Fuel system having pump prognostic functionality

• US 10,041,432 B2
• Filed: 01/09/2017
• Issued: 08/07/2018
• Est. Priority Date: 01/09/2017
• Status: Active Grant

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Puckett, Daniel Reese, Bashore, Bradley Scott, Sattler, Michael Edward, Marchionda, Michael Scott, Rayasam, Sasidhar, Nellutla, Kranti Kumar
• Primary Examiner(s): Vo, Hieu T
• Assistant Examiner(s): MANLEY, SHERMAN D
• Application Number:
  US15/401,911
• Publication Number:
  US 20180195458A1
• Time in Patent Office: 575 Days
• CPC Class Codes: F02D 2041/224 Diagnosis of the fuel system
• CPC Class Codes: F02D 2041/225 Leakage detection
• CPC Class Codes: F02D 2200/0602 Fuel pressure
• CPC Class Codes: F02D 2200/101 Engine speed
• CPC Class Codes: F02D 41/042 for stopping the engine
• CPC Class Codes: F02D 41/3082 Control of electrical fuel pumps
• CPC Class Codes: F02D 41/3836 Controlling the fuel pressure
• CPC Class Codes: F02D 41/3863 by controlling the flow out of the common rail, e.g. using pressure relief valves
• CPC Class Codes: F02M 2200/247 Pressure sensors
• CPC Class Codes: F02M 55/025 Common rails
• CPC Class Codes: F02M 63/0265 Pumps feeding common rails

Abstract

A fuel system is disclosed for use with an engine. The fuel system may have a plurality of fuel injectors, a common rail fluidly, a pump, and an outlet valve associated with the pump. The fuel system may also have a sensor configured to generate a signal indicative of a pressure of fuel in the common rail, and an electronic control module. The electronic control module may be configured to detect a zero-fueling condition, to determine a first pressure decay rate of the common rail during the zero-fueling condition while the pump is rotating, and to determine a second pressure decay rate of the common rail during the zero-fueling condition after the pump has stopped rotating. The electronic control module may also be configured to selectively generate a diagnostic flag associated with wear of the outlet valve based on the first and second pressure decay rates.

Claims

1. A fuel system for an engine, comprising:

a plurality of fuel injectors;

a common rail fluidly connected to the plurality of fuel injectors;

a pump configured to pressurize the common rail;

an outlet valve associated with the pump;

a sensor configured to generate a signal indicative of a pressure of fuel in the common rail; and

an electronic control module in communication with the sensor and configured to;

detect a zero-fueling condition;

determine a first pressure decay rate of the common rail during the zero-fueling condition while the pump is rotating;

determine a second pressure decay rate of the common rail during the zero-fueling condition after the pump has stopped rotating; and

selectively generate a diagnostic flag associated with wear of the outlet valve based on the first and second pressure decay rates.

2. The fuel system of claim 1, wherein the electronic control module is further configured to:

determine a third pressure decay rate of the common rail during the zero-fueling condition after the pump has stopped rotating; and

selectively generate the diagnostic flag associated with wear of the outlet valve based on the first, second, and third pressure decay rates.

3. The fuel system of claim 2, wherein the electronic control module is configured to selectively generate:

a first diagnostic flag associated with an early-hour warning; and

a second diagnostic flag associated with a late-hour warning.

4. The fuel system of claim 3, wherein:

the early-hour warning is associated with about 400 hrs. until failure of the pump; and

the late-hour warning is associated with about 50 hrs. until failure of the pump.

5. The fuel system of claim 3, wherein:

the first pressure decay rate is associated with a pressure range that is higher than pressure ranges associated with the second and third pressure decay rates; and

the pressure range associated with the second pressure decay rate is higher than the pressure range associated with the third pressure decay rate.

6. The fuel system of claim 5, wherein the electronic control module is configured to generate the first diagnostic flag when a ratio of the third pressure decay rate to the second pressure decay rate is greater than a level-1 ratio, the third pressure decay rate is higher than a prognostic limit, and a ratio of the first pressure decay rate to the second pressure decay rate is less than a level-2 ratio.

7. The fuel system of claim 6, wherein the electronic control module is configured to generate the second diagnostic flag when the ratio of the third pressure decay rate to the second pressure decay rate is greater than the level-1 ratio, the third pressure decay rate is higher than the prognostic limit, and the ratio of the first pressure decay rate to the second pressure decay rate is greater than the level-2 ratio.

