the conductive bore tubes will interact with the homogeneous background magnetic field to cause Lorenz forces to act on the bore tubes, resulting in vibration of the bore tubes. These vibrations interact with the homogeneous background magnetic field and cause further (secondary) eddy current generation within the bore tubes, in turn causing heating and inducing further (tertiary) eddy currents in neighbouring conductive surfaces through generation of secondary magnetic fields. The tertiary eddy currents will in turn produce tertiary magnetic fields. In addition to the unwelcome heating already described, the vibrations cause unpleasant noise for patients placed within the bore of the magnet for imaging.

The eddy currents produced in the material of the OVU bore tube will help to shield the bore tube of the thermal radiation shield stray magnetic fields from the gradient coils.

In a liquid cryogen bath cooled magnet, the liquid cryogen such as helium provides adequate cooling of the coils to prevent a quench happening as a result of eddy currents. However, more recent designs of superconducting magnets do not have coils cooled by immersion in liquid cryogen. Rather, the coils are arranged for cooling by thermal conduction through a cooled surface in mechanical contact with the coils. The cooling may be provided with a cryogen-filled thermosiphon, or by a cryogenic refrigerator thermally linked to the cooled surface. In such low-cryogen inventory magnets, the problem of unwanted gradient coil induced heating (GCIH) is urgent because the thermal resistance between the coil and the cooled surface is significantly higher then in the former liquid cryogen cooled magnets.

The present invention accordingly addresses the linked problems of providing shielding from stray magnetic fields and shielding from black body radiation from the thermal radiation shield bore tube. The present invention addresses these problems by providing cylindrical superconducting magnets and methods for manufacture thereof as defined in the appended claims.

The following patent publications relate generally to gradient coil interaction and the reduction of noise and vibration: DE 10 2006 000 923 B4; US 7535,225 B2; JP 2005279187 A; and US 2006/0266053 Al.

The present invention may be applied to any dry, or minimum-cryogen magnet, for example, the so called A2-bonded magnet', in which resin-impregnated coils are attached by their radially outer surface to a support structure. Other arrangements of magnets, such as various self-supporting resin impregnated structures, may also benefit from the present invention.

The above, and further, objects, characteristics and advantages of the present invention will become more apparent from the following description of certain embodiments thereof, in conjunction with the accompanying drawings, wherein: Figs. IA to 10(u) show several views of one series of embodiments of the present invention; Figs. 2A to 20(u) show several views of another series of embodiments of the present invention; and Fig. 3 shows the variation is resonant frequencies of aluminium tubes of various lengths.

The present invention addresses the problems of providing shielding from stray magnetic fields, and shielding from black body radiation from the thermal radiation shieki bore tube, for superconducting magnets having dry or minimum-cryogen inventory cooling arrangements by providing an electrically conductive shield cooled to cryogen temperature and interposed between the coils of the magnet and the bore tube of the conventional thermal radiation shield. In this way, the effects of OCR, gradient coil induced heating, are shielded from the coils. The conventional radiation shieki in a helium-cooled superconducting magnet system is typically cooled to a temperature of about 50K, while the shield of the present invention is cooled to approximately cryogen temperature, for example about 4K. For this reason, and for clarity and brevity of description, the shield of the present invention will be referred to as a 4K shield" in the following description, while the conventional thermal shield will be referred to simply as "thermal shield".

The combination of impregnated coils and thefr support structure is cooled to cryogenic temperatures, such as about 4K, to enable superconducting operation.

The assembly of magnet coils and its support structure will therefore be referred to

as the "cold mass" in the following description.

A first series of embodiments is illustrated by Figs. IA to 10(u), which show examples of a cooled tubular 4K shield mechanically mounted to the cold mass, to shi&d the magnet from the undesirable effects of Gd.

Figure IA shows a partial axial cross section of MR1 system including an A2-bonded magnet. Resin-impregnated superconducting coils 10 are bonded by their radially outer surfaces 12 to a tubular support structure 15 of greater diameter than the coils.

An electrically isolating filler layer 16 may be interposed between the coils 10 and the support structure 15. In the illustrated arrangement, the support structure is made up of a number of rings ISa, axially aligned and retained in position by retaining means not illustrated in the drawing. However) other support structures may be provided, such as a single continuous tube.

In the illustrated arrangement, the support structure 15 comprises a solid, thermally-conductive, mechanical support, for example made of aluminium, with cooling channels 22 running circumferentially around the support. These channels may carry a cryogen in liquid and/or gaseous state, to provide cooling by a cooling loop arrangement. In alternative embodiments, a solid thermal conductor, such as a copper or aluminium strap or braid, may be provided, connecting the support structure 15 to a cryogenic refrigerator (not illustrated).

