IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
|
출원번호 |
US-0068234
(2002-02-05)
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발명자
/ 주소 |
- Carter III, Howard
- Johnson, Richard N.
- Provost, Michael John
- Brown, John David
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출원인 / 주소 |
|
대리인 / 주소 |
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인용정보 |
피인용 횟수 :
7 인용 특허 :
10 |
초록
▼
A dual drive system for a hydraulic pump and an air boost compressor is provided. Reversible power is transmitted to a shaft connected to clockwise and counterclockwise over-running clutches connected to different vehicle or equipment subsystems. Reversing the drive allows power to be alternately tr
A dual drive system for a hydraulic pump and an air boost compressor is provided. Reversible power is transmitted to a shaft connected to clockwise and counterclockwise over-running clutches connected to different vehicle or equipment subsystems. Reversing the drive allows power to be alternately transmitted to one or the other of the subsystems. The invention includes utilizing the dual drive for hydraulic and air conditioning systems for an aircraft, with the provision of an additional drive motor providing constant power to one or more of the subsystems.
대표청구항
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1. A dual drive system for providing power to two subsystems, the dual drive system comprising:a dual-speed reversible electric motor, having a main shaft with a longitudinal main shaft axis, a first end, and a second end; a first over-running clutch assembly having a first output shaft, a first out
1. A dual drive system for providing power to two subsystems, the dual drive system comprising:a dual-speed reversible electric motor, having a main shaft with a longitudinal main shaft axis, a first end, and a second end; a first over-running clutch assembly having a first output shaft, a first output speed, and having a free-wheeling rotational direction, the first over-running clutch assembly being connected to and driven by the first end of the main shaft; a second over-running clutch assembly having a second output shaft, a second output speed, and an opposite free-wheeling rotational direction, the second over-running clutch assembly being connected to and driven by the second end of the main shaft; a first subsystem, connected to and driven by the first output shaft; and a second subsystem, connected to and driven by the second output shaft. 2. The system of claim 1, wherein the first over-running clutch assembly further includes a gear system arranged to one of reduce and increase the first output speed.3. The system of claim 1, wherein the second over-running clutch assembly further includes a second gear system arranged to one of reduce and increase the second output speed.4. A dual drive system for providing power to two subsystems, the dual drive system comprising:a reversible drive power source, having a main shaft with a longitudinal main shaft axis, a first end, and a second end; a first over-running clutch assembly having a first output shaft, a first output speed, and having a free-wheeling rotational direction, the first over-running clutch assembly being connected to and driven by the first end of the main shaft; a second over-running clutch assembly having a second output shaft, a second output speed, and an opposite free-wheeling rotational direction, the second over-running clutch assembly being connected to and driven by the second end of the main shaft; a first subsystem, connected to and driven by the first output shaft; a second subsystem, connected to and driven by the second output shaft; and a second drive power source, having a drive shaft with a longitudinal drive axis, arranged so that the drive shaft of the second drive power source is connected to and drives the second subsystem. 5. The system of claim 4, wherein the second drive power source is a single speed non-reversible electric motor.6. The system of claim 4, wherein the longitudinal drive axis of the drive shaft of the second drive power source is aligned co-linear with the longitudinal main shaft axis of the main shaft of the reversible drive power source.7. A dual drive system for providing power to two aircraft subsystems, the dual drive system comprising:a reversible drive power source incorporated in an aircraft, having a main shaft with a longitudinal main shaft axis, a first end, and a second end; a first over-running clutch assembly having a first output shaft, a first output speed, and having a free-wheeling rotational direction, the first over-running clutch assembly being connected to and driven by the first end of the main shaft; a second over-running clutch assembly having a second output shaft, a second output speed, and an opposite free-wheeling rotational direction, the second over-running clutch assembly being connected to and driven by the second end of the main shaft; a hydraulic pump, connected to and driven by the first output shaft; and an air compressor connected to and driven by the second output shaft. 8. The system of claim 7, wherein the reversible drive power source is a dual-speed reversible electric motor.9. The system of claim 7, wherein the first over-running clutch assembly further comprises a gear system arranged to reduce or increase the first output speed.10. The system of claim 9, wherein the gear system comprises a harmonic drive gear set.11. The system of claim 7, wherein the second over-running clutch assembly further comprises a second gear system arranged to reduce or increase the second output speed.12. The system of claim 7, wherein the air compressor is an air cycle machine arranged for air-cooling.13. The system of claim 12, further comprising:a second drive power source, having a drive shaft with a longitudinal drive axis, arranged so that the drive shaft of the second drive power source is connected to and drives the air compressor. 14. The system of claim 13, wherein the second drive power source is a single speed non-reversible electric motor with its longitudinal drive axis aligned co-linear with the longitudinal main shaft axis of the main shaft of the reversible drive power source.15. A dual drive system for providing power to two subsystems, the dual drive system comprising:a reversible drive power source, having a main shaft with a longitudinal main shaft axis, a first end, and a second end; a first over-running clutch assembly having a first output shaft, a first output speed, a harmonic drive gear set arranged to reduce or increase the first output speed, and having a free-wheeling rotational direction, the first over-running clutch assembly being connected to and driven by the first end of the main shaft; a second over-running clutch assembly having a second output shaft, a second output speed, and an opposite free-wheeling rotational direction, the second over-running clutch assembly being connected to and driven by the second end of the main shaft; a first subsystem, connected to and driven by the first output shaft; and a second subsystem, connected to and driven by the second output shaft.
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