ROTOR WEDGES AND METHODS OF MAKING ROTOR WEDGES

Abstract

A wedge for a wound rotor includes a wedge body. The wedge body has a first layer and one or more second layers interfused with one another to provide structural support and limit resistive heating of the wedge from current flow within the wedge body by windings spaced apart by the rotor wedge. Generator rotors and methods of making generator rotors are also described.

Claims

1. A method a making a rotor wedge for a wound rotor, comprising fusing a first layer and one or more second layers to form a wedge body.

2. The method as recited in claim 1, wherein fusing the first layer and the one or more second layers includes defining a wedge body having a longitudinal profile with a triangular shape, a stator face and an opposed apex, and first and second winding faces spanning the apex and the stator face on laterally opposite sides of wedge body wherein fusing the first and second layers includes fusing a particulate including titanium in an additive manufacturing apparatus.

3. The method as recited in claim 2, further comprising depositing an insulating layer over the first and second winding faces and the apex of the wedge body.

4. The method as recited in claim 3, further comprising coupling a heat transfer plate to the stator face of the wedge body.

5. The method as recited in claim 3, further comprising coupling a heat sink to a first longitudinal end of the wedge body.

6. The method as recited in claim 3, further comprising coupling a heat sink to a second longitudinal end of the wedge body.

7. The method as recited in claim 1, wherein the wedge body comprises titanium or titanium alloy.

8. The method as recited in claim 1, further comprising coupling a heat transfer plate to a stator face of the wedge body, extending along a longitudinal length of the wedge body.

9. The method as recited in claim 8, wherein the heat transfer plate includes a material having higher thermal conductivity than a material forming the wedge body.

10. The method as recited in claim 8, wherein the heat transfer plate includes aluminum or an aluminum alloy.

11. The method as recited in claim 1, wherein the wedge body has at least one channel extending between longitudinally opposite ends of the wedge body.

12. The method as recited in claim 11, wherein the wedge body has a major channel and a pair of minor channels, the major channel arranged laterally between the apex and the stator face of the wedge body, a first of the minor channels arranged laterally between the major channel and the first winding face, a second of the minor channels arranged laterally between the major channel and the second winding face of the wedge body.

13. The method as recited in claim 1, wherein the wedge body includes one or more cooling channels defined within the stator face and extending longitudinally along the wedge body.

14. The method as recited in claim 1, further comprising depositing an insulating layer over the winding faces and the apex of the wedge body, wherein the insulating layer extends contiguously between opposite longitudinal ends of the wedge body.

15. The method as recited in claim 14, wherein the insulating layer comprises a polymeric material.

16. The method as recited in claim 1, further comprising fixing a heat sink to a longitudinally end of the wedge body.

17. The method as recited in claim 16, wherein the heat sink includes a material having higher thermal conductivity than a material forming the wedge body.

18. The method as recited in claim 16, wherein the heat sink includes aluminum or aluminum alloy.

19. The method as recited in claim 16, wherein the heat sink includes a finned body longitudinally spaced apart from the wedge body.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0016] So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, embodiments thereof will be described in detail herein below with reference to certain figures, wherein:

[0017] FIG. 1 is a schematic view of an exemplary embodiment of an aircraft electrical system constructed in accordance with the present disclosure, showing a generator with a wound rotor;

[0018] FIG. 2 is perspective view of the wound rotor of FIG. 1, showing a rotor body with rotor wedges and windings arranged about the radial periphery of the rotor body;

[0019] FIG. 3 is a perspective view of the rotor wedge of FIG. 2, showing a wedge body having opposed longitudinal ends and a longitudinal profile;

[0020] FIG. 4 is a longitudinal end view of the rotor wedge of FIG. 2, showing the longitudinal profile and an insulating layer deposited over winding faces of the wedge body;

[0021] FIG. 5 is a longitudinal end view of the rotor wedge of FIG. 2, showing a coolant conduit defined in rotor wedge stator face and a heat transfer plate coupled to the stator face;

[0022] FIG. 6 is a perspective view of the rotor wedge of FIG. 2, showing heat sinks coupled to the rotor wedge at longitudinally opposite ends of the wedge body; and

[0023] FIGS. 7A-7E show a method of making a wound rotor for a liquid cooled synchronous machine generator, each figure schematically showing an operation of the method.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0024] Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of a wedge for a wound rotor 100 in accordance with the disclosure is shown in FIG. 2 and is designated generally by reference character 100. Other embodiments of rotor wedges, wound rotors and methods of making rotor wedges in accordance with the disclosure, or aspects thereof, are provided in FIGS. 1 and 3-7, as will be described. The systems and methods described herein can be used wound rotors, such as in generators in aircraft electrical systems, though the present disclosure is not limited to generators or to aircraft electrical systems in general.

