Method for recognizing erratic combustion

• US 5,433,107 A
• Filed: 06/30/1993
• Issued: 07/18/1995
• Est. Priority Date: 06/30/1992
• Status: Expired due to Term

• Current Assignee: Continental Automotive GmbH (Continental AG)
• Original Assignee: Siemens AG
• Inventors: Vogt, Thomas, Wier, Manfred, Angermaier, Anton
• Primary Examiner(s): RAEVIS, ROBERT R
• Application Number:
  US08/085,351
• Time in Patent Office: 748 Days
• Field of Search: 73/116, 73/117.3, 364/431.07, 364/431.08, 123/419, 123/436
• US Class Current: 73/114.03
• CPC Class Codes: G01M 15/11 by detecting misfire

Abstract

A method is provided for recognizing erratic combustion in a multicylinder internal combustion engine by using a time measuring device to measure successive time periods which a crankshaft needs to rotate through predetermined angles during operating strokes of successive cylinders. The method includes determining a static component by using a calculating device to subtract a time period of the next cylinder in an ignition order from the time period of a cylinder to be examined. The static component is multiplied with a standardizing factor by using the calculating device. A dynamic component is determined by using the calculating device to subtract a time period of a next cylinder in the ignition order from a time period of a preceding cylinder in the ignition order, and a dynamic component is negated. A change component for a lack of smoothness value is formed, the lack of smoothness value is multiplied with a weighting factor to form a weighted value, and the weighted value is set equal to zero if the weighted value is negative. A sliding average is formed from the weighted value in a sliding averaging process. A lack of smoothness value is determined from addition of the static component, the dynamic component, and the sliding average. A combustion misfire is recognized if the smoothness value falls below a given limit value.

Claims

1. A method for recognizing erratic combustion in a multicylinder internal combustion engine by using a time measuring device to measure successive time periods which a crankshaft needs to rotate through predetermined angles during operating strokes of successive cylinders, which comprises:

(a) determining a static component by using a calculating device to subtract a time period of the next cylinder in an ignition order from the time period of a cylinder to be examined;

(b) multiplying the static component with a standardizing factor by using the calculating device;

(c) determining a dynamic component by using the calculating device to subtract a time period of a next cylinder in the ignition order from a time period of a preceding cylinder in the ignition order, and negating the determined dynamic component;

(d) forming a change component by calculating a value (T_n-z -T_n)-(T_n -T_n+z), where T is a time period, n is an index indicating a cylinder, and z is an integer, and multiplying the value with a weighting factor, wherein the change component is set equal to zero if the change component is negative; and

wherein a sliding average is formed of the change component;

(e) determining a lack of smoothness value from addition of the static component, the dynamic component, and the sliding average; and

(f) recognizing a combustion misfire if the smoothness value falls below a given limit value.

2. The method according to claim 1, which comprises taking given limit value from performance curves determined as a function of load, rpm, and temperature of the engine.

3. The method according to claim 2, which comprises reading out performance values from the performance curves, buffer storing the performance values in a buffer store, and comparing lack of smoothness values and limit values for lack of smoothness for the same time periods.

4. The method according to claim 1, which comprises performing a sliding averaging process on the smoothness value GLUK_n according to the equation:

space="preserve" listing-type="equation">GLUK.sub.n =GLUK.sub.n-1 *(1-MITKO)+LUK.sub.n *MITKO,

wherein MITKO is an averaging constant having a range of values between 0 and 1, and LUK_n is the lack of smoothness value.

5. The method according to claim 1, which comprises calculating the standardizing factor NO of the static component as a function of a measuring window n-x through n+y of the dynamic component by the formula NO=x+y.

6. The method according to claim 5, which comprises selecting the measuring window for computing the dynamic component and the change component such that for given cylinders, the time period of the same mechanical segment of the crankshaft is measured.

7. The method according to claim 6, which comprises selecting the angular range of the crankshaft over which the time periods are measured, such that with respect to the top dead center of the motion of a respective piston, at an unfavorable operating point, it furnishes a maximum signal rise in the event of erratic combustion.