Method of manufacturing a superconducting magnet

Information

  • Patent Grant
  • 6735848
  • Patent Number
    6,735,848
  • Date Filed
    Monday, September 25, 2000
    23 years ago
  • Date Issued
    Tuesday, May 18, 2004
    20 years ago
Abstract
Method of manufacture a wide bore, high field superconducting magnet. The superconducting magnet has a plurality of superconducting coils impregnated with epoxy and nested within each other. An innermost one of the nested coils has a bore therethrough that defines a bore width of the magnet. The bore width is greater than approximately 100 millimeters. The nested coils are electrically connected in series and cooled to an operating temperature less than approximately 4 degrees K. The magnet also has external reinforcements on the coils that are applied prior to impregnating the coils with epoxy. An active protection circuit protects the coils in response to a quench in the magnet. The protection circuit includes heater elements positioned in thermal contact with the coils prior to impregnating the coils with epoxy. The magnet further has lead supports for supporting the lead wires with epoxy that extend from the coils.
Description




BACKGROUND OF THE INVENTION




The invention relates generally to a high field magnet and, particularly, to a high field superconducting magnet having a wide bore for use in a nuclear magnetic resonance (NMR) spectrometer.




The technique of NMR has proven to be a powerful and unique tool for the study of complex molecular structures. High current density superconducting magnets are particularly well suited to provide the magnetic field uniformity and persistence required for NMR. As a result, a relationship exists between the available range of application of NMR spectroscopy, in field and sample volume, and the state of the technology of high current density superconducting magnets. Traditionally, increased field strength in high resolution NMR magnets has been sought for the study of the structure of molecules of increasing size. The number of spectral lines associated with larger molecules requires the increased line separation and sensitivity afforded by higher fields. Recently, unexpected benefits of high fields have been realized due to mechanisms of line width minimization at fields being approached in available spectrometer magnets. As a result, the motivation for increased field strength in NMR magnets is greater than ever. There are currently a number of programs under way with the objective of NMR at 1 GHz, corresponding to 23.5 T, and above. The possibility of these high fields depends, as a necessary condition, on the availability of a superconductor and associated coil technology for that field.




Given the scientific and commercial importance of NMR and the associated spectrometer magnets, there is motivation to address the technology of high current density superconducting magnets. More specifically, very high field NMR magnet technology is desired for instrumentation to support high field NMR research and to provide a wide bore 900 MHz spectrometer magnet. Such a magnet is also desired because the technology development activities directed toward the requirements of the 900 MHz magnet specifically are also applicable generally to high field NMR magnets, to high field, high current density superconducting magnets, and more generally to many aspects of magnet technology regardless of the type of conductor and construction being employed.




Moreover, a high field magnet with a larger bore than presently available is desired. Those skilled in the art believe that such a wide bore or large bore magnet will serve as an essential stepping stone to 1 GHz or higher frequency systems. Due to the high stored energy of the 900 MHz system and the associated large magnetic forces, however, the production of a successful system is challenging.




In general, a magnet of this type employs Nb


3


Sn and NbTi conductors in a set of epoxy impregnated long solenoids plus compensation coils for uniformity. The high field and large bore result in large mechanical stress in the coils and large magnetic stored energy. Therefore, reinforcement of the windings and an active protection system is desired.




Moreover, magnetic field uniformity is critical to NMR. Ferromagnetic welds cause field inhomogeneity. Historically, magnet designs have avoided ferrous structural alloys to prevent potential field distortions from welds. This strategy is problematic in fabricating high field magnets because austenitic stainless steel is the preferred heat treatment material for bore tubes in Nb


3


Sn coils. Early high field NMR designs employed the removal of the bore tubes after heat treatment and epoxy impregnation. Bore tube removal is dangerous due to the risk of damaging the reacted Nb


3


Sn conductor and leads. A more practicable fabrication approach is to leave the stainless steel bore tubes in place. For this reason, a weld metal on the coil form that avoids magnetic fields is desired.




A major obstacle to producing a wide bore, high field magnet involves the relatively large mechanical stresses caused by the magnetic fields in the magnet. Energizing a wound coil with an electric current produces a magnetic field accompanied by an associated mechanical stress in the coil. As the strength of the magnetic field produced by the coil increases, the magnitude of the mechanical stress increases as well. In this instance, a magnetic coil wound with superconductor produces a very high field and, thus, mechanical stresses become an important design factor.




In general, superconductors are composite materials in the form of flat tapes or wires (round or rectangular). The composite conductor typically includes copper or silver for protection and stabilization in addition to a superconducting alloy or compound. The composite conductor may also have substantial fractions of other materials (e.g., bronze). Unfortunately, the materials normally found in high field superconductors are generally of low strength and the high temperature heat treatment and annealing to which such conductors are subject diminishes their strength even further. For this reason, a magnetic coil structure providing sufficient strength to withstand the high mechanical stresses that appear in the windings of a high field magnetic coil is desired. There have been some attempts at high strength versions of superconductors, but even these materials would benefit from additional high strength supporting materials in high field magnet applications.




Magnetic coils used for the production of high magnetic fields are often cylindrical in form. In a cylindrical coil, there are two main components to the mechanical forces in the windings. First, a force in a radially outward direction generally tends to expand the diameter of the coil. Second, an axial force at each end of the coil toward the center results in a pressure at the midplane of the coil and tends to make the coil shorter. Both of these forces can produce excess mechanical stress on the conductor. Therefore, magnet reinforcement is desired for containing the radial component of the force to limit the radial expansion of the windings as well as containing the axial component of the force to reduce the pressure on the conductor at the center of the coil about the midplane.




Those skilled in the art are familiar with reinforcing a cylindrical magnetic coil by applying structural material to the outside surface of the coil. The added material forms a secondary cylindrical structure in contact with the cylindrical structure of the coil windings. For example, high strength wire wound into place over the magnetic coil provides reinforcement for the conductor in the coil. This construction has strength in the radial direction, against the expansion of the hoops formed by the reinforcement winding, but can be weak in the axial direction, where any spaces between the turns in the reinforcement winding reduce the stiffness in the axial direction. External reinforcement of this type may be applied without additional bonding material, relying on winding tension alone to hold the reinforcement winding in position, but is commonly applied along with a bonding material such as epoxy. The epoxy serves to fill any gaps between the turns in the reinforcement winding and to increase the stiffness of the reinforcement in the axial direction.




Those skilled in the art recognize that the forces or stresses on the magnet increase as the strength of the magnetic field increases. The so-called Al5 high field superconductors, including Nb


3


Sn, are used to produce coils with the highest fields and forces but also tend to be the most brittle and subject to damage from mechanical stress. Unfortunately, the fabrication process for this type of coil places restrictions on the manner in which the reinforcement can be included in the design. One method of fabricating a high field superconducting coil, commonly referred to as “wind and react,” begins with winding the coil with an intermediate stage of conductor. The coil is then heat treated in a furnace at high temperature allowing the components of the intermediate stage conductor to react to form the final superconducting compound. The coil may then be finished by impregnation with an epoxy to secure the relatively weak, brittle superconducting wires and fragile insulation. Nb


3


Sn and the other Al5 superconductors, for example, are referred to as “wind and react” conductors because they undergo a heat treating process to form the actual superconducting material.




