METHOD AND A DEVICE FOR MONITORING A REDUNDANT MEASUREMENT SYSTEM
First Claim
1. A method of monitoring a redundant measurement system for an aeroengine, the method being executed by an electronic unit of said engine, said monitoring method comprising:
- a step of obtaining first measurements of a physical magnitude measured in said engine; and
a step of obtaining second measurements of said physical magnitude;
wherein the method comprises;
a step of calculating detection residues as a function of differences between the first measurements and the second measurements;
a step of determining a mean-jump flag representing a difference between the mean of the distribution of detection residues and the mean of a reference distribution;
a step of determining a variance-jump flag representing a difference between the variance of the distribution of the detection residues and the variance of the reference distribution;
a step of determining a change-of-slope flag representing a difference between the slope of the distribution of the detection residues and the slope of the reference distribution; and
a step of generating a diagnostic notice as a function of said mean-jump flag, of said variance-jump flag, and of said change-of-slope flag.
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Accused Products
Abstract
The invention relates to monitoring a redundant measurement system of an aeroengine by means of an electronic unit. The monitoring comprises a step of obtaining first measurements of a physical magnitude measured in said engine, and a step of obtaining second measurements of said physical magnitude. According to the invention, the method includes a step of calculating detection residues as a function of differences between the first and second measurements, a step of determining a mean-jump flag, a step of determining a variance-jump flag, a step of determining a change-of-slope flag, and a step of generating a diagnostic notice as a function of said mean-jump flag, of said variance-jump flag, and of said change-of-slope flag.
6 Citations
10 Claims
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1. A method of monitoring a redundant measurement system for an aeroengine, the method being executed by an electronic unit of said engine, said monitoring method comprising:
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a step of obtaining first measurements of a physical magnitude measured in said engine; and a step of obtaining second measurements of said physical magnitude; wherein the method comprises; a step of calculating detection residues as a function of differences between the first measurements and the second measurements; a step of determining a mean-jump flag representing a difference between the mean of the distribution of detection residues and the mean of a reference distribution; a step of determining a variance-jump flag representing a difference between the variance of the distribution of the detection residues and the variance of the reference distribution; a step of determining a change-of-slope flag representing a difference between the slope of the distribution of the detection residues and the slope of the reference distribution; and a step of generating a diagnostic notice as a function of said mean-jump flag, of said variance-jump flag, and of said change-of-slope flag. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
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10. A monitoring device for monitoring a redundant measurement system of an aeroengine, the device comprising:
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means for obtaining first measurements of a physical magnitude that is measured in said engine; and means for obtaining second measurements of said physical magnitude; wherein the device comprises; means for calculating detection residues as a function of differences between the first measurements and the second measurements; means for determining a mean-jump flag representing a difference between the mean of the distribution of detection residues and the mean of a reference distribution; means for determining a variance-jump flag representing a difference between the variance of the distribution of the detection residues and the variance of the reference distribution; means for determining a change-of-slope flag representing a difference between the slope of the distribution of the detection residues and the slope of the reference distribution; and means for generating a diagnostic notice as a function of said mean-jump flag, of said variance-jump flag, and of said change-of-slope flag.
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Specification