BACKGROUND OF THE INVENTION
The present invention relates generally to a super-conductive coil in a
synchronous rotating machine. The present invention in particular relates to a
support structure for super-conducting field windings in the rotor of a
synchronous machine. More particularly, the present invention relates to a rotor
in a synchronous machine.
Synchronous electrical machines having field coil windings include, but are not
limited to, rotary motors, and linear motors. These machines generally comprise
a stator and rotor that are electromagnetically coupled. The rotor may include a
multi-pole rotor core and one or more coil windings mounted on the rotor core.
The rotor cores may include a magnetically-permeable solid material, such as an
iron-core rotor.
Conventionally copper windings are commonly used in the rotors of synchronous
electrical machine. However, the electrical resistance of copper windings
(although low by conventional measurement) is sufficient to contribute to
substantial heating of the rotor and to diminish the power efficiency of the
machine. Recently, super-conducting (SC) coil windings have been developed for
motors. SC windings have effectively no resistance and are highly advantageous
rotor coil windings.
Iron-core rotors saturate at an air-gap magnetic field strength of about 2 Tesla.
Known super-conductive rotors employ air-core designs, with no iron in the
rotor, to achieve air-gap magnetic fields of 3 Tesla or higher. These high-air-gap
magnetic fields increased power densities of the electrical machine, and result in
significant reduction in weight and size of the machine. Air-core super-conductive
rotors require large amounts of super-conducting wire. The large amounts of SC
wire add to the number of coils required, the complexity of the coil supports, and
the cost of the SC coil windings and rotor.

High temperature SC coil field windings are formed of super-conducting materials
that are brittle, and must be cooled to a temperature at or below a critical temperature,
e.g., 27°K, to achieve and maintain super-conductivity. The SC windings may be
formed of a high temperature super-conducting material, such as a BSCCO
(BixSrxCaxCuxOx) based conductor.
Super-conducting coils have been cooled by liquid helium. After passing through the
windings of the rotor, the hot, used helium is returned as room-temperature gaseous
helium. Using liquid helium for cryogenic cooling requires continuous reliquefaction
of the returned, room-temperature gaseous helium, and such reliquefaction poses
significant reliability problems and requires significant auxiliary power.
Prior SC coil cooling techniques include cooling an epoxy-impregnated SC coil
through a solid conduction path from a cryocooler. Alternatively, cooling tubes in the
rotor may convey a liquid and/or gaseous cryogen to a porous SC coil winding that is
immersed in the flow of the liquid and/or gaseous cryogen. However, immersion
cooling requires the entire field winding and rotor structure to be at cryogenic
temperature. As a result, no iron can be used in the rotor magnetic circuit because of
the brittle nature of iron at cryogenic temperatures.
What is needed is a super-conducting field winding assemblage for an electrical
machine that does not have the disadvantages of the air-core and liquid-cooled super-
conducting field winding assemblages of, for example, known super-conductive
rotors.
In addition, high temperature super-conducting (HTS) coils are sensitive to
degradation from high bending and tensile strains. These coils must undergo
substantial centrifugal and other acceleration forces that stress and strain the coil
windings. Normal operation of electrical machines involves thousands of start-up and
shut-down cycles over the course of several years that result in low cycle fatigue
loading of the rotor, and apply bending moments that strain the rotor coil.
Furthermore, the HTS rotor coil winding should be capable of withstanding 25%
over-speed operation during rotor balancing procedures at ambient temperature, and

notwithstanding occasional over-speed conditions at cryogenic temperatures during
power generation operation. These over-speed conditions substantially increase the
centrifugal force loading on the windings over normal operating conditions.
SC coils used as the HTS rotor field winding of an electrical machine are subjected to
stresses and strains during cool-down and normal operation. They are subjected to
centrifugal loading, bending moments, torque transmission, and transient fault
conditions. To withstand the forces, stresses, strains and cyclical loading, the SC
coils should be properly supported in the rotor by a coil support system. These
support systems hold the SC coil(s) in the HTS rotor and secure the coils against the
tremendous centrifugal and other acceleration forces due to the rotation of the rotor.
Moreover, the coil support system protects the SC coils, and ensures that the coils do
not prematurely crack, fatigue or otherwise break.
A challenge to the development of a high temperature super-conducting (HTS)
electric machine is maintaining the structural integrity of the super-conducting field
coil. Due to the brittle coil, the critical current of a BSCCO based coil is sensitive to
the level of mechanical strain in the coil. Accordingly, the mechanical strain into the
SC coil should be minimized to maintain the optimal level of critical current.
A robust coil support is needed to minimize the mechanical strain in the SC coil for a
rotor of a synchronous machine. By minimizing the coil strain, the coil support
ensures that the coil retains its critical current capability. In addition to minimizing
coil strain, the coil support should not conduct heat from the rotor to the cryogenic
coil.
Developing support systems for HTS coil has been a difficult challenge in adapting
SC coils to HTS rotors. Examples of coil support systems for HTS rotors that have
previously been proposed are disclosed in U.S. Patents Nos. 5,548,168; 5,532,663;
5,672,921; 5,777,420; 6,169,353, and 6,066,906. However, these coil support
systems suffer various problems, such as being expensive, complex and requiring an
excessive number of components. There is a long-felt need for a HTS rotor having a

