Virtual fuel quality sensor

• US 7,383,816 B2
• Filed: 01/09/2006
• Issued: 06/10/2008
• Est. Priority Date: 01/09/2006
• Status: Active Grant

• Current Assignee: Innio Waukesha Gas Engines Incorporated
• Original Assignee: Dresser Incorporated (Nagano Keiki Company Limited)
• Inventors: Zurlo, James Richard
• Primary Examiner(s): Cronin; Stephen K.
• Assistant Examiner(s): Castro; Arnold
• Application Number:
  US11/328,425
• Publication Number:
  US 20070157903A1
• Time in Patent Office: 883 Days
• Field of Search: 123/406.3, 701/111
• US Class Current: 123/406.3
• CPC Class Codes: F02D 19/088 by estimation, i.e. without using direct measurements of a corresponding sensor
• CPC Class Codes: F02D 2200/0612 determined by estimation
• CPC Class Codes: F02D 41/0025 Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
• CPC Class Codes: F02P 5/1527 with means allowing burning of two or more fuels, e.g. super or normal, premium or regular
• CPC Class Codes: Y02T 10/30 Use of alternative fuels, e.g. biofuels
• CPC Class Codes: Y02T 10/40 Engine management systems

Abstract

A method of operating a multiple combustion chamber internal combustion engine includes advancing an ignition timing of a first subset of the combustion chambers from an operating ignition timing until a knock event is detected while concurrently operating the remaining combustion chambers at the operating ignition timing. A first knock margin of the first subset of combustion chambers is determined in relation to a difference between the operating ignition timing and the ignition timing at the knock event. A characteristic of a fuel supplied to the combustion chambers is determined in relation to at least the first knock margin.

Claims

1. A method of operating a multiple combustion chamber internal combustion engine comprising:

advancing an ignition timing of a first subset of the combustion chambers from an operating ignition timing until a knock event is detected while concurrently operating the remaining combustion chambers at the operating ignition timing;

determining a first knock margin of the first subset of combustion chambers in relation to a difference between the operating ignition timing and the ignition timing at the knock event;

advancing the ignition timing in a second subset of the combustion chambers from an operating ignition timing until a knock event is detected while concurrently operating the remaining combustion chambers at the operating ignition timing;

determining a second knock margin of the second subset of combustion chambers in relation to a difference between the operating ignition timing and the ignition timing at the knock event; and

determining a characteristic of a fuel supplied to the combustion chambers in relation to the first and second knock margins.

2. The method of claim 1 wherein determining a characteristic of the fuel supplied to the combustion chambers comprises determining a knock resistance of the fuel.

3. The method of claim 1 further comprising adjusting the operating ignition timing of the first subset of combustion chambers to a first operating ignition timing as a function of the knock margin determined for the first combustion chamber.

4. The method of claim 1 comprising adjusting the operating ignition timing of the second subset of combustion chambers to a second operating ignition timing as a function of the knock margin determined for the second combustion chamber.

5. The method of claim 4 wherein the first operating ignition timing and second operating ignition timing are different if the knock margin for the first subset of the combustion chambers is different than the second subset of the combustion chambers.

6. The method of claim 1 wherein the first subset is one of the multiple combustion chambers.

7. The method of claim 1 further comprising adjusting a fuel controller as a function of at least one of the first knock margin and the second knock margin.

8. The method of claim 7 further comprising adjusting a fuel controller to supply less fuel to the first subset of combustion chambers than is supplied to the second subset of combustion chambers if the first knock margin decreases.

9. The method of claim 7 further comprising adjusting a boost controller as a function of at least one of the first knock margin and the second knock margin.

10. A method comprising:

(i) advancing an ignition timing of one combustion chamber of a multiple combustion chamber engine from an operating ignition timing until a knock event is detected while concurrently operating the remaining combustion chambers at the operating ignition timing;

(ii) determining a knock margin of the one combustion chamber;

(iii) repeating operations (i) and (ii) for subsequent of the combustion chambers until a knock margin has been determined for a plurality of the combustion chambers; and

(iv) determining a characteristic of the fuel supplied to the combustion chambers in relation to the determined knock margins.

11. The method of claim 10 further comprising:

repeating operations (i)-(iii) a plurality of times;

determining from a difference in knock margin data between at least a first of the plurality of combustion chambers and another of the plurality of combustion chambers over the plurality of times that at least a portion of the change in knock margin of the first of the combustion chambers is due to a change in the first combustion chamber.

12. The method of claim 11 further comprising adjusting the operating ignition timing for the first the combustion chamber as a function of the change in knock margin.

13. The method of claim 11 further comprising adjusting at least one of an amount of fuel supplied to the first combustion chamber and an amount of boost supplied to the first combustion chamber as a function of the change in knock margin.

14. The method of claim 11 further comprising compiling knock margin data from the plurality of times operations (i)-(iii) are repeated and outputting the compiled knock margin data correlated to combustion chambers.

15. The method of claim 10 wherein determining a characteristic of the fuel supplied to the combustion chambers comprises determining a knock resistance of the fuel.

16. The method of claim 10 further comprising outputting information indicative of the knock margin.

17. The method of claim 10 wherein repeating operations (i) and (ii) for subsequent of the combustion chambers until a knock margin has been determined for a plurality of the combustion chambers comprises repeating operations (i) and (ii) until a knock margin has been determined for all of the combustion chambers.

18. A system for operating a multiple combustion chamber internal combustion engine, comprising a processor configured to perform operations comprising:

advancing an ignition timing of a first subset of the combustion chambers from an operating ignition timing until a knock event is detected while concurrently operating the remaining combustion chambers at the operating ignition timing;

determining a first knock margin of the first subset of combustion chambers in relation to a difference between the operating ignition timing and the ignition timing at the knock event;

advancing the ignition timing in a second subset of the combustion chambers from an operating ignition timing until a knock event is detected while concurrently operating the remaining combustion chambers at the operating ignition timing;

determining a second knock margin of the second subset of combustion chambers in relation to a difference between the operating ignition timing and the ignition timing at the knock event; and

determining a characteristic of a fuel supplied to the combustion chambers in relation to the first and second knock margins.

19. The system of claim 18 wherein the processor is further configured to perform operations comprising determining a knock resistance of the fuel supplied to the combustion chambers.

20. The system of claim 18 wherein the processor is further configured to perform operations comprising adjusting the operating ignition timing of the first subset of combustion chambers to a first operating ignition timing as a function of the knock margin determined for the first combustion chamber.