System for monitoring a set of components of a device
First Claim
1. A system for monitoring a set of components of an aircraft engine, comprising:
- circuitry configured to;
detect anomalies using a set of agents for detecting anomalies (a1, . . . , ai, . . . an) with each one of said agents being configured to receive measurements on physical parameters relating to a sub-set of components of said aircraft engine and to deliver an initial distribution of a probability of an anomaly,receive feedback information as well as the initial distributions of the probability of an anomaly coming from said set of agents,iteratively emerge current distributions of the probability of an anomaly in line with said feedback information, with said current distributions of the probability of an anomaly converging towards a set of optimum distributions of the probability of an anomaly in accordance with said feedback information,synthesise optimal distributions of the probability of an anomaly relating to at least one sub-set of interest of components of said aircraft engine in order to extract risks of an anomaly specific to said sub-set of interest, anddetermine operations of maintenance according to the risks of an anomaly.
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Accused Products
Abstract
A system for monitoring a set of components of a device, including: a detecting system including a set of agents for detecting anomalies, with each agent receiving measurements on physical parameters relating to a sub-set of components of a device and delivering an initial distribution of the probability of an anomaly; an acquiring system which receives feedback information and the initial distributions of the probability of an anomaly from the agents; an emerging system which iteratively emerges current distributions of the probability of an anomaly, with the current distributions of the probability of an anomaly converging towards a set of optimum distributions of the probability of an anomaly; and a synthesizing system which synthesizes optimum distributions of the probability of an anomaly relating to at least one sub-set of interest of components of the device in order to extract the risks of an anomaly specific to the sub-set of interest.
11 Citations
9 Claims
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1. A system for monitoring a set of components of an aircraft engine, comprising:
circuitry configured to; detect anomalies using a set of agents for detecting anomalies (a1, . . . , ai, . . . an) with each one of said agents being configured to receive measurements on physical parameters relating to a sub-set of components of said aircraft engine and to deliver an initial distribution of a probability of an anomaly, receive feedback information as well as the initial distributions of the probability of an anomaly coming from said set of agents, iteratively emerge current distributions of the probability of an anomaly in line with said feedback information, with said current distributions of the probability of an anomaly converging towards a set of optimum distributions of the probability of an anomaly in accordance with said feedback information, synthesise optimal distributions of the probability of an anomaly relating to at least one sub-set of interest of components of said aircraft engine in order to extract risks of an anomaly specific to said sub-set of interest, and determine operations of maintenance according to the risks of an anomaly. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. A method for monitoring a set of components of an aircraft engine, comprising:
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acquiring feedback information as well as initial distributions of a probability of an anomaly coming from a set of agents for detecting anomalies, with each one of said agents being configured to receive measurements on physical parameters relating to a sub-set of components of said aircraft engine before delivering an initial distribution of the probability of an anomaly, iteratively emerging current distributions of the probability of an anomaly in line with said feedback information, with said current distributions of the probability of an anomaly converging towards a set of optimum distributions of the probability of an anomaly in accordance with said feedback information, synthesising optimum distributions of the probability of an anomaly relating to at least one sub-set of interest of components of said aircraft engine in order to extract risks of an anomaly specific to said sub-set of interest, and determining operations of maintenance according to the risks of an anomaly.
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Specification