[0025] Referring to FIG. 1, an aircraft electrical system 10 is shown. Aircraft electrical system 10 includes a generator 104, a power bus 14, and a plurality of power consuming devices 16. An engine 18, e.g., an aircraft main engine or an auxiliary power unit, is operably connected to the generator 12 and arranged to provide mechanical rotation R of a wound rotor 102 (shown in FIG. 2) of generator 12. Generator 12 is electrically connected to the plurality of power consuming devices 16 by power bus 14 and is arranged to provide electrical power P to the plurality of power consuming devices 16 through power bus 14 using mechanical rotation R received from engine 18. It is contemplated that generator 12 be a synchronous machine electrical generator that, in certain embodiments, employs a liquid coolant 405 (shown in FIG. 6) to remove heat from wound rotor 102. Although described herein as a wound rotor for a generator, it is to be understood and appreciated that other types of electrical machines can also benefit from the present disclosure, such as electric motors and starter/generators by way of non-limiting example.

[0026] With reference to FIG. 2, wound rotor 102 is shown. Wound rotor 102 is supported for rotation about a rotation axis 106 and includes a core body 108, a first winding 110, a second winding 112, and rotor wedge 100. Core body 108 is constructed from an electrical steel material 114 and has a radially outer periphery 116 and a plurality of slots 118. Slots 118 are defined within periphery 116 and extend longitudinally along an axial length of core body 108.

[0027] First winding 110 and second winding 112 are seated within a common slot 118. Rotor wedge 100 is circumferentially interposed between first winding 110 and second winding 112 to retain first winding 110 and second winding 112 within core body 108 during rotation of wound rotor 102 about rotation axis 106. Collars 121 are arranged at longitudinally opposite ends of core body 108 radially overlap rotor wedge 100. In the illustrated exemplary embodiment wound rotor 100 has four windings and four rotor wedges. As will be appreciated by those of skill in the art in view of the present disclosure wound rotor 102 can have more than four windings or fewer than four windings, as suitable for an intended application. As will also be appreciated by those of skill in the art in view of the present disclosure, wound rotor 102 can have more than four rotor wedges or fewer than four rotor wedges, as suitable for an intended application.

[0028] With reference to FIG. 3, rotor wedge 100 is shown. Rotor wedge 100 has a wedge body 122 a plurality of layers, e.g., a first layer 146 (shown in FIG. 7A) and one or more second layer 148 (shown in FIG. 7A), interfused with one another to provide structural support and limit resistive heating of windings spaced apart by wedge body 122. In the illustrated exemplary embodiment wedge body 122 has a longitudinal profile 124. Longitudinal profile 124 has a generally polygonal shape bounded by a stator face 126, the exemplary polygonal shape illustrated in FIG. 3 being triangular and having an apex 128, a first winding face 130, and a second winding face 132. Stator face 126 has a planar shape or an arcuate shape, as suitable for an intended application.

[0029] First winding face 130 and second winding face 132 extend longitudinally on laterally opposite sides of wedge body 122. Apex 128 extends longitudinally along the length of wedge body 122 and bounds first winding face 130 and second winding face 132. It is contemplated that wedge body 122 be constructed from a wedge material 134 that has electrical resistivity higher than that of aluminum such that rotor wedge 100 generates relatively little (or no) heat. In certain embodiments wedge material 134 includes titanium or a titanium alloy, thereby providing a rotor wedge that is strong, light, and does not generate heat from current flow induced by magnetic fields in proximity to rotor wedge 100, e.g., to provide structural support to and limit resistive heating of the wedge caused by current flow within the wedge body by windings spaced apart by the rotor wedge. As will be appreciated by those of skill in the art in view of the present disclosure other polygonal shapes of longitudinal profile are possible within the scope of the present disclosure.