coil support system for a SC coil. The need also exists for a coil support system made
with low cost and easy-to-fabricate components.
BRIEF SUMMARY OF THE INVENTION
A coil support has been developed that has a split clamp that grasps the ends of a
race-track SC coil. The clamp provides rigidity and stiffness to the coil, and prevents
the coil from bending during centrifugal acceleration. By stiffening the coil, the
clamp minimizes strain in the coil and thereby retains the critical current capability of
the coil.
The split clamp is a free-floating attachment to the coil, and is not secured to the rotor.
Thus, the split clamp may be held at a cryogenic cold temperature along with the coil.
The free-floating clamp is thermally isolated from hot structures such as the rotor core
and end shaft collar. The free-floating clamp does not require insulation structures to
prevent heat from the rotor from conducting through the clamp into the coil.
The HTS rotor may be for a synchronous machine originally designed to include SC
coils. Alternatively, the HTS rotor may replace a copper coil rotor in an existing
electrical machine, such as in a conventional generator. The rotor and its SC coils are
described here in the context of a generator, but the HTS coil rotor is also suitable for
use in other synchronous machines.
The coil support system, including the split clamp, is useful in integrating the coil
support system with the coil and rotor. In addition, the coil support system facilitates
easy pre-assembly of the coil support system, coil and rotor core prior to final rotor
assembly. Pre-assembly reduces coil and rotor assembly time, improves coil support
quality, and reduces coil assembly variations.
In a first embodiment, the invention is a rotor for a synchronous machine comprising:
a rotor core; a super-conducting coil winding extending around at least a portion of
the rotor core, the coil winding having a coil end section adjacent an end of the rotor
core, and a coil support bracing the end section and being thermally isolated from the
rotor core.