The conventional process of externally reinforcing the coil involves applying the winding on the outside of the finished, epoxy impregnated coil. There are two major drawbacks to this method. In order to apply the reinforcement winding to the finished coil, after the coil is epoxy impregnated and essentially complete as an electrical winding, the coil must be refitted in the winding machine for the application of the reinforcement. This requirement is not severe for a small coil, but as the size of the coil increases for higher field magnets, this processing step becomes increasingly burdensome. Furthermore, this situation makes it difficult to achieve a strong bond between the reinforcement and the coil winding because the reinforcement winding is being applied over a completed, epoxy impregnated winding. The bond of fresh epoxy over already cured epoxy at the interface between the coil winding and the reinforcement winding will have a strength inferior to the shear strength within the windings themselves.




Although applying the reinforcement winding over the conductor winding after heat treatment, but before epoxy impregnation, would solve the problem of the epoxy bond strength, the conductor in the coil after heat treatment is sufficiently brittle that the application of the reinforcement before impregnation of the winding would present a large risk to the integrity of the conductor. Therefore, this option is not available.




For these reasons, an improved method of applying external reinforcement windings to a high field superconducting coil that achieves the objective of providing structural reinforcement in the radial and axial directions and which is compatible with the other process requirements of these coils is desired.




Adequate quench protection presents another obstacle to producing high field magnets. Since superconducting magnets are designed to produce high magnetic fields, they store relatively large amounts of magnetic energy in normal operation. Superconducting magnets are subject to a mode of failure, known as “quench,” in which the stored energy is suddenly converted into heat accompanied by the presence of large electrical voltages. A quench occurs when there is a transition from the superconducting state to the normal state of the conductor in some region of the coil. In the normal state, the conductor has an electrical resistance and is heated by the current in the magnet. If the region is of limited size, and all the energy of the magnet is deposited in the region, the energy density is high and the region will be likely to overheat. The excessive heat and voltage during a quench can damage a magnet's windings. Although systems are known for protecting the magnet from damage due to a quench fault condition, these conventional systems are not well-suited for high field superconducting magnets such as those desired for NMR.




With some superconducting magnets, it is possible to remove the stored energy from the coil using an external dump resistor and switch. When a quench detector senses the quench condition in the magnet, a protective circuit opens the switch to essentially create a series circuit of inductor and resistor. The magnet largely deposits its stored energy in the external resistor as it decays with a time constant characteristic of such circuits. Although this type of protection system may be suitable for superconducting magnets that operate at relatively high current in powered mode, an external dump of energy is not practical for NMR spectrometer magnets that operate at relatively low current in persistent mode.




One alternative to removing the magnetic stored energy during a quench condition is to dissipate the energy internally to the magnet windings. A quench is usually a local phenomenon and, thus, the energy will dissipate locally. In this instance, the local region will overheat and be damaged if enough energy is available in the magnet. Distributing the energy somewhat uniformly over the entire volume of the magnet will help prevent overheating any one portion of the windings. Conventional protection systems are available for distributing the stored energy in the magnet. The particular type of system used depends on the type of magnet involved.




In a single coil magnet, which is a single, thermally-connected structure, conventional protection techniques involve electrically subdividing the coil into sections and providing a shunt path for each section. The shunt may consist of a resistor in parallel with the coil section, a diode in parallel with the coil section, or a series combination of a resistor and a diode in parallel with the coil section. In the event of a quench in one section, the current can shift into the shunt parallel with that section, and reduce the heating in the section that quenched. This hopefully will provide sufficient time for the quench to propagate by thermal conduction to the other sections of the coil, increasing the volume of the coil over which the heat is dissipated and thereby reducing the temperature. Spreading the quench of a superconducting coil throughout the coil in the event that one region of the coil quenches is the basic purpose and function of quench protection systems for magnets that are internally protected. Protection systems differ in the way these objectives are achieved. Unfortunately, use of the shunt path to spread the quench only works for coil sections that are thermally connected. In a magnet of multiple independent coils, the quench cannot thermally propagate to other coil sections.




Therefore, a circuit is desired for the protection of large magnets with large stored energy and risk associated with quench that is able to spread the quench of a superconducting coil throughout the coil in the event that one region of the coil quenches.




Yet another problem associated with conventional magnet design involves the leads of the superconducting coil. Mechanical stress on the lead wire extending from a coil, resulting from Local Lorentz forces or relative motion between the coil and the surrounding support structure, for example, can damage the lead wire. Moreover, certain known high field superconductors formed by a high temperature heat treatment are relatively brittle. Thus, the amount of bending allowed by the superconductor is very limited after heat treatment. For this reason, the conductor is often wound while it is still relatively ductile prior to heat treatment. The conductor, however, must be placed in a final position before heat treatment, held in that position during heat treatment, and kept free from bending after heat treatment. Therefore, it is necessary to position the lead from a superconducting coil during winding and to maintain that position during and after heat treatment until the lead can be formed into a structure designed to prevent it from being damaged.




U.S. Pat. No. 5,739,689, the entire disclosure of which is incorporated herein by reference, discloses a superconducting NMR magnet configuration. U.S. Pat. Nos. 5,690,991 and 4,744,506, the entire disclosure of which are incorporated herein by reference, teach superconducting joints for use in superconducting magnets.




SUMMARY OF THE INVENTION




The invention meets the above needs and overcomes the deficiencies of the prior art by providing an improved 900 MHz wide bore NMR spectrometer magnet. Among the several objects and features of the present invention may be noted the provision of such magnet that provides increased field strength; the provision of such magnet that provides a higher spectrometer frequency; the provision of such magnet that permits a wide bore; and the provision of such magnet that is economically feasible.




Briefly described, a method of manufacturing a superconducting magnet embodying aspects of the invention begins with winding a plurality of superconducting coils. The method also includes the steps of impregnating the coils with epoxy and nesting the coils within each other. An innermost one of the nested coils has a bore through it that defines a bore width of the magnet. In this instance, the bore width is greater than approximately 100 millimeters. The method further includes electrically connecting the nested coils in series, cooling the nested coils to an operating temperature less than approximately 4 degrees K, and supplying power to the nested coils for charging the magnet.




Another embodiment of the invention is also directed to a method of manufacturing a superconducting magnet. The method begins with the steps of winding a plurality of superconducting coils and externally reinforcing at least one of the coils. The method continues with impregnating the coils with epoxy after the reinforcing step and nesting the coils within each other. The method further includes the steps of electrically connecting the nested coils in series, cooling the nested coils to an operating temperature less than approximately 4 degrees K, and supplying power to the nested coils for charging the magnet.




In yet another embodiment, a method of manufacturing a superconducting magnet begins with the steps of winding a plurality of superconducting coils and positioning a heater element in thermal contact with one or more of the coils for heating the coils in response to a quench in the magnet. The method continues with impregnating the coils with epoxy after positioning the heater element and nesting the coils within each other. The method further includes the steps of electrically connecting the nested coils in series, cooling the nested coils to an operating temperature less than approximately 4 degrees K, and supplying power to the nested coils for charging the magnet.




Another embodiment of the invention is directed to a method of manufacturing a superconducting magnet beginning with winding a plurality of superconducting coils. The method also includes placing a mold around one or more of the lead wires adjacent an end of the respective coil. In this method, the mold defines a generally frustoconical region surrounding at least a portion of the lead wire. The method continues with the step of impregnating the coils with epoxy, which causes the mold to fill with epoxy, and the step of nesting the coils within each other. The method further includes the steps of electrically connecting the nested coils in series, cooling the nested coils to an operating temperature less than approximately 4 degrees K, and supplying power to the nested coils for charging the magnet.




