Coordination of vehicle actuators during firing fraction transitions

• US 9,926,868 B2
• Filed: 10/20/2016
• Issued: 03/27/2018
• Est. Priority Date: 06/23/2016
• Status: Active Grant

• Current Assignee: GM Global Technology Operations LLC (General Motors Company), Tula Technology, Incorporated
• Original Assignee: GM Global Technology Operations LLC (General Motors Company), Tula Technology, Incorporated
• Inventors: Serrano, Louis J., Carlson, Steven E., Haase, Steven J., Dibble, Donavan L., Rayl, Allen B.
• Primary Examiner(s): Moubry, Grant
• Application Number:
  US15/298,542
• Publication Number:
  US 20170370309A1
• Time in Patent Office: 523 Days
• Field of Search: 123198 F, 123 9017, 123349, 123350, 701105
• CPC Class Codes: B60W 10/023 Fluid clutches
• CPC Class Codes: B60W 10/06 including control of combustion engines
• CPC Class Codes: B60W 2710/025 Clutch slip, i.e. difference between input and output speeds
• CPC Class Codes: B60W 30/188 Controlling power parameters of the driveline, e.g. determining the required power
• CPC Class Codes: F02D 17/02 Cutting-out cutting-out engines in multiple engine arrangements F02D25/04
• CPC Class Codes: F02D 2041/001 for engines with variable valve actuation
• CPC Class Codes: F02D 2250/21 during a transition between engine operation modes or states
• CPC Class Codes: F02D 37/02 one of the functions being ignition
• CPC Class Codes: F02D 41/0087 Selective cylinder activation, i.e. partial cylinder operation deceleration cut-off F02D41/123
• CPC Class Codes: F02D 41/0215 in relation with elements of the transmission
• CPC Class Codes: F02P 5/145 using electrical means
• CPC Class Codes: F02P 5/1504 with particular means during a transient phase, e.g. acceleration, deceleration, gear change during starting F02P5/1506
• CPC Class Codes: Y02T 10/40 Engine management systems

Abstract

A variety of methods and arrangements are described for controlling transitions between firing fractions during skip fire and potentially variable displacement operation of an engine. In general, cam first transition strategies are described in which the cam phase is changed to, or close to a target cam phase before a corresponding firing fraction change is implemented. When the cam phase change associated with a desired firing fraction change is relatively large, the firing fraction change is divided into a series of two or more firing fraction change steps—with each step using a cam first transition approach. A number of intermediate target selection schemes are described as well.

Claims

1. A method of controlling an engine to deliver a requested engine output, the method comprising:

(a) while the engine is operating at a first firing fraction and an associated first cam phase, determining a requested firing fraction that is different than the first firing fraction, the requested firing fraction being a second firing fraction having an associated second cam phase, the second cam phase being different than the first cam phase;

(b) selecting an intermediate firing fraction that is between the first and second firing fractions, the intermediate firing fraction having an associated intermediate cam phase;

(c) identifying the selected intermediate firing fraction as a target firing fraction and the intermediate cam phase as a target cam phase;

(d) initiating a transition from the first cam phase to one of the second cam phase or the target cam phase;

(e) after an actual cam phase is at or within a predetermined range of the target cam phase transitioning to the target firing fraction;

(f) when the target firing fraction is not the second firing fraction, selecting a next firing fraction having an associated next cam phase and setting the target firing fraction to be the next firing fraction and setting the target cam phase to be the next cam phase and causing the cam phase to transition towards the next cam phase or the second cam phase; and

(g) iteratively repeating (e) and (f) until the requested firing fraction is reached; and

(h) directing operation of the engine during the transitions to deliver the requested engine output, whereby an actual commanded firing fraction changes over a course of the transition.

2. The method as recited in claim 1 wherein when the first firing fraction is greater than one half and the target firing fraction is less than one half, the intermediate firing fraction is one half.

3. The method as recited in claim 1 wherein:

an engine controller that directs the firing fraction transitions has a defined set of potential operational firing fractions;

at various particular operating conditions, only an associated subset of the potential operational firing fractions are designated as candidates for use;

the firing fraction candidates for use do not always include all potential operational firing fractions that are capable of delivering the requested engine output; and

each target firing fraction is selected from the firing fraction candidates for use at current operating conditions.

4. The method as recited in claim 3 wherein the intermediate firing fraction is determined by selecting the lowest firing fraction candidate that has an associated cam phase within a predefined range of the first cam phase at the current operating conditions.

5. The method as recited in claim 3 wherein the next firing fraction is determined by selecting the lowest firing fraction candidate that has an associated cam phase within a predefined range of the previous target cam phase.

6. The method as recited in claim 5 wherein the predefined range of the target cam phase is no more than about ±

3 degrees of crank shaft angle at the current operating conditions.

7. The method as recited in claim 3 wherein each selected next firing fraction is the lowest firing fraction candidate that has an associated cam phase within the predefined range of the immediately preceding target firing fraction, or the next lower firing fraction candidate when no lower firing fraction candidate has an associated cam phase within the predefined range.

8. The method as recited in claim 3 wherein each selected next firing fraction is the next lower firing fraction candidate.