As is conventional in many types of superconducting magnet structure, the coils are enclosed within an outer vacuum chamber (OVC) 18, and thermal radiation shield 20 is interposed between the magnet structure and the OVC. A gradient coil assembly 30 is also illustrated. Solid thermal insulation, such as layers of aluminised polyester may be provided in the space between the thermal shield 20 and the OVC 18.

According to this embodiment of the present invention, a 4K shield is provided by mounting a thermally conductive tube 24 onto the cold mass. In the illustrated embodiment, this is achieved using thermally conductive nuts, bolts and spacers.

These provide mechanicaHy rigid mounting points 25 and a degree of thermal conductMty between the tube 24 and the support structure 15. The 4K shield is completed by annular end pieces 28, which may be constructed of arcs of a thermally conductive material such as aluminium, welded, bolted or otherwise thermaHy and mechanically attached to the tube 24 and the support structure 15. The mounting points 26 may be provided at circumferential intervals around the tube, at a single axia' distance d from each end of the coil support 15. Alternatively, further mounting points 26a may be provided at other distances axial distance d from each end of the coil support 15. The mounting points at various axial positioned may be aligned at particular circumferential positions, or may be misaligned for reasons to be explained below.

As the mounting points need to resist motion of the tube 24, which is subjected to high-frequency cyclical forces, the mounting points must be constructed in such a way that they will not become loose as a result of those forces, and the resulting vibration of the tube. For example, joints between the mounting points 26, the tube 24 and the support structure 15 may be bolted and glued in the manner illustrated.

Alternatively, such joints may be formed by welding, or a similar process such as brazing or soldering. Such joints are believed to be resistant to high-frequency low amplitude vibrations which they are likely to encounter in embodiments of the present invention. The various components involved, such as bolts, mounting points and tube 24 should be thermally matched, so that joints do not loosen due to differential thermal contraction of the various components.

The coils 10 are then substantially shielded from black-body radiation from the thermal shield 20. The electrical conductivity of the material of the 4K shield means that it will also shield the coils from magnetic fields generated by the gradient coils 30.

In operation, the 4K shield 24, 28 is kept at a nominal temperature of less than 5K, in this example. It is in thermal contact with the support structure 22 which is cooled to about 4K for instance by a cooling loop which causes cooled cryogen to circulate through channels 22. In an alternative arrangement, a conductor such as copper or aluminium straps or braids may be connected between support structure 15 and a cryogenic refrigerator or other surface cooled to about 4K, for example by liquid helium.

Fig. I B shows a detailed part-axial cross section view of a variant of the arrangement of Fig. IA. hi this variant, a thermal link 32, for example a solid aluminium or copper strap, or a braid or laminate of aluminium or copper, is thermally connected between the tube 24 and the support structure 15 of the cold mass. Each end of the thermal link is connected at joint 35 in a thermally conductive manner to its respective component, for example by screws, nuts and bolts as illustrated. Other thermally conductive connecting means may be used, such as welding, brazing, soldering, clamping or crimping. A such joints 35 need to remain intact despite the motion of the tube 24, which is subjected to high-frequency cyclical forces, the joints must be constructed in such a way that they will not become loose as a result of those forces, and the resulting vibration of the tube. For example, the joints 35 may be bolted and glued in the manner illustrated. Alternatively, such joints may be formed by welding, or a similar process such as brazing or soldering. Such joints are believed to be resistant to high-frequency low amplitude vibrations which they are likely to encounter in embodiments of the present invention. The various components involved, such as bolts, support structure 15 and tube 24 should be thermally matched, so that joints do not loosen due to differential thermal contraction of the various components.

In such an arrangement, it is not necessary for the annular end piece 28 of the 4K shield to be in direct thermal or mechanical contact with the tube 28. Layers of solid insulation 34, such as aluminised polyester sheets, may be positioned between the coils 10 and the tube 24. This serves to reduce any black-body radiation from the tube 24 which reaches the coils 10.

Fig. 1C shows a simple model of thermal conduction in a structure according to Fig. IA or lB. A thermal load 0, due to black body radiation and/or GC1H, is incident upon tube 24 of the 4K shield. The thermal load passes through thermally conductive path 28, 26, 32, which may be one or more of the thermal link 32, the annular end-piece 28 and the mounting points 26, to the support structure 15. The support structure is cooled by cooling channels 22, or an equivalent cooling method such as a solid conductor to a cryogenic refrigerator (not illustrated). The thermal load 0 is accordingly removed from the structure by the cooling method.

