Methods and systems for improving boost response

Patent metadata

Field	Value
Publication number	US-9714620-B2
Application number	US-201514928965-A
Country	US
Kind code	B2
Filing date	Oct 30, 2015
Priority date	Oct 30, 2015
Publication date	Jul 25, 2017
Grant date	Jul 25, 2017

Abstract

Methods and systems are provided for improving boost response in a turbocharged engine. In one example, a method may include in response to a tip-out following a tip-in, when an exhaust catalyst temperature is within a threshold range, deactivating fuel injectors to the engine and increasing air flow to an exhaust turbine based on a desired increase in a turbine speed to maintain the turbine speed at or above a threshold speed.

First claim

The invention claimed is:

1. A method for a boosted engine, comprising:
in response to determining, with an engine controller, a deceleration event, and with the engine controller: deactivating fuel injectors to all cylinders of the engine while increasing airflow through a turbine of a turbocharger in response to a temperature of an exhaust catalyst downstream of the turbine determined to be between an upper threshold and a lower threshold.

2. The method of claim 1 , wherein the deceleration event is initiated subsequent to a tip-in event.

3. The method of claim 2 , wherein during the tip-in event, an amount of accelerator pedal depression is greater than a threshold amount.

4. The method of claim 2 , wherein the deceleration event is a tip-out to a closed air intake throttle condition.

5. The method of claim 1 , wherein increasing airflow through the turbine includes increasing an opening of an air intake throttle positioned in an air intake passage of the engine upstream of a compressor of the turbocharger.

6. The method of claim 5 , wherein an amount of opening of the air intake throttle is based on a turbine speed.

7. The method of claim 6 , wherein increasing air flow through the turbine further includes closing a turbine wastegate and closing a high pressure exhaust gas recirculation valve.

8. The method of claim 1 , further comprising, during the deceleration event, stopping the airflow through the turbine responsive to the temperature increasing above the upper threshold while maintaining deactivation of the fuel injectors.

9. The method of claim 8 , wherein stopping the airflow through the turbine includes closing an air intake throttle.

10. The method of claim 1 , further comprising, in response to detecting accelerator pedal application, adjusting airflow through the turbine and activating one or more of the deactivated fuel injectors, the adjusting and the activation based on a current engine load demand.

11. A method for an engine, comprising:
in response to determining, with an engine controller, a deceleration fuel shut-off event, when a temperature of an exhaust catalyst, determined with the engine controller, is between an upper threshold and a lower threshold, maintaining a turbine speed of a turbocharger above a threshold speed.

12. The method of claim 11 , wherein the deceleration fuel shut-off event occurs responsive to a tip-out after a tip-in to a wide open throttle condition.

13. The method of claim 12 , wherein maintaining the turbine speed includes increasing air flow through a turbine, with the engine controller, during the deceleration fuel shut-off event.

14. The method of claim 13 , wherein increasing air flow through the turbine includes closing a wastegate coupled across the turbine, closing a high pressure exhaust gas recirculation valve, and increasing an opening of an air intake throttle positioned within an air intake passage of the engine upstream of a compressor of the turbocharger.

15. The method of claim 14 , further comprising, during the deceleration fuel shut-off event, stopping the air flow through the turbine responsive to the exhaust catalyst temperature increasing above the upper threshold, the stopping including closing the air intake throttle.

16. The method of claim 15 , further comprising, in response to detecting application of an accelerator pedal, terminating the deceleration fuel shut-off event and adjusting air flow through the turbine based on a current engine load demand; and wherein terminating the deceleration fuel shut-off event includes activating one or more fuel injectors based on the current engine load demand.

17. The method of claim 14 , further comprising opening a compressor bypass valve coupled across the compressor responsive to the exhaust catalyst temperature reaching a second threshold; wherein the second threshold is less than the upper threshold and greater than the lower threshold.

18. A turbocharged engine system, comprising:
an engine including a plurality of cylinders, an intake manifold and an exhaust manifold;
a compressor coupled to the intake manifold and driven by a turbine coupled to the exhaust manifold;
an air intake throttle positioned within an intake passage upstream of the compressor, the intake passage coupling the compressor with ambient air;
an exhaust catalyst coupled within an exhaust passage downstream of the turbine, the exhaust passage coupling the catalyst with ambient air;
each of the plurality of cylinders having one fuel injector for injecting fuel to the cylinder;
an accelerator pedal for receiving an operator torque request; and
a controller having executable instructions stored in a non-transitory memory for:
in response to an accelerator pedal tip-out event initiated subsequent to a tip-in event, deactivating all fuel injectors;
during a first condition, flowing air from the ambient to the turbine via the compressor and the engine while maintaining deactivation of the fuel injectors;
during a second condition, flowing air from the ambient to the turbine via the engine by passing the compressor while maintaining deactivation of the fuel injectors; and
during a third condition, stopping flowing air to the turbine while maintaining deactivation of the fuel injectors;
wherein the first condition includes an exhaust catalyst temperature between a lower threshold and a first upper threshold;
wherein the second condition includes the exhaust catalyst temperature at or above the first upper threshold and below a second upper threshold, the second upper threshold greater than the first upper threshold; and
wherein the third condition includes the exhaust catalyst temperature at or above the second upper threshold.

19. The system of claim 18 , wherein flowing air to the turbine includes increasing an opening of the air intake throttle based on a desired turbine speed.

20. The system of claim 19 , wherein the controller includes further instructions for: in response to application of the accelerator pedal subsequent to the tip-out event, activating one or more fuel injectors and adjusting flow through the turbine based on an operator torque demand.

Assignees

• Ford Global Tech Llc

Inventors

• Kuechler Peter Douglas
• Saberwal Dev
• Bates Kevan
• Losch Trevor
• Lesniak Justin
• Simon Michael M S

Classifications

• F01N3/2006

  Periodically heating or cooling catalytic reactors, e.g. at cold starting or overheating (by electrically controlling the supply of combustible mixture or its constituents only F02D41/0235) · CPC title

• F02D17/02

  Cutting-out (cutting-out engines in multiple engine arrangements F02D25/04) · CPC title

• F02D41/0005

  during deceleration · CPC title

• F02D41/0087 Primary

  Selective cylinder activation, i.e. partial cylinder operation (deceleration cut-off F02D41/123) · CPC title

• F02D41/0007

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