A superconducting magnet embodying aspects of the invention includes a plurality of superconducting coils impregnated with epoxy and nested within each other. An innermost one of the nested coils has a bore through it that defines a bore width of the magnet. In this instance, the bore width is greater than approximately 100 millimeters. The nested coils are electrically connected in series and cooled to an operating temperature less than approximately 4 degrees K.




Another embodiment of the invention is a superconducting magnet having a plurality of superconducting coils impregnated with epoxy and nested within each other. The nested coils are electrically connected in series and cooled to an operating temperature less than approximately 4 degrees K. The magnet also includes an external reinforcement on at least one of the coils. The external reinforcement is applied prior to impregnating the coil to be reinforced with epoxy.




Yet another embodiment of the invention is a superconducting magnet having a plurality of superconducting coils impregnated with epoxy and nested within each other. The nested coils are electrically connected in series and cooled to an operating temperature less than approximately 4 degrees K. The magnet also includes an active protection circuit for protecting one or more of the coils in response to a quench in the magnet. The protection circuit has at least one heater element for heating the protected coil. The heater element is positioned in thermal contact with the protected coil prior to impregnating the coil with epoxy.




In another embodiment, a superconducting magnet includes a plurality of superconducting coils impregnated with epoxy and nested within each other. The nested coils are electrically connected in series and cooled to an operating temperature less than approximately 4 degrees K. The coils have lead wires extending from them and the magnet has a lead support for supporting each of the lead wires with epoxy adjacent an end of the respective coil.




Alternatively, the invention may comprise various other methods and systems.











Other objects and features will be in part apparent and in part pointed out hereinafter.




BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a perspective view of a wide bore, high field superconducting magnet, having portions shown in section, according to a preferred embodiment of the invention.





FIG. 2

is a cross sectional view of the magnet of FIG.


1


.





FIG. 3

is a cross sectional view of one coil of the magnet of

FIG. 1

having an integral reinforcement winding thereon.





FIG. 4

is an enlarged, fragmentary, cross sectional view of the coil and reinforcement winding of FIG.


3


.





FIG. 5

is a schematic diagram of an active quench protection circuit for use with the magnet of FIG.


1


.





FIGS. 6A and 6B

are front plan and perspective views, respectively, of a heater element for use with the protection circuit of FIG.


5


.





FIGS. 7A and 7B

are front plan and perspective views, respectively, of another heater element for use with the protection circuit of FIG.


5


.





FIG. 8

is an exploded, perspective view of a lead support structure for use with the magnet of FIG.


1


.





FIG. 9

is a front plan of a lead cone assembly formed by the support structure of FIG.


8


.





FIG. 10

is a cross sectional view of the lead cone assembly of FIG.


9


.





FIG. 11

illustrates exemplary stress data for the lead cone assembly of FIG.


9


.











Corresponding reference characters indicate corresponding parts throughout the drawings.




DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS




Referring now to the drawings,

FIGS. 1 and 2

show a wide bore, high resolution NMR magnet


100


. The magnet


100


preferably provides a spectrometer frequency of 900 MHz and a field of 21.1 T in operation within a cryostat (not shown) at approximately 1.8 degrees K. In general, magnet


100


has a plurality of coils


102


of high current density Nb


3


Sn and NbTi conductors in a set of epoxy impregnated long solenoids. Magnet


100


also includes a set of compensation coils


104


for uniformity. The high field and the relatively large bore, indicated generally at


106


, cause large mechanical stress in the coils


102


in addition to large magnetic stored energy. Advantageously, magnet


100


includes lumped external reinforcement


108


for handling the stress in coils


102


and employs an active quench protection system


112


(see FIG.


5


). The layout of magnet


100


, including its individual coils


102


, is shown in cross section in FIG.


2


. The five inner most coils


102




a


-


102




e


are preferably constructed with bronze process, multifilimentary Nb


3


Sn superconductor. In this embodiment, the five outer coils, i.e., coils


102




f,




102




g


and


104




a


-


104




c,


are constructed using monolithic NbTi superconductor; the two coils


102




f


,


102




g


being long solenoids and the three coils


104




a


-


104




c


completing a set of compensation coils.




In a preferred embodiment of the invention, the warm bore width of bore


106


is approximately 110 mm and the cold bore width of bore


106


is approximately 138 mm. The largest coil height is approximately 1.5 m and its maximum outside diameter is approximately 878 mm. Other main magnet parameters of the 900 MHz wide bore magnet


100


include a current of 290 A, inductance of 953 H and stored energy of 40 MJ (see Table I).




The magnet


100


preferably has a standard configuration for NMR, especially with combined requirements of high field and uniformity. As described above, coils


102


preferably include low temperature superconductors (e.g., Nb


3


Sn and NbTi conductors) having a cryogenic operating temperature of approximately 1.8 degrees K.

FIG. 2

shows the five inner Nb


3


Sn solenoids


102




a


-


102




e


surrounded by two NbTi solenoids


102




f


,


102




g


and three compensation coils


104




a


-


104




c.


The compensation coils


104


in this embodiment are also windings of NbTi. Preferably, magnet


100


also has a plurality of shim coils external to the coil compensation set


104


. It is to be understood that a four coil compensation set is also contemplated. Such a four coil set may lead to an increase in size, however, because it has counter wound coils.




With a warm bore width on the order of 100 mm or more, bore


106


is significantly larger than that of a conventional standard bore high resolution NMR magnet. In general, a wide bore raises problems for the room temperature shims of increasing high order. The present invention preferably configures the wide bore 900 MHz magnet


100


in two different modes. First, a high resolution mode employs a room temperature shim set of conventional standard bore diameter. Second, the larger bore shim set has fewer high order shims and results in a reduction of achievable field uniformity, as might be appropriate for solid state NMR and micro-imaging.




As described above, the 900 MHz magnet


100


is generally an assembly of Nb


3


Sn and NbTi coils


102


,


104


. The first five inner coils


102




a


-


102




e


are preferably made using Nb


3


Sn wind and react technology. A separate grade of rectangular conductor is wound on each stainless steel coil form. In a preferred embodiment, coils


102




c


-


102




g


have external reinforcement


108


(see

FIGS. 3 and 4

) wound thereon. The conductors in magnet coils


102


,


104


and in the reinforcement windings


108


are preferably insulated with glass fiber (e.g., S-2) and impregnated with epoxy. As described below, the reinforcements


108


are applied prior to epoxy impregnation of the reinforced coils


102




c


-


102




g,


and prior to heat treatment for the Nb


3


Sn coils


102




c


-


102




e,


to ensure a strong bond between the conductor winding and the reinforcement winding.




High quality bronze process conductors of increasingly high critical current density in increasingly large cross section help provide advances in field strength of superconducting NMR magnets. As an example, a conductor with a cross sectioned area of 6.35 mm


2


sets the operating current at 290 A. For example, a bronze process Nb


3


Sn monolith conductor from VAC may be used based on persistent joint requirements, n-value and mechanical properties of conductor. With respect to the construction of the NbTi coils, Intermagnetics General Corporation supplies a suitable NbTi monolith conductor, also having S-2 glass fiber insulation. Table I provides exemplary parameters for 900 MHz wide bore magnet


100


.















TABLE I











PARAMETER




VALUE













Central field




21.1 T







Operating temperature




1.8° K.