In order to function as a suitable radiation shield, in addition to having sufficient thermal conductivity to carry away heat which reaches the 4K shield, tube 24 should also have a radially outer surface (i.e. the surface which faces the coils 10) with low emissivity. The low emissivity requirement may be achieved by suitable selection and preparation of the material of the thermal shield, but may alternatively be achieved by attaching a high reflectivity foil to the surface such as the aluminised polyester sheet 34 shown in Fig. 13, or adhesive aluminium tape.

In order to function to shield stray magnetic fields, the tube 24 should have good electrical conductivity and a radial thickness 1 which is significantly larger than the skin depth of the magnetic field in the material of the tube. Preferably, the thickness t of the tube is at least twice the skin depth.

To provide effective magnetic and thermal shielding we require that the tube is stiff.

The resonance frequencies of the tube need to be higher than the operating frequencies of the gradient coils of the MRI scanner. A desirable feature of 4K shields using a tube 24 structure is that it is highly tuneable' and some features which may enable this are shown in the drawings, and will be described below. Such features will reduce oscillation of the tube within the background magnetic field, and so will reduce the generation of secondary and tertiary eddy currents with the associated heating and noise.

Typically, gradient coils 30 are operated in clinical applications at frequencies in the range from 50 to about 3000 Hz. It is desirable that the vibration modes of the tube are at frequencies which are higher than 3000 Hz. Certain aspects of the present invention are dedicated to ensuring that this condition is met.

The resonance frequency of a tube with length L, average radius a, radial thickness t, density p, Young's modulus E, and Poisson ratio 1u, radially clamped at an end is given by ("Vibration of Shells and Plates' Werner Soedel, eq. 6.12.3): t 1 iE nura a __ 2uflp l21ji,f2)\. L where m is the mode number.

In an example embodiment of the invention, the tube 24 may be an aluminium tube with a radius of 450 mm and a thickness t of 3 mm. The resonant frequendes for oscillation by circumferential expansion and contraction in the radial direction for different lengths of such tubes are shown in Fig. 3. Fig. 3 shows that oscillation by circumferential expansion and contraction at higher axial resonant modes remains at the fundamental frequency for a long tube, of 1400mm, while oscillation at higher axial modes occurs at rapidly increasing frequencies for shorter tubes, in this case being particularly pronounced in the case of the shortest tubes of axial length 200mm.

The typical length of the magnet is 1400mm. Fig. 3 shows that the resonant frequencies do not vary significantly between the resonant modes. For shorter tube lengths, such as tube length less than 300 mm, there is a significant upward shift of the resonance frequencies for higher modes.

In the context of the present invention, then, it may be appreciated that the resonant frequency of the tube 24 may be increased by forming it out of several separately mounted short tubes, each of 200-300mm length for example, rather than one long one of 1400mm length.

Fig. ID(i) schematically illustrates the oscillation of a single tube 24. While the amplitude of such vibrations is exaggerated for clarity, it can be seen that the surface of the tube oscillates at antinodes 60. When this occurs in a background magnetic field, as with the magnet systems of the present invention, eddy currents and heating will be induced in the material of the tube.

Fig. ID(ii) schematically illustrates the improved situation in which the tube 24 of the 4K shield is divided axially into multiple parts 24a. As discussed above, each of these shorter tubes will have higher resonant frequencies, and which suitable arrangements of mounting points may easily ensure do not resonate at frequencies of operation of the gradient coils of the imaging system.

The amplitude of oscillation is reduced in arrangements where the tube is divided axially. It is particularly important that the mounting points be resistant to loosening by vibration, by using glued boas, welding or similar, and ensuring that any fixed components such as bolts are thermally matched to the adjacent fixed components.

Rather than providing a number of separate, separately mounted, short tubes 24a, much the same effect of increasing the resonant frequency is obtained by providing a radial constraint to the tube at similar intervals, at 200-300mm axial intervals for example. Most simply, and referring to Fig. IA, this may be achieved by providing a set of mounting points 26 spaced around the circumference of the tube 24 at axial intervals of 200-300mm. As the tube is restrained every 200-300mm, those parts of the tube between the sets of mounting points oscillate as a constrained tube of length 200-300mm, and so the tube has a rather higher set of resonant frequencies than wouki be the case with a single tube running the length of the magnet. The same comments apply as in the preceding paragraph in relation to ensuring that the mounting points are resistant to loosening by vibration and/or differential thermal contraction of components.

Another way of increasing the resonant frequency of the tube would be to increase its thickness t, as can be seen from the above equation, but this will be at the expense of material and wire cost, since the diameter of the coils 10 would have to increase accordingly, to accommodate the increased thickness of the tube 24 without reducing the useful bore diameter.