In a second embodiment, the invention is a method for supporting a super-conducting
coil winding on a rotor core of a synchronous machine comprising the steps of:
bracing an end section of the coil winding with an end coil support; assembling the
coil winding, end coil support and rotor core; attaching a rotor end shaft to the rotor
core; and thermally isolating the coil support from the rotor core and shaft.
In a third embodiment, the invention is a rotor for a synchronous machine comprising:
a rotor core having at least one rotor core end orthogonal to a longitudinal axis of the
rotor; at least one end shaft attached to the rotor core end; a race-track super-
conducting (SC) coil winding extending around the rotor core and having a coil end
section adjacent the rotor end; a coil support brace attached to the coil end section and
thermally isolated from the rotor core and rotor end shaft.
BRIEF DESCRIPTION OF THE ACCOMPANYING DRAWINGS
The accompanying drawings in conjunction with the text of this specification describe
an embodiment of the invention.
FIGURE 1 is a schematic side elevational view of a synchronous electrical machine
having a super-conductive rotor and a stator.
FIGURE 2 is a perspective view of an exemplary race-track super-conducting coil
winding.
FIGURE 3 is an exploded view of the components of a high temperature super-
conducting (HTS) rotor.
FIGURES 4 to 6 are perspective views showing the assembly process for the HTS
rotor shown in FIGURE 3.
DETAILED DESCRIPTION OF THE INVENTION
FIGURE 1 shows an exemplary synchronous generator machine 10 having a stator 12
and a rotor 14. The rotor includes field winding coils that fit inside the cylindrical
rotor vacuum cavity 16 of the stator. The rotor fits inside the rotor vacuum cavity of
the stator. As the rotor turns within the stator, a magnetic field 18 (illustrated by
dotted lines) generated by the rotor and rotor coils moves/rotates through the stator
and creates an electrical current in the windings of the stator coils 19. This current is
output by the generator as electrical power.
The rotor 14 has a generally longitudinally-extending axis 20 and a generally solid
rotor core 22. The solid core 22 has high magnetic permeability, and is usually made
of a ferromagnetic material, such as iron. In a low power density super-conducting
machine, the iron core of the rotor is used to reduce the magnetomotive force (MMF),
and, thus, minimize the amount of super-conducting (SC) coil wire needed for the coil
winding. For example, the solid iron rotor core may be magnetically saturated at an
air-gap magnetic field strength of about 2 Tesla.
The rotor 14 supports at least one longitudinally-extending, race-track shaped, high-
temperature super-conducting (HTS) coil winding 34 (See Fig. 2). The HTS coil
winding may be alternatively a saddle-shape or have some other shape that is suitable
for a particular HTS rotor design. A coil support system is disclosed here for a race-
track SC coil winding. The coil support system may be adapted for coil
configurations other than a race-track coil mounted on a solid rotor core.
The rotor includes a collector end shaft 24, and a drive end shaft 30, that are
supported by bearings 25. The collector end shaft includes collector rings 78 that
provide an external electrical contact to the SC coil via coil contacts 79. The collector
end shaft 24 also has a cryogen transfer coupling 26 to a source of cryogenic cooling
fluid used to cool the SC coil windings in the rotor. The cryogen transfer coupling 26
includes a stationary segment coupled to a source of cryogen cooling fluid and a
rotating segment which provides cooling fluid to the HTS coil. The drive shaft 30 of
the rotor may be driven by a power turbine via drive coupling 32.
FIGURE 2 shows an exemplary HTS race-track field coil winding 34. The SC field
winding coils 34 of the rotor includes a high temperature super-conducting (SC) coil
36. Each SC coil includes a high temperature super-conducting conductor, such as a
BSCCO (BixSrxCaxCuxOx) conductor wires laminated in a solid epoxy impregnated

winding composite. For example, a series of BSCCO 2223 wires may be laminated,
bonded together and wound into a solid epoxy impregnated coil.
SC wire is brittle and easy to be damaged. The SC coil is typically layer wound SC
tape that is epoxy impregnated. The SC tape is wrapped in a precision coil form to
attain close dimensional tolerances. The tape is wound around in a helix to form the
race-track SC coil 36.
The dimensions of the race-track coil are dependent on the dimensions of the rotor
core. Generally, each race-track SC coil encircles the magnetic poles of the rotor
core, and is parallel to the rotor axis. The coil windings are continuous around the
race-track. The SC coils form a resistance-free electrical current path around the rotor
core and between the magnetic poles of the core. The coil has electrical contacts 79
that electrically connect the coil to the collector rings 78.
Fluid passages 38 for cryogenic cooling fluid are included in the coil winding 34.
These passages may extend around an outside edge of the SC coil 36. The
passageways provide cryogenic cooling fluid to the coil and remove heat from the
coil. The cooling fluid maintains the low temperatures, e.g., 27°K, in the SC coil
winding needed to promote super-conducting conditions, including the absence of
electrical resistance in the coil. The cooling passages have an input fluid port 39 and
an output port 41 at one end of the rotor core. These fluid (gas) ports 39,, 41 connect
the cooling passages 38 on the SC coil to passages that lead to the cryogen transfer
coupling 26.
Each HTS race-track coil winding 34 has a pair of generally-straight side portions 40
parallel to a rotor axis 20, and a pair of end portions 54 that are perpendicular to the
rotor axis. The side portions of the coil are subjected to the greatest centrifugal
stresses. Accordingly, the side portions are supported by a coil support system that
counteract the centrifugal forces that act on the coil.
The end sections 54 of the coil winding are subjected to significant bending moments
as the rotor is accelerated and decelerated during operation of the machine. The end
coil sections 54 extend radially across the end 56 of the rotor. Because the end
section extends radially, the acceleration of the coil end section varies along its
length. Thus, there are bending moments applied to the coil end section during
acceleration and deceleration of the rotor. The bending moments applied to the end
section may be more pronounced than any bending moments applied to the side
section 40 of the coil.
Bending in a SC coil imparts mechanical strain to the brittle SC coil. Excessive strain
in a SC coil can degrade the capacity of the coil to handle a critical current in super-
conducting conditions. Accordingly, a coil support is needed for the end section 54 of
the coil that prevents excessive bending of and strain in the coil. A split clamp 58
(Fig. 3) is applied to the coil end section. The split clamp imparts rigidity to the coil
end section, and thereby prevents excessive bending and strain in the coil end section
54.
FIGURE 3 shows an exploded view of a rotor core 22 and coil support system for a
high temperature super-conducting coil. The coil support system includes a split
clamp 58 formed of a pair of plates 60 that sandwich the end section 54 of the coil. In
addition, the coil support system includes supports for the long side 40 of the coil.
These coil side 40 supports include tension rods 42 connected to channel housings 44.
The housings hold and support the side portions 40 of the coil winding 34 in the rotor.
While one tension rod and channel housing is shown in FIGURE 3, the coil support
system will generally include a series of tension rods that each have coil support
housings at both ends of the rod. The tension rods and channel housings prevent
damage to the coil winding during rotor operation, support the coil winding with
respect to centrifugal and other forces, and provide a protective shield for the coil
winding.
The principal loading of the HTS coil winding 34 in an iron core rotor is from
centrifugal acceleration during rotor rotation, and from the acceleration and
deceleration of rotor during shut-down and start-up. An effective coil structural
support is needed to counteract the forces that act on the coil.

