Combustion pressure monitoring system for a combustion engine

• US 8,146,409 B2
• Filed: 07/22/2008
• Issued: 04/03/2012
• Est. Priority Date: 08/06/2007
• Status: Active Grant

• Current Assignee: GM Global Technology Operations LLC (General Motors Company)
• Original Assignee: GM Global Technology Operations LLC (General Motors Company)
• Inventors: Catanese, Alessandro, Parisi, Filippo, Pisoni, Eugenio, Monferrato, Claudio
• Primary Examiner(s): MCCALL, ERIC SCOTT
• Application Number:
  US12/177,782
• Publication Number:
  US 20090038385A1
• Time in Patent Office: 1,351 Days
• Field of Search: 731/141.6, 731/141.7, 731/142.2, 731/141.8
• US Class Current: 73/114.16
• CPC Class Codes: G01L 23/30 Means for indicating consecutively positions of pistons or cranks of internal-combustion engines in combination with pressure indicators
• CPC Class Codes: G01M 15/08 by monitoring pressure in cylinders

Abstract

A pressure monitoring system for a combustion engine includes, but is not limited to of combustion chambers and pressure sensors associated to at least some of the combustion chambers. A multiplexer has inputs connected to at least a first one and a second one of the pressure sensors. A non-zero phase shift exists between the operating cycles of first and second ones of the combustion chambers associated to the first and second pressure sensors. A controller controls the multiplexer to output data from the first pressure sensor while the first combustion chamber is in a predetermined portion of its operating cycle and pressure data from the second pressure sensor while the second combustion chamber is in the predetermined portion of its operating cycle.

Claims

1. A pressure monitoring system for a combustion engine, comprising:

a first combustion chamber;

a second combustion chamber;

a first pressure sensor associated with the first combustion chamber

a second pressure sensor associated with the second combustion chamber;

a multiplexer connected to the first pressure sensor and the second pressure sensor; and

a controller configured to control the multiplexer to produce first pressure data from the first pressure sensor while the first combustion chamber is in a predetermined portion of an operating cycle comprising an instant of injecting fuel into at least one of the first combustion chamber and the second combustion chamber and second pressure data from the second pressure sensor while the second combustion chamber is in said predetermined portion of the operating cycle of the second combustion chamber, wherein the operating cycle of the first combustion chamber is identical to the operating cycle of the second combustion chamber but for a non-zero phase shift therebetween.

2. The pressure monitoring system of claim 1, wherein the predetermined portion of the operating cycle comprises an instant of igniting an air/fuel mixture in at least one of the first combustion chamber and the second combustion chamber.

3. The pressure monitoring system of claim 1, wherein the first combustion chamber and the second combustion chamber have intake valves and exhaust valves and the predetermined portion of the operating cycle of the first combustion chamber and the second combustion chamber excludes opening times of said intake values and said exhaust valves.

4. The pressure monitoring system of claim 1, wherein an analog-to-digital converter is connected to an output of said multiplexer.

5. The pressure monitoring system of claim 1, wherein the first pressure sensor is configured to sample the pressure in the first combustion chamber at a plurality of predetermined crankshaft angles.

6. The pressure monitoring system of claim 1, wherein the controller is configured to determine a pressure maximum from said first pressure data and said second pressure data and to carry out an adjustment of said predetermined portion of the operating cycle so that the pressure maximum is detected at a predetermined location of said predetermined portion.

7. The pressure monitoring system of claim 6, wherein the controller is configured to carry out said adjustment based only on pressure data obtained in a combustion-free operating cycle.

8. The pressure monitoring system of claim 1, wherein a buffer memory is connected to an output of said multiplexer.

9. The pressure monitoring system of claim 8, wherein a buffer memory is configured to store a pressure sample in association to each of the plurality of predetermined crankshaft angles.

10. A pressure monitoring system for a combustion engine, comprising:

a first combustion chamber;

a second combustion chamber;

a first pressure sensor associated with the first combustion chamber

a second pressure sensor associated with the second combustion chamber;

a multiplexer connected to the first pressure sensor and the second pressure sensor; and

a controller configured to control the multiplexer to produce first pressure data from the first pressure sensor while the first combustion chamber is in a predetermined portion of an operating cycle and second pressure data from the second pressure sensor while the second combustion chamber is in said predetermined portion of the operating cycle of the second combustion chamber, wherein the operating cycle of the first combustion chamber is identical to the operating cycle of the second combustion chamber but for a non-zero phase shift therebetween,

wherein the controller is further configured to determine a pressure maximum from said first pressure data and said second pressure data and to carry out an adjustment of said predetermined portion of the operating cycle so that the pressure maximum is detected at a predetermined location of said predetermined portion.

11. The pressure monitoring system of claim 10, wherein the controller is configured to carry out said adjustment based only on pressure data obtained in a combustion-free operating cycle.

12. The pressure monitoring system of claim 10, wherein the predetermined portion of the operating cycle comprises an instant of injecting fuel into at least one of the first combustion chamber and the second combustion chamber.

13. The pressure monitoring system of claim 10, wherein the first combustion chamber and the second combustion chamber have intake valves and exhaust valves and the predetermined portion of the operating cycle of the first combustion chamber and the second combustion chamber excludes opening times of said intake values and said exhaust valves.

14. The pressure monitoring system of claim 10, wherein the predetermined portion of the operating cycle comprises an instant of igniting an air/fuel mixture in at least one of the first combustion chamber and the second combustion chamber.

15. The pressure monitoring system of claim 10, wherein an analog-to-digital converter is connected to an output of said multiplexer.

16. The pressure monitoring system of claim 10, wherein the first pressure sensor is configured to sample the pressure in the first combustion chamber at a plurality of predetermined crankshaft angles.

17. The pressure monitoring system of claim 10, wherein a buffer memory is connected to an output of said multiplexer.

18. The pressure monitoring system of claim 17, wherein a buffer memory is configured to store a pressure sample in association to each of the plurality of predetermined crankshaft angles.