IP Library Granted Patent US 10,345,194
Granted Patent B2
US 10,345,194 · App. 14/575,096 · Granted Jul 9, 2019

Detection device for initiating failures of a mechanical system

Inventor: Valerio Gerez (Yerres, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
G01M15/00G01H1/003G01M15/12G01M15/14G01N29/04
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Quick Facts
Patent No.
US 10,345,194
App. No.
14/575,096
Granted
Jul 9, 2019
Kind
B2
Abstract

A method and a device for detection of initiating failures in a mechanical system. The device includes an acquisition circuit to acquire packets of endogenic and exogenic time signals corresponding to measurements of endogenic and exogenic parameters specific to the mechanical system respectively, at successive instants, and a chopping circuit to chop a passband of the endogenic signal packets into a determined set of frequency sub-bands, at each instant in the successive instants. The device further includes a calculation circuit to determine a corresponding estimating signal for each frequency sub-band at each instant in the successive instants; and a detection circuit to receive each estimating signal and the corresponding exogenic signal packets during the successive instants, and to detect any deviation in each estimating signal representing initiating failures of the machine in iso-context.

Claims (20)

1. A device for detection of initiating failures in a mechanical system composed of a machine or part of a machine on a test bench, the device comprising:

an acquisition circuit configured to acquire packets of endogenic and exogenic time signals corresponding to measurements of endogenic and exogenic parameters specific to said mechanical system respectively, at successive instants;

a chopping circuit configured to chop a passband of said endogenic signal packets into a determined set of frequency sub-bands, at each instant in said successive instants;

a calculation circuit configured to determine a corresponding estimating signal for each frequency sub-band at each instant in said successive instants; and

a detection circuit configured to receive each said estimating signal and the corresponding exogenic signal packets during said successive instants, and to detect any deviation in each said estimating signal representing initiating failures of said machine in iso-context.

2. The device according to claim 1 , wherein said estimating signal is an RMS (Root Mean Square) signal, in each frequency sub-band.

3. The device according to claim 1 , wherein said acquisition circuit is further configured to:

receive an endogenic signal at each instant in said successive instants, representing measurements of endogenic parameters and an exogenic signal representing measurements of exogenic parameters, said exogenic signal being acquired at a predetermined low frequency (fs1) and said endogenic signal being acquired at a predetermined high frequency (fs2), and

chop said endogenic and exogenic signals in time into said endogenic and exogenic time signal packets respectively.

4. The device according to claim 1 , wherein said chopping circuit comprises a determined set of filters adapted to chop the passband of endogenic signal packets into a set of consecutive frequency sub-bands.

5. The device according to claim 4 , wherein the calculation circuit is configured to under-sample each estimating signal corresponding to each frequency sub-band at a same sampling frequency as a low frequency fs1 of exogenic time signals.

6. The device according to claim 5 , wherein the detection circuit is configured to calculate a probability of deviation conditioned by the corresponding exogenic time signals for each estimating signal, said estimating signal and said corresponding exogenic signals being sampled at the same said low frequency fs1.

7. The device according to claim 1 , wherein said endogenic measurements comprise vibration measurements and/or acoustic measurements, and said exogenic measurements comprise context measurements among the following measurements: pressure measurements, temperature, torque and speed measurements of at least part of the elements of said mechanical system.

8. The device according to claim 1 , wherein said machine is an aircraft engine or a component of an aircraft engine.

9. A method of detecting initiating failures in a mechanical system composed of a machine or part of a machine on a test bench, the method comprising:

acquiring endogenic and exogenic time signal packets at successive instants corresponding to endogenic parameter measurements and exogenic parameter measurements specific to said mechanical system respectively;

chopping a passband of said endogenic signal packets into a determined set of frequency sub-bands at each instant in said successive instants;

determining an estimating signal corresponding to each frequency sub-band at each instant in said successive instants;

receiving each said estimating signal and the corresponding exogenic signal packets during said successive instants; and

detecting any deviation in each said estimating signal representative of initiating failures of said machine, in iso-context.

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 Apr 1, 2015
From: GEREZ, VALERIO
To: SNECMA
Reel/Frame 035307/0792 →
Priority Claims (1)
FR 13 63177 · Dec 20, 2013 · national
Continuity (1)
Related Publication 20150177101A1 · Jun 25, 2015