A 3 mm thick aluminium tube has been found adequate to provide the required shiekiing. If the tube is made of a commercially pure" grade of aluminium, such as is known as Al 1200, the skin depth at 1000 Hz is 0.6mm. This is a relatively cheap option and has significant manufacturing advantages. For a very pure grade of aluminium with a RRR (Residual Resistivity Ratio) of 1000, the skin depth at 1000 Hz is 0.1mm. Such a material may be 99.999% pure, colloquially known as "five-nines" or SN purity. The dissipation in the high purity aluminium will be significantly less, meaning that eddy currents in the tube will generate much less heat, although the magnitude of the eddy currents, and so the magnetic fields generated by them, will be rather greater.

Fig. IE shows another variant of the embodiment of Fig. IA. In this arrangement, cryogen-filled cooling loops are provided by conductive omega-section tubes 36, thermally and mechanically attached to the tube 24 and the support structure 15, for example by welding, soldering or brazing. These serve to cool both the support structure 15 and the tube 24, reducing the need for thermal conduction between the tube 24 and the support structure 15. Separate cooling loops may be provided for the support structure 15 and the tube 24, or a single cooling loop may be provided, which includes both omega-section tubes 36 shown in Fig. I E. Fig. 1 F illustrates a variant which may be employed in any of the above-described embodiments. In this variant, annular end piece 28 is welded 38 both to the support structure 15 and to the tube 24. In this variant, good thermal conduction is provided through the welds 38 and the annular end pieces 28.

Fig. I G(i) shows another embodiment of the invention, in which a tube 24 formed of a commercial grade of aluminium such as A11200, as above, is clad with a layer 40 of very high (e.g. SN) purity grade of aluminium. Because of the high cost of the high purity material, its thickness can be limited to about 0.5 mm due to the mechanical support provided by the tube 24 of commercial grade aluminium. Such a configuration has the advantage of limiting Lorentz forces and stresses during a quench, due to the high conductivity of the SN cladding and the structural strength of the commercia' grade tube.

Fig. IG(ii) shows another embodiment of the invention, in which a tube 24 formed of a commercial grade of aluminium such as Al 1200, as above, is clad with lengths of superconducting wire 42 in a basket-weave arrangement. As the tube 24 will be cooled to below the transition temperature of the superconducting wire, then the wire 42 forms a layer of very low electrical resistance to exclude stray gradient-coil generated magnetic flux from the vicinity of the coils, but also resists the generation of large eddy currents as the structure will have appreciable electrical resistance in closed electrical paths.

Figs. 2A-2C(ii) illustrate a further series of embodiments of the invention, which include a 4K shield in the form of a conductive cladding bonded or otherwise fixed directly to the magnet coils.

As shown in Fig. 2A, this embodiment resembles that of Fig. IA at least in that it includes coils 10 bonded on their radially outer surfaces 12 to a support structure 15 containing cooling channels 22. As illustrated, an optional electrically isolating layer 16 is provided between the radially outer surface of the coils and the mechanical support structure 15. The OVC 18, therma shield 20 and gradient coil assembly 30 are as described above.

According to this embodiment of the invention, a closely-coupled 4K shield 100 is provided, in mechanical contact with each coil 10. The closely-coupled 4K shield may be manufactured from high-purity aluminium foil, or a superconducting foil. It is preferably electrically and thermally isolated from the associated coil 10 by an electrically and thermally insulating layer 102, for example of resin-impregnated glass fibre cloth.

This embodiment has the advantage of using a much thinner 4K shield 100, which occupies much less space than the 4K shield of Figs. IA-1G(ii) and has a much higher resonant frequency by virtue of being directly connected to the mechanically stiff cold mass 10, 15.

As the thermal impedance between the shield 100 and coils 10 will necessarily be lower in the embodiment of Fig. 2A than in the embodiment of Fig. 1A, the dissipation in the shield must be reduced to a very low level to prevent unacceptable heating of the coils which are in close proximity. The required low dissipation may be achieved by ensuring that the close-coupled 4K shield has a low electrical resistivity. This may be achieved by forming the close-coupled 4K shield of high purity aluminium cladding (e.g. having a RRR >1500 at zero field); or of a superconducting material such as NbTi foil.

Fig. 2A more specifically illustrates an embodiment in which the close-coupled 4K shiekl 100, formed as a cladding over each coil, is welded 104 to the support structure 15, which is preferably made of aluminium, like the 4K shield. It may be found difficult to weld a superconducting material to the support structure. As iflustrated, it may be found beneficial to form a lip 106 in the material of the support structure, to assist in the welding step.