The end sections 54 of the coil winding 34 are adjacent the opposite ends 56 of the
rotor core. A split-clamp 58 braces each of the coil end sections to better enable the
coil end sections to withstand bending moments. The split clamp at each coil end 54
includes a pair of opposite plates 60 between which are sandwiched the end section 54
of the coil winding 34. The surface of each clamp plate includes channels 116, 118
(Fig. 6) to receive the coil winding 34 and the cooling fluid and electrical connections
39, 41, 79 to the winding.
The split clamp 58 stiffens the end section of the coil so as to minimize the bending of
the end section. The split clamp reduces the strain in the coil by reducing the bending
of the end-section of the coil. The split clamp may be formed of aluminum, Inconel
alloys or stainless steel. The materials also have similar thermal expansion coefficient
to the super-conducting laminated BSCCO 2223 super-conducting wire. Thus, the
clamp has similar thermal expansion and contraction characteristics as does the coil.
The split plates 60 of the clamp may be bonded together with the coil end section
sandwiched between the plates. Alternatively, the plates may be assembled together
with bolts, such that a small gap for the coil remains between the plates.
The coil support system, including the split clamps, is preferably non-magnetic so as
to preserve ductility at cryogenic temperatures, since ferromagnetic materials become
brittle at temperatures below the Curie transition temperature and cannot be used as
load carrying structures.
The split clamp 58 is surrounded by, but is not in contact with, a collar 62 of the
motor end shaft 24, 30. The collar 62 of each end shaft is coupled to an end 56 of the
rotor core 22. Although only one collar is shown in Figure 3, there are normally
collars on both end shafts and attached to both ends of the core. The collar 62 is a
thick disk of non-magnetic material, such as stainless steel, the same as or similar to
the material, that forms the rotor shafts. Indeed, the collar is part of the rotor shaft
The collar has a slot 64 orthogonal to the rotor axis and sufficiently wide to receive
and clear the split clamp 58. The split clamp is separated by a vacuum from the side-
wall 66 of the collar. The hot side-walls 66 of the slot collar are spaced apart from the
cold split clamp so they do not come in contact with each other.
The collar 62 may include a recessed disk area 68 (which is bisected by the slot 64) to
receive a raised disk region 70 of the rotor core (see opposite side of rotor core for
raised disk region to be inserted in opposite collar). The insertion of the raised disk
region on the end 56 of the rotor core into the recessed disk 68 provides support to the
rotor core in the collar, and assists in aligning the rotor core and collars. In addition,
the collar may have a circular array of bolt holes 72 extending longitudinally through
the collar and around the rim of the collar. These bolt holes correspond to matching
threaded bolt holes 74 that extend partially through the rotor core. Threaded bolts
(not shown) extend through these longitudinal bolt holes 72, 74 and secure the collars
to the rotor core.
A side coil support is needed along the side sections 40 of the coil that experience the
most centrifugal acceleration. To support the side sections 40 of the coil, the tension
rods 42 span between the sections of the coil and attach to the channel housings 44
that grasp opposite side sections of the coil. The tension rods extend through conduits
46, e.g., apertures, in the rotor core so that the rods may span between side sections of
the same coil or between adjacent coils.
The conduits 46 are generally cylindrical passages in the rotor core having a straight
axis. The diameter of the conduits is substantially constant, except at their ends near
the recessed surfaces of the rotor. At their ends, the conduits may expand to a larger
diameter to accommodate a non-conducting cylindrical tube 52 that provides slidable
bearing surface and thermal isolation between the rotor core and the tension rod. The
tube is held in the core conduit by a lock-nut 84.
The axes of the conduits 46 are generally in a plane defined by the race-track coil. In
addition, the axes of the conduits are perpendicular to the side sections of the coil to
which are connected the tension rods that extends through the conduits. Moreover,
the conduits are orthogonal to and intersect the rotor axis, in the embodiment shown
here. The number of conduits and the location of the conduits will depend on the
location of the HTS coils and the number of coil housings needed to support the side
sections of the coils.

