阅读说明：本技术 用于具有超导定子的风力涡轮发电机的旋转电枢 (Rotating armature for a wind turbine generator with a superconducting stator ) 是由 D·A·托里 张伟 M·E·费尔米利 J·W·布雷 S·N·阿沙 H·P·J·德波克 尹 于 2018-06-27 设计创作，主要内容包括：提出了一种电枢。该电枢包括具有多个线圈的电枢绕组,其中多个线圈中的每个线圈与相邻线圈间隔开,并且包括第一侧部分和第二侧部分。该电枢还包括第一电绝缘绕组外壳。此外,该电枢包括设置在距第一电绝缘绕组外壳的径向距离处的第二电绝缘绕组外壳,其中电枢绕组设置在第一电绝缘绕组外壳和第二电绝缘绕组外壳之间。此外,电枢包括设置在电枢绕组的多个线圈的第一侧部分和第二侧部分之间的电绝缘线圈侧分隔件。还提出了包括电枢的超导发电机和具有这样的超导发电机的风力涡轮。(An armature is presented. The armature includes an armature winding having a plurality of coils, wherein each coil of the plurality of coils is spaced apart from an adjacent coil and includes a first side portion and a second side portion. The armature also includes a first electrically insulated winding housing. Furthermore, the armature comprises a second electrically insulated winding shell arranged at a radial distance from the first electrically insulated winding shell, wherein the armature winding is arranged between the first and the second electrically insulated winding shells. Further, the armature includes an electrically insulating coil-side separator disposed between the first side portion and the second side portion of the plurality of coils of the armature winding. Superconducting generators including armatures and wind turbines having such superconducting generators are also presented.)

1. A wind turbine, comprising:

a rotor including a plurality of blades;

a shaft coupled to the rotor; and

a superconducting electrical generator coupled to the rotor via the shaft and configured to operate via the rotor, wherein the superconducting electrical generator comprises:

a stationary generator field;

a superconducting field winding disposed on the stationary generator field; and

an armature disposed concentrically with the stationary generator field, wherein the armature comprises:

an armature winding comprising a plurality of coils, wherein each coil of the plurality of coils is spaced apart from an adjacent coil and comprises a first side portion and a second side portion;

a first electrically insulated winding housing;

a second electrically insulated winding housing disposed at a radial distance from the first electrically insulated winding housing, wherein the armature winding is disposed between the first and second electrically insulated winding housings;

an electrically insulated coil-side separator disposed between the first and second side portions of the plurality of coils of the armature winding; and

a plurality of electrically insulating spacers, wherein at least one electrically insulating spacer is disposed between adjacent first side portions and between adjacent second side portions, and wherein one or more of the plurality of electrically insulating spacers includes at least one cooling channel configured to facilitate a flow of a cooling fluid therethrough to facilitate cooling of the armature winding.

2. The wind turbine of claim 1, wherein the first and second electrically insulated winding shells comprise a fiber reinforced composite material.

3. The wind turbine of claim 1, wherein the electrically insulated coil-side separator comprises a non-ferromagnetic material.

4. The wind turbine of claim 1, wherein the at least one cooling channel is positioned at one or more sidewalls of the one or more spacers, within a body of the one or more spacers, or both.

5. The wind turbine of claim 1, wherein the plurality of coils are secured together with the first electrically insulated winding shell, the second electrically insulated winding shell, and the electrically insulated coil-side separator via an adhesive.

6. The wind turbine of claim 1, further comprising one or more cooling manifolds fluidly coupled to the at least one cooling channel to supply the cooling fluid to the at least one cooling channel.

7. The wind turbine of claim 1, wherein the at least one cooling channel comprises at least one surface feature to facilitate cooling of the armature winding.

8. The wind turbine of claim 7, wherein the at least one surface feature comprises one or more dimples, one or more fins, one or more protrusions, one or more ridges, or a combination thereof.

9. The wind turbine of claim 1, wherein the superconducting electrical generator further comprises:

a container at least partially enclosing the armature winding; and

a charging system fluidly coupled to the tank and configured to supply pressurized fluid to the armature windings.

10. The wind turbine of claim 9, wherein the superconducting generator further comprises a pressure sensor coupled to the vessel to sense a pressure of the pressurized fluid within the vessel.

11. The wind turbine of claim 10, wherein the superconducting generator further comprises a pressure relief valve to limit the pressure of the pressurized fluid within the vessel to a threshold fluid pressure value.

12. An armature for an electric machine comprising:

an armature winding comprising a plurality of coils, wherein each coil of the plurality of coils is spaced apart from an adjacent coil;

a first electrically insulated winding housing; and

a second electrically insulated winding shell disposed at a radial distance from the first electrically insulated winding shell, wherein the armature winding is disposed between the first and second electrically insulated winding shells.

13. The armature of claim 12, further comprising a plurality of electrically insulating spacers disposed between adjacent coils.

14. An armature as claimed in claim 13, and wherein one or more of the plurality of electrically insulating spacers comprises at least one cooling channel configured to facilitate the flow of a cooling fluid therethrough to assist in the cooling of the armature windings.

15. The armature of claim 14, further comprising one or more cooling manifolds fluidly coupled to the at least one cooling channel to supply the cooling fluid to the at least one cooling channel.

16. The armature of claim 14, wherein the at least one cooling channel comprises at least one surface feature to facilitate cooling of the armature winding.

17. A superconducting electrical generator comprising:

a stationary generator field;

a superconducting field winding disposed on the stationary generator field; and

an armature disposed concentrically with the stationary generator field, wherein the armature comprises:

an armature winding comprising a plurality of coils, wherein each coil of the plurality of coils is spaced apart from an adjacent coil and comprises a first side portion and a second side portion;

a first electrically insulated winding housing;

a second electrically insulated winding housing disposed at a radial distance from the first electrically insulated winding housing, wherein the armature winding is disposed between the first and second electrically insulated winding housings; and

an electrically insulated coil-side separator disposed between the first and second side portions of the plurality of coils of the armature winding.

