A rotating electrical machine, such as an aircraft starter-generator, that may be operated in either a DC motor mode or an AC generator mode. The machine includes a conventionally wound main stator that is selectively configurable as a multi-pole AC stator and a multi-pole DC stator. The machine al
A rotating electrical machine, such as an aircraft starter-generator, that may be operated in either a DC motor mode or an AC generator mode. The machine includes a conventionally wound main stator that is selectively configurable as a multi-pole AC stator and a multi-pole DC stator. The machine also includes rotor windings that are configured to be selectively coupled to either an exciter or a plurality of commutator segments, and DC brushes that are selectively moveable into, and out of, electrical contact with the commutator segments, to thereby electrically couple and decouple a DC power source to and from, respectively, the rotor windings.
대표청구항▼
We claim: 1. A gas turbine engine starter-generator, comprising: a housing; a main rotor rotationally mounted within the housing; and a main stator mounted within the housing and at least partially surrounding at least a portion of the main rotor, the main stator selectively configurable as an M-po
We claim: 1. A gas turbine engine starter-generator, comprising: a housing; a main rotor rotationally mounted within the housing; and a main stator mounted within the housing and at least partially surrounding at least a portion of the main rotor, the main stator selectively configurable as an M-pole AC stator or an N-pole DC stator, M and N each integers greater than one, wherein: when the main stator is configured as the M-pole, multi-phase AC stator, each phase consists of two or more stator winding circuits electrically coupled in parallel with one another, and when the main stator is configured as the N-pole DC stator, the stator winding circuits associated with each phase are directly connected in series with one another. 2. The starter-generator of claim 1, further comprising: a control circuit electrically coupled to at least the main stator and operable to selectively configure the main stator as the M-pole AC stator or the N-pole DC stator. 3. The starter-generator of claim 2, further comprising: a plurality of windings wound on at least a portion of the main stator; and a plurality of stator switches electrically coupled between selected ones of the main stator windings, each of the stator switches having at least a first position and a second position, wherein the main stator is configured as the M-pole AC stator with the plurality of switches in the first position, and is configured as the N-pole DC stator with plurality of switches in the second position. 4. The starter-generator of claim 3, wherein the control circuit comprises: switch control circuitry operable to move the plurality of switches between at least the first position and the second position. 5. The starter-generator of claim 1, further comprising: an exciter rotor rotationally mounted in the housing, the exciter rotor having a plurality of windings wound thereon; an exciter stator having a plurality of windings wound thereon, the exciter stator mounted within the housing and located at least partially around at least a portion of the exciter rotor; and one or more rectifier assemblies electrically coupled in series between the exciter rotor windings and the main rotor windings. 6. The starter-generator of claim 5, further comprising: a plurality of main rotor windings wound on at least a portion of the main rotor, each of the main rotor windings adapted to selectively receive DC current from either the rectifier assemblies or a DC power source. 7. The starter-generator of claim 6, further comprising: at least two brushes adapted to electrically couple to the DC power source and selectively moveable into, and out of, electrical contact with at least a portion of the main rotor, whereby the brushes are electrically coupled to, and decoupled from, respectively, the main rotor windings. 8. The starter generator of claim 1, further comprising: a DC power source electrically coupled in series with the main stator when the main stator is configured as an N-pole DC stator. 9. The starter-generator of claim 1, wherein M is unequal to N. 10. The starter-generator of claim 9, wherein N=(M/2). 11. A stator, comprising: a main stator body; a plurality of stator coils wound around at least a portion of the main body in a configuration that allows the stator to be selectively configured as an M-pole AC stator or an N-pole DC stator, M and N each integers greater than one, wherein: when the stator is configured as the M-pole AC stator, each phase consists of two or more stator winding circuits electrically coupled in parallel with one another, and when the stator is configured as the N-pole DC stator, the stator winding circuits associated with each phase are directly connected in series with one another. 12. The stator of claim 11, further comprising: a plurality of stator switches electrically coupled between selected ones of the stator coils, each of the stator switches having at least a first position and a second position. 13. The stator of claim 12, wherein the stator is configured as the M-pole AC stator with the stator switches in the first position, and is configured as the N-pole DC stator with the stator switches in the second position. 14. The stator of claim 11, wherein M is unequal to N. 15. The stator of claim 14, wherein N=(M/2).
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (24)
Shekhawat Sampat (Monmouth NJ) Tumpey John J. (Monmouth NJ) Widdis James C. (Monmouth NJ), Aircraft engine electric start system without a separate exciter field inverter.
Glennon Timothy F. (Rockford IL) Mehl Byron R. (Belvidere IL) Thollot Pierre (Rockford IL) Krinickas Alexander (Rockford IL), Brushless generator having AC excitation in generating and starting modes.
Carr Kenneth R. (Redmond WA) Shippling James A. (Rockford IL) Weber Leland E. (Rockford IL) McArthur Malcolm J. (Rockford IL), Controlled starting method for a gas turbine engine.
Xu,Mingzhou; Chen,Wei; Duddeck,Michael W.; Pearson,Wayne T.; Scherzinger,William M., Gas turbine engine starter generator that selectively changes the number of rotor poles.
Xu, Mingzhou; Pearson, Wayne T.; Yao, Yuan; Lengel, Jim; Anghel, Cristian E., Gas turbine engine starter-generator exciter starting system and method including a capacitance circuit element.
Scott Harold C. ; Bednorz Ardel R. ; Johnson G. Weylin ; Anderson William J ; Davis Mitchell K. ; Tally Henry, Light weight rotor and stator with multiple coil windings in thermal contact.
Scott Harold C. ; Bednorz Ardel R. ; Johnson G. Weylin ; Anderson William J ; Davis Mitchell K. ; Tally Henry ; Pandya Kandarp I., Light weight rotor and stator with multiple coil windings in thermal contact.
Cameron Scott W. (Milpitas CA), Method and apparatus for starting a sensorless polyphase DC motor in dual-coil mode and switching to single coil mode at.
Couture Pierre (Boucherville CAX) Francoeur Bruno (Beloeil CAX) Lambert Ghislain (Beloeil CAX), Method and apparatus for starting up a synchronous machine.
Rozman Gregory I. (Rockford IL) Markunas Albert L. (Roscoe IL) Nuechterlein Paul E. (Rockford IL), Starter/generator system with variable-frequency exciter control.
Xu, Mingzhou; Chen, Wei; Pearson, Wayne T.; Scherzinger, William M.; Duddek, Michael W., Gas turbine engine starter generator with AC generator and DC motor modes.
Nakagawa,Masanori; Endou,Masahiko; Shinba,Kaoru; Yamamoto,Katsumi; Sugisawa,Yoshihiro, Inverter controlled generator set and method for controlling the same.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.