Cold bore




 138 mm







Maximum outer diameter of windings




 878 mm







Maximum height of windings




1500 mm







Weight Nb


3


Sn conductor




 921 kg







Weight Nb


3


Sn reinforcement




 593 kg







Weight NbTi conductor




1273 kg







Weight NbTi reinforcement




 824 Kg







Operating current




 290 A







Inductance




 953 H







Stored energy




 40 MJ















The amount of superconductor used for each coil


102


,


104


, i.e., the fraction of superconducting component in the conductor of each coil, depends directly on the maximum field and the critical current density of the superconductor. Those skilled in the art recognize that persistent decay and n-value considerations dictate operating at a fraction of the critical current in an NMR magnet. In lower fields, given the typically higher n-values at lower fields, higher fractions of critical current may be used. Typical fractions for all coils


102


,


104


in magnet


100


span the range of 0.6 to 0.7.




The copper in each conductor in the 900 MHz magnet


100


is selected on the basis of protection considerations. In one embodiment, the copper content is designed to meet the requirements for protection alone, and not to satisfy the mechanical requirements of the windings. The actual amount of copper used is a function of the entire design and performance of the protection system.




As described above, an improved method of externally reinforcing the windings of a high field superconducting coil is needed to provide structural reinforcement in both the radial and axial directions while being compatible with the other process requirements of these coils. Those skilled in the art recognize the magnetic and thermal loads during operation of a superconducting magnet cause stresses within the magnet. In a preferred embodiment of the invention, magnet


100


includes additional material on at least some of the coils


102


for mechanical support due to the large mechanical forces and the limited allowable tangential strain in coils


102


. Preferably, the additional material for mechanical support of the magnet's windings is supplied in the form of external reinforcement windings


108


. In the illustrated embodiment, the reinforcement windings


108


support the Nb


3


Sn conductors of coils


102




c


-


102




e


and the NbTi conductors of coils


102




f,




102




g


in a like manner.




Referring now to

FIGS. 3 and 4

, the magnetic coil construction of the present invention provides selected coils


102


with external reinforcement winding


108


. In a reinforced coil


102


, the conductor and the reinforcement wire are first wound in sequence and then epoxy impregnated together in a common epoxy impregnation and cure process. The result is a composite structure that is continuous in the bonding matrix material (i.e., the epoxy and any additional fiber introduced for insulation and reinforcement of the epoxy) even though it contains two types of windings (i.e., the superconductor and reinforcement wire). This coil configuration, referred to as having integral external reinforcement, achieves the primary objectives of radial and axial mechanical support of the conductor windings in a superior manner by having essentially the same strength at the interface between coil


102


and reinforcement


108


as within the two.




The process for preparing reinforced coils


102


preferably begins during an intermediate stage of winding when the conductor is still ductile and not as susceptible to damage (e.g., prior to heat treating the Nb


3


Sn conductor). Reinforcement


108


in the form of a wire is then wound directly over the conductor in a process that is essentially the same as the process for winding coil


102


. In this embodiment of the invention, the wound coil


102


and reinforcement winding


108


are then placed in a furnace for heat treatment if needed to react the conductor in coil


102


to produce a superconductive material. Following heat treatment, the combined coil assembly


102


,


108


is filled with epoxy in a standard vacuum impregnation process creating a high strength bond between the epoxy, the superconductor of coil


102


, and the wire of reinforcement winding


108


.




The reinforcement winding


108


, including any insulation on the wire and between layers of wire, must be compatible with the heat treatment. In a preferred embodiment of the invention, reinforcement


108


is a winding of stainless steel wire of high strength and low magnetic permeability. An alloy such as 316, 316L, or 316 LN is suitable, for example. Stainless steel provides a suitable material for use in external reinforcement winding


108


because of its high strength and stiffness. Moreover, stainless steel maintains a high degree of strength even when subjected to the high temperatures associated with heat treatment of conductors


104


. It is also contemplated that reinforcement winding


108


uses a steel reinforcement wire including a fraction of copper. A suitable insulation for the reinforcement wire is glass fiber braid (e.g., E-glass or S-glass), which is compatible with the heat treatment and the subsequent epoxy impregnation. In a general sense, external reinforcement


108


maintains mechanical integrity and prevents wire motion in coils


102


.




It is contemplated that the wire in reinforcement winding


108


may be round or rectangular in cross section (e.g., a fraction of a millimeter to several millimeters in width) and may be applied with or without insulation. The steel wire may or may not have some fraction of copper content. If the wire has a copper fraction, however, the copper fraction is preferably relatively constant along the length of the wire. For example, a useful copper fraction is in the range of approximately 5% to approximately 25% of the total wire cross section.




In general, limiting the strain in epoxy impregnated coils, such as coils


102


, is desired to preserve epoxy bonding and mechanical integrity of the windings. Strain limitation in Nb


3


Sn coils, for example, is related to the strain dependence of the critical current. For strain limitation, high modulus in a reinforcement is a benefit. Since a rather large amount of reinforcement


108


is desired for coils


102


, the 900 MHz magnet


100


preferably uses steel reinforcement overbanding. Any amount of steel used in a high uniformity magnet raises questions about magnetic materials effects on uniformity. In this embodiment, a preferred maximum permeability criterion for magnet


100


is, for example, 1.02.




Although wax is widely used for impregnation in NMR magnets, wax has significant limitations in coils of increasing stress, such as those in a wide bore, high field magnet. As the size and stress levels in a magnet increase, wax is not satisfactory. There is also a relation between the manner of reinforcement and the impregnant. In a coil of high strength conductor, the design might allow each turn individually to carry a large stress. When the conductor is relatively weak or brittle, however, external reinforcement is often used to support the relatively large axial forces on the coil. With respect to magnet


100


, shear at the interface between the conductor and reinforcement wire windings transfers the stress on coil


102


into external reinforcement


108


. Epoxy provides a strong impregnation material to accommodate stress transfer in magnet


100


. In fact, the epoxy impregnation of the conductor windings in coil


102


, the epoxy impregnation of the stainless steel/copper reinforcement overbanding


108


, and the epoxy bond of the interface between the two are important to ensuring a sound mechanical structure of each reinforced coil assembly


102


,


108


.




Advantageously, the external reinforcements


108


according to the invention provide good mechanical integrity in the axial as well as in the radial direction to sustain the mechanical load on coils


102


. Ensuring that reinforcement


108


is well filled and bonded to the epoxy permits treating the reinforcement winding mechanically in a manner similar to the conductor windings.




When two windings are in proximity, such as coil


102


and reinforcement winding


108


, a mutual magnetic coupling exists between the windings. As a result of this coupling, when one of the windings is energized with a changing current, the resultant field induces voltages and, if continuous, induces currents in the other winding. As such, if a reinforcement is wound on a conductor coil in a manner that the reinforcement wires are electrically shorted to themselves, the voltages induced in the reinforcement winding will cause current flow and electrical dissipation. As the size of the coil increases, these losses become increasingly unacceptable. As a result, the reinforcement


108


on large coils such as coils


102


is preferably treated like the conductor and wound in a manner so that the turns are electrically insulated from one another. This is possible in the present invention by using a glass fiber insulation on the reinforcement wires of reinforcement


108


, which is compatible with the high temperature heat treatment. In this instance, reinforcement winding


108


is preferably terminated in electrical leads connected together through a diode. The diode may be connected to the superconducting coil


102


and operate at the reduced temperature of the coil. For example, a cryogenic grade high current press pack diode is suitable for cold service.