18. The armature of claim 17, further comprising a plurality of electrically insulating spacers, wherein at least one of the plurality of electrically insulating spacers is disposed between adjacent first side portions and between adjacent second side portions.

19. The armature of claim 18, wherein one or more of the plurality of electrically insulating spacers comprises at least one cooling channel configured to facilitate a flow of a cooling fluid therethrough to facilitate cooling of the armature windings.

20. A method of forming an armature, the method comprising:

disposing a first electrically insulative housing on the base;

disposing an armature winding on the first electrically insulated winding housing, wherein the armature winding comprises a plurality of coils comprising a first side portion and a second side portion;

disposing an electrically insulating coil-side separator between the first and second side portions of the plurality of coils; and

disposing a second electrically insulative housing over the second side portion of the plurality of coils.

21. The method of claim 20, further comprising disposing a plurality of first electrically insulating spacers such that at least one of the plurality of first electrically insulating spacers is disposed between adjacent first side portions of the plurality of coils.

22. The method of claim 20, further comprising disposing a second plurality of electrically insulating spacers such that at least one of the second plurality of electrically insulating spacers is disposed between adjacent second side portions of the plurality of coils.

23. The method of claim 20, further comprising disposing a shield on the second electrically insulative housing.

Technical Field

Embodiments of the present description relate generally to wind turbines, and in particular to wind turbines including superconducting generators.

Background

Conventional superconducting machines, such as conventional superconducting generators, typically include a field winding and an armature. The armature includes a conventional ferromagnetic core and an armature winding disposed on the conventional ferromagnetic core. The armature windings are generally formed using conventional materials, such as copper or aluminum. However, the field winding comprises superconducting wires, which support very high current densities without causing any dissipation. Due to the high current density in the field windings, the superconducting wires of conventional superconducting generators produce very high magnetic fields, e.g., about 7 tesla or more, when in operation. This increased magnetic field caused by the superconducting wire is generally higher than the saturation flux density of conventional ferromagnetic materials. In addition, the armature is also heated due to the current in the armature winding, resulting in a shortened life of the armature insulation system in the superconducting generator.

Disclosure of Invention

According to one embodiment of the invention, a wind turbine is presented. The wind turbine includes a rotor having a plurality of blades. The wind turbine also includes a shaft coupled to the rotor and a superconducting generator coupled to the rotor via the shaft and configured to operate via the rotor. The superconducting generator includes a stationary generator field, a superconducting field winding disposed on the stationary generator field, and an armature disposed concentrically with the stationary generator field. The armature includes an armature winding having a plurality of coils, wherein each coil of the plurality of coils is spaced apart from an adjacent coil and includes a first side portion and a second side portion. The armature also includes a first electrically insulated winding housing. Furthermore, the armature comprises a second electrically insulated winding shell arranged at a radial distance from the first electrically insulated winding shell, wherein the armature winding is arranged between the first and the second electrically insulated winding shells. Further, the armature includes an electrically insulating coil-side separator disposed between the first side portion and the second side portion of the plurality of coils of the armature winding. Additionally, the armature includes a plurality of electrically insulating spacers, wherein at least one electrically insulating spacer is disposed between adjacent first side portions and between adjacent second side portions, and wherein one or more of the plurality of electrically insulating spacers includes at least one cooling channel configured to facilitate a flow of a cooling fluid therethrough to facilitate cooling of the armature windings.

According to another embodiment of the present invention, an armature is provided. The armature includes an armature winding having a plurality of coils, wherein each coil of the plurality of coils is spaced apart from an adjacent coil. The armature also includes a first electrically insulated winding housing. Furthermore, the armature comprises a second electrically insulated winding shell arranged at a radial distance from the first electrically insulated winding shell, wherein the armature winding is arranged between the first and the second electrically insulated winding shells.

According to yet another embodiment of the present invention, a superconducting electrical generator is provided. The superconducting generator includes a stationary generator field, a superconducting field winding disposed on the stationary generator field, and an armature disposed concentrically with the stationary generator field. The armature includes an armature winding having a plurality of coils, wherein each coil of the plurality of coils is spaced apart from an adjacent coil and includes a first side portion and a second side portion. The armature also includes a first electrically insulated winding housing. Furthermore, the armature comprises a second electrically insulated winding shell arranged at a radial distance from the first electrically insulated winding shell, wherein the armature winding is arranged between the first and the second electrically insulated winding shells. Further, the armature includes an electrically insulating coil-side separator disposed between the first side portion and the second side portion of the plurality of coils of the armature winding.

Drawings

These and other features, aspects, and advantages of the present specification will become better understood when the following detailed description is read with reference to the accompanying drawings in which like characters represent like parts throughout the drawings, wherein:

FIG. 1 is a schematic view of an example wind turbine according to an embodiment of the present description;

FIG. 2 is a schematic view of a superconducting electrical generator according to one embodiment of the present description;

FIG. 3 is a cross-sectional view of a portion of an armature used in the superconducting electrical generator of FIG. 2, according to one embodiment of the present description;

FIG. 4 is a cross-sectional view of a portion of an armature used in the superconducting electrical generator of FIG. 2, according to another embodiment of the present description;

FIG. 5 is a cross-sectional view of a portion of an armature used in the superconducting electrical generator of FIG. 2 according to another embodiment of the present description;

FIG. 6 is a cross-sectional view of a portion of an armature used in the superconducting electrical generator of FIG. 2 according to yet another embodiment of the present description;

FIG. 7 is a schematic depicting a portion of an inner surface of a cooling channel having surface features in accordance with an embodiment of the present description;

FIG. 8 is a schematic view of a cooling manifold that may be connected to an armature having the configuration depicted in FIG. 5, according to one embodiment of the present description;

fig. 9 is a perspective view of a portion of an armature according to one embodiment of the present description;

fig. 10 is a flow diagram of a method for assembling the armature depicted in any of fig. 3-5 in accordance with an embodiment of the present description; and

fig. 11A to 11G depict the structure of the armature in various steps of the method of fig. 10.

