The present disclosure relates to rotating machines, and more particularly, to rotating machines incorporating stator coils.
A rotating electric machine includes a stator coil assembly having multiple stator coils. Machines incorporating high temperature superconductor (HTS) stator materials experience a significant increase in the field electromotive forces generated by the windings and increased flux and power densities of the machines as compared to conventional “non-superconducting” rotating machines incorporating iron-toothed stators. Furthermore, in HTS based electrical machines, the stator coils are the sole recipients of the Lorenz magnetic force, in contrast to conventional stators where most of the force is dissipated through the iron teeth.
The stator coils are positioned radially about the perimeter of a cylindrical support structure. The desired number of magnetic poles dictates the number of stator coils included in the assembly. “Racetrack” type stator coils have two straight sections disposed parallel to a center axis of the cylindrical support structure and two end turn regions linking the straight sections. The straight sections are the active sections through which current must flow to electromagnetically engage a rotor assembly, causing it to rotate.
In addition to the heat generated by the rotor assembly, the stator assembly also generates a considerable amount of heat that must be removed in order for the superconducting machine to operate efficiently. In conventional “non-superconducting” rotating machines, iron teeth are utilized between the individual stator coil assemblies, which act as heat sinks and remove the heat generated by the stator assembly. However, in superconducting machines, the flux density is so great between these stator coil assemblies that these iron teeth would immediately become saturated, resulting in Eddy current heating and operating inefficiency.
According to an aspect of the disclosure, a stator coil assembly includes a cylindrical support tube with first and second pluralities of stator coils disposed radially around the support tube. Each stator coil includes first, second, third, and fourth linear segments, each having first and second planar broad sides. The second and fourth linear segments extend in parallel along a first axis with the first and second broad sides of the second and fourth linear segments lying in a common plane. The first and third linear segments extend in parallel along a second axis perpendicular to the first axis. Transition segments having first and second planar broad sides each join a pair of the linear segments. In one configuration, the transition segment comprises three curved portions. The transition segments of the first plurality of stator coils define curvatures away from the center axis and the transition segments of the second plurality of stator coils define curvatures towards the center axis such that the first and third linear segments are disposed at a substantially equal radial distance from the center axis. The planar broad sides of the transition segments joined to the first linear segment lie in planes parallel to the planar broad sides of the first linear segment, and the planar broad sides of the transition segments joined to the third linear segment lie in planes parallel to the planar broad sides of the third linear segment. In some embodiments, an axis normal to the first planar broad side of each segment intersects a common center axis. Also, the first, second, third, and fourth linear segments define substantially rectangular cross sections.
In some embodiments, the stator coil includes a shell with at least one pancake coil disposed within the shell and comprising a plurality of conductive wires wherein the linear segments have substantially uniform cross-sectional area and substantially uniform cross-sectional wire density. The stator coil includes a plurality of bundles of conductive wires where in one aspect the conductive wires comprise Litz wires. At least one spacer having opposing sides is positioned between the pancake coil and the shell, an opposing side of the spacer and the pancake coil define in part a cooling channel. In one example, a plurality of pancake coils are disposed within the shell along with a plurality of spacers positioned between the pancake coils and the shell, as well as between the pancake coils, defining a plurality of coolant channels. In another aspect, an inlet coolant manifold is disposed at a first end of the support tube and an outlet coolant manifold is disposed at a second end of the support tube. The fourth linear segments of the stator coils are joined to the inlet coolant manifold for introducing a flow of a coolant through the stator coils and the second linear segments of the stator coils are joined to the outlet coolant manifold for receiving the flow of coolant out of the stator coils.
The details of one or more embodiments of the invention are set forth in the accompanying drawings and the description below. Other features and advantages of the invention will be apparent from the description and drawings, and from the claims.
Like reference symbols in the various drawings indicate like elements.
Referring to
A rotor assembly 516 rotates within stator assembly 512. As with stator assembly 512, rotor assembly 516 includes rotor winding assemblies 5181−n. In the same 33,000 horsepower superconducting machine design, rotor assembly 516 includes sixteen rotor winding assemblies 5141−n. These rotor winding assemblies, during operation, generate a magnetic flux that links rotor assembly 516 and stator assembly 512.
By supplying power through supply voltage 520 to stator coil assemblies 5141−n, machine 510 is brought up to its operating speed. The torque generated by this now-rotating rotor assembly 516 is transferred to a load 521 (e.g., a propeller shaft of a ship, a conveyor belt on a production line, the drive wheels of a diesel locomotive, etc.). The rotor winding assemblies 5141−n are mounted on a support structure 517 which is connected to a first flange 519 that transfers the motor torque to a torque tube 522. Torque tube 522 is connected to a second flange 523, which is connected to an output shaft 524. Flanges 519 and 523 may be incorporated into torque tube 522 or may be separate assemblies.