Integral external reinforcement of coils


102


as described herein provides several advantages over the prior art. For example, reinforcement


108


is wound directly over conductor coil


102


prior to heat treatment and epoxy impregnation. At this stage, the conductor is still in its ductile form, which eliminates the risk associated with directly winding an external reinforcement on a brittle, heat treated conductor. In other words, integral reinforcement


108


eliminates the need to apply reinforcement in a second operation, and provides the full shear strength of the impregnated windings


102


. Also, there is only one setup of each coil


102


in the winding process, as opposed to two windings if an external reinforcement is applied over a finished coil. Integral external reinforcement provides yet another important benefit in that a high quality epoxy composite is achieved throughout coil


102


and reinforcement winding


108


with high strength at the interface between the two materials. In this embodiment of the invention, reinforcement


108


is subject to the annealing and softening of the heat treatment. It is counter-intuitive to anneal a strengthening material in this manner, which helps explain why conventional practice has taught away from integral external reinforcement. Advantageously, the amount of anneal softening that occurs during the heat treatment leaves reinforcement


108


with sufficient strength to meet the design parameters of magnet


100


. The fiber insulation on the wire used in reinforcement winding


108


results in material properties in the reinforcement region being similar to that of the conductor regions.




As is well known in the art, superconducting coils


102


may be subject to quench, a malfunction the result of which is the sudden and rapid discharge of the quenched coil. As a secondary result of this discharge, there is the potential for a large induced voltage in the reinforcement windings


108


. Shorting the lead wires of each reinforcement winding


108


together will eliminate this voltage by allowing current flow in reinforcement winding


108


during the quench. This configuration, however, also allows current flow in reinforcement


108


during the charging of coil


102


, resulting in unacceptable energy losses. Magnet


100


provides a solution to this problem by including a diode across the leads associated with each reinforcement winding


108


. During charging of the coils


102


, the diodes prevent currents in reinforcement windings


108


and eliminate the resultant energy loss. In the event of a quench, the voltage exceeds the diode threshold and the respective diode conducts, eliminating the potentially high voltage.




In addition, when one of the coils


102


quenches, the dissipation of energy stored in magnet


100


warms the respective conductor


104


. Since the thermal conductivity to reinforcement


108


is generally limited, reinforcement


108


tends to stay cooler than conductor


104


. In other words, the natural thermal diffusion into reinforcement winding


108


is generally insufficient to adequately reduce the temperature difference between conductor


104


and reinforcement


108


. The temperature increase in the respective conductor


104


causes a thermal expansion in both diameter and length. The expansion in turn results in a shear stress between the conductor of coil


102


and its reinforcement


108


, particularly for long coils


102


. One preferred embodiment of the present invention provides a relatively small fraction of copper in addition to the steel wire in reinforcement winding


108


. Advantageously, the copper provides a mechanism for warming reinforcement


108


and, thus, helps eliminate the source of thermal stress in the quenched coil


102


. It is to be understood that the wire forming each reinforcement winding


108


may be generally round or rectangular in cross section. For example, such wire may have a stainless steel core covered by a copper jacket and glass fiber braid insulation as shown in

FIG. 4

or have a copper core covered by a stainless steel jacket and glass fiber braid insulation.




Those skilled in the art recognize that transferring energy from a winding to an electrical secondary may be used to limit the amount of energy that needs to be dissipated in the winding. In this instance, however, the energy being transferred is not intended for cooling coil


102


but for warming the secondary, i.e., reinforcement winding


108


. The amount of energy transferred is relatively small and provides little cooling of the windings. Referring now to the reinforcement windings


108


of magnet


100


, the time constant must be sufficiently long for transferring inductive energy from conductor


104


into reinforcement


108


. The time constant associated with a pure steel reinforcement winding is relatively short to the extent that little energy is transferred even when the diode conducts and current flows in the secondary circuit formed by reinforcement


108


. Thus, one preferred embodiment of the invention employs a reinforcement wire having a small fraction of copper in addition to steel. Such reinforcement wire has a greater conductivity than stainless steel alone, which increases the time constant of the secondary winding formed by reinforcement


108


. Preferably, the amount of copper in reinforcement


108


is small enough to keep from unduly weakening reinforcement


108


.




Referring further to quench conditions in superconducting magnets, spreading the quench from a local region of a coil throughout the entire coil provides a much greater region for energy to dissipate as heat and, thus, decreases the energy density in the local region. This greatly reduces the potential for overheating and is the basic purpose and function of internal quench protection systems for magnets. The present invention involves the active protection circuit


112


for protecting large multi-coil magnets, such as magnet


100


. Protection circuit


112


preferably includes a network of heater elements


114


to cause a global quench in magnet


100


if a quench occurs in any single coil


102


. Preferably, the individual heater elements


114


are distributed about each coil


102


and among a number of separate coils


102


and are attached in thermal contact with the coils


102


. In this configuration, heater elements


114


can spread a quench more quickly than the natural process of thermal conduction.




In a preferred embodiment, an active quench detector


116


monitors voltages across coils


102


via a series of voltage taps


118


to identify when a quench condition begins in any one of the monitored coils


102


. Upon identification of a quench condition, an external power source


120


responsive to the quench detector circuit


116


drives a protection switch


122


for enabling the network of heaters


114


. The protection switch


122


, connected in parallel with the heater network, causes the stored energy of magnet


100


itself to power heater elements


114


. In this manner, heaters


114


distribute and dissipate the stored energy over all of the coils


102


. The majority of the main magnet current flows in the heater network during the forced global quench, delivering as much as 35 kW, for example, at full current.




The heaters


114


preferably reside on an outside surface of coils


102


. On the reinforced coil assemblies, heaters


114


are preferably positioned between coil


102


and reinforcement


108


. The performance of the protection system


112


relies on achieving low activation times for normalization of protection switch


122


and initiation of the global quench. Those skilled in the art will recognize that, on most coils


102


, placing heaters


114


under the reinforcement windings


108


shields the heaters


114


from the cooling influence of the superfluid helium, as is generally true for the outside surface of coils


102


themselves.




An important feature of heaters


114


is that they are in good thermal contact with coils


102


. This permits quench protection system


112


of the present invention to operate very quickly to prevent quench conditions from damaging the magnet coils


102


. In general, if heaters


114


are applied to coils


102


in close proximity to the conductor windings before the epoxy impregnation process, they are more likely to be in better thermal contact with the conductor windings. It is to be understood, however, that heaters


114


may be applied to coils


102


before or after the epoxy impregnation process without deviating from the scope of the invention.




As is well known in the art, high mechanical stress in the windings of a superconducting coil can lead, indirectly, to a quench. Whenever there is an input of heat in a local region of a coil such that the temperature is raised sufficiently, characterized by the critical temperature of the superconductor at the operating conditions, a coil is likely to quench. One source of heat is localized cracking of the epoxy encapsulant, which is accompanied by stress relief and energy release. Heater element


114


, epoxied into or onto coil


102


, represents a local feature that can be associated with increased stress. Absent the improvements described below, the presence of heater


114


may cause epoxy cracking and become the source of a quench. One possible configuration for heater element


114


is a flat strip of normal, non-superconducting, metal having a relatively high resistivity. The strip may be applied to the coil before or after epoxy impregnation. Included in an appropriate circuit, the ohmic loss in the strip provides the heat to cause the spread of quench in the coil. Unfortunately, the combination of thermal contraction from cool-down and displacement during operation of such strip is accompanied by high stress and the potential for epoxy cracking at the heater element.




Referring now to

FIGS. 6A and 6B

and

FIGS. 7A and 7B

, a preferred embodiment of the invention employs a flat metallic braid as heater element


114


to reduce the likelihood of epoxy cracking. The metallic braid heater element


114


behaves electrically as a resistive element to produce heat and mechanically in a manner to limit the stress about the heater in coil


102


.