Detailed Description

In an effort to provide a concise description of these embodiments, all features of an actual implementation may not be described in the specification. It should be appreciated that in the development of any such actual implementation, as in any engineering or design project, numerous implementation-specific decisions may be made to achieve the developers' specific goals, such as compliance with system-related and business-related constraints.

Unless defined otherwise, technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this specification belongs. The terms "first," "second," and the like, as used herein do not denote any order, quantity, or importance, but rather are used to distinguish one element from another. Furthermore, the terms "a" and "an" do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item. The use of "including," "comprising," or "having" and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. The terms "connected" and "coupled" are not restricted to physical or mechanical connections or couplings, and can include electrical connections or couplings, whether direct or indirect.

As used herein, the terms "may" and "may be" denote the possibility of occurrence within a set of circumstances; possess specified characteristics, features or functions; and/or qualify another verb by expressing one or more capabilities, or possibilities associated with the qualified verb. Thus, usage of "may" and "may be" indicates that the modified term is apparently appropriate, capable of being (capable), or suitable for the indicated capability, function, or usage, while taking into account that in some instances the modified term may sometimes not be appropriate, capable, or suitable for the indicated capability, function, or usage.

As will be described in detail below, various embodiments of a wind turbine are presented. The wind turbine includes a rotor having a plurality of blades. The wind turbine also includes a shaft coupled to the rotor and a superconducting generator coupled to the rotor via the shaft and configured to operate via the rotor. In some embodiments, a superconducting generator includes a stationary generator field, a superconducting field winding disposed on the stationary generator field, and an armature disposed concentrically with the stationary generator field.

In some embodiments, the armature includes an armature winding having a plurality of coils, wherein each coil of the plurality of coils is spaced apart from an adjacent coil and includes a first side portion and a second side portion. The armature also includes a first electrically insulated winding housing. Furthermore, the armature comprises a second electrically insulated winding shell arranged at a radial distance from the first electrically insulated winding shell, wherein the armature winding is arranged between the first and the second electrically insulated winding shells. Further, the armature includes an electrically insulating coil-side separator disposed between the first side portion and the second side portion of the plurality of coils of the armature winding.

In certain embodiments, the armature may further comprise a plurality of electrically insulating spacers, wherein at least one electrically insulating spacer is disposed between adjacent first side portions and between adjacent second side portions, and wherein one or more of the plurality of electrically insulating spacers comprises at least one cooling channel configured to facilitate a cooling fluid flow therethrough to facilitate cooling of the armature windings.

Referring now to FIG. 1, a schematic view of an example wind turbine 100 is presented, according to one embodiment of the present description. Wind turbine 100 may be configured to use wind energy to generate electrical power. The wind turbine 100 described and illustrated in the embodiment of FIG. 1 includes a horizontal-axis configuration. However, in some embodiments, wind turbine 100 may include a vertical axis configuration (not shown) in addition to or as an alternative to a horizontal axis configuration. Wind turbine 100 may be coupled to a power grid, such as, but not limited to, for receiving electrical power from the power grid to drive operation of wind turbine 100 and/or its associated components and/or for supplying electrical power generated by wind turbine 100 to the power grid. Wind turbine 100 may be coupled to an electrical load (not shown) to supply the electrical load with electrical power generated by wind turbine 100.

Wind turbine 100 may include a body 102 (sometimes referred to as a "nacelle") and a rotor 104 coupled to body 102. The rotor 104 is configured to rotate relative to the body 102 about an axis of rotation 106. In the embodiment of FIG. 1, nacelle 102 is shown mounted on a tower 108. However, in some other embodiments, the wind turbine 100 may include a nacelle, which may be disposed adjacent to the ground and/or the water surface.

Rotor 104 may include a hub 110 and a plurality of blades 112 (sometimes referred to as "airfoils") extending radially outward from hub 110 for converting wind energy into rotational energy. Although rotor 104 is described and illustrated herein as having three blades 112, rotor 104 may have any number of blades 112. Rotor 104 may have blades 112 of any shape, and may have blades 112 of any type and/or any configuration, whether such shape, type, and/or configuration is described and/or illustrated herein.

In some embodiments, the nacelle 102 may house, in whole or in part, one or more of the superconducting electrical generator 114 and the shaft 116. The superconducting electrical generator 114 may be coupled to the rotor 104 via a shaft 116 and configured to operate via the rotor 104. For example, rotation of rotor 104 due to wind energy, in turn, causes a rotating element (e.g., an armature) of superconducting generator 114 to rotate via shaft 116. In some embodiments, the shaft 116 may also include a gearbox (not shown). In certain embodiments, the use of a gearbox may increase the operating speed of the superconducting generator 114 and reduce the torque requirements for a given power level. The presence or absence of a gearbox is not critical to the embodiments of the superconducting electrical generator 114 described herein.

The superconducting electrical generator 114 is configured to generate electrical power based at least on rotation of the armature. According to some embodiments described herein, the superconducting generator 114 may be configured to handle increased current amplitudes as compared to conventional generators. The superconducting electrical generator 114 may be implemented in the form of a synchronous generator. The superconducting generator 114 will be described in more detail in connection with fig. 2.

Fig. 2 is a schematic diagram of a superconducting electrical generator 200 according to one embodiment of the present description. The superconducting electrical generator 200 may represent one embodiment of a superconducting electrical generator 114 for use in the wind turbine 100 of FIG. 1. Without limiting the scope of the present application, superconducting generator 200 may be used in any application other than a wind turbine. Although superconducting generator 200 depicted in fig. 2 is a radial field machine, embodiments of the present description are also applicable to axial field or transverse field superconducting generators.

As depicted in fig. 2, the superconducting electrical generator 200 includes a stationary generator field 202 and an armature 204 disposed in a housing 206. In particular, fig. 2 depicts an exploded view of a superconducting generator 200 to separately illustrate a stationary generator field 202 and an armature 204.

