Apparatus for a high speed sleeveless rotor
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0846980
(2010-07-30)
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등록번호 |
US-8232702
(2012-07-31)
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발명자
/ 주소 |
- Zywot, Jan
- Jia, Xiaochuan
- Austin, Norman K.
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출원인 / 주소 |
|
대리인 / 주소 |
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인용정보 |
피인용 횟수 :
4 인용 특허 :
9 |
초록
▼
A high-speed sleeveless rotor for an electric machine is provided. The rotor includes a shaft rotatable about a longitudinal axis, and a rotor core circumscribing at least a portion of the shaft wherein the rotor core includes an axially oriented slot. The slot includes a radially outer slot opening
A high-speed sleeveless rotor for an electric machine is provided. The rotor includes a shaft rotatable about a longitudinal axis, and a rotor core circumscribing at least a portion of the shaft wherein the rotor core includes an axially oriented slot. The slot includes a radially outer slot opening, a radially inner slot floor, and a slot sidewall extending therebetween. The slot floor includes a topstick attachment member extending radially outward from the slot floor and configured to engage a topstick positioned in the slot opening and the slot sidewall includes a shoulder configured to engage the topstick, preventing radially outward movement of the topstick.
대표청구항
▼
1. A high-speed sleeveless rotor for an electric machine, said rotor comprising: a shaft rotatable about a longitudinal axis; anda rotor core circumscribing at least a portion of said shaft, said rotor core comprising an axially oriented slot, said slot comprising a radially outer slot opening, a ra
1. A high-speed sleeveless rotor for an electric machine, said rotor comprising: a shaft rotatable about a longitudinal axis; anda rotor core circumscribing at least a portion of said shaft, said rotor core comprising an axially oriented slot, said slot comprising a radially outer slot opening, a radially inner slot floor, and a slot sidewall extending therebetween, said slot floor comprising a topstick attachment member extending radially outward from said slot floor and configured to engage a topstick positioned in said slot opening, said slot sidewall comprising a shoulder configured to engage the topstick, preventing radially outward movement of the topstick, said topstick attachment member comprising a slot configured to engage a complementarily-shaped tab in the topstick. 2. A rotor in accordance with claim 1, wherein said shaft is hollow, said rotor further comprising a cooling oil system comprising: one or more oil tubes positioned in said slot, said oil tubes configured to retain a flow of cooling oil within said oil tubes; andan oil tube connector configured to couple the one or more oil tubes in flow communication with the hollow interior of said shaft. 3. A rotor in accordance with claim 1, wherein said topstick is configured to engage said shoulder and said topstick attachment member such that centrifugal forces tending to move said topstick radially outward are opposed by said shoulder and said topstick attachment member. 4. A rotor in accordance with claim 1, further comprising one or more electrical winding sets positioned within said slot. 5. A rotor in accordance with claim 1, wherein said rotor core comprises a plurality of laminations stacked together in a face-to-face orientation. 6. A rotor in accordance with claim 1, wherein said rotor core comprises a plurality of laminations each having a substantially circular cross-section and outer peripheral edge wherein said outer peripheral edges form an outer peripheral surface of said rotor core. 7. A rotor in accordance with claim 1, wherein said topstick attachment member comprises a tab configured to engage a complementarily-shaped slot in the topstick. 8. A rotor in accordance with claim 1, further comprising a topstick wedge configured to engage said topstick attachment member and said topstick such that centrifugal forces tending to move said topstick radially outward are opposed by said topstick attachment member through said topstick wedge. 9. A high-speed sleeveless rotor for an electric machine, said rotor comprising: a plurality of laminations each having an outer peripheral edge stacked face-to-face along a rotor shaft forming a rotor core having an outer peripheral surface comprising the edges of the plurality of laminations;a plurality of axial slots spaced at a predetermined interval in the circumferential direction of the rotor core, each axial slot closed by a topstick extending at least partially along a length of the slot, each axial slot comprising:an engagement surface configured to engage a radially outer lip of the topstick;a side wall extending radially inwardly toward a slot floor; andan attachment member extending radially outward from said slot floor, said attachment member configured to engage at least one of the topstick and a topstick wedge such that centrifugal forces generated in one or more components positioned within the slot are shared between said attachment member and said engagement surface. 