Since it is relatively thin and flat, heater element


114


promotes the transfer of heat to the conductor windings of coil


102


and is compatible with other design features, such as the ability to be placed between coil


102


and reinforcement


108


. Preferably, heater element


114


is a braid of ductile, resistive metal or alloy. Advantageously, a braid construction is significantly more compliant than a uniform strip, even when it is impregnated with epoxy as part of the coil construction. Thus, heater


114


according to the present invention serves to greatly decrease the stress at the heater during the operation of the superconducting coil. For example, heater element


114


is a flat braid of fine stainless steel wires about 1 cm wide and about 0.1 mm thick. The width of the braid may vary from a few millimeters to a few centimeters and its thickness may be several times thicker than 0.1 mm. A rolling operation may be used to substantially reduce the thickness of such a braid. In a preferred embodiments, layers of glass cloth insulate the braid to electrically isolate heater element


114


from the windings of coil


102


. The glass cloth fills with epoxy during the impregnation and forms an epoxy-glass insulator layer between heater element


114


and coil


102


.




As shown in

FIGS. 6A and 6B

and

FIGS. 7A and 7B

, protection circuit heater element


114


preferably includes electrical connectors


124


attached to its ends for facilitating the connection to the electrical circuit provided for quench protection. In an alternative embodiment, external wires connect directly to the braid. The ends of heater element


114


also extend away from the body of coil


102


to allow easy attachment of external wires to the electrical connectors.

FIGS. 6A and 6B

illustrate one embodiment in which heater element


114


is a generally straight section of braid, extending from one end of coil


102


axially to the other, with the ends of element


114


extending in both directions past the length of coil


102


to facilitate electrical connection at the ends of heater element


114


. Alternatively, the heater element is generally U-shaped, having a hairpin bend as shown in

FIGS. 7A and 7B

, or another shape that results in both ends of heater element


114


being at one end of coil


102


.




Due to the brittle nature of heat treated Nb


3


Sn coils, there is some advantage to applying heater elements


114


to coils


102


prior to heat treatment. In this instance, the potential to damage the superconducting windings during application of heater element


114


after heat treatment and before epoxy impregnation is greatly reduced. Heater element


114


preferably comprises a flat braid of a resistive, high temperature metal or alloy, applied without any organic based insulations that would be subject to decomposition during heat treatment. As such, heater element


114


is capable of sustaining the high temperatures during the heat treating process and meets the needs of Nb3Sn wind and react coil technology.




Although described above with respect to coils


102


, it is to be understood that heater elements


114


may also be applied to compensation coils


104


. A protection diode preferably bridges compensation coils


104


to prevent asymmetric quench.




Referring now to

FIGS. 8-10

, the present invention provides a system for fabricating and supporting a lead wire


126


of a superconducting coil, such as any one of coils


102


,


104


. For simplicity, the lead


126


will be discussed with respect to a single coil


102


, although it is to be understood that the invention is applicable to any of the coils


102


,


104


or other winding configuration. Those skilled in the art recognize that superconducting coils


102


,


104


each have leads


126


formed during fabrication of the coils through which the coils are electrically energized.




The lead wire


126


preferably extends through a hole or opening


128


in an end flange


130


. In the illustrated embodiment, the end flange


130


is part of a coil form


132


on which the conductor is wound to form coil


102


. The present invention encompasses application to the brittle superconductors that are placed into and held in a fixed position during coil winding by means of some structure for lead support during fabrication. In this instance, a copper stabilizing member, or stabilizer,


136


constitutes a lead support structure providing mechanical support and positioning of lead wire


126


prior to heat treatment of the conductor. The stabilizer


136


preferably has a channel


140


therethrough in which lead wire


126


is positioned. A cover strip


142


holds lead


126


in the channel


140


of stabilizer


136


. Preferably, the hole


128


in end flange


130


is large enough to accommodate an epoxy lead cone


144


that is eventually formed in that space.




During winding of coil


102


, and for subsequent processing, additional support for lead


126


immediately as it exits the windings may be provided in the form of curved shoe pieces (not shown) that are positioned in the lead exit hole


128


and held by end flange


130


. The shoe pieces help maintain the position of stabilizer


136


. In placing the wire into lead exit hole


128


, the lead wire


126


is bent to a curvature for matching the size of hole


128


and the position of the lead supporting structure of the shoe pieces and stabilizer


136


. Since lower field superconductors such as NbTi are ductile and do not require a heat treatment, the lead supporting structure helps position the conductor at the lead exit during winding but otherwise may be omitted.




During the heat treatment, the conductor is held in a fixed position by the support structure, including copper stabilizer


136


, into which it was positioned. After heat treatment, without moving the conductor, lead wire


126


is preferably soldered into the copper channel


140


. At this time, the shoes, which helped to position the conductor just at the point of leaving the windings, are removed without disturbing the position of the conductor. Removing the shoes leaves only lead wire


126


and one end of stabilizer


136


within hole


128


in end flange


130


.




Without disturbing lead


126


, an epoxy cone mold


146


is preferably positioned within lead exit hole


128


about lead wire


126


. The mold


146


form a boundary of a region about the lead


126


. In a preferred embodiment of the invention, this region defines a generally conical support structure, or lead cone assembly


144


, when mold


146


is filled with epoxy (and filler material). Prior to epoxy impregnation, mold


146


is preferably filled with a material such a glass fiber, quartz fiber, alumina, or possibly other materials that are commonly used to make filled epoxy composites. The end of the stabilizer


136


extends into the conical region defined by mold


146


and is surrounded by the filler material. After filling, the top of the conical region is defined by a cover plate (not shown). In one embodiment, mold


146


is aluminum. Treating mold


146


with an epoxy release agent will facilitate its removal following the impregnation process. It is to be understood that the term “conical” as used herein is intended to include other shapes without deviating from the scope of the present invention (e.g., lead cone assembly


144


may be truncated, or generally frustoconical).




During the vacuum impregnation process, the void and fiber region within the windings is filled with epoxy. At the same time, the filled region of mold


146


surrounding lead


126


is filled with epoxy. After the epoxy is cured, the excess epoxy about the body of coil


102


may be removed. Removing mold


146


reveals the conical-shaped filled epoxy structure, i.e., lead cone assembly


144


, about lead


126


. Since it is filled with epoxy and cured along with the windings, the resulting lead cone


144


is integrally formed with coil


102


making issentially an extension of the windings. Lead cone


144


surrounds, encapsulates and supports the lead wire


126


. Advantageously, lead cone


144


also encapsulates and holds the end of copper stabilizer


136


to protect the point at which lead


126


enters and is soldered to the stabilizer channel


140


.




The present invention applies to coils that are epoxy impregnated, such as by a vacuum impregnation process, but use with a wet layup epoxy process is also contemplated.




Referring now to

FIG. 10

, the design of mold


146


preferably leaves a region of clearance between epoxy cone


144


and the inside of the end flange hole


128


. This space allows the windings of coil


102


to move relative to the end flange


130


of coil form


132


without cone


144


coming into contact with end flange


130


.





FIG. 11

illustrates exemplary stress data for lead cone assembly


144


. The computed material properties of cone


144


with an alumina powder filler show increased stiffness and increased differential thermal contraction in comparison with an E-glass fiber filler. As a consequence, maximum thermal stress is found to be significantly higher with the alumina filler in a comparison with 50% filler fraction.