A stationary generator field 202 is disposed adjacent to an armature 204. As used herein, in one embodiment, the term "disposed adjacent" with respect to the positioning of the stationary generator field 202 and the armature 204 refers to the relative positioning of the stationary generator field 202 and the armature 204 such that the armature 204 is surrounded by the stationary generator field 202 (e.g., as shown in fig. 2). In another embodiment, the term "disposed adjacent" refers to the relative positioning of the stationary generator field 202 and the armature 204 such that the stationary generator field 202 is surrounded by the armature 204 (not shown). In yet another embodiment, the term "disposed adjacent" refers to the relative positioning of the stationary generator field 202 and the armature 204 such that the stationary generator field 202 and the armature 204 are disposed side-by-side (not shown).

Furthermore, in some embodiments, superconducting generator 200 may also include superconducting field windings 208 disposed on fixed generator field 202. Superconducting field windings 208 may include one or more coils made using conductive materials that transition to a superconducting state at a sufficiently low temperature. Such materials include niobium-tin alloys, niobium-titanium alloys, magnesium diboride alloys, any of a variety of ceramic materials that have exhibited superconducting properties, or combinations thereof. Typically, conductive materials (including materials such as, but not limited to, copper, aluminum, anodized aluminum, silver, gold, or combinations thereof) are used in conjunction with the superconducting alloy to improve mechanical properties. In certain embodiments, a low weight conductive material may be used to increase or at least maintain the power density of superconducting generator 200. In some embodiments, superconducting generator 200 may also include a suitable arrangement (not shown) for cooling superconducting field windings 208 to an ultra-low temperature.

For example, in some embodiments, when superconducting generator 200 is deployed as superconducting generator 114 in wind turbine 100, armature 204 may be coupled to rotor 104 of wind turbine 100 via shaft 116 or via both shaft 116 and the gearbox. Accordingly, armature 204 may rotate due to rotation of rotor 104 caused by wind energy. Due to the rotation of armature 204, superconducting generator 200 may generate electrical power from the voltage induced in the armature windings as they move through the magnetic field established by superconducting field windings 208. The details of the structure of the armature 204 will be described in conjunction with fig. 3 to 8.

Turning now to fig. 3, a cross-sectional view 300 of portion 3 (as labeled in fig. 2) of armature 204 used in superconducting generator 200 of fig. 2 is presented, according to one embodiment of the present description. Reference numerals 30 and 32 represent the radial and axial directions of the armature 204, respectively. As depicted in fig. 3, in some embodiments, the armature 204 may include an armature winding 302, a first electrically insulated winding housing 304, a second electrically insulated winding housing 306, an electrically insulated coil-side separator 308, and a base 310 (also sometimes referred to as a mandrel).

The first electrically insulated winding housing 304 may be disposed on a base 310.The base 310 may be formed using a solid block or lamination of one or more ferromagnetic materials. The second electrically insulated winding housing 306 is disposed at a radial distance (f) from the first electrically insulated winding housing 304R _d ) To (3). In some embodiments, the first and second electrically insulated winding shells 304, 306 may be formed using a fiber reinforced composite material. Non-limiting examples of these fiber-reinforced composites may include G-10, G-11, F-24, FR-4, other fiber-reinforced polymers, or combinations thereof. The armature winding 302 is disposed between a first electrically insulated winding housing 304 and a second electrically insulated winding housing 306, as depicted in fig. 3.

Further, optionally, in certain embodiments, the armature 204 may include a shield 311 disposed on the second electrically insulated winding housing 306. The use of the shield 311 maintains magnetic flux from the superconducting field winding 208 to remain in the radial direction 30, thereby enhancing the magnetic coupling between the stationary generator field 202 and the armature winding 302. Advantageously, due to this improved magnetic coupling between the armature windings 302 and the stationary generator field 202, the electromagnetic performance of the superconducting generator 200 may be improved. The shield 311 may be formed using a ferromagnetic material. In some embodiments, the shield 311 may be laminated to reduce losses associated with induced current (as in conventional motors). With respect to the position of the shield 311 depicted in fig. 3, the superconducting field windings 208 may be located radially inside the first electrically insulating housing 304. With the superconducting field winding 208 radially outward of the armature winding, the shield 311 will be adjacent the first electrically insulating housing 304. In this case, the shield 311 may replace the base 310 during armature assembly.

The armature winding 302 includes a plurality of coils 312A, 312B, 312C, 312D, and 312E. The coils 312A, 312B, 312C, 312D, and 312E are collectively referred to hereinafter as coils 312. Although five coils 312A-312E are depicted in the cross-sectional view 300 of fig. 3, any number of coils may be employed in the armature 204 without limiting the scope of the present description. The coils 312 will be configured as phase windings, the number of which is determined by the designer. Non-limiting examples of conductive materials used to form the coil 312 may include copper, aluminum, silver, gold, or combinations thereof.

In some embodiments, as depicted in fig. 3, the coils 312 are spaced apart from one another. For example, each coil of the plurality of coils 312 is spaced apart from an adjacent coil. The space between adjacent coils 312 may serve as or be used as a cooling conduit where a cooling fluid, such as air, may pass therethrough. Advantageously, the configuration of the armature 204 depicted in fig. 3 facilitates reducing the operating temperature of the armature 204. Additionally, in certain embodiments, the coils 312 may be coated with an electrically insulating coating such that the flow of cooling fluid may not affect the electrical operation of the superconducting generator 200.