The tension rods support the coil especially well with respect to centrifugal forces as
the rods extend substantially radially between the sides of the coil winding. Each
tension rod is a shaft with continuity along the longitudinal direction of the rod and in
the plane of the race-track coil. The longitudinal continuity of the tension rods
provides lateral stiffness to the coils which provides rotor dynamics benefits.
Moreover, the lateral stiffness permits integrating the coil support with the coils so
that the coil can be assembled with the coil support prior to final rotor assembly. Pre-
assembly of the coil and coil support reduces production cycle, improves coil support
quality, and reduces coil assembly variations. The race-track coil is supported by an
array of tension members that span the long sides of the coil. The tension rod coil
support members are pre-assembled to coil.
The HTS coil winding and structural support components are at cryogenic
temperature. In contrast, the rotor core is at ambient "hot" temperature. The coil
supports are potential sources of thermal conduction that would allow heat to reach
the HTS coils from the rotor core. The rotor becomes hot during operation. As the
coils are to be held in super-cooled conditions, heat conduction into the coils is to be
avoided. The rods extend through apertures, e.g., conduits, in the rotor but are not in
contact with the rotor. This lack of contact avoids the conduction of heat from the
rotor to the tension rods and coils.
To reduce the heat leaking away from the coil, the coil support is minimized to reduce
the thermal conduction through support from heat sources such as the rotor core.
There are generally two categories of support for super-conducting winding: (i)
"warm" supports and (ii) "cold" supports. In a warm support, the supporting
structures are thermally isolated from the cooled SC windings. With warm supports,
most of the mechanical load of a super-conducting (SC) coil is supported by structural
members spanning from cold to warm members.
In a cold support system, the support system is at or near the cold cryogenic
temperature of the SC coils. In cold supports, most of the mechanical load of a SC
coil is supported by structural members which are at or near a cryogenic temperature.
The exemplary coil support system disclosed here is a cold support in that the tension
rods and associated housings that couple the tension rods to the SC coil windings are
maintained at or near a cryogenic temperature. Because the supporting members are
cold, these members are thermally isolated, e.g., by the non-contact conduits through
the rotor core, from other "hot" components of the rotor.
A dowel pin 80 connects the housing 44 to the end of the tension rod. Each channel
housing 44 is a U-shaped bracket having legs that connect to a tension rod and a
channel to receive the coil winding 34. The U-shaped channel housing allows for the
precise and convenient assembly of the support system for the coil. A series of
channel housings may be positioned end-to-end along the side of the coil winding.
The channel housings collectively distribute the forces that act on the coil, e.g.,
centrifugal forces, over substantially the entire side sections 40 of each coil.
The channel housings 44 prevent the side sections 40 of the coils from excessive
flexing and bending due to centrifugal forces. The coil supports do not restrict the
coils from longitudinal thermal expansion and contraction that occur during normal
start/stop operation of the gas turbine. In particular, thermal expansion is primarily
directed along the length of the side sections. Thus, the side sections of the coil slide
slightly longitudinally with respect to the channel housing and tension rods.
The transfer of the centrifugal load from the coil structure to a support rod is through
the channel housing that fits around the coil outside surface and side straight sections,
and is doweled by pins 80 to a wide diameter end of the tension rod. The U-shaped
channel housings are formed of a light, high strength material that is ductile at
cryogenic temperatures. Typical materials for channel housing are aluminum,
Inconel, or titanium alloys, which are non-magnetic. The shape of the U-shaped
housing may be optimized for low weight and strength.
The dowel pin 80 extends through apertures in the channel housing and tension rod.
The dowel may be hollow for low weight. Locking-nuts (not shown) are threaded or
attached at the ends of the dowel pin to secure the U-shaped housing and prevent the
sides of the housing from spreading apart under load. The dowel pin can be made of
high strength Inconel or titanium alloys. The tension rods are made with larger

