Control of a partial cylinder deactivation engine

• US 8,839,766 B2
• Filed: 03/13/2013
• Issued: 09/23/2014
• Est. Priority Date: 03/30/2012
• Status: Active Grant

• Current Assignee: Tula Technology, Incorporated (BorgWarner Incorporated)
• Original Assignee: Tula Technology, Incorporated (BorgWarner Incorporated)
• Inventors: Serrano, Louis J.
• Primary Examiner(s): SOLIS, ERICK R
• Application Number:
  US13/799,389
• Publication Number:
  US 20130255626A1
• Time in Patent Office: 559 Days
• Field of Search: 123/481, 123/198.F, 123/198.DB, 123/198.DC
• US Class Current: 123/481
• CPC Class Codes: F02D 2250/21 during a transition between engine operation modes or states
• CPC Class Codes: F02D 41/0087 Selective cylinder activation, i.e. partial cylinder operation deceleration cut-off F02D41/123

Abstract

A variety of methods and arrangements for managing transitions between operating states for an engine are described. In one aspect, an engine is operated in a particular operating state. A transition is made to another operating state. During that transition, the engine is operated in a skip fire manner.

Claims

1. A method for managing transitions between operational states of an internal combustion engine having a plurality of working chambers, the method comprising:

operating the engine in one of a first displacement and a second displacement, each displacement having an associated fixed set of active working chambers, wherein the number of active working chambers associated with the first displacement is different than the number of active working chambers associated with the second displacement and wherein the number of active working chambers associated with each of the first and second displacements is greater than zero;

making a transition between the first displacement and the second displacement; and

operating the engine in a skip fire manner during the transition wherein the transition between the first and second displacements has a duration of less than two seconds and wherein during skip fire operation at least one of the active working chambers is fired during a first working cycle, skipped during a subsequent second working cycle and fired during a third working cycle that is subsequent to the second working cycle, the first, second and third working cycles occurring during the transition.

2. A method as recited in claim 1 wherein the first and second displacements each involve different, predetermined numbers of non-deactivatable working chambers that are fired at every engine cycle during a particular operational state.

3. A method as recited in claim 1 wherein operating the engine in a skip fire manner involves deactivating at least one selected working cycle of at least one selected working chamber and firing at least one selected working cycle of at least one selected working chamber wherein individual working chambers are sometimes deactivated and sometimes fired.

4. A method as recited in claim 1 wherein the operating of the engine in a skip fire manner further comprises:

generating a firing sequence that includes one or more firing and skip commands for operating the working chambers of the engine;

determining which working chamber a particular skip command would be applied to;

if the skip command involves a deactivatable working chamber, skipping the deactivatable working chamber; and

if the skip command involves a non-deactivatable working chamber, firing the non-deactivatable working chamber.

5. A method as recited in claim 1 wherein the operating of the engine in a skip fire manner further comprises:

determining a selected working chamber for which a firing or skip command is required;

determining whether the selected working chamber is deactivatable;

if the selected working chamber is deactivatable, applying a firing algorithm to generate a firing or skip command for the selected working chamber; and

if the selected working chamber is non-deactivatable, arranging for the firing of the selected working chamber without applying the firing algorithm.

6. A method as recited in claim 1 wherein the operating of the engine in a skip fire manner further comprises:

selecting a firing fraction from a library of one or more predetermined firing fractions wherein each firing fraction indicates a percentage of working chambers to fire to deliver a desired output;

determining a firing sequence based on the firing fraction; and

operating one or more of the working chambers of the engine based on the firing sequence.

7. A method as recited in claim 6 wherein the selected firing fraction is selected based on one selected from the group consisting of a fill rate and an emptying rate of an intake manifold.

8. A method as recited in claim 1 wherein the operating of the engine in a skip fire manner further comprises:

selecting a firing sequence from a library of one or more predetermined firing sequences.

19. A method as recited in claim 1 wherein the number of active working chambers associated with the first displacement is the total number of working chambers in the engine.

22. A method as recited in claim 1 wherein the first, second and third working cycles are not necessarily sequential working cycles.

23. A method as recited in claim 1 wherein:

the first and second displacements involve different, pre-determined numbers of active working chambers and wherein every active working chamber is fired at every engine cycle while the engine is being operated in the first and second displacements; and

the skip fire engine operation does not require any active working chamber to be fired at every engine cycle.