Further, each of the coils 312 includes a first side portion, a second side portion, and an end portion. For example, the coil 312A includes a first side portion 314A, a second side portion 316A, and end portions 318A, 320A (not shown in fig. 3, see fig. 11C-11G). The coil 312B includes a first side portion 314B, a second side portion 316B, and end portions 318B, 320B (not shown in fig. 3, see fig. 11C-11G). The coil 312C includes a first side portion 314C, a second side portion 316C, and end portions 318C, 320C (not shown in fig. 3, see fig. 11C-11G). The coil 312D includes a first side portion 314D, a second side portion 316D, and end portions 318D, 320D (not shown in fig. 3, see fig. 11C-11G). The coil 312E includes a first side portion 314E, a second side portion 316E, and end portions 318E, 320E (not shown in fig. 3, see fig. 11C-11G). The first side portions 314A, 314B, 314C, 314D, 314E are collectively referred to hereinafter as first side portions 314. The second side portions 316A, 316B, 316C, 316D, 316E are collectively referred to hereinafter as second side portions 316. Further, the end portions 318A, 318B, 318C, 318D, 318E are collectively referred to hereinafter as end portions 318. Further, the end portions 320A, 320B, 320C, 320D, 320E are collectively referred to hereinafter as end portions 320. Further, in some embodiments, the first and second side portions 314, 316 are radially and tangentially displaced relative to each other and are connected by an end portion (not shown in fig. 3). For example, in such a configuration, radially adjacent first and second side portions 314, 316 belong to different coils 312. For example, the first side portion 314A and the second side portion 316A belong to different coils. These different coils 312 may be of the same phase or different phases.

Further, in some embodiments, an electrically insulative coil-side separator 308 is disposed between a first side portion 314 and a second side portion 316 of the coil 312. The electrically insulating coil-side spacer 308 provides electrical insulation along the length between the first side portion 314 and the second side portion 316. For example, the electrically isolated coil side spacers 308 may be formed using non-ferromagnetic material(s), such as G-10, FR-4, G-11, F-24, or other fiber reinforced polymers, or combinations thereof.

In some embodiments, in a configuration of the armature 204 as depicted in fig. 2 in which the armature 204 is surrounded by the stationary generator field 202, the second electrically insulated winding housing 306 may form the outermost support structure of the armature winding 302, and the first electrically insulated winding housing 304 may form the innermost support structure disposed on the base 310 of the armature 204. In this case, the shield 311 would be adjacent to the first electrically insulative housing 304. In this case, the shield 311 may replace the base 310 during armature assembly.

In certain embodiments, the second electrically insulated winding housing 306 may have a constant or substantially constant radius along the effective length of the superconducting electrical machine 200. As used herein, the term "effective length" refers to the length of one of the first side portion 314 or the second side portion 316. Further, in some configurations of the armature 204, the radius of the second electrically insulated winding housing 306 may vary (increase or decrease) around the end portions 318, 320 of each of the coils 312 to support the end portions 318, 320 of each of the coils 312. This support provided to the end portions 318, 320 enhances the mechanical integrity of the armature 204. Further, the second electrically insulated winding housing 306 may also act as a baffle for directing cooling air along the coil 312. In some embodiments, other elements, such as seals (not shown), for preventing cooling fluid from leaking from the armature 204 may be provided on the second electrically insulated winding housing 306.

In some embodiments, the plurality of coils 312 are secured together with the first electrically insulated winding housing 304, the second electrically insulated winding housing 306, and the electrically insulated coil-side divider 308 using an adhesive 309. For example, the first side portion 314 of the coil 312 is secured with the first electrically insulated winding housing 304 and the electrically insulated coil side divider 308 via the adhesive 309. In addition, the second side portion 316 of the coil 312 is secured with the second electrically insulated winding housing 306 and the electrically insulated coil side divider 308 via an adhesive 309. It will be appreciated that the adhesive 309 holds the plurality of coils 312 in place in the face of tangential and radial magnetic forces exerted on the coils 312 due to currents flowing in the armature windings 302 within the magnetic field generated by the superconducting field windings 208.

Furthermore, in some embodiments, the armature 204 may also include a plurality of electrically insulating spacers, as depicted in fig. 4 and 5. Referring now to fig. 4, a cross-sectional view 400 of portion 3 (see fig. 2) of armature 204 used in superconducting generator 200 of fig. 2 is presented, according to another embodiment of the present description. As depicted in fig. 4, the armature 204 may include a plurality of electrically insulating spacers 402A, 404A, 402B, 404B, 402C, 404C, 402D, and 404D. For simplicity of illustration, eight electrically insulating spacers are labeled with reference numerals 402A, 404A, 402B, 404B, 402C, 404C, 402D, and 404D. The electrically insulating spacers 402A, 402B, 402C, 402D are collectively referred to hereinafter as electrically insulating spacers 402. Similarly, electrically insulating spacers 404A, 404B, 404C, 404D are collectively referred to hereinafter as electrically insulating spacers 404.

In some embodiments, at least one electrically insulating spacer is disposed between adjacent first side portions 314 and between adjacent second side portions 316. For example, as depicted in fig. 4, electrically insulating spacer 402A is disposed between first side portions 314A and 314B, electrically insulating spacer 402B is disposed between first side portions 314B and 314C, electrically insulating spacer 402C is disposed between first side portions 314C and 314D, and electrically insulating spacer 402D is disposed between first side portions 314D and 314E. Further, an electrically insulating spacer 404A is disposed between second side portions 316A and 316B, an electrically insulating spacer 404B is disposed between second side portions 316B and 316C, an electrically insulating spacer 404C is disposed between second side portions 316C and 316D, and an electrically insulating spacer 404D is disposed between second side portions 316D and 316E.

In certain embodiments, the electrically insulating spacers 402, 404 may include one or more protrusions (not shown) to help improve the grip (grip) of the electrically insulating spacers 402, 404 with one or more of the first electrically insulating winding shell 304, the second electrically insulating winding shell 306, and the electrically insulating coil-side spacer 308. For example, electrically insulating spacer 402 may include a protrusion on one or more of a top surface and a bottom surface of electrically insulating spacer 402 that face electrically insulating coil-side spacer 308 and first electrically insulating winding housing 304, respectively. Additionally, for example, electrically insulating spacer 404 may include a protrusion on one or more of a top surface and a bottom surface of electrically insulating spacer 404 that face second electrically insulating winding housing 306 and electrically insulating coil-side spacer 308, respectively.