diameter ends that are machined with two flats 86 at their ends to fit the U-shaped
housing and coil width. The flat ends 86 of the tension rods abut the inside surface of
the HTS coils, when the rod, coil and housing are assembled together. This assembly
reduces the stress concentration at the hole in the tension rod that receives the dowel.
The coil support system of tension rods 42, channel housings 44 and split-clamp 58
may be assembled with the HTS coil windings 34 as both are mounted on the rotor
core 22. The tension rods, channel housings and clamp provide a fairly rigid structure
for supporting the coil windings and holding the coil windings in place with respect to
the rotor core.
Each tension rod 42 extends through the rotor core, and may extend orthogonally
through the axis 20 of the rotor. Conduits 46 through the rotor core provide a passage
through which extend the tension rods. The diameter of the conduits is sufficiently
large to avoid having the hot rotor walls of the conduits be in contact with the cold
tension rods. The avoidance of contact improves the thermal isolation between the
tension rods and the rotor core.
The rotor core 22 is typically made of magnetic material such as iron, while the rotor
end shafts are typically made of non-magnetic material such as stainless steel. The
rotor core and end shafts are typically discrete components that are assembled and
securely joined together by either bolting or welding.
The iron rotor core 22 has a generally cylindrical shape suitable for rotation within the
rotor cavity 16 of the stator 12. To receive the coil winding, the rotor core has
recessed surfaces 48, such as flat or triangular regions or slots. These surfaces 48 are
formed in the curved surface of the cylindrical core and extending longitudinally
across the rotor core. The coil winding 34 is mounted on the rotor adjacent the
recessed areas 48. The coils generally extend longitudinally along an outer surface of
the recessed area and around the ends of the rotor core. The recessed surfaces 48 of
the rotor core receive the coil winding. The shape of the recessed area conforms to
the coil winding. For example, if the coil winding has a saddle-shape or some other

shape, the recess(es) in the rotor core would be configured to receive the shape of the
winding.
The recessed surfaces 48 receive the coil winding such that the outer surface of the
coil winding extends to substantially an envelope defined by the rotation of the rotor.
The outer curved surfaces 50 of the rotor core when rotated define a cylindrical
envelope. This rotation envelope of the rotor has substantially the same diameter as
the rotor cavity 16 (see Fig. 1) in the stator.
The gap between the rotor envelope and stator cavity 16 is a relatively-small
clearance, as required for forced flow ventilation cooling of the stator only, since the
rotor requires no ventilation cooling. It is desirable to minimize the clearance
between the rotor and stator so as to increase the electromagnetic coupling between
the rotor coil windings and the stator windings. Moreover, the rotor coil winding is
preferably positioned such that it extends to the envelope formed by the rotor and,
thus, is separated from the stator by only the clearance gap between the rotor and
stator.
The rotor core may be encased in a metallic cylindrical shield (not shown) that
protects the super-conducting coil winding 34 from eddy currents and other electrical
currents that surround the rotor and provides the vacuum envelope as required to
maintain hard vacuum around the cryogenic components of the rotor. The cylindrical
shield may be formed of a highly-conductive material, such as a copper alloy or
aluminum.
The SC coil winding 34 is maintained in a vacuum. The vacuum may be formed by
the shield which may include a stainless steel cylindrical layer that forms a vacuum
vessel around the coil and rotor core.
FIGURES 4, 5 and 6 show schematically the assembly process for the coil support
structure and coil winding in the rotor. As shown in FIGURE 4, before the rotor core
is assembled with the collars and other components of the rotor, the tension rods 42
are inserted into each of the conduits 46 that extend through the rotor core. The
insulator tube 52 at each end of each tension rod is placed in the expanded end at each
end of the conduits 46. The tube 52 is locked in place by a retainer locking-nut 84.
When the tension rods are assembled in the rotor core 22, the coil windings are ready
to be inserted onto the core.
As shown in FIGURE 5, the SC coil 36 is inserted onto the rotor core such that the
flat ends 86 of the tension rods 42 abut the inside surface of the side sections 40 of the
SC coil. Once the winding has been inserted over the ends of the tension bar, the
channel housings 44 are inserted over the SC coil. The channel housings are secured
to the ends of the tension bars by inserting dowels 80 through the apertures in the
tension rod and channel housing 104, 108, respectively.
The channel housing 44 includes a slot along its upper inside surface which receives
the cooling conduit 38 and holds that conduit against the coil 36.
The plurality of channel housings effectively hold the coil in place without affectation
by centrifugal forces. Although the channel housings are shown as having a close
proximity to one another, the housings need only be as close as necessary to prevent
degradation of the coil caused by high bending and tensile strains during centrifugal
loading, torque transmission, and transient fault conditions.
The channel housings and tension rods may be assembled with the coil winding
before the rotor core and coils are assembled with the collar and other components of
the rotor. Accordingly, the rotor core, coil winding and coil support system can be
assembled as a unit before assembly of the other components of the rotor and of the
synchronous machine.
FIGURE 6 shows the assembly of the split clamp 58 that is formed by clamp plates
60. The clamp plates 60 sandwiched between them the end sections 54 of the coil
winding. The split clamp provides structural support for the ends of the coil winding
34. The plates 60 of the split clamp include on their inside surfaces channels 116 that
receive the coil winding. Similarly, the plates include channels 118 for the
input/output lines 39, 41 for the gases and for the input and output current connections
79 to the coil. Once the coil supports, coil, collar and rotor core are assembled, this
unit is ready to be assembled into the rotor and synchronous machine.
While the invention has been described in connection with what is presently
considered to be the most practical and preferred embodiment, it is to be understood
that the invention is not to be limited to the disclosed embodiment, but on the
contrary, is intended to cover all embodiments within the spirit of the appended
claims.

