[특허]Double-sided starter/generator for aircrafts

General Electric Company

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""	따옴표 내의 구문과 완전히 일치하는 문서만 검색	예) "Transform and Quantization"

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Double-sided starter/generator for aircrafts

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	H02K-001/04
미국특허분류(USC)	310/112; 310/114; 310/266
출원번호	UP-0567850 (2006-12-07)
등록번호	US-7750521 (2010-07-26)
발명자 / 주소	Qu, Ronghai Kern, John M. Wu, Wei De Bedout, Juan M. Shah, Manoj R. El-Refaie, Ayman Mohamed Fawzi
출원인 / 주소	General Electric Company
대리인 / 주소	McNees Wallace & Nurick, LLC
인용정보	피인용 횟수 : 8 인용 특허 : 24

초록
▼

An electromagnetic machine for extracting power from a turbine engine includes an outer rotor and an inner rotor rotatably supported adjacent to a stator. The stator is disposed between the inner and outer rotors. The stator has an inner set of windings disposed on an inner surface adjacent to the inner rotor, and an outer set of windings on an outer surface of the stator adjacent to the outer rotor. A plurality of permanent magnets are disposed on an inner surface of the outer rotor element and on an outer surface of the inner rotor element. Air gaps are defined between the outer surface of the stator and the outer permanent magnets, and between the inner surface of the stator portion and the inner permanent magnets. The inner stator windings form a set of multiple-phase windings, and the outer stator windings form a set of multiple-phase windings.

대표
청구항
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The invention claimed is: 1. An electromagnetic machine for extracting electrical power from a gas turbine engine comprising: an outer rotor element and an inner rotor element rotatably supported adjacent to a fixed stator portion, the stator portion disposed concentrically between the inner and outer rotor elements about a central axis; opposing frame portions connected at a first end and a second end of the stator portion to support the stator portion within the gas turbine engine; the stator portion having an inner set of stator windings disposed on a radially inner surface of the stator portion adjacent to the inner rotor, and an outer set of stator windings disposed on a radially outer surface of the stator portion adjacent to the outer rotor; the inner rotor element driven by a first turbine shaft and the outer rotor element driven by a second turbine shaft of the gas turbine engine, each of the first turbine shaft and the second turbine shaft independently rotatable with respect to the other of the first turbine shaft and the second turbine shaft, the first turbine shaft and the second turbine shaft concurrently rotatable in the same or in opposite directions and controllably operable at matching velocity or at separate and distinct velocities; a plurality of outer permanent magnets disposed on an inner surface of the outer rotor element and a plurality of inner permanent magnets disposed on an outer surface of the inner rotor element; an outer air gap defined between the outer surface of the stator portion and the outer permanent magnets, and an inner air gap defined between the inner surface of the stator portion and the inner permanent magnets; the inner stator windings electrically interconnected to form a first set of multiple-phase windings and the outer stator windings electrically interconnected to form a second set of multiple-phase windings for powering an electrical load. 2. The electromagnetic machine of claim 1, wherein the stator windings disposed in slots defined between pairs of tooth portions. 3. The electromagnetic machine of claim 1, wherein the inner and outer stator windings are arranged side-by-side within the slots. 4. The electromagnetic machine of claim 1, wherein the inner and outer stator windings are toroidally-wound around the stator tooth portions. 5. The electromagnetic machine of claim 1, wherein the inner and outer stator windings are arranged at least one layer. 6. The electromagnetic machine of claim 1, wherein the inner and outer stator windings are arranged one winder to a slot. 7. The electromagnetic machine of claim 1, wherein the inner stator windings are interconnected to form one set of multiple-phase windings, and the outer stator windings are interconnected to form a second set of multiple-phase windings. 8. The electromagnetic machine of claim 1, also comprising: a plurality of converters, each of the converters connected to a set of windings to independently drive the associated phase winding. 9. The electromagnetic machine of claim 1, wherein the first turbine shaft is connected to a high pressure (HP) turbine and the second turbine shaft is connected to a low pressure (LP) turbine. 10. The electromagnetic machine of claim 1, wherein the opposing frame portions include axial openings at opposing ends of the machine, and at least two bearings for rotatably supporting the LP shaft and the HP shaft connected to the inner and outer rotor elements. 11. The electromagnetic machine of claim 1, wherein the stator portion includes a plurality of outer tooth portions defining a first set of slots therebetween, and a plurality of inner tooth portions defining a second set of slots therebetween, the outer stator windings retentively positioned within the first set of slots and the inner stator windings retentively positioned within the second set of slots. 12. The electromagnetic machine of claim 1, wherein the stator portion further comprising a lamination stack structurally reinforced through compression by a plurality of circumferentially spaced bolts arranged parallel with the axis in a yoke portion of the stator portion. 13. The electromagnetic machine of claim 12, wherein the bolt shafts and at least one bolt end being insulated from the lamination stack and frame structures by a plurality of insulator tubes and insulator rings to avoid induced electrical currents and resulting losses and heating. 14. The electromagnetic machine of claim 1, also comprising an air cavity between outer stator windings and an air cavity between the inner stator windings for air-cooling the windings. 15. A gas turbine engine comprising; a high pressure turbine and a low pressure turbine disposed in the gas turbine engine in serial flow communication, and an electrical machine arranged coaxially with the high pressure turbine and the low pressure turbine; a shaft of the high pressure turbine and a shaft of the low pressure turbine concurrently rotatable in the same or in opposite directions, and controllably operable at matching velocity or at separate and distinct velocities; the electrical machine comprising: a fixed stator element, a first rotor element and a second rotor element, the first and second rotor elements independently rotatable with respect to the stator element; the first rotor element mechanically connected with the shaft of the high pressure turbine, and the second rotor element being mechanically connected with the shaft of the low pressure turbine; the stator element having an inner multiple-phase winding set and an outer multiple-phase winding set wound thereon, each of the winding sets configured to generate separate power outputs or to receive a separate excitation power source, the inner and outer winding sets being mutually exclusive; a plurality of outer permanent magnets disposed on an inner surface of the outer rotor element and a plurality of inner permanent magnets disposed on an outer surface of the inner rotor element; an outer air gap defined between the outer surface of the stator portion and the outer permanent magnets, and an inner air gap defined between the inner surface of the stator portion and the inner permanent magnets; wherein each of the first and second rotor elements are configured to generate electrical power through electromagnetic coupling with the stator element when driven by the associated high or low pressure turbine shaft, or to electrically drive the associated high or low pressure turbine shaft when excited by an external electrical power source.

이 특허에 인용된 특허 (24)

이 특허를 인용한 특허 피인용횟수: 8

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Double-sided starter/generator for aircrafts

초록
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대표
청구항
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이 특허에 인용된 특허 (24)

이 특허를 인용한 특허 피인용횟수: 8

IPC 상위 출원인

과제정보

상세정보조회

원문조회

IPC 상세정보(version : 201201)

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특허 상세정보

Double-sided starter/generator for aircrafts

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대표청구항 ▼

이 특허에 인용된 특허 (24)

이 특허를 인용한 특허 피인용횟수: 8

IPC 상위 출원인

과제정보

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

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