9. An engine controller for managing transitions between operational states of an internal combustion engine having a plurality of working chambers, the engine controller comprising:

a fire control unit arranged to operate the engine in one of a first displacement and a second displacement, each displacement having an associated fixed set of active working chambers wherein the number of active working chambers associated with the first displacement is different than the number of active working chambers associated with the second displacement and wherein the number of active working chambers associated with each of the first and second displacements is greater than zero; and

a firing timing determination module arranged to generate a firing sequence that operates at least one or more of the working chambers of the engine in a skip fire manner during a transition between the first and second displacements wherein the transition between the first and second displacements has a duration of less than five seconds and wherein during skip fire operation at least one of the active working chambers is fired during a first working cycle, skipped during a subsequent second working cycle and fired during a third working cycle that is subsequent to the second working cycle, the first, second and third working cycles occurring during the transition.

10. An engine controller as recited in claim 9 wherein the first and second operational states each involve different, predetermined numbers of non-deactivatable working chambers that are fired at every engine cycle during a particular displacement.

11. An engine controller as recited in claim 9 wherein the operation of the engine in a skip fire manner involves deactivating at least one selected working cycle of at least one selected working chamber and firing at least one selected working cycle of at least one selected working chamber wherein individual working chambers are sometimes deactivated and sometimes fired.

12. An engine controller as recited in claim 9 wherein the firing timing determination module is further arranged to:

generate a firing sequence that includes one or more firing and skip commands for operating the working chambers of the engine;

determinine which working chamber a particular skip command would be applied to;

if the skip command involves a deactivatable working chamber, skip the deactivatable working chamber; and

if the skip command involves a non-deactivatable working chamber, fire the non-deactivatable working chamber.

13. An engine controller as recited in claim 9 wherein the firing timing determination module is further arranged to:

determine a selected working chamber for which a firing or skip command is required;

determine whether the selected working chamber is deactivatable;

if the selected working chamber is deactivatable, apply a firing algorithm to generate a firing or skip command for the selected working chamber; and

if the selected working chamber is non-deactivatable, arrange for the firing of the selected working chamber without applying the firing algorithm.

14. An engine controller as recited in claim 9 further comprising a firing fraction signal library that includes a library of one or more predetermined firing fractions, each firing fraction indicating a percentage of working chambers to fire to deliver a desired output wherein the engine controller is arranged to select a firing fraction from the library and wherein the firing timing determination module is arranged to determine the firing sequence based on the selected firing fraction.

15. An engine controller as recited in claim 14 wherein the selected firing fraction is selected based on one selected from the group consisting of a fill rate and an emptying rate of an intake manifold.

16. An engine controller as recited in claim 9 further comprising a firing decision sequence library that stores one or more predetermined firing sequences wherein the firing timing determination module is arranged to select the firing sequence from the library.

20. A method as recited in claim 9 wherein the number of active working chambers associated with the first displacement is the total number of working chambers in the engine.

17. A method for managing transitions between operational states of an internal combustion engine having a plurality of working chambers, the method comprising:

operating the engine in one of a first displacement and a different, second displacement, each displacement having an associated fixed set of active working chambers wherein the number of active working chambers associated with the first displacement is different than the number of active working chambers associated with the second displacement and wherein the number of active working chambers associated with each of the first and second displacements is greater than zero;

making a transition between the first displacement and the second displacement;

during the transition, selecting a firing parameter from the group consisting of a plurality of predetermined firing fractions stored in a firing fraction library and a plurality of firing sequences stored in a firing sequence library; and

operating the engine in a skip fire manner during the transition to deliver the selected firing parameter wherein during skip fire operation at least one of the active working chambers is fired during a first working cycle, skipped during a subsequent second working cycle and fired during a third working cycle that is subsequent to the second working cycle, the first, second and third working cycles occurring during the transition.

18. A method as recited in claim 17 wherein the first and second displacements each involve different, predetermined numbers of non-deactivatable working chambers that are fired at every engine cycle during a particular operational state.

21. A method as recited in claim 17 wherein the number of active working chambers associated with the first displacement is the total number of working chambers in the engine.