9. The method as recited in claim 3 wherein:

when at least one of the firing fraction candidates that is lower than the first firing fraction has an associated cam phase within a predefined range of the first cam phase at the current operating conditions, the intermediate firing fraction is the lowest firing fraction candidate that has an associated cam phase within the predefined range; and

when no lower firing fraction candidate has an associated cam phase within the predefined range, the intermediate firing fraction is either a predefined firing fraction or the next lower firing fraction candidate.

10. The method as recited in claim 1 wherein during each firing fraction transition, a commanded firing fraction and a commanded intake manifold pressure are changed during the transition in a manner that helps provide the desired engine output throughout the transition.

11. The method as recited in claim 1 wherein when the requested firing fraction changes during a transition to a new requested firing fraction that is higher than a then current firing fraction, a firing fraction immediately begins transitioning to the new requested firing fraction.

12. The method as recited in claim 1 wherein when the requested firing fraction changes during a transition to a new requested firing fraction that is lower than a then current firing fraction, the transition continues according to the method of claim 1 to the new requested firing fraction and a new second cam phase associated with the new requested firing fraction.

13. The method as recited in claim 1 wherein:

an engine controller that directs the firing fraction transitions has a defined set of firing fraction candidates;

each target firing fraction is selected from the firing fraction candidates for use at current operating conditions.

14. The method as recited in claim 1 wherein the target firing fraction is a lesser fraction than the first firing fraction.

15. The method as recited in claim 1 wherein the set of available firing fractions only includes one and fractions having a denominator that is not greater than nine.

16. A method of controlling an engine to deliver a requested engine output, the method comprising:

while the engine is operating at a first firing fraction having an associated first cam phase, determining a desired second firing fraction and an associated second cam phase, the second cam phase being different than the first cam phase;

initiating a transition from the first cam phase to the second cam phase;

after an actual cam phase is at or within a predetermined range of the second cam phase transitioning to the second firing fraction, wherein transition to the second firing fraction is initiated only after the actual cam phase is at or within the predetermined range of the second cam phase; and

directing operation of the engine during the transitions to deliver the requested engine output, whereby an actual commanded firing fraction gradually changes over a course of the transition from the first firing fraction to the second firing fraction.

17. An engine controller arranged to direct skip fire operation of an engine, the engine controller being configured to:

(a) direct operation of the engine at a first firing fraction and a first cam phase;

(b) while the engine is operating at the first firing fraction and the first cam phase, determine a requested firing fraction that is different than the first firing fraction, the requested firing fraction being a second firing fraction having an associated second cam phase, the second cam phase being different than the first cam phase;

(c) select an intermediate firing fraction that is between the first and second firing fractions, the intermediate firing fraction having an associated intermediate cam phase;

(d) identify the selected intermediate firing fraction as a target firing fraction and the intermediate cam phase as a target cam phase;

(e) initiate a transition from the first cam phase to one of the second cam phase or the target cam phase;

(f) after an actual cam phase is at or within a predetermined range of the target cam phase transition to the target firing fraction;

(g) when the target firing fraction is not the second firing fraction, select a next firing fraction having an associated next cam phase and set the target firing fraction to be the next firing fraction and set the target cam phase to be the next cam phase and cause the cam phase to transition towards the next cam phase or the second cam phase; and

(h) iteratively repeat (f) and (g) until the second cam phase and second firing fraction are reached; and

(i) direct operation of the engine during the transitions to deliver the requested engine output, whereby an actual commanded firing fraction changes over a course of the transitions.

18. The engine controller as recited in claim 17, wherein the engine controller has a defined set of potential operational firing fractions;

at various particular operating conditions, only an associated subset of the potential operational firing fractions are designated as candidates for use;

the firing fraction candidates for use do not always include all potential operational firing fractions that are capable of delivering the requested engine output; and

each target firing fraction is selected from the firing fraction candidates for use at current operating conditions.

19. The engine controller as recited in claim 17 further configured to handle changes in the requested firing fraction that occur during a transition by:

when the requested firing fraction changes during a transition to a new requested firing fraction that is higher than a then current firing fraction, immediately begin transitioning to the new requested firing fraction; and

when the requested firing fraction changes during a transition to a new requested firing fraction that is lower than the then current firing fraction, the transition continues to the new requested firing fraction and a new second cam phase associated with the new requested firing fraction.

20. An engine controller arranged to direct skip fire operation of an engine, the engine controller being configured to:

direct operation of the engine at a first firing fraction and a first cam phase;

while the engine is operating at the first firing fraction and the first cam phase, determine a desired second firing fraction and an associated second cam phase, the second cam phase being different than the first cam phase;

initiate a transition from the first cam phase to the second cam phase;

after an actual cam phase is at or within a predetermined range of the second cam phase direct a transition to the second firing fraction, wherein the transition to the second firing fraction is initiated only after the actual cam phase is at or within the predetermined range of the second cam phase; and

direct operation of the engine during the cam phase and firing fraction transitions to deliver the requested engine output, whereby an actual commanded firing fraction changes over a course of the transition from the first firing fraction to the second firing fraction.