Method for controlling a marine internal combustion engine

• US 10,094,321 B1
• Filed: 05/17/2017
• Issued: 10/09/2018
• Est. Priority Date: 05/17/2017
• Status: Active Grant

• Current Assignee: Brunswick Corporation
• Original Assignee: Brunswick Corporation
• Inventors: Anschuetz, Steven M., Przybyl, Andrew J., O'Brien, William P., Snyder, Matthew W., Osthelder, Robert R.
• Primary Examiner(s): Nguyen, Hung Q
• Assistant Examiner(s): MO, XIAO EN
• Application Number:
  US15/597,752
• Time in Patent Office: 510 Days
• CPC Class Codes: F02D 2041/1422 Variable gain or coefficients
• CPC Class Codes: F02D 2200/604 Engine control mode selected by driver, e.g. to manually start particle filter regeneration or to select driving style
• CPC Class Codes: F02D 37/02 one of the functions being ignition
• CPC Class Codes: F02D 41/04 Introducing corrections for particular operating conditions F02D41/14 takes precedence
• CPC Class Codes: F02D 41/1454 the characteristics being an oxygen content or concentration or the air-fuel ratio
• CPC Class Codes: F02D 41/1495 Detection of abnormalities in the air/fuel ratio feedback system
• CPC Class Codes: F02D 41/22 Safety or indicating devices for abnormal conditions in air/fuel ratio feedback systems F02D41/1495, in electric control linkage F02D11/107, in purge control systems F02M25/0809
• CPC Class Codes: F02D 41/222 relating to the failure of sensors or parameter detection devices
• CPC Class Codes: F02D 41/2422 Selective use of one or more tables
• CPC Class Codes: F02D 41/2454 Learning of the air-fuel ratio control
• CPC Class Codes: F02D 41/345 Controlling injection timing F02D41/365 takes precedence
• CPC Class Codes: F02P 5/045 combined with electronic control of other engine functions, e.g. fuel injection in general F02D37/02
• CPC Class Codes: F02P 5/1502 using one central computing unit
• 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: F02P 5/1514 with means for optimising the use of registers or of memories, e.g. interpolation
• CPC Class Codes: Y02T 10/40 Engine management systems

Abstract

Controlling a marine engine includes operating the engine according to an initial set of mapped parameter values to achieve a first target fuel-air equivalence ratio, determining a first actual fuel-air equivalence ratio, and using a feedback controller to minimize a difference between the first target and actual ratios. Feedback controller outputs are used to populate an initial set of adapt values to adjust combustion parameter values from the initial set of mapped parameter values. The method includes transitioning to operating the engine according to a subsequent set of mapped parameter values to achieve a different target fuel-air equivalence ratio. The method includes determining a second actual fuel-air equivalence ratio, using the feedback controller to minimize a difference between the second target and actual ratios, and using feedback controller outputs to populate a subsequent set of adapt values to adjust combustion parameter values from the subsequent set of mapped parameter values.

Claims

1. A method for controlling a marine internal combustion engine, the method being carried out by a control module and comprising:

operating the engine according to an initial set of mapped parameter values that correspond to a combustion parameter, the initial set of mapped parameter values being configured to achieve a first target fuel-air equivalence ratio in a combustion chamber of the engine;

determining a first actual fuel-air equivalence ratio in the combustion chamber;

using a feedback controller to minimize a difference between the first target fuel-air equivalence ratio and the first actual fuel-air equivalence ratio;

using outputs of the feedback controller to populate an initial set of adapt values by which to adjust combustion parameter values determined from the initial set of mapped parameter values;

transitioning to operating the engine according to a subsequent set of mapped parameter values that correspond to the combustion parameter, the subsequent set of mapped parameter values being configured to achieve a second, different target fuel-air equivalence ratio in the combustion chamber; and

after the step of transitioning, determining a second actual fuel-air equivalence ratio in the combustion chamber, using the feedback controller to minimize a difference between the second target fuel-air equivalence ratio and the second actual fuel-air equivalence ratio, and using the outputs of the feedback controller to populate a subsequent set of adapt values by which to adjust combustion parameter values determined from the subsequent set of mapped parameter values.

2. The method of claim 1, wherein the initial set of adapt values is unique from the subsequent set of adapt values, and further comprising populating only one of the initial set of adapt values and the subsequent set of adapt values at a time.

3. The method of claim 2, further comprising:

measuring current values of engine operating conditions;

beginning the step of transitioning in response to the engine operating conditions meeting predetermined criteria; and

ceasing populating the initial set of adapt values in response to beginning the step of transitioning.

4. The method of claim 3, further comprising beginning populating the subsequent set of adapt values in response to completing the step of transitioning.

5. The method of claim 4, further comprising filtering in at least one of an output and a gain of the feedback controller to minimize the difference between the second target fuel-air equivalence ratio and the second actual fuel-air equivalence ratio in response to completing the step of transitioning.