Persistent joints are positioned in relatively low field at the ends of the lead support structures. The joints include splice joints within coils and termination joints at the start and finish of coils. Nb


3


Sn splice joints are over metallurgy technology. All other joints, including Nb


3


Sn—NbTi and NbTi—NbTi joints are superconducting solder technology. Bucking coils are preferably employed to decrease the field at the joints. The bucking coils are especially useful on the Nb


3


Sn—NbTi joints. The coils will be persistent, wound of single core conductor, with persistent joint and switches. Individual coils are connected through NbTi leads and an intermediate NbTi—NbTi joint. The interconnection lead must be flexible t the extent required by relative coil motions, and must be stable.




The magnet


100


also employs two persistent switches, i.e., a main switch and a protection switch. In one embodiment, the switches contain NbTi/CuNi matrix conductor in a seven strand cable. The switches are bifilar wound and epoxy impregnated. The main switch is situated in the 4 degrees K container due to the heat load and helium consumption during ramping. The protection switch is in parallel with the protection heater network and capable of rapid turn on. When the protection switch is normal, during the operation of the heaters, it experiences heating as a parallel resistor, and must be designed accordingly.




Protection of epoxy impregnated magnets requires careful design and analysis of all factors that affect the winding temperature rise before it reaches quench temperature. Among these factors is the AC loss due to current and field change as a result of the current transfer between coils after the protection diodes voltages exceed their critical values.




Protection of large energy stored epoxy impregnated magnets requires using diodes across many sections of magnet


100


system to allow for inductive current transfer from sections with normal zones to the other superconducting sections. As a result, the current decays in one section and increases in the other sections leaving the total field almost unchanged at the beginning of a quench. As a result, the transverse field loss is very small at that time; however in the circuit where the normal zone exists, the self-field losses can contribute to the acceleration of the normal zone propagation and it is expected that the coils in that circuit to normalize faster than other circuits.




Magnetic field uniformity is critical to NMR. Ferromagnetic welds cause field in homogeneity. Historically, magnet designs have avoided ferrous structural alloys to prevent potential field distortions from welds. This strategy is problematic in fabricating high field magnets because austenitic stainless steel is the preferred heat treatment material for bore tubes in niobium-tin coils. Early high field NMR designs employed the removal of the bore tubes after heat treatment and epoxy impregnation. Bore tube removal is dangerous due to the risk of damaging the reacted NbTi conductor and leads. A more practicable fabrication approach is to leave the stainless steel bore tubes in place. The weld metal on the coil form must then have a low permeability to avoid distorting magnetic fields. Low permeability is accomplished by producing zero ferrite welds. This involves the selection of base metals and welding alloys, the welding process, and supporting magnetic permeability measurement results.




A Nb


3


Sn coil requires a form that will support and geometrically define its windings during heat treatment. Previous NMR coil constructions have employed the removal of the bore tubes after heat treatment and epoxy impregnation. The strategy was to avoid the potential field distortion issues by removing all suspect material. Bore tube removal after heat treatment is dangerous due to the risk of damaging the Nb


3


Sn conductor and insulation. The risk and potential for breakage increases with larger more massive coil assemblies. A more practicable fabrication approach, in large magnets, is to leave the stainless steel bore tubes in place.




Preferably, the coil form steel is low in permeability to avoid large magnetic field distortions. As an example, the permeability limit for the 900 MHz magnet


100


of the present invention is μ/μ


0


=1.020. Coil form welds must also meet this permeability limit as their spatial distribution is typically quite asymmetric in a magnet.




In view of the above, it will be seen that the several objects of the invention are achieved and other advantageous results attained.




As various changes could be made in the above constructions and methods without departing from the scope of the invention, it is intended that all matter contained in the above description and shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.



Claims
  • 1. A method of manufacturing a superconducting magnet comprising:winding a plurality of superconducting coils including winding at least one coil of wind and react conductor; externally reinforcing the wind and react coil; heat treating, after externally reinforcing, the wind and react coil to react the wind and react conductor; impregnating, after heat treating, the coils with epoxy; nesting the coils within each other, an innermost one of the nested coils having a bore therethrough defining a bore width of the magnet, said bore width being greater than approximately 100 millimeters; electrically connecting the nested coils in series; cooling the nested coils to an operating temperature less than approximately 4 degrees K; and supplying power to the nested coils for charging the magnet.
  • 2. A method of manufacturing a superconducting magnet comprising:winding a plurality of superconducting coils; externally reinforcing at least one of the coils; impregnating, after externally reinforcing, the coils with epoxy; nesting the coils within each other, an innermost one of the nested coils having a bore therethrough defining a bore width of the magnet, said bore width being greater than approximately 100 millimeters; electrically connecting the nested coils in series; cooling the nested coils to an operating temperature less than approximately 4 degrees K; and supplying power to the nested coils for charging the magnet.
  • 3. The method of claim 2 wherein the reinforcing step includes winding a reinforcement wire around the at least one of the coils to be externally reinforced.
  • 4. The method of claim 3 wherein the reinforcement wire is electrically insulated with a high temperature insulation.
  • 5. The method of claim 4 wherein the high temperature insulation is a glass fiber braid.
  • 6. The method of claim 3 wherein the reinforcement wire is electrically insulated and wherein the step of winding the reinforcement wire includes preventing electrical short circuits of the reinforcement wire to itself.
  • 7. The method of claim 3 wherein the reinforcement wire is steel.
  • 8. The method of claim 3 wherein the reinforcement wire includes steel and copper.
  • 9. The method of claim 3 wherein the reinforcement wire wound on the at least one of the coils to be externally reinforced defines an external reinforcement winding, said external reinforcement winding having a pair of leads extending therefrom, and further comprising the step of connecting the leads of the external reinforcement winding with a diode.
  • 10. A method of manufacturing a superconducting magnet comprising:winding a plurality of superconducting coils; protecting at least one of the coils with a heater element for heating the protected at least one of the coils in response to a quench in the magnet, said heater element comprising a substantially flat metallic braid; impregnating the coils with epoxy; nesting the coils within each other, an innermost one of the nested coils having a bore therethrough defining a bore width of the magnet, said bore width being greater than approximately 100 millimeters; electrically connecting the nested coils in series; cooling the nested coils to an operating temperature less than approximately 4 degrees K; and supplying power to the nested coils for charging the magnet.
  • 11. The method of claim 10 wherein the braid comprises a resistive metal.
  • 12. The method of claim 10 further comprising rolling the braid to lessen its thickness.
  • 13. The method of claim 10 wherein the braid is generally U-shaped.
  • 14. A method of manufacturing a superconducting magnet comprising:winding a plurality of superconducting coils; protecting at least one of the coils with a heater element for heating the protected at least one of the coils in response to a quench in the magnet, said protecting including positioning the heater element in thermal contact with the protected at least one of the coils; impregnating, after positioning the heater element, the coils with epoxy; nesting the coils within each other, an innermost one of the nested coils having a bore therethrough defining a bore width of the magnet, said bore width being greater than approximately 100 millimeters; electrically connecting the nested coils in series; cooling the nested coils to an operating temperature less than approximately 4 degrees K; and supplying power to the nested coils for charging the magnet.
  • 15. A method of manufacturing a superconducting magnet comprising:winding a plurality of superconducting coils, said winding the superconducting coils including winding one or more coils of wind and react conductor; heat treating the one or more wind and react coils to react the wind and react conductor; protecting at least one of the coils with a heater element for heating the protected at least one of the coils in response to a quench in the magnet, said protecting positioning the heater element in thermal contact with the protected at least one of the coils; impregnating, after heat treating and positioning the heater element, the coils with epoxy; nesting the coils within each other, an innermost one of the nested coils having a bore therethrough defining a bore width of the magnet, said bore width being greater than approximately 100 millimeters; electrically connecting the nested coils in series; cooling the nested coils to an operating temperature less than approximately 4 degrees K; and supplying power to the nested coils for charging the magnet.
  • 16. A method of manufacturing a superconducting magnet comprising:winding a plurality of superconducting coils; supporting, with epoxy, one or more lead wires extending from the superconducting coils, said supporting includes placing a mold around the one or more of the lead wires adjacent an end of the superconducting coils and filling the mold with a filler material, said mold defining a generally frustoconical region surrounding at least a portion of the one or more of the lead wires; impregnating, after filling the mold, the coils with epoxy; nesting the coils within each other, an innermost one of the nested coils having a bore therethrough defining a bore width of the magnet, said bore width being greater than approximately 100 millimeters; electrically connecting the nested coils in series; cooling the nested coils to an operating temperature less than approximately 4 degrees K; and supplying power to the nested coils for charging the magnet.
  • 17. The method of claim 16 further comprising the step of securing a portion of the one or more of the lead wires within a stabilizing member, at least a portion of said stabilizing member being adapted to extend into the mold.
  • 18. A method of manufacturing a superconducting magnet comprising the steps of:winding a plurality of superconducting coils; externally reinforcing at least one of the coils; impregnating the coils with epoxy following the reinforcing step; nesting the coils within each other; electrically connecting the nested coils in series; cooling the nested coils to an operating temperature less than approximately 4 degrees K; and supplying power to the nested coils for charging the magnet.
  • 19. The method of claim 18 wherein the step of winding the superconducting coils includes winding one or more coils of wind and react conductor and heat treating the one or more wind and react coils to react the wind and react conductor following the reinforcing step and prior to the impregnating step.
  • 20. The method of claim 18 wherein the reinforcing step includes winding a reinforcement wire around the at least one of the coils to be externally reinforced.
  • 21. The method of claim 20 wherein the reinforcement wire is electrically insulated with a high temperature insulation.
  • 22. The method of claim 21 wherein the high temperature insulation is a glass fiber braid.
  • 23. The method of claim 20 wherein the reinforcement wire is electrically insulated and wherein the step of winding the reinforcement wire includes preventing electrical short circuits of the reinforcement wire to itself.
  • 24. The method of claim 20 wherein the reinforcement wire is steel.
  • 25. The method of claim 20 wherein the reinforcement wire includes steel and copper.
  • 26. The method of claim 20 wherein the reinforcement wire wound on the at least one of the coils to be reinforced defines an external reinforcement winding, said external reinforcement winding having a pair of leads extending therefrom, and further comprising the step of connecting the leads of the external reinforcement winding with a diode.
  • 27. A method of manufacturing a superconducting magnet comprising the steps of:winding a plurality of superconducting coils; positioning a heater element in thermal contact with one or more of the coils for heating the coils in response to a quench in the magnet; impregnating the coils with epoxy following the step of positioning the heater element; nesting the coils within each other; electrically connecting the nested coils in series; cooling the nested coils to an operating temperature less than approximately 4 degrees K; and supplying power to the nested coils for charging the magnet.
  • 28. The method of claim 27 wherein the heater element comprises a substantially flat metallic braid.
  • 29. The method of claim 28 wherein the braid comprises a resistive metal.
  • 30. The method of claim 28 further comprising rolling the braid to lessen its thickness.
  • 31. The method of claim 28 wherein the braid is generally U-shaped.
  • 32. The method of claim 27 wherein the step of winding the superconducting coils includes winding one or more coils of wind and react conductor and heat treating the one or more wind and react coils to react the wind and react conductor following the step of positioning the heater element and prior to the impregnating step.
CROSS-REFERENCE TO RELATED APPLICATION

