IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0978190
(2010-12-23)
|
등록번호 |
US-8176897
(2012-05-15)
|
발명자
/ 주소 |
- Guglielmo, Kennon H.
- Walser, Michael
- Walser, Randy
- Shouse, Kenneth R.
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
4 인용 특허 :
9 |
초록
▼
The invention includes a very fast voice coil actuator, in the range of 2-5 millisecond full stroke response with high force, a circuit board located in the enclosure, a pressure sensor sensing pressure internal to the system which in the preferred embodiment is located in the actuator cap assembly
The invention includes a very fast voice coil actuator, in the range of 2-5 millisecond full stroke response with high force, a circuit board located in the enclosure, a pressure sensor sensing pressure internal to the system which in the preferred embodiment is located in the actuator cap assembly but could be located in other locations, a diaphragm, a link plate, a mating ring, and a mechanical pressure regulator. An electronic pressure regulator receives pressure commands from the engine control module in a manner similar to receiving pulse width from an engine control module to an injector and calculates the required new pressure command. A novel feature of the present invention includes the Delta P control and the control of the regulator based on direct feedback of pressure.
대표청구항
▼
1. A fuel system, comprising: a fuel mixer including a fuel inlet;an engine control module; anda fuel pressure regulator coupled to the engine control module and the fuel mixer, the fuel pressure regulator comprising: a pressure sensor that is operable to detect a fuel inlet pressure at the fuel inl
1. A fuel system, comprising: a fuel mixer including a fuel inlet;an engine control module; anda fuel pressure regulator coupled to the engine control module and the fuel mixer, the fuel pressure regulator comprising: a pressure sensor that is operable to detect a fuel inlet pressure at the fuel inlet and use the fuel inlet pressure to generate a first pressure signal;a microprocessor operable to receive the first pressure signal from the pressure sensor and a second pressure signal from the engine control module and generate a third pressure signal that is related to a difference between the first pressure signal and the second pressure signal;an actuator coupled to the microprocessor and operable to receive the third pressure signal, wherein the actuator includes an actuator member coupled to at least one flexure element that provides the actuator member with a predetermined range of motion; anda pressure actuated regulator device coupled to the actuator member, wherein, in response to the actuator receiving the third pressure signal, the actuator member moves along the predetermined range of motion to cause the pressure-actuated regulator device to adjust the fuel pressure in the fuel line. 2. The system of claim 1, wherein the at least one flexure element comprises a pair of flexures elements in a spaced apart orientation. 3. The system of claim 1, wherein the at least one flexure element comprises a perimeter that is secured to the housing. 4. The system of claim 1, wherein the at least one flexure element comprises a plurality of spiral shaped members extending from a secured section and each coupled to the actuator member to provide the actuation member with the predetermined range of motion. 5. The system of claim 1, wherein the actuator member comprises a rod. 6. The system of claim 1, wherein the predetermined range of motion is linear. 7. The system of claim 1, further comprising: a casing housing the pressure sensor, the microprocessor, the actuator, and the pressure actuated regulator device. 8. The system of claim 1, wherein the at least one flexure element is fabricated from a single piece of material and includes a moveable section operable to flex relative to a secured section to provide the actuator member with the predetermined range of motion. 9. The system of claim 1, wherein the fuel mixer includes a air inlet and the first pressure signal is related to the difference between the fuel inlet pressure at the fuel inlet and an air inlet pressure at the air inlet. 10. A fuel supply system, comprising: a carburetor including a carburetor fuel inlet;an electronic fuel pressure regulator including a regulator fuel outlet that is coupled to the carburetor fuel inlet, the electronic fuel pressure regulator comprising: a microprocessor operable to receive an operating pressure signal related to a fuel pressure between the regulator fuel outlet and the carburetor fuel inlet and generate an actuator signal that is related to a difference between the operating pressure signal and a desire pressure signal;an actuator coupled to the controller and operable to receive the actuator signal, wherein the actuator includes a rod coupled to a moveable section on at least one flexure element, wherein the moveable section provides the actuator member with a predetermined range of motion; anda valve coupled to the rod, wherein the rod is operable to move in response to the actuator receiving the actuator signal, and wherein movement of the rod results in movement of the valve to adjust the fuel pressure in the fuel line. 11. The system of claim 10, wherein the carburetor includes a carburetor air inlet and the operating pressure signal is related to a difference between the fuel pressure between the regulator fuel outlet and the carburetor fuel inlet and an air pressure at the carburetor air inlet. 12. An electronic pressure regulator for use with a gaseous fuel internal combustion engine having an engine control module, a fuel line source having an outlet in communication with the engine, a fuel line including a controllable valve for regulating the gaseous fuel pressure at the outlet, and a venturi carburetor in communication with the fuel line outlet and the engine, wherein the actuator used to control the valve has flexures. 13. An electronic pressure regulator, comprising: a controller operable to provide an actuator signal that is related to a pressure difference based on a fuel pressure in a fuel line and a desired fuel pressure;an actuator coupled to the controller and operable to receive the actuator signal, wherein the actuator includes an actuator member coupled to at least one flexure element, and wherein the at least one flexure element includes a secured section that is secured to a housing and a moveable section that is coupled to the actuator member and provides the actuator member with a predetermined range of motion; anda pressure actuated regulator device coupled to the actuator member, wherein the actuator member is operable to move in response to the actuator receiving the actuator signal, and wherein movement of the actuator member results in movement of the pressure-actuated regulator device to adjust the fuel pressure in the fuel line. 14. The electronic pressure regulator of claim 13, wherein the at least one flexure element comprises a pair of flexures elements in a spaced apart orientation. 15. The electronic pressure regulator of claim 13, wherein the secured section of the at least one flexure element comprises a perimeter of the at least one flexure element that is secured to the housing. 16. The electronic pressure regulator of claim 13, wherein the moveable section of the at least one flexure element comprises a plurality of spiral shaped members extending from the secured section and each coupled to the actuator member. 17. The electronic pressure regulator of claim 13, wherein the predetermined range of motion is linear. 18. The electronic pressure regulator of claim 13, further comprising: a casing housing the controller, the actuator, and the pressure actuated regulator device. 19. The electronic pressure regulator of claim 13, wherein the at least one flexure element is fabricated from a single piece of material, and the moveable section of the at least one flexure element is operable to flex relative to the secured section to provide the actuator member with the predetermined range of motion. 20. The electronic pressure regulator of claim 13, wherein the pressure difference based on the fuel pressure in the fuel line and the desired fuel pressure is further based on a difference between the fuel pressure and an air pressure in an air line.
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