As shown in Fig. 2A, one edge of the close-coupled 4K shield may be welded 104 to the support structure, while the other edge 107 may be attached by an adhesive. For example, various resin adhesives sold by Emerson and Cuming under the STYCAST brand may be found suitable. The primary thermal path from the 4K shield 100 to the support structure 15 will be through the weld 104, having lower thermal impedance than the adhesive joints at the other end 107. Nevertheless, the greater surface area and tolerable thermal impedance of the adhesive joint at 107 means that a useful degree of thermal conduction also takes place through the adhesive joints. The electrically isolating layers 16, 102 should withstand voltages of 5kV or more, to ensure that the electrical isolation does not break down in the case of a quench.

Fig. 2B illustrates a simple thermal model of the structure of Fig. 2A The electrically isolating layers 16, 102 are represented as thermal impedances. As illustrated, a thermal load 0 is provided by black body radiation from thermal shield 20 towards coils 10. This thermal load is intercepted by the close-coupled 4K shield 100. In the illustrated model, it is assumed that both edges of the close-coupled 4K shield are attached to the support structure 15 with equal thermal conductivity) and that the edges are joined to the support structure at equal distances from cooling channels 22 of equal temperature. In these conditions, the thermal load 0 will divide equally between the two radially-directed parts of the close coupled 4K shield 100, and a thermal load of 0/2 will flow along each, as shown in Fig. 2B.

Fig. 2C(i) shows an intermediate stage in a method of manufacturing a structure as shown in Fig. 2A. As is conventional in the formation of resin-impregnated coils, a mould is formed of a journal surface 108 and two annular retaining plates 110.

Pressed channel pieces 112 of high-purity aluminium or superconducting foil are positioned inside the mould, at least substantially covering the interior surfaces of the mould formed by the journal surface 108 and the annular retaining plates 110. An axially-extending gap 114 may be left between adjacent channel pieces 112, or at least some of them. Such gaps will reduce eddy currents during ramping and quench, but will allow some thermal load to reach the coils. ln an alternative arrangement, neighbouring channel pieces 112 may be positioned to overlap, with an electrically isolating layer placed between them to prevent electrical conduction between one channel piece and the next. A layer of porous electrically insulating material 116, such as glass fibre cloth, is provided over the inner surfaces of the channel pieces 112.

With the mould prepared in this way, a coil is wound into the mould in the conventional manner. Once winding of the coil is complete, a radially outer part of the mould, shown in phantom at 120 is positioned over the coils to complete the mould cavity. As is conventional, a crust layer of glass cloth may be wound over the coil, within the mould cavity or a crust layer of glass beads may be provided within the mould cavity, between the radially outer surface of the coil and the radially inner surface of the radially outer part 120 of the mould. The coil, the electrically insulating layer 116 and the crust layer 16 are then impregnated with resin which is cured, as is conventional. The electrically insulating layer 116 becomes electrically isolating layer 102 as shown in Fig. 2A. In arrangements such as shown in Fig. 2A, the radially outer part of the mould 120 may be a section of the support structure. ln this case, the radially inner surface of the radially outer part 120 of the mould may be treated to provide a good bond between the section of the support structure and the resin of the coil. ln other arrangements, radially inner surface of the radially outer part 120 of the mould may be treated with a release compound to ensure that it does not bond to the resin of the coil, and the resin impregnated coil so formed may then be bonded to another support structure in a separate bonding step.

Preferably, and as illustrated in Fig. 2C(i), one edge 118 of each channel piece 112 protrudes from the mould, and remains above the level of the resin during the impregnation step. This ensures that those edges remain clean, so that they may easily be welded, as shown at 104 in Fig. 2A.

The method described with reference to Fig. 20(i) may be referred to as a "single step" process, as the coils are formed, impregnated and provided with a close-coupled 4K shield 100 all in the same processing step.

In contrast, Fig. 20(u) shows an intermediate stage in a "two-step" method of manufacturing a structure as shown in Fig. 2A. Ln this method, coils 10 are wound, impregnated and bonded to support structure 15 by any convenient, conventional method. For example, the coil may be wound into a mould similar to that shown in Fig. 20(i) and bonded to support structure 15 during the impregnation step, or may be impregnaled separately and bonded to the support structure in a separate step.

An electrically isolating layer, as at 116 in Fig. 20(i), may be applied to the coils during the winding and impregnations step. Alternatively, no such layer may be applied at that stage.

In the second step of this method, channel pieces 112 are affixed to cover the axial and radially inner surfaces of the coils 10. This may be achieved by applying a layer of epoxy resin adhesive, for example any of various resin adhesives sold by Emerson and Cuming under the STYCAST brand may be found suitable. Alternatively, and if no electrically isolating layer is provided on the coil during the winding and impregnation step, the inner surfaces of the channel pieces 112 may be covered with an uncured resin-impregnated electrically isolating layer 116 such as glass fibre cloth. The channel pieces 112 are then applied to the coil, and the resin-impregnated electrically isolating layer 116 cured, to bond the channel pieces 112 onto the coils.