This application claims the benefit of commonly assigned Provisional Application Serial No. 60/156,081, filed Sep. 24, 1999, the entire disclosure of which is incorporated herein by reference.

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT

This invention was made with Government support under Cooperative Agreement Nos. DMR-9016241 and/or DMR-9527035 awarded by the National Science Foundation. The Government has certain rights in this invention.

US Referenced Citations (15)
Number Name Date Kind
4500860 Vermilyea Feb 1985 A
4744506 Thornton May 1988 A
4808954 Ito Feb 1989 A
4895831 Laskaris Jan 1990 A
5581220 Rodenbush et al. Dec 1996 A
5606300 Koyama et al. Feb 1997 A
5689223 Demarmels et al. Nov 1997 A
5690991 Xu et al. Nov 1997 A
5721522 Roth et al. Feb 1998 A
5739689 Roth et al. Apr 1998 A
5872500 Gore Feb 1999 A
5884489 Retz et al. Mar 1999 A
5900792 Havens et al. May 1999 A
5917393 Kupiszewski et al. Jun 1999 A
6081987 Kalsi et al. Jul 2000 A
Non-Patent Literature Citations (12)
Entry
Eyssa, Markiewicz, “Quench Simulation and Thermal Diffusion in Epoxy-Impregnated Magnet System,” 5 IEEE Trans. Applied Superconductivity, No. 2, 487-90 (1995).
Markiewicz, Dixon, Eyssa, Schwartz, Swenson, Van Sciver, Schneider-Muntau, “25 T High Resolution NMR Magnet Program and Technology,” 32 IEEE Trans. Magnetics, No. 4, 2586-89 (1996).
Markiewicz, Bonney, Dixon, Eyssa, Swenson, Schneider-Muntau, “Technology of 1 Ghz NMR superconducting magnets,” 216 Physica B, 200-02 (1996).
Swenson, Dixon, Markiewicz, “Measurement of Thermal Contraction Properties for NbTi and Nb3Sn Composites,” 7 IEEE Trans. Applied Superconductivity, No. 2, 408-11 (1997).
Swenson, Markiewicz, “Development of Quench Protection Heaters for Superconducting Solenoids,” 7 IEEE Trans. Applied Superconductivity, No. 2, 402-03 (1997).
Dixon, Walsh, Markiewicz, Swenson, “Mechanical Properties of Epoxy Impregnated Superconducting Solenoids,”32 IEEE Trans. Magnetics, No. 4, 2917-20 (1996).
Swenson, Eyssa, Markiewicz, “Quench Protection Heater Design for Superconducting Solenoids,” 32 IEEE Trans. Magnetics, No. 4, 2659-62 (1996).
Eyssa, Markiewicz, Miller, “Quench , Thermal, and Magnetic Analysis Computer Code for Superconducting Solenoids,” 7 IEEE Trans. Applied Superconductivity, No. 2, 159-62 (1997).
Markiewicz, “1 Ghz NMR spectroscopy: innovation in magnet technology,” 9 Solid State Nuclear Magnetic Resonance, 73-76 (1997).
Markiewicz, Dixon, Eyssa, Schwartz, Swenson, Schneider-Muntau, “The Evolution of Adiabatically Stable Magnet Technology for High Field Nuclear Magnetic Resonance,” High Magnetic Fields: Application, Generation, Materials, World Scientific, River Edge, NJ, 287-295 (1997).
Dixon, Markiewicz, Pickard, Swenson, “Critical Current and n-Value of Nb3Sn Conductors for the Wide Bore 900 MHZ NMR Magnet,” 9 IEEE Trans. Applied Superconductivity, No. 2, 2513-16 (1999).
Eyssa, Markiewicz, Swenson, “Quench Heater Simulation for Protection of Superconducting Coils,” 9 IEEE Trans. Applied Superconductivity, No. 2, 1117-20 (1999).
Provisional Applications (1)
Number Date Country
60/156081 Sep 1999 US