Further, in some embodiments, one or more of the electrically insulating spacers 402, 404 may include at least one cooling channel configured to facilitate a cooling fluid flowing therethrough to facilitate cooling of the armature windings 302. For example, in the embodiment of fig. 4, each of the electrically insulating spacers 402, 404 is shown to include one cooling channel 406 therein. The cooling channels 406 may extend along the length of the respective electrically insulating spacers 402, 404. In certain other embodiments, at least one cooling channel may be formed on a sidewall of one or more of the electrically insulating spacers 402, 404 (see fig. 5).

Referring now to fig. 5, a cross-sectional view 500 of portion 3 of armature 204 used in superconducting electrical generator 200 of fig. 2 is provided, according to yet another embodiment of the present description. For example, in the embodiment of fig. 5, each of the electrically insulating spacers 402, 404 is shown to include a plurality of cooling channels 502 on its sidewalls 504, 506. The cooling channels 502 may extend along the length of the respective electrically insulating spacers 402, 404. During operation of the superconducting generator 200, a cooling fluid may be passed through such cooling channels 406, 502 to facilitate cooling of the armature 204. It will be appreciated that the internal flow cooling channels 406 may support any type of gaseous or condensed cooling fluid, such as air or a glycol-water mixture. In certain embodiments, because the cooling channels 502 are in close proximity to the coils 312, the cooling channels 502 may be used to facilitate the flow of a gaseous cooling fluid.

Furthermore, in the embodiment of fig. 3-5, a set of armature windings 302, electrically insulated coil side spacers 308, and a second electrically insulated winding housing 306 are shown disposed between the first electrically insulated winding housing 304 and the shield 311. However, in some other embodiments, two or more such groups of armature winding 302, electrically insulated coil side separator 308, and second electrically insulated winding housing 306 may be disposed between first electrically insulated winding housing 304 and shield 311 to produce a winding having more than two layers without limiting the scope of the present description.

In the embodiments of fig. 3-5 and 11A-11G, the armature windings 302 are shown arranged in a double stacked distribution configuration. However, without limiting the scope of this description, the armature windings 302 may be arranged in various other configurations including, but not limited to, a multilayer winding, an integer slot chord winding, a fractional pitch coil winding, a full pitch coil winding, a single layer winding such as a half-coil concentric winding or a full-coil concentric winding (see fig. 6), a soft winding, a fractional slot concentrated winding, a distributed winding, a spiral winding, or combinations thereof. Further, the armature winding 302 may be a single phase winding or a multi-phase winding, such as a three-phase winding. Referring now to fig. 6, a cross-sectional view 600 of portion 3 of armature 204 for use in the superconducting electrical generator of fig. 2 is provided, according to yet another embodiment of the present description. According to the embodiment of fig. 6, the armature 204 may include an armature winding 602 having coils 604A, 604B, 604C, 604D, and 604E. These coils 604A, 604B, 604C, 604D, and 604E are single layer coils, as shown in fig. 6. The coils 604A, 604B, 604C, 604D, and 604E are disposed between the first electrically insulated winding housing 304 and the second electrically insulated winding housing 306. The armature winding 602 may be a single phase winding or a multi-phase winding, such as a three-phase winding.

Although not shown in fig. 6, in some embodiments, it is also contemplated to use electrically insulating spacers, such as electrically insulating spacer 402, between adjacent ones of coils 604A, 604B, 604C, 604D, and 604E. Additionally, the electrically insulating spacers disposed between adjacent ones of the coils 604A, 604B, 604C, 604D, and 604E may further include at least one cooling channel, such as cooling channel 406 or 502, to facilitate the flow of a cooling fluid therethrough to facilitate cooling of the armature winding 602.

To facilitate enhanced cooling of the armature 204, in some embodiments, the cooling channels 406, 502 may include certain surface features. For example, fig. 7 shows a schematic diagram 700 depicting a portion of an inner surface 702 of a cooling channel 406, 502 including such surface features 704 according to one embodiment of the present description. For example, the surface features 704 as shown in fig. 7 are formed in the shape of dimples (dimples). It should be noted that surface features, such as one or more fins, one or more bumps (bump), one or more ridges, may also be formed in the inner surface of the cooling passages 406, 502 without limiting the scope of the present description. Advantageously, these surface features 704 increase the surface area of the cooling channels 406, 502 for contact with cooling fluid flowing through the cooling channels 406, 502, thereby enhancing cooling of the armature 204.

Referring now to fig. 8, a schematic diagram of a cooling manifold 800 that may be connected to the armature of fig. 5 is presented, according to one embodiment of the present description. A cooling manifold 800 may be attached to the armature 204 to supply cooling fluid to the cooling channels 502. When passing through the cooling channels 502, the cooling fluid absorbs heat from the armature windings 302. In some embodiments, the cooling manifold 800 may also provide a return path for such heated cooling fluid.

As depicted in fig. 8, the cooling manifold 800 may include one or more conduits, such as conduits 802, 804, and a distributor 806 including one or more outlets 808. The distributor 806 may be configured to divide the cooling fluid received from the conduits 802, 804 into one or more streams of cooling fluid, with one stream being supplied to each of the one or more outlets 808. In some embodiments, the cooling manifold 800 may be designed to have a number of outlets 808 equal to the number of cooling channels 502 of one of the electrically insulating spacers 402, 404.

In some embodiments, the conduits 802 and 804 may be used to supply cooling fluid through a distributor 806 and outlet 808 on one end of the armature 204. On the other end of the armature 204, other cooling manifolds similar to the cooling manifold 800 may be coupled to where conduits 802 and 804 may facilitate collection of cooling fluid via the cooling channels 406 or 502. Alternatively, in certain embodiments, it may not be necessary to collect cooling fluid, in which case cooling manifold 800 need only supply cooling fluid to cooling channels 406 or 502.

In some embodiments, a plurality of such cooling manifolds 800 may be connected to the armature 204. For example, one cooling manifold 800 may be connected to each of the electrically insulating spacers 402, 404 of fig. 5. In some other embodiments, the cooling channels 502 in the armature 204 may be fluidly connected to each other. In this configuration of the armature 204, the cooling manifold 800 may be fluidly coupled to the cooling channel 502 of one of the electrically insulating spacers 402, 404.