8. The fuel system of claim 5, wherein the first pressure decay rate is associated with a pressure range that is about 2 to 2.5 times a normal operating pressure.

9. The fuel system of claim 5, wherein the electronic control module is configured to cause the pump to raise the pressure of the common rail to a first range prior to determining the first pressure decay rate.

10. The fuel system of claim 9, wherein the electronic control module is configured to buzz the injectors to lower the pressure of the common rail prior to determining the second pressure decay rate and again prior to determining the third pressure decay rate.

11. The fuel system of claim 9, wherein the electronic control module is configured to determine the first pressure decay rate based on an average of multiple pressure measurements taken while the pump is still rotating during the zero-fueling condition.

12. The fuel system of claim 11, wherein the electronic control module is configured to determine each of the second and third pressure decay rates based on two pressure measurements spaced apart from each other by a tuneable time period.

13. A fuel system, comprising:

a plurality of fuel injectors;

a common rail fluidly connected to the plurality of fuel injectors;

a pump configured to pressurize the common rail;

an outlet valve associated with the pump;

a sensor configured to generate a signal indicative of a pressure of fuel in the common rail; and

an electronic control module in communication with the sensor and configured to;

detect a zero-fueling condition;

determine a first pressure decay rate of the common rail during the zero-fueling condition while the pump is rotating;

determine a second pressure decay rate of the common rail during the zero-fueling condition after the pump has stopped rotating in association with a first pressure range;

determine a third pressure decay rate of the common rail during the zero-fueling condition after the pump has stopped rotating in association with a second pressure range that is lower than the first; and

selectively generate;

an early-hour flag associated with wear of the outlet valve when a ratio of the third pressure decay rate to the second pressure decay rate is greater than a level-1 ratio, the third pressure decay rate is higher than a prognostic limit, and a ratio of the first pressure decay rate to the second pressure decay rate is less than a level-2 ratio; and

a late-hour diagnostic flag associated with wear of the outlet valve when the ratio of the third pressure decay rate to the second pressure decay rate is greater than the level-1 ratio, the third pressure decay rate is higher than the prognostic limit, and the ratio of the first pressure decay rate to the second pressure decay rate is greater than the level-2 ratio.

14. A method of prognosticating health of a fuel system, the method comprising:

detecting a zero-fueling condition;

determining a first pressure decay rate of a common rail during the zero-fueling condition while an associated pump is rotating;

determining a second pressure decay rate of the common rail during the zero-fueling condition after the pump has stopped rotating; and

selectively generating a diagnostic flag corresponding to wear of an outlet valve associated with the pump based on the first and second pressure decay rates.

15. The method of claim 14, further including determining a third pressure decay rate of the common rail during the zero-fueling condition after the pump has stopped rotating, wherein selectively generating the diagnostic flag includes selectively generating the diagnostic flag based on the first, second, and third pressure decay rates.

16. The method of claim 15, wherein selectively generating the diagnostic flag includes generating:

a first diagnostic flag associated with an early-hour warning; and

a second diagnostic flag associated with a late-hour warning.

17. The method of claim 16, wherein:

the early-hour warning is associated with about 400 hrs. until failure of the pump; and

the late-hour warning is associated with about 50 hrs. until failure of the pump.

18. The method of claim 17, wherein:

the first pressure decay rate is associated with a pressure range that is higher than pressure ranges associated with the second and third pressure decay rates; and

the pressure range associated with the second pressure decay rate is higher than the pressure range associated with the third pressure decay rate.

19. The method of claim 18, wherein generating the first diagnostic flag includes generating the first diagnostic flag when a ratio of the third pressure decay rate to the second pressure decay rate is greater than a level-1 ratio, the third pressure decay rate is higher than a prognostic limit, and a ratio of the first pressure decay rate to the second pressure decay rate is less than a level-2 ratio.

20. The method of claim 19, wherein generating the second diagnostic flag includes generating the second diagnostic flag when the ratio of the third pressure decay rate to the second pressure decay rate is greater than the level-1 ratio, the third pressure decay rate is higher than the prognostic limit, and the ratio of the first pressure decay rate to the second pressure decay rate is greater than the level-2 ratio.