Method, devices and computer program for assisting in the diagnostic of an aircraft system, using failure condition graphs

Patent metadata

Field	Value
Publication number	US-8996340-B2
Application number	US-201113276632-A
Country	US
Kind code	B2
Filing date	Oct 19, 2011
Priority date	Oct 22, 2010
Publication date	Mar 31, 2015
Grant date	Mar 31, 2015

Abstract

A diagnostic system of an aircraft, comprising a plurality of sub-systems at least one of which performs monitoring and notification of at least one detected event, using graphs of feared events. After a message of notification of occurrence of the detected event has been received, a set of feared events linked to this message is created from the graph of feared events, and logic expressions are constructed according to logic links represented in the graph of feared events. A group of feared events then is created according to elements of the logic expressions. The minimal vertexes of the logic expressions associated with the feared events of the group are calculated and form a diagnosis of the system.

First claim

The invention claimed is:

1. A method for establishing an aid in diagnosis of a complex system of an aircraft comprising a plurality of sub-systems, at least one sub-system of the plurality of sub-systems comprising circuitry configured to monitor and provide notifications regarding at least one detected event,
the method using:
a failure condition graph at least partially modeling the complex system, the failure condition graph comprising a plurality of peaks, each peak being connected by a logic implication relationship to at least one other peak of the plurality of peaks, the plurality of peaks comprising:
one peak representing a failure condition event; and
one peak representing only at least one element of the complex system, the at least one element being able to break down, and

the method comprising:
receiving at least one message of notification of occurrence of the at least one detected event;
creating a set of failure events, each said failure event of the set of failure events being associated with a peak of the failure condition graph linked to the at least one received notification message;
for each said failure event of the set of failure events, constructing, from the failure condition graph, at least one logic expression leading to the failure event, the at least one logic expression being based on elements of the complex system;
creating at least one group of failure events of the set of failure events, the at least one element being common to two logic expressions linked to two separate failure events of the at least one group, the logic expressions associated with the failure events of the at least one group representing a diagnosis relating to the at least one detected event; and
determining minimal vertexes of the logic expressions of the failure events of the at least one group of failure events, the minimal vertexes forming minimal diagnoses of the diagnosis relating to the at least one detected event.

2. The method according to claim 1 ,
wherein the failure condition graph of failure events further comprises at least one peak representing a message associated with the at least one detected event, and
wherein the method further comprises identifying, in the failure condition graph, at least one peak representing a message according to the at least one received message, each said failure event of the set of failure events being associated with a peak of the failure condition graph linked to the at least one notification message via the at least one identified peak.

3. The method according to claim 1 , further comprising performing at least one of displaying, storing, and transmitting the diagnosis relating to the at least one detected event.

4. The method according to claim 1 , wherein the failure condition graph further comprises at least one sub-graph of failure events, the at least one sub-graph of failure events at least partially modeling one of the sub-systems of the plurality of sub-systems.

5. The method according to claim 1 , wherein the failure condition graph further comprises at least one peak representing a logic operation, at least one of the logic expressions comprising a logic operation represented by a peak of the failure condition graph.

6. A non-transitory computer-readable storage medium storing computer-readable instructions that, when executed by a computer, cause the computer to perform the method according to claim 1 .

7. A maintenance system for an aircraft comprising processing circuitry configured to perform the method according to claim 1 .

8. The maintenance system according to claim 7 , further comprising transmitting circuitry configured to transmit the diagnosis to a system distant from the maintenance system.

9. The maintenance system according to claim 7 or claim 8 configured to operate with an aircraft.

10. A data processing system comprising:
circuitry configured to receive information items relating to at least one message of notification of occurrence of at least one event detected by monitoring and notification circuitry of a sub-system of a complex system of an aircraft comprising a plurality of sub-systems; and
processing circuitry configured to perform the method of claim 1 .

11. The method according to claim 1 , wherein the one peak representing the failure condition event represents an interface between two of the plurality of sub-systems.

12. The method according to claim 1 , wherein the one peak representing only the at least one element of the complex system that is able to break down is associated with a triggering of the failure condition event.

13. The method according to claim 1 , wherein said receiving the at least one message includes receiving a plurality of messages according to a batch mode.

14. The method according to claim 1 ,
wherein the failure condition graph includes a plurality of peaks representing only at least one element of the complex system that are able to break down, each of said plurality of peaks representing different elements of the complex system that are able to break down,
wherein the diagnosis is expressed by the failure condition graph in terms of starting from said plurality of peaks representing different elements of the complex system that are able to break down, and
wherein the method further comprises determining a minimal vertex of regarding said plurality of peaks representing different elements of the complex system that are able to break down.

15. A method for establishing an aid in diagnosis of a complex system of an aircraft comprising a plurality of sub-systems, at least one sub-system of the plurality of sub-systems comprising circuitry configured to monitor and provide notifications regarding at least one detected event,
the method using:
a failure condition graph at least partially modeling the complex system, the failure condition graph comprising a plurality of peaks, each peak being connected by a logic implication relationship to at least one other peak of the plurality of peaks, the plurality of peaks comprising:
one peak representing a failure condition event; and
one peak representing only at least one element of the complex system, the at least one element being able to break down, and

the method comprising:
receiving at least one message of notification of occurrence of the at least one detected event;
creating a set of failure events, each said failure event of the set of failure events being associated with a peak of the failure condition graph linked to the at least one received notification message;
for each said failure event of the set of failure events, constructing, from the failure condition graph, at least one logic expression leading to the failure event, the at least one logic expression being based on elements of the complex system; and
creating at least one group of failure events of the set of failure events, the at least one element being common to two logic expressions linked to two separate failure events of the at least one group, the logic expressions associated with the failure events of the at least one group representing a diagnosis relating to the at least one detected event,
wherein the failure condition graph includes a plurality of peaks representing only at least one element of the complex system that are able to break down, each of said plurality of peaks representing different elements of the complex system that are able to break down,
wherein the diagnosis is expressed by the failure condition graph in terms of starting from said plurality of peaks representing different elements of the complex system that are able to break down,

Assignees

• Cheriere Vincent
• Abelin Christophe
• Roger Jeremy
• Vilalta-Estrada Laia
• Airbus Sas
• Airbus Operations Sas

Inventors

• Cheriere Vincent
• Abelin Christophe
• Roger Jeremy
• Vilalta-Estrada Laia

Classifications

• G06F11/0748

  in a remote unit communicating with a single-box computer node experiencing an error/fault (remote testing G06F11/2294) · CPC title

• G06F11/079 Primary

  Root cause analysis, i.e. error or fault diagnosis (in a hardware test environment G06F11/22; in a software test environment G06F11/36) · CPC title

• G05B23/0248

  Causal models, e.g. fault tree; digraphs; qualitative physics · CPC title

• G06F11/0739

  in a data processing system embedded in automotive or aircraft systems · CPC title