As in the embodiment of Fig. 20(i), edges 118 should be kept free of resin, so as not to interfere with a welding step 104. As in other embodiments, the conductive channel pieces 112 may be welded or adhesively bonded to the support structure 15.

The channel pieces are preferably of high purity aluminium, such as SN purity aluminium, as discussed above, or superconducting foil such as NbTi foil. Other materials may be used, but high purity aluminium is presently found to be easily available, relatively cheap and highly conductive.

In all cases, it is imperative that robust electrical insulation, and significant thermal insulation, 102, is placed between the coils 10 and the channel pieces 112 forming the 4K shield, to prevent electrical breakdown during a quench, and to limit the amount of heat transferred to the coils 10 through the thermal resistance of isolating layer 102. It is also desirable to include breaks 114 between channel pieces 112 to prevent excessive eddy current heating of the 4K shield 100 during ramping of the magnet.

The present invention accordingly provides a 4K shield useful in reducing the risk of gradient coil interaction, either by induced heating or stray magnetic fields, which might cause quenching in the superconducting coils of dry or minimum-cryogen magnet systems. The shield also serves to reduce gradient coil induced heating GCIH at 4K in such a magnet system.

In one group of embodiments, the 4K shield comprises a cooled tube spaced away from the coils but mounted to the cold mass in such a way as to present less impedance to heat flow from the 4K shield to the cooling arrangement than the route through the coils themselves. The shield supports may be arranged such that the main resonant frequencies of the 4K shield are higher than those excited during imaging. In one embodiment, the 4K shield is faced with high conductivity material to minimise the heat-load to the cooling system. Particular advantages of this embodiment are ease of manufacture, ease of achieving the required electrical insulation integrity, good thermal separation between the coil and shield and very good scope for dynamic tuning of the shield system.

In another group of embodiments, the coils are provided with cooled high conductivity cladding, closely mechanically coupled to the coils. These embodiments take up less radial space and readily achieve the requirement of high resonant frequency (>3000Hz) by virtue of being fixed to the stiff cold-mass. The main challenge of such arrangements is to minimise the heat conducted to the coil from the closely coupled shield. This may be achieved by the use of high conductivity materials and careful choice of the insulating layer between the coils and cladding.

The first group of embodiments, using a cooled tube, has the advantages of manufacturing ease and the relative ease of achieving the required 5kV voltage isolation The 4K shields provided by the present invention provide black-body radiation shielding for the coils, and provide magnetic shielding for the coils such that the coil temperature increase due to GUlF-f remains below the threshold which would make the magnet quench. These objectives may be achieved, according to the present invention, with minimum dissipation of heat in the cooled components and in a manner that is easy to manufacture, that can be implemented in the minimum possible radial space and that achieves the required voltage isolation between the magnet coUs and ground potential.

Claims (30)

