IP Library Granted Patent US 10,393,624
Granted Patent B2
US 10,393,624 · App. 14/400,374 · Granted Aug 27, 2019

Information processor system for monitoring a complex system

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Quick Facts
Patent No.
US 10,393,624
App. No.
14/400,374
Granted
Aug 27, 2019
Kind
B2
Abstract

An information processor system for monitoring a complex system and including a mechanism receiving at least one piece of event detection information associated with a detection time and a mechanism generating at least one remanent confidence level value that decreases over time starting from the detection time.

Claims (21)

1. An sensor system for monitoring a complex system comprising:

at least one sensor placed in a particular location in the complex system and configured to detect one or more physical magnitudes whenever a variation is detected relative to a threshold;

processing circuitry configured to

receive at least one piece of event detection information from the at least one sensor associated with a detection time, a fault flag being associated with the at least one piece of event detection information, where the received at least one piece of event detection information includes a magnitude level of a fault indicated by the fault flag and an initial confidence level;

generate at least one remanent confidence level value that decreases from the initial confidence level over time starting from the detection time, the remanent confidence level value being associated with the fault flag and the magnitude level associated with the received at least one piece of event detection information; and

when a new piece of event detection information is received that is associated with the fault flag and includes an initial confidence level and a same magnitude level as the at least one piece of event detection information, generate an integrated remanent confidence level value for the new piece of event detection information which is based on the initial confidence level that is included in the new piece of event detection information and the remanent confidence level value that exists at a time when the new piece of event detection information is received,

wherein the at least one piece of detection information associated with a detection time is included in a failure message including at least a failure time, the initial confidence level, and a failure identifier.

2. The sensor system according to claim 1 , wherein the remanent confidence level value is associated with at least one failure magnitude value selected as a function of a failure magnitude value associated with the detection time.

3. The sensor system according to claim 1 , wherein the processing circuitry is configured to generate at least two remanent confidence level values, each associated with a malfunction magnitude value, each of the at least two remanent confidence level values varying independently of the other.

4. The sensor system according to claim 1 , wherein the processing circuitry is configured to generate at least two remanent confidence level values each associated with a different malfunction magnitude value, and reset to zero one of the at least two remanent confidence level values that was non-zero at a previous time when the other remanent confidence level value becomes non-zero at a current time.

5. The sensor system according to claim 1 , wherein, the remanent confidence level value is a raw value.

6. The sensor system according to claim 1 , wherein the initial confidence level and the raw remanent confidence level value are combined to give the integrated remanent confidence value by an addition.

7. The sensor system according to claim 1 , wherein a duration from which the remanent confidence level value is zero may be set by a user, for a single fault flag, or for a plurality of fault flags.

8. The sensor system according to claim 1 , wherein a decreasing relationship may be set by a user for the remanent confidence level value, for a single fault flag, or for a plurality of fault flags.

9. The sensor system according to claim 1 , wherein the complex system is an engine.

10. An sensing method for monitoring a complex system, the method comprising:

detecting, by at least one sensor placed in a particular location in the complex system, one or more physical magnitudes whenever a variation is detected relative to a threshold

receiving at least one piece of event detection information from the at least one sensor associated with a detection time, a fault flag being associated with the at least one piece of event detection information, where the received at least one piece of event detection information includes a magnitude level of a fault indicated by the fault flag and an initial confidence level;

generating at least one remanent confidence level value that decreases from the initial confidence level over time starting from the detection time, the remanent confidence level value being associated with the fault flag and the magnitude level associated with the received at least one piece of event detection information; and

when a new piece of event detection information is received that is associated with the fault flag and includes an initial confidence level and a same magnitude level as the at least one piece of event detection information, generating an integrated remanent confidence level value for the new piece of event detection information which is based on the initial confidence level that is included in the new piece of event detection information and the remanent confidence level value that exists at a time when the new piece of event detection information is received,

wherein the at least one piece of detection information associated with a detection time is included in a failure message including at least a failure time, the initial confidence level, and a failure identifier.

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 Nov 11, 2014
From: LE GONIDEC, SERGE; MALIKOV, DIMITRI; BERECHET, ION; BERECHET, STEFAN
To: SNECMA
Reel/Frame 034143/0719 →