IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
UP-0498660
(2006-08-03)
|
등록번호 |
US-7658069
(2010-04-02)
|
발명자
/ 주소 |
- Weber, Olaf
- Kiener, Timm
- Shutty, John
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
1 인용 특허 :
13 |
초록
▼
A method for monitoring and diagnosing an air charger system for use in an engine assembly having pre-existing sensors, having the steps of providing an air charger having a turbine and a compressor operatively coupled to one another. Providing a control unit for monitoring a plurality of operating
A method for monitoring and diagnosing an air charger system for use in an engine assembly having pre-existing sensors, having the steps of providing an air charger having a turbine and a compressor operatively coupled to one another. Providing a control unit for monitoring a plurality of operating conditions of the engine assembly. The control unit calculates an expected value of a selected operating condition based upon at least another of the plurality of operating conditions. Comparing the expected value and at least another of the plurality of operating conditions. Diagnosing a fault condition, if present, based upon the expected value and said at least another of said plurality of operating conditions being outside a predetermined tolerance.
대표청구항
▼
What is claimed is: 1. A method for monitoring and diagnosing an air charger system for an engine assembly having pre-existing sensors, said method comprising the steps of: providing a secondary air charger system having a turbine in fluid communication with the intake flow path of said engine asse
What is claimed is: 1. A method for monitoring and diagnosing an air charger system for an engine assembly having pre-existing sensors, said method comprising the steps of: providing a secondary air charger system having a turbine in fluid communication with the intake flow path of said engine assembly, and a compressor in fluid communication with the path of exhaust gas flow of said engine assembly, said turbine and said compressor operatively coupled to one another; providing a control unit for monitoring a plurality of operating conditions of said secondary air charger; providing at least one of said pre-existing sensors, at least one known condition, and a combination thereof, to be used for monitoring of said plurality of operating conditions of said secondary air charger; providing a throttle in operative fluid communication with said turbine for controlling the flow through said turbine, wherein said at least one known condition is a known commanded position of said throttle; providing one of said pre-existing sensors to be a mass air flow sensor, said mass air flow sensor being located upstream of said throttle and said secondary air charger system; said control unit calculating an expected value of a selected operating condition based upon at least one of said plurality of operating conditions; comparing said expected value and at least another of said plurality of operating conditions; and diagnosing a fault condition, if present, based upon said expected value and said at least another of said plurality of operating conditions being outside a predetermined tolerance. 2. The method for monitoring and diagnosing a secondary air charger system of claim 1, further comprising the step of monitoring said plurality of operating conditions after diagnosing said fault condition. 3. The method for monitoring and diagnosing a secondary air charger system of claim 1, further comprising the step of clearing said fault condition and monitoring said operating conditions if said expected value is within said predetermined tolerance of said at least another of said plurality of operating conditions. 4. The method for monitoring and diagnosing a secondary air charger system of claim 1, further comprising the step of said pre-existing sensors further comprising at least one of a pressure sensor, an oxygen sensor, a temperature sensor, and a combination thereof. 5. The method for monitoring and diagnosing a secondary air charger system of claim 1, further comprising the step of determining an air pressure in an intake of said engine assembly. 6. The method for monitoring and diagnosing a secondary air charger system of claim 1, further comprising the step of determining an ambient air pressure. 7. The method for monitoring and diagnosing a secondary air charger system of claim 1, further comprising the step of determining a temperature in an intake of said engine assembly. 8. The method for monitoring and diagnosing a secondary air charger system of claim 1, further comprising the step of said control unit calculating an expected throttle position based upon said operating conditions. 9. The method for monitoring and diagnosing a secondary air charger system of claim 8, further comprising the step of comparing said commanded throttle position to said calculated expected throttle position and diagnosing a fault condition based upon said commanded throttle position and said calculated expected throttle position being outside a predetermined tolerance. 10. The method for monitoring and diagnosing a secondary air charger system of claim 1, further comprising the step of providing a turbine valve in operative fluid communication with said turbine for controlling the flow of gaseous fluid exiting said turbine. 11. A method for monitoring and diagnosing an air charger system for use in an engine assembly having pre-existing sensors, said method comprising the steps of: providing a secondary air charger having a turbine in fluid communication with the intake flow path of said engine assembly, and a compressor in fluid communication with the path of exhaust gas flow of said engine assembly, said turbine and said compressor operatively coupled to one another; providing a control unit interfaced with a plurality of sensors; providing at least one of said plurality of sensors, at least one known condition, and a combination thereof, to be used for monitoring of said plurality of operating conditions of said secondary air charger; providing a throttle in operative fluid communication with said turbine for controlling the flow through said turbine, wherein said known condition is a known commanded position of said throttle; providing one of said plurality of sensors to be a mass air flow sensor, said mass air flow sensor being located upstream of said throttle and said secondary air charger system; monitoring said plurality of operating conditions of said secondary air charger by way of inputs from said plurality of sensors; said control unit calculating an expected value of a selected one of said plurality of operating conditions based upon data collected from at least one of said plurality of sensors, at least one known value, and a combination thereof; comparing said expected value and data collected from said mass airflow sensor; diagnosing a fault condition, if present, based upon said expected value and said data collected from said mass airflow sensor being outside a predetermined tolerance, and clearing said fault condition if said expected value is within said predetermined tolerance of said data collected from said mass airflow sensor. 12. The method for monitoring and diagnosing a secondary air charger system of claim 11, wherein said plurality of sensors is at least one of a pressure sensor, a temperature sensor, an oxygen sensor, and a combination thereof. 13. The method for monitoring and diagnosing a secondary air charger system of claim 11, further comprising the step of determining an air pressure in an intake of said engine assembly. 14. The method for monitoring and diagnosing a secondary air charger system of claim 11, further comprising the step of determining an ambient air pressure. 15. The method for monitoring and diagnosing a secondary air charger system of claim 11, further comprising the step of determining a temperature in an intake of said engine assembly. 16. A secondary air charger system for use in an engine assembly having at least an engine, said secondary air charger system comprising: a turbine in fluid communication with an intake of said engine; an intake located upstream of and operable for providing airflow into said secondary air charger system and being in fluid communication with said turbine; a throttle in operative fluid communication with said intake located upstream of said secondary air charger system, wherein said throttle is in parallel with said turbine and controls the flow from said intake located upstream of said secondary air charger system through said turbine; a compressor in fluid communication with said intake located upstream of said secondary air charger system, wherein said compressor is operatively coupled to said turbine, and compressed air is emitted from said compressor and enters an exhaust of said engine; and a plurality of sensors for monitoring operating conditions of said secondary air charger system and diagnosing a fault condition upon failure of emitting compressed air from said compressor, one of said plurality of sensors being a mass air flow sensor, said mass air flow sensor being located upstream of said throttle and said secondary air charger system; wherein one of said operating conditions is a known commanded position of said throttle. 17. The secondary air charger system of claim 16, wherein said at least one sensor is a pressure sensor, a temperature sensor, an oxygen sensor, and a combination thereof. 18. The secondary air charger system of claim 16, further comprising a turbine valve in operative fluid communication between said engine and said turbine for controlling the flow exiting said turbine. 19. The secondary air charger system of claim 16, further comprising a control unit interfaced with said at least one sensor, wherein the data collected from said at least one sensor by said control unit is compared to a predetermined value based upon said operating conditions of said engine assembly to determine if said air charger system is functioning properly.
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