1. CLAIMS: 1. A cylindrical superconducting magnet comprising a plurality of axially-aligned annular coils of superconducting wire, arranged for cooling by thermal conduction through a cooled surface in mechanical contact with the coils, the coils being provided with a thermal radiation shield between their radially inner surface and their axis, characterised in that the thermal radiation shield comprises a metal layer in thermal contact with the cooled surface.
2. 2. A cylindrical superconducting magnet according to any preceding claim wherein a thermal resistance between the metal layer and the cooled surface is less than each respective thermal resistance between each of the coils and the cooled layer.
3. 3. A cylindrical superconducting magnet according to claim I or claim 2, wherein the metal layer comprises a cylinder of metal, mechanically and thermally joined to the cooled surface.
4. 4. A cylindrical superconducting magnet according to claim 3, wherein the thermal radiation shield is mechanically and thermally joined to the cooled surface at axial and circumferential intervals.
5. 5. A cylindrical superconducting magnet according to claim 3 or claim 4, wherein the thermal radiation shield is axially divided into a plurality of cylinders, each mechanically and thermally joined to the cooled surface.
6. 6. A cylindrical superconducting magnet according to any of claims 3-5, wherein the thermal radiation shield is mechanically and thermally joined to the cooled surface at axial and circumferential intervals of 0.3m or less.
7. 7. A cylindrical superconducting magnet according to any preceding claim, wherein the thermal radiation shield comprises a cylinder of a first metal of a first conductivity, mechanically and thermally joined to the cooled surface, with a cladding of a second metal of a second conductivity, greater than the first conductivity, applied to the radially inner surface of the cylinder.
8. 8. A cylindrical superconducting magnet according to claim 7 wherein the second metal cladding comprises aluminium of at least 99.999% purity.
9. 9. A cylindrical superconducting magnet according to claim 7 wherein the second metal comprises a pattern of superconducting wires.
10. 10. A cylindrical superconducting magnet according to claim 1, wherein the thermal radiation shield comprises a conformal layer of metal foil, applied over the radially inner surface of each coil, and wherein a thermally insulating layer is interposed between each coils and the metal foil layer.
11. 11. A cylindrical superconducting magnet according to claim 10, wherein the conformal layer of metal foil is also applied over axially-directed surfaces of each coil, and wherein the thermally insulating layer is also interposed between each coils and the metal foil layer on the axially-directed surfaces.
12. 12. A cylindrical superconducting magnet according to claim 10 or claim 11, wherein the layer of metal foil is provided with breaks in electrical conductivity.
13. 13. A cylindrical superconducting magnet according to claim 12, wherein the breaks in electrical conductivity are directed in a direction parallel to the axis, thereby to restrict circumferential conductivity of the layer of metal foil.
14. 14. A method of manufacturing a cylindrical superconducting magnet according to claim 1, comprising the steps of: -providing a mould comprising a journal surface (108) and two annular retaining plates (1 10); -positioning electrically conductive channel pieces (112) inside the mould, at least substantially covering the interior surfaces of the mould formed by the journal surface (108) and the annular retaining plates (110); -providing a ayer of porous electrically insulating material (116) over the inner surfaces of the channel pieces (112); -winding a coil (10) into the mouki; -positioning a radially outer part (120) of the mould over the coils to complete a mould cavity; -impregnating the coil, and the electrically insulating layer (116) with resin which is then cured; and -removing the journal surface (108) and the two annular retaining plates (110).
15. 15. A method according to claim 14 wherein the electrically conductive channel pieces are composed of high-purity aluminium or superconducting foil.
16. 16. A method according to claim 14 or claim 15 wherein an axially-extending gap (114) is left between adjacent channel pieces (112), or at least some of them.
17. 17. A method according to claim 14 or claim 15 wherein neighbouring channel pieces (112) are positioned to overlap, with an electrically isolating layer placed between them to prevent electrical conduction between one channel piece and the next.
18. 18. A method according to any of claims 14-17 wherein a crust layer of glass cloth is wound over the coil, within the mould cavity, between a radially outer surface of the coil and a radially inner surface of the radially outer part (120) of the mould, the crust layer being impregnated with resin during the impregnation step.
19. 19. A method according to any of claims 14-17 wherein a crust layer of glass beads is provided within the mould cavity, between the radially outer surface of the coil and the radially inner surface of the radially outer part (120) of the mould, the crust layer being impregnated with resin during the impregnation step.
20. 20. A method according to any of claims 14-19 wherein the radially outer part of the mould (120) is a section of the support structure, the radially inner surface of the radially outer part (120) of the mould being treated to provide a good bond between the section of the support structure and the resin.
21. 21. A method according to any of claims 14-19 wherein the radially inner surface of the radially outer part (120) of the mould is treated with a release compound to ensure that it does not bond to the resin of the coil, and the resin impregnated coil so formed is bonded to another support structure in a separate bonding step.
22. 22. A method according to any of claims 14-21, wherein an edge (114) of each channel piece 112 protrudes from the mould, and remains above the evel of the resin during the impregnation step.
23. 23. A method of manufacturing a cylindrical superconducting magnet according to claim 1, comprising the steps of: -winding, impregnating and bonded to support structure (15) of a coil (10); -applying an electrically isolating layer (102; 116) over the axial and radially inner surfaces of the cois; -affixing channel pieces (112) are affixed over the electrically isolating layer to cover the axial and radially inner surfaces of the coils.
24. 24. A method according to claim 23 wherein the channel pieces are affixed by a layer of epoxy resin adhesive.
25. 25. A method according to claim 23 or claim 24 wherein the electrically isolating layer is applied by lining a mould with an electrically isolating filler layer (116), winding the coil within the fiUer layer, and impregnating the filler layer with a resin during a step of impregnating the coil.