[0030] One challenge to fabricating rotor wedges using materials like titanium and titanium alloys is the relatively high cost of titanium to cost using traditional subtractive manufacturing techniques. To overcome this problem wedge body 122 is constructed using an additive manufacturing technique where a plurality of layers, e.g., a first layer 146 (shown in FIG. 7A) and a second layer 148 (shown in FIG. 7A), are fused to one another. An example of a suitable additive manufacturing technique is rapid plasma deposition. Constructing wedge body 122 with a plurality of layers can reduce the cost of wedge body 122. In certain embodiments the cost of manufacturing wedge body 122 from titanium or titanium alloy is on the order of 25% to 50% that of fabricating wedge body 122 using a subtractive manufacturing technique. Use of an additive manufacturing technique also allows for incorporating of features in wedge body 122 that could otherwise be prohibitively expensive using subtractive manufacturing techniques, such as voids and/or hollows within wedge body 122.

[0031] For example, in the illustrated exemplary embodiment wedge body 122 has a plurality of channels defined within its interior for reducing the weight of wedge body 122. In this respect wedge body 122 has a major channel 136, a first minor channel 138, and a second minor channel 140. Major channel 136 extends longitudinally along the length of wedge body 122 between a first longitudinal end 142 and a longitudinally opposite second longitudinal end 144. Major channel 136 is arranged radially relative to rotation axis 106 (shown in FIG. 2) between apex 128 and stator face 126.

[0032] First minor channel 138 extends longitudinally along the length of wedge body 122 between first longitudinal end 142 and second longitudinal end 144, and is arranged between major channel 136 and first winding face 130. Second minor channel 140 also extends longitudinally along the length of wedge body 122 between first longitudinal end 142 and second longitudinal end 144, and is arranged between major channel 136 and second winding face 132. Although three weight reduction channels are shown in the illustrated exemplary embodiment, those of skill in the art will readily appreciate in view of the present disclosure that wedge body can have fewer than three channels or more than three channels, as suitable for an intended application. As will also be appreciated by those of skill in the art in view of the present disclosure, channels having shapes other than circular can also be defined within wedge body 122, as suitable for an intended application.

[0033] With reference to FIG. 4, a rotor wedge 200 is shown. Rotor wedge 200 is similar to rotor wedge 100 (shown in FIG. 2) and additionally includes an insulating layer 201. Insulating layer 201 includes a polymeric material 203 deposited over surfaces of wedge body 222 in abutting first winding 110 (shown in FIG. 2) and second winding 112 (shown in FIG. 2). In the illustrated exemplary embodiment insulating layer 201 is deposited over first winding face 230, apex 228, and second winding face 232 and along the longitudinal length of wedge body 222. Insulating layer 201 is not disposed over stator face 226.

[0034] It is contemplated that polymeric material have electrical insulating properties similar to polyimide, e.g., Kapton®, available from the E. I. du Pont de Nemours and Company Corporation of Wilmington, Del. Being deposited on first winding face 130 and second winding face 132, polymeric material 203 eliminates the need to incorporate insulating sheets that otherwise can be required in wound rotors between windings and rotor wedges, simplifying assembly wound rotor 202. Examples of suitable polymeric materials include polyether ether ketone (PEEK), available from Victrex PLC of Lancashire, United Kingdom.

[0035] With reference to FIG. 5, a rotor wedge 300 is shown. Rotor wedge 300 is similar to rotor wedge 100 (shown in FIG. 2) and additionally includes a heat transfer plate 301. Heat transfer plate 301 is coupled to stator face 326 of wedge body 322, extends, longitudinally along the length of wedge body 322, and includes a plate material 303. Plate material 303 has thermal conductivity that is higher than the thermal conductivity of wedge material 334. This allows for heat generated an air gap 305 defined between rotor wedge 300 and a stator 307 to transfer into heat transfer plate 301, and therethrough to longitudinally opposite ends of rotor wedge 300 for removal. It is contemplated that plate material 303 have electrical conductivity and/or magnetic permeability that is greater than that of wedge material 334. In certain embodiments plate material 303 includes aluminum or an aluminum alloy. In accordance with certain embodiments wedge material 334 can include titanium or a titanium alloy directly coupled to heat transfer plate 301 at stator face 326.