10. A rotor in accordance with claim 9, wherein said component comprises at least one of a field winding and an oil cooling tube. 11. A rotor in accordance with claim 9, wherein said attachment member comprises at least one of a tab configured to engage a complementarily-shaped slot in at least one of the topstick and a topstick wedge and a slot configured to engage a complementarily-shaped tab in the at least one of the topstick and the topstick wedge. 12. A rotor in accordance with claim 9, further comprising a hollow shaft, said rotor further comprising a cooling oil path comprising an oil cooling tube extending axially in said slot, a respective cooling oil connection configured to couple the oil cooling tube in flow communication with said hollow shaft. 13. A rotor in accordance with claim 12, wherein said oil cooling path is a closed path such that the one or more components outside of the cooling oil path are not in contact with oil. 14. A rotor in accordance with claim 9, wherein said topstick wedge is configured to engage said attachment member and said topstick such that centrifugal forces acting on the topstick are transferred to the attachment member through the topstick wedge. 15. A lamination for a laminated core of an electric machine, said lamination comprising a unitary planar body comprising: an outer peripheral edge;an inner peripheral edge spaced radially from said outer peripheral edge; anda plurality of openings that extend through said body from said outer peripheral edge radially inwardly such that said openings are arcuately spaced about said body, said openings each comprising a slot floor edge between said outer peripheral edge and said inner peripheral edge, said slot floor edge comprising a topstick attachment member extending radially outward therefrom and configured to engage at least one of a topstick and a topstick wedge. 16. A lamination in accordance with claim 15 wherein said outer peripheral edge comprises an outer peripheral surface of said laminated core. 17. A lamination in accordance with claim 15 wherein said opening is sized to receive at least one of a rotor winding and a cooling oil tube when said laminated core is fully assembled. 18. A lamination in accordance with claim 15 wherein said outer peripheral edge defines a substantially circular cross-section of said lamination, and said inner peripheral edge defines a bore substantially concentric with said substantially circular cross-section of said lamination. 19. A lamination in accordance with claim 15 wherein said topstick attachment member comprises at least one of a tab configured to engage a complementarily-shaped slot in the topstick and a slot configured to engage a complementarily-shaped tab in the topstick.
이 특허에 인용된 특허 (9)
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Serge Boyer FR; Regine Sutra-Orus FR; Stephane Tregine-Regent FR; Alain Tardy FR; Claude Barbier FR; Philippe Buron FR; Patrick Ribardiere FR; Marcel Louarn FR, Device for starting a gas turbine in an aircraft.
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Taneja, Dinesh N.; Huang, Hao; Padgett, Gary A.; Zywot, Jan; Wirsch, Jr., Paul J.; Abbas, Mohamed A., Dual-structured aircraft engine starter/generator.
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Franchet, Michel; Picard, Jean-Louis, Integrated starter/generator for a turbomachine.
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Anghel,Cristian E.; McGinley,Ray M., Method and apparatus for controlling an engine start system.
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Eick,Chris D.; Futa, Jr.,Paul W.; Laidlaw,Mitchell J.; Libera,Anthony C.; Purcell,Donald M., Method to control starter/generator cooling fuel flow during engine starting.
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Katagiri Masayuki,JPX ; Kobayashi Kazutaka,JPX, Motor having magnetic slot closure for salient poles.
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Glennon Timonthy F., PMG main engine starter/generator system.
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DeLuca Kenneth M. ; Poag Andrew F. ; Ketterer Charles P. ; Horst Gary E., Self-locking retaining member for use in a dynamoelectric device.
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Pittard Glenn C. ; Jacobs Scott A., Winding wedge retention to maintain coil form.
이 특허를 인용한 특허 (4)
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Huang, Hao; Karipides, David Dimitri, Aircraft engine constant frequency starter/generator.
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Krause, Joseph Paul; Patel, Dhaval; Abels, Jan Henry, Generator motor wedge with wide arm span and reduced stress levels.
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Lemmers, Jr., Glenn C., Generator/motor wedge with lamination interface for reduced stress levels.
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Kubo, Kaoru; Mizutani, Ryoji; Kato, Hiroki; Yamada, Eiji; Chinen, Shintaro; Hiramoto, Kenji; Nakai, Hideo, Rotor for rotating electrical device.
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