26. 26. A method according to claim 24 wherein the steps of applying an electrically isolating layer and affixing channel pieces comprises covering inner surfaces of the channel pieces with an uncured resin-impregnated electrically isolating ayer (116); applying the channel pieces to the coil, and curing the resin-impregnated electrically isolating layer, to bond the channe pieces onto the coils.
27. 27. A method according to any of claims 14-26, further comprising the step of welding the channel pieces to the support structure.
28. 28. A method according to any of claims 14-26, further comprising the step of adhesively bonding the channel pieces to the support structure.
29. 29. A cylindrical superconducting magnet substantially as described and/or as iflustrated in Figs. 1A-2B of the accompanying drawings.
30. 30. A method of manufacturing a cyIindrica superconducting magnet substantially as described and/or as illustrated in Figs. 2C(i) -2C(ii) of the accompanying drawings.Amendments to claims have been filed as follows 1. A cylindrical superconducting magnet comprising a plurality of axially-aligned annular coils of superconducting wire, arranged for cooling by thermal conduction through a cooled surface in mechanical contact with the coils, the coils being provided with a thermal radiation shield between their radially inner surface and their axis, the thermal radiation shield comprising a conformal layer of metal foil in thermal contact with the cooled surface, applied over the radially inner surface of each coil, and wherein a thermally insulating layer is interposed between each coil and the metal foil layer, characterised in that.the conformal layer of metal foil is also applied over axially-directed surfaces of each coil, and wherein the thermally insulating layer is also interposed between each coils and the metal foil layer on the axially-directed surfaces. Co2. A cylindrical superconducting magnet according to any preceding claim wherein a thermal resistance between the metal layer and the cooled surface is less than each respective thermal resistance between each of the coils and the cooled layer.3. A cylindrical superconducting magnet according to claim I or claim 2, wherein the layer of metal foil is provided with breaks in electrical conductivity.4. A cylindrical superconducting magnet according to claim 3, wherein the breaks in electrical conductivity are directed in a direction parallel to the axis, thereby to restrict circumferential conductivity of the layer of metal foil.5. A method of manufacturing a cylindrical superconducting magnet according to claim 1, comprising the steps of: -providing a mould comprising a journal surface (108) and two annular retaining plates (110); -positioning electrically conductive channel pieces (112) inside the mould, at least substantially covering the interior surfaces of the mould formed by the journal surface (108) and the annular retaining plates (110); -providing a layer of porous electrically insulaUng material (116) over the inner surfaces of the channel pieces (112); -winding a coil (10) into the mouki; -positioning a radially outer part (120) of the mould over the coils to complete a mould cavity; -impregnating the coil, and the electrically insulating layer (116) with resin which is then cured; and -removing the journal surface (108) and the two annular retaining plates (110).6. A method according to claim 5 wherein the electrically conductive channel pieces are composed of high-purity aluminium or superconducting foil.7. A method according to claim 5 or claim 6 wherein an axially-extending gap 04 (114) is left between adjacent channel pieces (112)7 or at least some of them.v-'1 15 00 8. A method according to claim 5 or claim 6 wherein neighbouring channel pieces (112) are positioned to overlap7 with an electrically isolating layer placed between them to prevent electrical conduction between one channel piece and the next.9. A method according to any of claims 5-8 wherein a crust layer of glass cloth is wound over the coil, within the mould cavity, between a radially outer surface of the coil and a radially inner surface of the radially outer part (120) of the mould, the crust layer being impregnated with resin during the impregnation step.10. A method according to any of claims 5-8 wherein a crust layer of glass beads is provided within the mould cavity, between the radially outer surface of the coil and the radially inner surface of the radially outer part (120) of the mould, the crust layer being impregnated with resin during the impregnation step.11. A method according to any of claims 5-10 wherein the radially outer part of the mould (120) is a section of the support structure, the radially inner surface of the radially outer part (120) of the mould being treated to provide a good bond between the section of the support structure and the resin.12. A method according to any of claims 5-10 wherein the radially inner surface of the radially outer part (120) of the mould is treated with a release compound to ensure that it does not bond to the resin of the coil, and the resin impregnated coil so formed is bonded to another support structure in a separate bonding step.13. A method according to any of claims 5-12, wherein an edge (114) of each channel piece (112) protrudes from the mould, and remains above the level of the resin during the impregnation step.14. A method of manufacturing a cylindrical superconducting magnet according to claim 1, comprising the steps of: -winding, impregnating and bonding a coil (10) to a support structure (15); -applying an electrically isolating layer (102; 116) over the axial and radially inner (\J surfaces of the coils; -affixing channel pieces (112) over the electrically isolating layer to cover the axial co and radially inner surfaces of the coils.15. A method according to claim 14 wherein the channel pieces are affixed by a layer of epoxy resin adhesive.16. A method according to claim 14 or claim 16 wherein the electrically isolating layer is applied by lining a mould with an electrically isolating filler layer (116), winding the coil within the filler layer, and impregnating the filler layer with a resin during a step of impregnating the coil.17. A method according to any of claims 4-16, further comprising the step of welding the channel pieces to the support structure.18. A method according to any of claims 4-16, further comprising the step of adhesively bonding the channel pieces to the support structure.19. A cylindrical superconducting magnet substantially as described and/or as illustrated in Figs. IA-IS of the accompanying drawings.20. A method of manufacturing a cyIindrica superconducting magnet substantially as described and/or as illustrated in Figs. 1G(i) -1C(ii) of the accompanying drawings. (4 Co (4