[0036] As also shown in FIG. 5, rotor wedge 300 can have one or more coolant conduit 309 defined within wedge body 322. The one or more coolant conduit 309 is arranged to convey a coolant fluid longitudinally along the length of rotor wedge 300 to remove heat generated by windage across heat transfer plate 301. In the illustrated exemplary embodiment the one or more coolant conduit 309 is defined within stator face 326 and is bounded by heat transfer plate 301 at a radially outer portion of wedge body 322. As will be appreciated by those of skill in the art, arranging the one or more coolant conduit 309 allows for removal of heat from heat transfer plate 301 directly, without the need to communicate the heat through wedge material 334.

[0037] With reference to FIG. 6, a rotor wedge 400 is shown. Rotor wedge 400 is similar to rotor wedge 100 (shown in FIG. 2) and additional includes a heat sink 401. Heat sink 401 has a plurality of fins 403 arranged to receive a coolant flow 405 to transfer heat from rotor wedge 400 and is coupled to first longitudinal end 442. It is contemplated that heat sink 401 be constructed from a heat sink material 407 having thermal conductivity that is higher than the thermal conductivity of wedge material 434 forming wedge body 422. In the illustrated exemplary embodiment heat sink 401 is a first heat sink and rotor wedge 400 includes a second heat sink 409. Second heat sink 409 is coupled to second longitudinal end 444 and on an end of wedge body 422 opposite first heat sink 401. In accordance with certain embodiments, a heat transfer plate 411 can couple first heat sink 401 to second heat sink 409, first heat sink 401 and second heat sink 409 in turn both being coupled to wedge body 422 through heat transfer plate 411.

[0038] Referring now to FIGS. 7A-7E, a method of making a rotor wedge for wound rotor is shown. As shown in FIG. 7A, method includes fusing 510 a first layer 146 to a second layer 148 to form wedge body 122. It is contemplated that first layer 146 be proximate to first longitudinal end 142, second layer 148 be proximate to second longitudinal end 144 and arranged on a side of first layer 146 opposite first longitudinal end 142, and that successive layers thereafter be fused to second layer 148. Via an additive manufacturing technique, wedge body 122 is constructed layerwise in the longitudinal direction. Each layer can include titanium or titanium alloy 504 fused using an additive manufacturing technique. Examples of suitable additive manufacturing techniques include rapid plasma deposition (RPD) process tool 502. Exemplary RPD processes include those employing RPD process tools such as the MERKE IV RPD workstation, available from Norsk Titanium AS of Honefoss, Norway.

[0039] Once wedge body 122 is formed heat transfer plate 303 can be coupled to stator face 126 of wedge body 122 in a coupling operation 520, as shown in FIG. 7B. Coupling can be accomplished, for example, utilizing a friction stir welding operation 522 coupling the aluminum forming heat transfer plate 303 to the titanium forming wedge body 122. Although a friction stir welding operation is shown it is to be understood and appreciated that other welding techniques may also be employed.

[0040] Insulating layer 201 is then deposited in a deposition operation 530 over wedge body 122, as shown in FIG. 7C. Deposition of insulating layer 201 can be through a VICOTE™ deposition process tool 532 such as those available from Victrex PLC of Lancashire, United Kingdom. It is contemplated that insulating layer be deposited over first winding face 130, second winding face 132, and apex 128 of wedge body 122. As will be appreciated by those of skill in the art in view of the present disclosure, performing deposition operation 530 subsequent to coupling operation 520 prevents the heat associated with welding operation 522 from disturbing insulating layer 201.

[0041] First heat sink 401 and second heat sink 409 can be coupled to longitudinally opposite first end 442 and second end 444 in a heat sink assembly operation 540 as shown in FIG. 7D. Heat sink operation 540 can occur prior to deposition operation 530 or after deposition operation 530, as operationally suitable. Once assembly of rotor wedge 100 is complete rotor wedge 100 can be seated in core body 108 within common slot 118 and between first winding 110 and second winding 112 in a wound rotor assembly operation 550, as shown in FIG. 7E.

[0042] The methods and systems of the present disclosure, as described above and shown in the drawings, provide for rotor wedges with superior properties including good structural strength, relatively low heat generation, and good heat transfer capability for removing heat generated from windage losses. In certain embodiments, wedges described herein have integrated heat conduction structures, simplifying assembly of generator rotors employing the wedges. In accordance with certain embodiments, wedges described herein have integrated insulation, simplifying assembly of generator rotors employing the wedges. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that change and/or modifications may be made thereto without departing from the scope of the subject disclosure.