Method for operating a turbocharger arrangement and control unit for a turbocharger arrangement

Patent metadata

Field	Value
Publication number	US-9303556-B2
Application number	US-201213399827-A
Country	US
Kind code	B2
Filing date	Feb 17, 2012
Priority date	Feb 21, 2011
Publication date	Apr 5, 2016
Grant date	Apr 5, 2016

Abstract

A method for operating a turbocharger arrangement of an internal combustion engine, the turbocharger arrangement comprising a low-pressure and a high-pressure turbocharging stage arranged sequentially, the low-pressure turbo-charging stage comprising a low-pressure turbine with a sensorless low-pressure turbine bypass valve, is provided. The method comprises evaluating at least one sensor signal of the turbocharger arrangement for detecting a failure mode of the sensorless low-pressure turbine bypass valve. In this way, the low-pressure turbine bypass valve may be monitored for degradation without utilizing a position sensor.

First claim

The invention claimed is:

1. A method for operating a turbocharger system of an internal combustion engine including an electronic control unit including non-transitory instructions stored in memory, comprising:
evaluating via the electronic control unit at least one sensor signal of the turbocharger system for detecting a failure mode of a sensorless low-pressure turbine bypass valve coupled across a low-pressure turbine, the low-pressure turbine positioned downstream of a high-pressure turbine, the turbines arranged sequentially in an exhaust path, the at least one sensor signal continuously evaluated during operation of the internal combustion engine for detecting the failure mode of the sensorless low-pressure turbine bypass valve; and
upon detection of the failure mode of the sensorless low-pressure turbine bypass valve, adjusting a high-pressure turbine bypass valve coupled across the high-pressure turbine via the electronic control unit to maintain a desired boost pressure.

2. The method according to claim 1 , wherein the at least one sensor signal is a signal representative of intake mass air-flow, boost pressure, compressor pressure ratio, compressor outlet temperature, exhaust flow, exhaust pressure downstream of the low-pressure turbine, and/or turbocharger speed.

3. The method according to claim 1 , further comprising evaluating the at least one sensor signal to determine at least one physical parameter of the turbocharger system, the at least one physical parameter being discriminative with respect to a mode of operation of the sensorless low-pressure turbine bypass valve.

4. The method according to claim 3 , wherein the at least one physical parameter of the turbocharger system is exhaust flow, intake mass airflow, boost pressure, exhaust pressure downstream of the low-pressure turbine, and/or low-pressure turbocharger speed.

5. The method according to claim 1 , further comprising evaluating via the electronic control unit the at least one sensor signal of the turbocharger system to detect the failure mode of the sensorless low-pressure turbine bypass valve depending on an engine operating point.

6. The method according to claim 1 , wherein the at least one sensor signal and at least one physical parameter of the turbocharger system and a function representative of a mode of operation of the sensorless low-pressure turbine bypass valve is filtered.

7. The method according to claim 1 , further comprising operating the turbocharger system according to a first control mode and upon detection of the failure mode of the sensorless low-pressure turbine bypass valve, operating the turbocharger system according to a second control mode.

8. The method according to claim 7 , wherein the first control mode is a low-speed/torque control mode and in the second control mode the high-pressure turbine bypass valve is set more closed than in the first control mode.

9. The method according to claim 8 , wherein the first control mode is a high-speed/torque control mode and, if the failure mode of the sensorless low-pressure turbine bypass valve is fully closed, the high-pressure turbine bypass valve is set fully open and a torque setpoint is limited, and/or if the failure mode of the low-pressure turbine bypass valve is fully open, a boost pressure is controlled by the high-pressure turbine bypass valve.

10. The method according to claim 1 , further comprising evaluating via the electronic control unit a supply signal of the sensorless low-pressure turbine bypass valve to determine the failure mode of the sensorless low -pressure turbine bypass valve.

11. A method for controlling a low-pressure turbocharger wastegate for a turbocharger system for an engine including a high-pressure turbocharger, comprising:
during first conditions of engine operation, closing a high-pressure turbine bypass valve by a first amount in response to the wastegate being unable to close via an electronic control unit including non-transitory instructions stored in memory;
during second conditions of engine operation, actuating the high-pressure turbine bypass valve to maintain a desired boost pressure in response to the wastegate being unable to close via the electronic control unit; and
wherein the first conditions comprise at least low engine speed and the second conditions comprise at least high engine speed.

12. The method of claim 11 , further comprising determining engine speed and wherein the low engine speed comprises an engine speed being below a threshold, and the high engine speed comprises the engine speed being at or above the threshold.

13. The method of claim 12 , further comprising determining a position of the wastegate based on a speed of the low-pressure turbocharger wastegate, engine speed, and engine load.

14. The method of claim 12 , further comprising, during the second conditions, fully opening the high-pressure turbine bypass valve in response to the wastegate being unable to open.

15. The method of claim 12 , further comprising, during the first conditions, actuating the high-pressure turbine bypass valve to maintain desired boost pressure in response to the wastegate being in a closed position.

16. The method of claim 12 , further comprising, during the second conditions, in response to the wastegate being in a desired position, fully opening the high-pressure turbine bypass valve.

17. The method of claim 12 , wherein the first conditions comprise low engine speed and low engine load, and wherein the second conditions comprise high engine speed and high engine load.

18. An engine turbocharger system, comprising:
a high-pressure turbocharger including a first turbine, a first compressor, and a high-pressure turbine bypass valve;
a low-pressure turbocharger including a second turbine arranged downstream of the first turbine, a second compressor, a compressor bypass valve, and a wastegate; and
a controller including non-transitory instructions stored in memory to:
determine degradation of the wastegate based on an undesired wastegate position for a current engine speed and load; and
when the wastegate is stuck open and unable to close during low speed and load conditions, close the compressor bypass valve and adjust a position of the high-pressure turbine bypass valve in response to degradation of the wastegate to maintain desired boost pressure.

19. The engine turbocharger system of claim 18 , wherein degradation of the wastegate is determined based on a speed of the second turbine, engine load, and engine speed, and wherein the controller includes further instructions to, when the wastegate is stuck open and unable to close during high speed and load conditions, open the compressor bypass valve and adjust a position of the high-pressure turbine bypass valve to maintain desired boost pressure.

Assignees

• Chevalier Alain Marie Roger
• Petrovic Simon
• Bartsch Arno
• Ford Global Tech Llc

Inventors

• Chevalier Alain Marie Roger
• Petrovic Simon
• Bartsch Arno

Classifications

• F02B2039/164

  the temperature of the pump, of the pump drive or the pumped fluid being limited · CPC title

• Y02T10/40

  Engine management systems · CPC title

• F02D41/221

  relating to the failure of actuators or electrically driven elements · CPC title

• F02D41/0007

  for control of turbo-charged or super-charged engines (control of the pumps per se F02B37/12) · CPC title

• F01N2900/1406

  Exhaust gas pressure · CPC title