IP Library Granted Patent US 8,484,145
Granted Patent B2
US 8,484,145 · App. 13/139,741 · Granted Jul 9, 2013

Standardizing data used for monitoring an aeroengine

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Quick Facts
Patent No.
US 8,484,145
App. No.
13/139,741
Granted
Jul 9, 2013
Kind
B2
Abstract

A method and a system for standardizing data used for monitoring an aeroengine, and including: operating over time to collect time-series measurements from the aeroengine; calculating from the time-series measurements a set of indicators Y=(y 1 , . . . , y j , . . . , y m ) specific to elements of the engine; identifying from the time-series measurements an exogenous data set X=(x 1 , . . . , x n ) representative of external context acting on the set of indicators Y; defining a conditional multidimensional model simultaneously handling the indicators of the set of indicators Y while taking account of the exogenous data set X to form a set of estimators Ŷ=(ŷ 1 , . . . , ŷ j , . . . , ŷ m ) corresponding to the set of indicators Y=(y 1 , . . . , y j , . . . , y m ); and normalizing each estimator ŷ j as a function of a reference value for the corresponding indicator y j and of a difference between each estimator ŷ j and corresponding indicator y j so as to form a set of standardized values {tilde over (Y)}=({tilde over (y)} 1 , . . . , {tilde over (y)} j , . . . , {tilde over (y)} m ).

Claims (26)

1. A method of standardizing data used for monitoring an aeroengine, the method comprising:

collecting time-series measurements over time concerning said aeroengine;

from said time-series measurements, calculating a set of indicators Y=(y 1 , . . . , y j , . . . , y m ) that are specific to elements of said engine;

from said time-series measurements, identifying an exogenous data set X=(x 1 , . . . , x n ), representative of external context acting on said set of indicators Y;

for each indicator y j of said set of indicators Y, constructing a projection space E (j) =σ(Y (j) , X) generated by analytic transformations of a subset of indicators Y (j) =(y 1 , . . . y j−1 , y j+1 , . . . y m ) comprising all of the indicators of said set of indicators Y except each said indicator y j and by said exogenous data set X;

for each indicator y j of said set of indicators Y, calculating a corresponding estimator ŷ j by projecting said indicator y j using a regression technique onto said projection space E (j) =σ(Y (j) , X), thereby forming a set of estimators Ŷ=(ŷ 1 , . . . , ŷ j , . . . , ŷ m ) corresponding to said set of indicators Y=(y 1 , . . . , y j , . . . , y m ); and

normalizing each estimator ŷ j as a function of a reference value for the corresponding indicator y j and of a difference between each said estimator ŷ j and said corresponding indicator y j to form a set of standardized values {tilde over (Y)}=({tilde over (y)} 1 , . . . {tilde over (y)} j , . . . , {tilde over (y)} m ).

2. A method according to claim 1 , wherein said time-series measurements are collected during normal operation of said aeroengine.

3. A method according to claim 1 , wherein each standardized value {tilde over (y)} j is calculated by adding a mean or reference value for the corresponding indicator y j to a difference between the corresponding indicator y j and the corresponding estimator ŷ j , using the following equation: {tilde over (y)} j = y j +(y j −ŷ j ).

4. A method according to claim 1 , further comprising analyzing robustness of each estimator using a cross evaluation technique serving to select an optimum projection space.

5. A method according to claim 1 , wherein said projection space is constructed using expert criteria with help of physical formulations of relationships between the indicators and between the indicators and the exogenous data.

6. A method according to claim 1 , wherein said space is constructed automatically by using a neural network.

7. A method according to claim 6 , wherein said neural network is a model having nodes.

8. A method according to claim 1 , wherein the indicators of said set of indicators Y=(y 1 , . . . , y j , . . . , y m ) are specific to physical and/or logical elements of said engine.

9. A method according to claim 1 , wherein the indicators of said set of indicators Y=(y 1 , . . . , y j , . . . , y m ) are calculated using expert criteria by constructing an FMECA.

10. A method according to claim 1 , wherein the indicators are identified by referencing particular points or particular functions summarizing details or shapes of certain curves representative of said time-series measurements.

11. A method according to claim 1 , wherein the exogenous data X=(x 1 , . . . , x n ) acting on the indicators is identified using expert criteria by dependency analysis enabling context data associated with the indicators to be listed.

12. A method according to claim 1 , wherein said regression is a linear regression.

13. A system for standardizing data used for monitoring an aeroengine, the system comprising:

means for operating over time to collect time-series measurements from said aeroengine;

means for calculating from said time-series measurements a set of indicators Y=(y 1 , . . . y j , . . . , y m ) specific to elements of said engine;

means for identifying from said time-series measurements an exogenous data set X=(x 1 , . . . , x n ) representative of external context acting on said set of indicators Y;

means for constructing for each indicator y j of said set of indicators Y, a projection space E (j) =σ(Y (j) , X) generated by analytic transformations of a subset of indicators Y (j) =(y 1 , . . . , y j−1 , y j+1 , . . . , y m ) comprising all of the indicators of said set of indicators Y except each said indicator y j , and by said exogenous data set X;

means for calculating for each said indicator y j of said set of indicators Y a corresponding estimator ŷ j by using a regression technique to project each said indicator y j onto said projection space E (j) =σ(Y (j) , X), forming a set of estimators Ŷ=(ŷ 1 , . . . , ŷ j , . . . , ŷ m ) corresponding to said set of indicators Y=(y 1 , . . . , y j , . . . , y m ); and

means for normalizing each estimator ŷ j as a function of a reference value for the corresponding indicator y j and of a difference between each said estimator ŷ j and said corresponding indicator y j so as to form a set of standardized values {tilde over (Y)}=({tilde over (y)} 1 , . . . , {tilde over (y)} j , . . . , {tilde over (y)} m ).

14. A non-transitory computer readable medium including computer executable instructions for implementing the standardization method according to claim 1 when executed by a processor.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 7, 2011
From: LACAILLE, JEROME
To: SNECMA
Reel/Frame 026864/0703 →