System and method for determining turbine degradation and mitigating turbine degradation in a variable geometry turbocharger

Patent metadata

Field	Value
Publication number	US-9410475-B2
Application number	US-201414300147-A
Country	US
Kind code	B2
Filing date	Jun 9, 2014
Priority date	Jun 9, 2014
Publication date	Aug 9, 2016
Grant date	Aug 9, 2016

Abstract

A method for operating a vehicle system is described herein. The method includes indicating a variable geometry turbine degradation based on a comparison of a modeled set of turbine pressure values and a sensed set of turbine pressure values, each set of turbine pressure values including a pressure value upstream of the turbine and a pressure value downstream of the turbine and the variable geometry turbine positioned downstream of an engine cylinder.

First claim

The invention claimed is:

1. An engine system comprising:
a variable geometry turbocharger including a compressor positioned in an intake sub-system in fluidic communication with the engine and a turbine positioned in an exhaust sub-system in fluidic communication with the engine, the turbine including a plurality of adjustable vanes and a turbine inlet and a turbine outlet;
an electronic control sub-system including instructions stored in memory executable by a processor to:
in response to throttle tip-in, determine a sensed turbine inlet pressure and a sensed turbine outlet pressure based on signals received from sensors adjacent to the turbine inlet and the turbine outlet;
determine a modeled turbine inlet pressure and a modeled turbine outlet pressure based on a turbine inlet pressure model and turbine outlet pressure model; and
indicate variable geometry turbine degradation based on a comparison of the modeled and sensed turbine inlet pressures and turbine outlet pressures.

2. The engine system of claim 1 , where the electronic control sub-system includes instructions stored in memory executable by a processor to, in response to the variable geometry turbine degradation, select a turbine degradation mitigation action from a group of turbine degradation mitigation actions based on the comparison of the modeled and sensed turbine inlet pressures and turbine outlet pressures.

3. The engine system of claim 2 , where the group of turbine degradation mitigation actions includes adjustment of a turbine bypass valve in the engine system, adjustment of an exhaust gas recirculation (EGR) valve in the engine system, adjustment of a throttle in the engine system, and adjustment of fuel injection in the engine system.

4. A method for operating an engine system, comprising:
indicating a variable geometry turbine degradation based on a comparison of a modeled set of turbine pressure values and a sensed set of turbine pressure values, each set of turbine pressure values including a pressure value upstream of the turbine and a pressure value downstream of the turbine, the variable geometry turbine positioned downstream of an engine cylinder.

5. The method of claim 4 , where a ratio of the upstream pressure value and the downstream pressure value in each of the sensed set of turbine pressure values and the modeled set of turbine pressure values are compared to determine the indicated variable geometry turbine degradation.

6. The method of claim 5 , where the variable geometry turbine degradation is determined when a difference between the pressure ratios is outside a range that is greater than an error threshold of the modelled set of pressure values and the sensed set of turbine pressure values as well as an expected pressure range variability mapped for a condition the engine is operating in for a set time that exceeds normal response time ranges of the turbocharger.

7. The method of claim 4 , where a change in pressure across the turbine in each of the sensed set of turbine pressure values and the modeled set of turbine pressure values are compared to determine variable geometry turbine degradation.

8. The method of claim 7 , where the variable geometry turbine degradation is determined when a difference between the sensed change in pressure across the turbine and the modeled change in pressure across the turbine is greater than a pre-defined pressure difference threshold that is greater than an expected model accuracy and pressure variability for the engine population at an operation point.

9. The method of claim 4 , where the modeled set of turbine pressure values are determined based on orifice flow using input parameters for exhaust mass flow, modeled or measure turbine vane position, and exhaust temperature.

10. The method of claim 4 , further comprising, in response to determining the variable geometry turbine degradation, selecting a turbine degradation mitigation action from a group of turbine degradation mitigation actions based on the comparison of the modeled set of turbine pressure values and the sensed set of turbine pressure values.

11. The method of claim 4 , where the turbine vane degradation includes slow or non-responsive vanes in the variable geometry turbine.

12. The method of claim 4 , where the modeled set of turbine pressure values is a function of a modeled turbine vane position.

13. The method of claim 4 , where determining the variable geometry turbine degradation is initiated in response to a throttle tip-in event.

14. A method for operating an engine system comprising:
during a first operating condition selecting a first turbine degradation mitigation action from a group of turbine degradation mitigation actions including adjustment of a turbine bypass valve, adjustment of an exhaust gas recirculation (EGR) valve, adjustment of a throttle, and adjustment of fuel injection; and
during a second operating condition selecting a second turbine degradation mitigation action from the group of turbine degradation mitigation actions, the second turbine degradation mitigation action different from the first turbine degradation mitigation action and the second operating condition different from the first operating condition.

15. The method of claim 14 , where the first turbine degradation mitigation action and the second turbine degradation action are sequentially implemented.

16. The method of claim 14 , where the first turbine degradation mitigation action and the second turbine degradation action are implemented at overlapping time intervals when it is determined that the first operating condition does not resolve turbine degradation.

17. The method of claim 14 , where the first turbine degradation mitigation action and the second turbine degradation mitigation action are selected based on a comparison of a modeled set of turbine pressure values and a sensed set of turbine pressure values, each set of turbine pressure values including a pressure value upstream of the turbine and a pressure value downstream of the turbine.

18. The method of claim 14 , further comprising during a third operating condition selecting a third turbine degradation mitigation action from the group of turbine degradation mitigation actions, the third turbine degradation mitigation action different from the second turbine degradation mitigation action and first turbine degradation mitigation action.

19. The method of claim 18 , further comprising during a fourth operating condition selecting a fourth turbine degradation mitigation action from the group of turbine degradation mitigation actions, the third turbine degradation mitigation action different from the third turbine degradation mitigation action, the second turbine degradation mitigation action, and first turbine degradation mitigation action.

20. The method of claim 14 , where adjustment of a throttle includes limiting throttle adjustment to a predetermined range and adjustment of fuel injection includes limiting fuel injection to a predetermined range.

Assignees

• Ford Global Tech Llc

Inventors

• Morelli Anthony
• Fulton Brien Lloyd
• Kostrzewski Thomas
• Smith Jason Ronald
• Pohlkamp Kyle

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F02B39/16

  Other safety measures for, or other control of, pumps · CPC title

• F02M25/077

  Mechanical Engineering · mapped topic

• F02M25/0706

  Mechanical Engineering · mapped topic

• F02B37/22 Primary

  by varying cross-section of exhaust passages or air passages {, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits} (F02B37/24 takes precedence) · CPC title