6. The method of claim 3, wherein the step of transitioning further comprises:

transitioning from operating the engine according to an initial value of the combustion parameter determined from the initial set of mapped parameter values to operating the engine according to a subsequent value of the combustion parameter determined from the subsequent set of mapped parameter values; and

ramping from an initial adapt value determined from the initial set of adapt values to a subsequent adapt value determined from the subsequent set of adapt values.

7. The method of claim 6, further comprising determining both the initial adapt value and the subsequent adapt value based on a speed of the engine and a torque demand on the engine.

8. The method of claim 3, wherein the initial and subsequent sets of mapped parameter values contain nominal mapped parameter values, and the method further comprises:

determining a nominal combustion parameter value from one of the initial and subsequent sets of mapped parameter values;

determining an adapt value from a corresponding one of the initial and subsequent sets of adapt values; and

multiplying the nominal combustion parameter value by the adapt value to determine an adapted combustion parameter value according to which the engine is operated.

9. The method of claim 3, further comprising adjusting the combustion parameter values from the initial and subsequent sets of mapped parameter values by the initial and subsequent sets of adapt values, respectively, and overwriting the initial and subsequent sets of mapped parameter values with the respective adjusted combustion parameter values.

10. The method of claim 1, wherein the combustion parameter is a quantity of fuel to be supplied to the combustion chamber.

11. The method of claim 1, wherein one of the first and second target fuel-air equivalence ratios is greater than or equal to 1 and the other of the first and second target fuel-air equivalence ratios is less than 1.

12. A method for controlling a marine internal combustion engine, the method being carried out by a control module and comprising:

operating the engine according to an initial set of mapped fuel quantity values, the initial set of mapped fuel quantity values being configured to achieve a first target fuel-air equivalence ratio in a combustion chamber of the engine;

determining a first actual fuel-air equivalence ratio in the combustion chamber;

using a feedback controller to minimize a difference between the first target fuel-air equivalence ratio and the first actual fuel-air equivalence ratio;

using outputs of the feedback controller to populate an initial set of fuel trim values by which to adjust fuel quantity values determined from the initial set of mapped fuel quantity values;

transitioning to operating the engine according to a subsequent set of mapped fuel quantity values, the subsequent set of mapped fuel quantity values being configured to achieve a second, different target fuel-air equivalence ratio in the combustion chamber; and

after the step of transitioning, determining a second actual fuel-air equivalence ratio in the combustion chamber, using the feedback controller to minimize a difference between the second target fuel-air equivalence ratio and the second actual fuel-air equivalence ratio, and using the outputs of the feedback controller to populate a subsequent set of fuel trim values by which to adjust fuel quantity values determined from the subsequent set of mapped fuel quantity values.

13. The method of claim 12, wherein the initial set of fuel trim values is unique from the subsequent set of fuel trim values, and further comprising populating only one of the initial set of fuel trim values and the subsequent set of fuel trim values at a time.

14. The method of claim 13, further comprising:

measuring current values of engine operating conditions;

beginning the step of transitioning in response to the engine operating conditions meeting predetermined criteria; and

ceasing populating the initial set of fuel trim values in response to beginning the step of transitioning.

15. The method of claim 14, further comprising beginning populating the subsequent set of fuel trim values in response to completing the step of transitioning.

16. The method of claim 15, further comprising filtering in at least one of an output and a gain of the feedback controller to minimize the difference between the second target fuel-air equivalence ratio and the second actual fuel-air equivalence ratio in response to completing the step of transitioning.

17. The method of claim 14, wherein the step of transitioning further comprises:

transitioning from operating the engine according to an initial fuel quantity value determined from the initial set of mapped fuel quantity values to operating the engine according to a subsequent fuel quantity value determined from the subsequent set of mapped fuel quantity values; and

ramping from an initial fuel trim value determined from the initial set of fuel trim values to a subsequent fuel trim value determined from the subsequent set of fuel trim values.

18. The method of claim 17, further comprising determining both the initial fuel trim value and the subsequent fuel trim value based on a speed of the engine and a torque demand on the engine.

19. The method of claim 14, wherein the initial and subsequent sets of mapped fuel quantity values contain nominal mapped fuel quantity values, and the method further comprises:

determining a nominal fuel quantity value from one of the initial and subsequent sets of mapped fuel quantity values;

determining a fuel trim value from a corresponding one of the initial and subsequent sets of fuel trim values; and

multiplying the nominal fuel quantity value by the fuel trim value to determine an adapted fuel quantity value according to which the engine is operated.

20. The method of claim 12, wherein one of the first and second target fuel-air equivalence ratios is greater than or equal to 1 and the other of the first and second target fuel-air equivalence ratios is less than 1.