WE CLAIM
1. A rotor (14) in a synchronous machine (10), the rotor (14) comprising :
a rotor core;
a super-conducting coil winding (34) extending around at least a portion
of the rotor core (22), said coil winding (34) having a coil end section (54)
adjacent an end of said rotor core (22); and
an end coil support (58) attached to and bracing said coil end section (54)
and being thermally isolated from said rotor core (22), wherein the end
coil support (58) abuts at least one side surface of said coil end section
(54), wherein said at least one side surface is in a plane substantially
parallel to a rotor axis (20) and said end coil support (58) is wider than a
width of the coil end section (54) and abuts an entirety of the width of the
at least one side surface of the coil end section (54).
2. A rotor as claimed in claim 1, wherein said at least one side surface of
said coil end section is a pair of side surfaces of the coil end section (54),
and said end coil support (58) is a split clamp having a pair of opposing
surfaces (60) abutting the pair of side surfaces of the coil end section
(54), wherein said opposing surfaces are each in a plane substantially
parallel to said rotor axis (20).

3. A rotor as claimed in claim 1, wherein said at least one side surface of
said coil end section (54) is a pair of side surfaces of the coil end section
(54), and the end coil support (58) comprises a pair of plates (60)
between which sandwich the coil end section (54) and said pair of plates
(60) each has a plate surface abutting one of the pair of side surfaces
(40) of the coil end section (54), wherein said plate surfaces (60) are each
in a respective plane substantially parallel to said rotor axis (20).
4. A rotor as claimed in claim 1, comprising a cryogenic coupling (26)
providing cooling fluid to said coil winding (34), wherein said end coil
support (58) is cooled by conduction from said coil winding (34).
5. A rotor as claimed in claim 1, comprising a rotor end shaft (24,30) having
a slot (64) to receive said coil end section (54) and end coil support (58),
and said end shaft (24, 30) is thermally isolated from said end coil support
(58).
6. A rotor as claimed in claim 1, wherein said end coil support (58) braces an
entire length of said coil end section (54).
7. A rotor as claimed in claim 1, wherein said end coil support (58) is
transverse to an axis (20) of the rotor core (22).

8. A rotor as claimed in claim 1, comprising a second coil end section (54)
adjacent a second end of said rotor core (22), and a second coil support
(58) bracing the second end coil end section (54).
9. A rotor as claimed in claim 1, comprising side coil supports attached to a
long side section of said coil (34).
10. A rotor as claimed in claim 9, wherein said side coil supports (58)
comprises at least one tension rod (42) extending transversely through
said rotor core (22), and coil housings (44) attached to opposite ends of
the tension rod (42), wherein said coil housings (44) each attached to an
opposite long side section of the coil (34).
11.A rotor as claimed in claim 10, wherein said tension rod (42) extends
through a conduit (46) in the rotor core (22).
12. A method for supporting a super-conducting coil winding on a rotor core
of a synchronous machine, the method comprising the steps of:
a. bracing an end section of the coil winding with an end coil support
attached to at least one side of the end section in a plane
substantially parallel to a rotor core axis, and wherein the end coil
support is wider than the at least one side of the end section of the
coil winding and abuts an entirety of a width of the side of the end
section;