Fig. 9 is a perspective view 900 of a portion of an armature 902 according to one embodiment of the present description. As depicted in fig. 9, the armature 902 may have a configuration similar to that depicted in any of fig. 3-5. Additionally, the armature 902 may include a reservoir 904, an inflation system 906, a pressure sensor 908, and a pressure relief valve 910.

The receptacle 904 may be arranged such that the armature windings 302 are at least partially enclosed by the receptacle 904. The container 904 may provide a pressure-tight seal around at least the end portions 318, 320 of the coils 312 of the armature winding 302. In some embodiments, the container 904 may include a first container half 912 and a second container half 914. The first container half 912 may be configured such that the end portion 318 of the coil 312 is enclosed by the first container half 912. Further, the second half 914 may be arranged such that the end portion 320 of the coil 312 is enclosed by the second half 914.

The inflation system 906 may be fluidly coupled to the reservoir 904 and configured to supply pressurized fluid to the armature windings 302. Non-limiting examples of pressurized fluids may include air, helium (He), neon (Ne), argon (Ar), hydrogen (H)₂) Nitrogen (N)₂) Sulfur hexafluoride (SF6), or combinations thereof. For example, the inflation system 906 may include a pump (not shown) or a compressor (not shown) to generate the pressurized fluid to be supplied to the container 904. As will be appreciated, due to the surrounding armature winding 302The voltage capability of the armature winding 302 may be increased in the presence of the pressurized fluid. As a result, the armature winding 302 may operate at an increased voltage as compared to an armature without such an arrangement of the vessel 904 and the plenum system 906.

Further, in certain embodiments, a pressure sensor 908 may be fluidly coupled to the vessel 904 to sense the pressure of the pressurized fluid within the vessel 904. The information about the sensed pressure may be used by a controller (not shown) associated with the superconducting generator 200 to increase the voltage level of the armature winding 302 corresponding to the sensed pressure. Furthermore, supplying pressurized fluid to the reservoir 904 may also advantageously cool the armature 902 and/or increase the efficiency of a superconducting generator using such an armature 902. In certain embodiments, the pressure relief valve 910 may be operable to limit the pressure of the pressurized fluid within the vessel 904 to the threshold fluid pressure value 904. For example, when the pressure of the pressurized fluid reaches above a threshold fluid pressure value, the pressure relief valve 910 may be activated to relieve the pressure of the pressurized fluid within the container 904. For example, the threshold fluid pressure value may be less than or equal to a safe operating pressure that the container 904 may withstand.

Fig. 10 is a flow diagram 1000 of a method for assembling the armature depicted in any of fig. 3-5 in accordance with one embodiment of the present description. Fig. 11A-11G depict the structure of the armature in corresponding steps of the flowchart 1000 of fig. 10. Thus, the flowchart 1000 of fig. 10 is described in conjunction with the structures depicted in fig. 11A-11G. It should be noted that for simplicity of illustration, the method of fig. 10 and the structure depicted in fig. 11A-11G are described with reference to a portion of the armature 204. Further, depending on the configuration of the cooling channels in the electrically insulating spacers 402, 404, the method of fig. 10 may be performed to form an armature 204 having the configuration depicted in either of fig. 4 or 5. For simplicity of explanation, the same reference numerals as used in fig. 4 are used in fig. 11A to 11G.

At step 1002, a base 310 is provided. For example, the base 310 (see fig. 11A) may have a cylindrical shape. In FIG. 11A, a portion 1100 of the base 310 is depicted. Non-limiting examples of materials used to form the base 310 may include fiber reinforced polymers, such as G-10. In some embodiments, the base 310 may be formed by machining a solid block of material. In some other embodiments, the base 310 may be formed by stacking a plurality of laminates, such as the laminate forming the shield 311. Further, as indicated by step 1004, the first electrically insulated winding housing 304 may be disposed on the base 310. For example, at step 1004, a structure 1102 as depicted in FIG. 11B may be obtained. In some embodiments, the first electrically insulated winding housing 304 in the form of a sheet of material may be wound on the base 310, as depicted in fig. 11B. As will be appreciated, the first electrically insulated winding housing 304 need not be limited to a tube having a constant radius. In some embodiments, the radius of the first electrically insulated winding housing 304 is adjustable along the length of the armature 204 to support the end portions 318, 320 of the coil 312.

Further, at step 1006, the armature winding 302 is disposed on the first electrically insulated winding housing 304, wherein the armature winding 302 includes a plurality of coils 312 having a first side portion 314 and a second side portion 316. More particularly, the coil 312 may be arranged such that a first side portion 314 of the coil 312 may be secured to the first electrically insulated winding housing 304. Optionally, in some embodiments, at step 1007, a plurality of first electrically insulating spacers, such as electrically insulating spacers 402, may be disposed such that at least one first electrically insulating spacer 402 of the plurality of first electrically insulating spacers 402 is disposed between adjacent first side portions 314 of the plurality of coils 312. For example, at step 1007, a structure 1104 as depicted in fig. 11C may be obtained. In some embodiments, the coils 312 and electrically insulating spacers 402 are arranged alternately. Electrically insulating spacers 402 may be formed using techniques including, but not limited to, extrusion, pultrusion, machining, stamping, water jet cutting, or additive manufacturing. Electrically insulating spacers 402 serve to properly space the first side portion 314 around the periphery of the armature 204. In one embodiment, electrically insulating spacer 402 may include cooling channels 406. In another embodiment, electrically insulating spacer 402 may include cooling channels 502. In yet another embodiment, the electrically insulating spacers 402 may extend beyond the straight sections (e.g., side portions 314, 316) of the coil 312 and into the end portions 318, 320 of the coil 312 to facilitate the flow of cooling fluid along the longer sections of the coil 312.