Output shaft 524 is supported by a pair of bearing plates 526, 528, one at each end of rotor assembly 516. The bearing plate 526 on the drive end 530 of superconducting rotating machine 510 contains a passage 532 through which output shaft 524 passes. Additionally, bearing plate 528 may also have a passage through which the output shaft 524 passes. Bearing plates 526, 528 position rotor assembly 516 at the proper position within stator assembly 512 so that rotor assembly 516 can freely rotate within stator assembly 512 while maintaining the proper gap “g” between rotor assembly 516 and stator assembly 512.
Referring to
Referring to
The transition segment 70 includes three curved portions. The transition segments 70 of the inner stator coils 20 define curvatures away from the center axis 15, while the transition segments 70 of the outer stator coils 25 define curvatures towards the center axis 15 such that the axially aligned linear segment 50, 60 of the inner and outer stator coils 20, 25 are disposed at a substantially equal radial distance from the center axis 15.
Referring to
In another aspect, the stator coils 20, 25 are cooled by introducing a flow of coolant through the cross-section via the one or more coolant channels 125. The forced liquid coolant may comprise de-ionized water or dielectric oil. The coolant enters the first end turn region 41 of the stator coil 20, 25 and exits the second end turn region 42 opposite of the first end turn region 41. In one embodiment using oil as the coolant, thin coolant channels 125 are employed. Preferably, cooling channels 125 with cross-sections of about 1 mm wide can achieve a surface heat transfer coefficient of about 1000 W/mK. Furthermore, an effective flow velocity is about 3 m/s with a Nusselt number of between about 7 to 10.
Referring to
A number of embodiments of the invention have been described. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and scope of the invention. Accordingly, other embodiments are within the scope of the following claims. For example, the stator coils 20, 25 may have cross-sectional geometries other than rectangular.
The following applications are hereby incorporated by reference into the subject application as if set forth herein in full: (1) U.S. application Ser. No. 09/632,599, filed Aug. 4, 2000, entitled “Superconducting Synchronous Machine Field Winding Protection” (Atty. Docket No. 05770-112001/ASC-458); (2) U.S. application Ser. No. 09/632,602, filed Aug. 4, 2000, entitled “Segmented Rotor Assembly For Superconducting Rotating Machines” (Atty. Docket No. 05770-123001/ASC-490); (3) U.S. application Ser. No. 09/632,600, filed Aug. 4, 2000, entitled “Exciter For Superconducting Rotating Machinery” (Atty. Docket No. 05770-121001/ASC-487); (4) U.S. application Ser. No. 09/632,601, filed Aug. 4, 2000, entitled “Stator Support Assembly For Superconducting Rotating Machines” (Atty. Docket No. 05770-124001/ASC-491); (5) U.S. application Ser. No. 09/480,430, filed Jan. 11, 2000, entitled “Exciter and Electronic Regulator for Rotating Machinery” (Atty. Docket No. 05770-101001/ASC-424); (6) U.S. application Ser. No. 09/480,397, filed Jan. 11, 2000, entitled “Stator Construction For Superconducting Rotating Machines” (Atty. Docket No. 05770-102001/ASC445); (7) U.S. application Ser. No. 09/481,480, filed Jan. 11, 2000, entitled “Internal Support for Superconducting Wires” (Atty. Docket No. 05770-105001/ASC-448); (8) U.S. Ser. No. 09/480,396, filed Jan. 11, 2000, entitled “Cooling System for HTS Machines” (Atty. Docket No. 05770-108001/ASC-456); (9) U.S. application Ser. No. 09/415,626, filed Oct. 12, 1999, entitled “Superconducting Rotating Machine” (Atty. Docket No. 05770-099001/ASC-438); (10) U.S. application Ser. No. 60/266,319, filed Jan. 11, 2000, entitled “HTS Superconducting Rotating Machine” (Atty. Docket No. 05770-106001/ASC-450); (11) U.S. application Ser. No. 09/905,611, filed Jul. 13, 2001, entitled “Enhancement of Stator Leakage Inductance in Air-Core Machines” (Atty. Docket No. 05770-158001/ASC-544); and (12) U.S. application Ser. No. 09/956,328, filed Sep. 19, 2001, entitled “Axially-Expandable EM Shield” (Atty. Docket No. 05770-168001/ASC-597).