b. assembling the coil winding, end coil support and rotor core;
c. attaching a rotor end shaft to said rotor core; and
d. thermally isolating the end coil support from the rotor core and the
rotor end shaft.
13. A method as claimed in claim 12, wherein said at least one side surface of
said end section is a pair of side surfaces on the end section, and wherein
the end section is braced with a split clamp having a pair of opposing
surfaces abutting the pair of side surfaces, wherein said opposing surfaces
are each in a respective plane substantially parallel to said rotor axis.
14. A method as claimed in claim 12, wherein the assembling step comprises
inserting the end section of the coil and the coil support into a slot of the
rotor end shaft.
15. A method as claimed in claim 12, wherein said at least one side surface of
said end section is a pair of side surfaces of the coil end section, and the
bracing step comprises applying plates to the pair of side surfaces of the
end section, wherein the plates have opposite surfaces that are
substantially parallel to the rotor coil axis.
16.A method as claimed in claim 12, comprising cryogenically cooling the coil,
and cooling said end coil support by heat transfer between the coil and
the coil support.

17. A rotor for a synchronous machine, the rotor comprising:
a rotor core (22) having at least one rotor core end orthogonal to a
longitudinal axis (20) of the rotor (14);
at least one end shaft (24, 30) attached to said rotor core end;
a race-track super-conducting (SC) coil winding (34) extending around
said rotor core (22) and having a coil end section (54) adjacent said rotor
end; and
a coil support brace (58) attached to said coil end section (54) and
thermally isolated from said rotor core (22) and the rotor end shaft (24,
30), wherein the coil support brace (58) abuts an entirety of a width of at
least one side surface of the coil end section (54), wherein said at least
one side surface is in a plane substantially parallel to the axis (20) of the
rotor (22), and said coil support brace (58) is wider than the at least one
side surface of the coil end section (54), and covers the end section (54).
18.A rotor as claimed in claim 17, wherein said coil support brace (58) is a
split clamp.
19.A rotor as claimed in claim 17, wherein the coil support brace (58)
comprises a pair of plates (60) between which are sandwiched the coil
end section (54).

20.A rotor as claimed in claim 17, comprising a cryogenic coupling (26)
providing cooling fluid to said coil winding (34), wherein said coil support
(58) is cooled by conduction from said coil winding (34).
21. A rotor as claimed in claim 17, wherein said rotor end shaft (24, 30) has a
slot (64) to receive said coil end section (54) and coil support (58), and
said end shaft is thermally isolated from said coil support (58).
22. A rotor as claimed in claim 17, wherein said coil support brace (54) covers
an entire length of said coil end section (54).
23. A rotor as claimed in claim 17, wherein said coil support brace (54) is
transverse to an axis (20) of the rotor core.
24. A rotor as claimed in claim 17, comprising a second coil end section (54)
adjacent a second end of said rotor core (22), and a second coil support
(58) brace attached to the second coil end section.
25. A rotor as claimed in claim 17, comprising coil side supports attached to a
long side section of said coil.
26.A rotor as claimed in claim 17, comprising at least one tension rod (42)
extending transversely through said rotor core (22), and coil housings
(44) attached to opposite ends of the tension rod (42), wherein said coil
housings (44) each attached to an opposite long side section of the coil
(34).

27. A rotor as claimed in claim 17, wherein said tension rod (42) extends
through a conduit (46) in the rotor core (22).

This invention relates to a rotor (14) in a synchronous machine (10), the rotor
(14) comprising; a rotor core; a super-conducting coil winding (34) extending
around at least a portion of the rotor core (22), said coil winding (34) having a
coil end section (54) adjacent an end of said rotor core (22); and an end coil
support (58) attached to and bracing said coil end section (54) and being
thermally isolated from said rotor core (22), wherein the end coil support (58)
abuts at least one side surface of said coil end section (54), wherein said at least
one side surface is in a plane substantially parallel to a rotor axis (20) and said
end coil support (58) is wider than a width of the coil end section (54) and abuts
an entirety of the width of the at least one side surface of the coil end section
(54).