Further, at step 1008, an electrically insulative coil-side separator 308 may be disposed between the first and second side portions 314, 316 of the coil 312. Thus, at step 1008, the structure 1106 depicted in FIG. 11D may be obtained. Since each coil 312 is closed, the electrically insulating coil-side separator 308 may be inserted as a sheet pulled through each coil 312. The ends of the sheets may overlap to provide sufficient insulation integrity. The electrically insulating coil-side separator 308 is configured to maintain a spacing between the first side portion 314 and the second side portion 316 of the coil 312 such that they do not physically contact. Additionally, in some embodiments, the axial length of the electrically insulated coil side separator 308 may be selected such that the electrically insulated coil side separator 308 reaches the end portions 318, 320 of the coil 312. Further, the electrically insulated coil side separator 308 may act as a flow separator for separating the air flow inside the armature. The split flow results in more efficient cooling of the end portions 318, 320 of the coil 312. In some embodiments, the electrically insulated coil-side separator 308 may be designed to follow (follow) the coil 312 around the end portions 318, 320 as the end portions 318, 320 loop through a circular spiral at the axial extent (extend) of the respective coil 312, thereby creating a contoured (contoured) baffle for directing a cooling fluid, such as air. In such a configuration, the electrically insulative coil-side spacer 308 may have a shape similar to a teardrop shape when viewed in an r-z cross-section (not shown).

Additionally, at step 1010, optionally, a plurality of second electrically insulating spacers, such as electrically insulating spacers 404, are disposed such that at least one second electrically insulating spacer 404 is disposed between adjacent second side portions 316 of the plurality of coils 312. Electrically insulating spacers 404 may be formed using techniques including, but not limited to, extrusion, pultrusion, machining, stamping, cutting with water jets, or additive manufacturing. The electrically insulating spacers 404 serve to properly space the first side portion 314 (depicted in fig. 4 or 5) around the periphery of the armature so that a structure 1108 as depicted in fig. 11E may be obtained at step 1010. In one embodiment, the electrically insulating spacer 404 may include cooling channels 406. In another embodiment, the electrically insulating spacer 404 may include cooling channels 502. In yet another embodiment, the electrically insulating spacers 404 may extend into the end portions 318, 320 of the coil 312 to facilitate cooling fluid flow over a longer length along the coil 312.

Further, at step 1012, a second electrically insulated winding housing 306 may be disposed on the second side portion 316 of the coil 312. In particular, the second electrically insulated winding housing 306 may be disposed on the resulting structure 1108 of fig. 11E. In some embodiments, the second electrically insulated winding housing 306 may be wound on the structure 1108 to obtain the structure 1110, as depicted in fig. 11F. As will be appreciated, the second electrically insulated winding housing 306 need not be limited to a tube having a constant radius. In some embodiments, the radius of the second electrically insulated winding housing 306 may be adjusted along the length of the armature 204 to support the end portions 318, 320 of the coil 312.

In some embodiments, when a sheet of composite fibers is used as the first electrically insulated winding shell 304, the second electrically insulated winding shell 306, and the electrically insulated coil side spacer 308, the resulting armature structure may be impregnated with a suitable resin and then cured to form a solid structure of the armature 204. Such composite fiber sheets may be pre-tackified with a determined amount of resin to give the armature 204 improved structural stability and to facilitate armature assembly. In certain embodiments, a silicone rubber packing may be used to retain the cooling channels 406, 502. The silicone rubber filler may be removed after the armature 204 is cured.

In some other embodiments, sheets pre-impregnated with resin may be used as the first electrically insulated winding housing 304, the second electrically insulated winding housing 306, and the electrically insulated coil side separator 308. When sheets pre-impregnated with resin are used, the resulting armature 204 may be heated to cure the resin, thereby bonding the elements of the armature 204 together. In certain embodiments, once the electrically insulated coil side separator 308 is disposed, one or more slots are cut into the electrically insulated coil side separator 308. The coil 312 is then inserted into the slot. After the coil 312 is inserted, the slot may be sealed.

Further optionally, at step 1014, a shield 311 is disposed on the second electrically insulated winding housing 306. For example, a passive shield is disposed around structure 1110 to obtain structure 1112 as depicted in fig. 11G. Advantageously, the use of the shield 311 improves the electromagnetic performance of the superconducting electrical generator 200 using the armature 204. The shield 311 may be formed using a ferromagnetic material. In some embodiments, the shield 311 may be formed by stacking a plurality of laminations around the second electrically insulated winding housing 306.

In some embodiments, in the method of fig. 10, if steps 1007 and 1010 are omitted, the method of fig. 10 may result in forming an armature similar to armature 300 of fig. 3.

According to embodiments described herein, an improved wind turbine, such as wind turbine 100, and an improved superconducting generator, such as superconducting generators 114, 200, are provided. According to some embodiments herein, improvements in the wind turbine 100 and the superconducting generators 114, 200 may be realized at least in part due to the enhanced configuration of the armature 204.

As previously noted, the armature 204 includes various elements, such as first and second electrically insulated winding housings 304, 306, electrically insulated coil-side spacers 308, and electrically insulated spacers 314, 316, which are formed using non-ferromagnetic and electrically insulating materials. In addition, the armature 204 does not include ferromagnetic teeth. Advantageously, the absence of ferromagnetic material near the armature winding 312 reduces the insulation requirements of the armature winding 312. Furthermore, by using electrically insulating spacers 314, 316, the space between adjacent armature windings 312 is better utilized for structural support, insulation, and cooling without detracting from the magnetic operation of the armature windings. Further, due to the use of non-ferromagnetic and electrically insulating materials, the armature winding 312 may operate at the increased magnetic field generated by the superconducting field winding 208. Additionally, using electrically insulating spacers 314, 316 instead of ferromagnetic teeth reduces the harmonic spectrum of the magnetic field in the air gap between the stationary generator field 202 and the armature 204.

This written description uses examples to disclose the invention, including the preferred embodiments, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims. Aspects of the various embodiments described, as well as other known equivalents for each such aspect, may be mixed and matched by one of ordinary skill in this art to construct additional embodiments and techniques in accordance with principles of this application.