IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0330591
(2008-12-09)
|
등록번호 |
US-8237416
(2012-08-07)
|
발명자
/ 주소 |
- Rozman, Gregory I.
- Roy, Kevin P.
|
출원인 / 주소 |
- Hamilton Sundstrand Corporation
|
대리인 / 주소 |
Carlson, Gaskey & Olds, PC
|
인용정보 |
피인용 횟수 :
7 인용 특허 :
20 |
초록
▼
A generator and associated power supply system has a prime mover for driving a shaft to rotate. A pair of permanent magnets is associated with the rotating shaft. A first stator winding is associated with a first of said permanent magnets, with a customer DC bus for providing a first relatively low
A generator and associated power supply system has a prime mover for driving a shaft to rotate. A pair of permanent magnets is associated with the rotating shaft. A first stator winding is associated with a first of said permanent magnets, with a customer DC bus for providing a first relatively low voltage to the customer DC bus. A second of said permanent magnets is associated with a second stator winding, and an engine accessory DC bus. The engine accessory DC bus provides power to a motor controller and associated accessory motors associated with the prime mover. The engine accessory DC bus is provided with a second relatively high voltage from the second stator winding.
대표청구항
▼
1. A generator and associated power supply system comprising: a prime mover for driving a shaft to rotate;at least a pair of permanent magnets associated with said shaft;a first stator winding set associated with a first of said permanent magnets, said first stator winding set associated with a cust
1. A generator and associated power supply system comprising: a prime mover for driving a shaft to rotate;at least a pair of permanent magnets associated with said shaft;a first stator winding set associated with a first of said permanent magnets, said first stator winding set associated with a customer DC bus, and providing a first voltage to said customer DC bus, said first winding set including a three-phase stator winding and a control winding; anda second of said permanent magnets being associated with a second stator winding set, and communicating with an engine accessory DC bus, said engine accessory DC bus providing power to a motor controller and an associated motor for an accessory associated with said prime mover, said engine accessory DC bus being provided with a second voltage from said second stator winding set, said second stator winding set including a three-phase stator winding and a control winding, and said second voltage being higher than said first voltage; andsaid engine accessory bus communicates with a plurality of motor controllers and a plurality of motors, and said plurality of motors includes at least a fuel and oil pump motor for said prime mover. 2. The system as set forth in claim 1, wherein said prime mover is a gas turbine engine. 3. The system as set forth in claim 1, wherein said customer DC bus is associated with components on an airplane. 4. The system as set forth in claim 1, wherein both of said winding sets ultimately communicate with a bi-directional DC/DC converter. 5. The system as set forth in claim 1, wherein said first voltage is on the order of 28 volts and said second voltage is over 100 volts. 6. The system as set forth in claim 5, wherein said second voltage is on the order of 270 volts. 7. The system as set forth in claim 6, wherein said first voltage is 28 volts and said second voltage is 270 volts. 8. The system as set forth in claim 1, wherein a current sensor provides a sensed current to a regulator, and said regulator communicating with said control winding in each of said first and second winding sets. 9. A generator and associated power supply system comprising: a prime mover for driving a shaft to rotate;at least a pair of permanent magnets associated with said shaft;a first stator winding associated with a first of said permanent magnets, said first stator winding associated with a customer DC bus, and providing a first voltage to said customer DC bus;a second of said permanent magnets being associated with a second stator winding, and communicating with an engine accessory DC bus, said engine accessory DC bus providing power to a motor controller and an associated motor for an accessory associated with said prime mover, said engine accessory DC bus being provided with a second voltage from said second stator winding, said second voltage being higher than said first voltage;both of said windings ultimately communicating with a bi-directional DC/DC converter; andsaid bi-directional DC/DC converter, allows the power from said first stator winding to be also directed to said engine accessory DC bus, and allows the power from said second stator winding to be selectively sent to said customer DC bus, as necessary. 10. The system as set forth in claim 9, wherein said engine accessory bus communicates with a plurality of motor controllers and a plurality of motors. 11. The system as set forth in claim 10, wherein said plurality of motors include at least a fuel and oil pump motor for said prime mover. 12. The system as set forth in claim 9, wherein said first voltage is on the order of 28 volts and said second voltage is over 100 volts. 13. The system as set forth in claim 12, wherein said first voltage is 28 volts and said second voltage is 270 volts. 14. A generator and associated power supply system comprising: a prime mover for driving a shaft to rotate;at least a pair of permanent magnets associated with said shaft;a first stator winding set associated with a first of said permanent magnets, said first stator winding set associated with a customer DC bus, and providing a first voltage to said customer DC bus;a second of said permanent magnets being associated with a second stator winding set, and communicating with an engine accessory DC bus, said engine accessory DC bus providing power to a plurality of motor controllers and associated motors for accessories associated with said prime mover, and including at least a fuel pump motor and an oil pump motor, said engine accessory DC bus being provided with a second voltage from said second stator winding set;said prime mover being a gas turbine engine, said customer DC bus being associated with components on an airplane;both of said winding sets ultimately communicate with a bi-directional DC/DC converter, that allows the power from said first stator winding set to be also directed to said engine accessory DC bus, and allows the power from said second stator winding set to be selectively sent to said customer DC bus, as necessary; andsaid first voltage being on the order of 28 volts and said second voltage being on the order of 270 volts. 15. The system as set forth in claim 14, wherein each of said first and second stator winding sets includes a three-phase stator winding, and a control winding. 16. The system as set forth in claim 15, wherein a current sensor provides a sensed current to a regulator, and said regulator communicating with said control winding in each of said first and second winding sets. 17. The system as set forth in claim 14, wherein said first voltage is 28 volts and said second voltage is 270 volts.
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