Methods and systems for identifying aircraft faults
A method for identifying aircraft faults, comprising: receiving aircraft health dataset comprising plurality of maintenance identifiers which each identify aircraft fault; storing diagnostics database storing plurality of part identifiers which each identify part of aircraft which is possible cause of generation of at least one maintenance identifier; generating graph of plurality of maintenance identifiers and plurality of edges in which maintenance identifiers are connected to one another by edge if maintenance identifiers are identified by common part identifier in diagnostics database; extracting clique from graph, clique comprising plurality of maintenance identifiers and respective plurality of edges of graph; determining intersection between at least two edges of clique; identifying candidate part identifier which is common to intersecting edges of clique, candidate part identifier identifying part of aircraft which is possible cause of generation of at least some of maintenance identifiers of clique; and outputting candidate part identifier.
1. A method of performing maintenance on an aircraft, the method comprising:
receiving, at a processing arrangement which incorporates a processor and a memory, an aircraft health dataset comprising a plurality of maintenance identifiers, each maintenance identifier of the plurality of maintenance identifiers identifying an aircraft fault;
storing, at the processing arrangement, a diagnostics database storing a plurality of part identifiers, each part identifier of the plurality of part identifiers identifying a part of the aircraft which is a possible cause of the generation of at least one maintenance identifier;
generating, by the processing arrangement, a graph of the plurality of maintenance identifiers and a plurality of edges in which maintenance identifiers are connected to one another by an edge of the plurality of edges when the maintenance identifiers are identified by a common part identifier in the diagnostics database;
extracting, by the processing arrangement, a clique from the graph by enumerating a maximal clique in the graph, the clique comprising a plurality of the maintenance identifiers and a respective plurality of edges of the graph;
identifying, by the processing arrangement, a candidate part identifier which is common to at least two edges of the clique, the candidate part identifier identifying a part of the aircraft which is a possible cause of the generation of at least some of the maintenance identifiers of the clique;
outputting, from the processing arrangement, the candidate part identifier; and
performing a maintenance task on the aircraft by replacing or servicing the part of the aircraft which is identified by the candidate part identifier.
2. The method of claim 1 , wherein enumerating a maximal clique in the graph comprises performing, by the processing arrangement, a Bron-Kerbosch algorithm.
3. The method of claim 2 , wherein the method further comprises:
extracting, by the processing arrangement, a monochromatic maximum clique in the graph.
4. The method of claim 1 , wherein the method further comprises:
extracting, by the processing arrangement, a further clique from the graph, the further clique comprising a further plurality of the maintenance identifiers and a respective further plurality of edges of the graph; and
identifying, by the processing arrangement, a further candidate part identifier which is common to at least two edges of the further clique, the further candidate part identifier identifying a further part of the aircraft which is a possible cause of the generation of at least some of the further maintenance identifiers of the further clique.
5. The method of claim 4 , wherein extracting a further clique from the graph comprises:
enumerating a further maximal clique in the graph.
6. The method of claim 5 , wherein enumerating a further maximal clique in the graph comprises performing, by the processing arrangement, a Bron-Kerbosch algorithm.
7. The method of claim 6 , wherein the method further comprises:
extracting, by the processing arrangement, a further monochromatic maximum clique in the graph.
8. The method of claim 7 , wherein the method further comprises:
ranking, by the processing arrangement, the clique and the further clique by size.
9. The method of claim 7 , wherein the method further comprises:
ranking, by the processing arrangement, the clique and the further clique by monochromaticity.
10. The method of claim 1 , wherein the method further comprises:
receiving, at the processing arrangement, an updated aircraft health dataset; and
checking, by the processing arrangement, whether any maintenance messages have been cleared in response to the maintenance task being performed.
11. A system for performing maintenance on an aircraft comprising:
a processor and a memory, the memory storing executable instructions which, when executed by the processor, cause the processor to:
receive an aircraft health dataset comprising a plurality of maintenance identifiers, each maintenance identifier of the plurality of maintenance identifiers identifying an aircraft fault;
store a diagnostics database storing a plurality of part identifiers, each part identifier of the plurality of part identifiers identifying a part of the aircraft which is a possible cause of the generation of at least one maintenance identifier;
generate a graph of the plurality of maintenance identifiers and a plurality of edges in which maintenance identifiers are connected to one another by an edge of the plurality of edges when the maintenance identifiers are identified by a common part identifier in the diagnostics database;
extract a clique from the graph by enumerating a maximal clique in the graph, the clique comprising a plurality of the maintenance identifiers and a respective plurality of edges of the graph;
identify a candidate part identifier which is common to at least two edges of the clique, the candidate part identifier identifying a part of the aircraft which is a possible cause of the generation of at least some of the maintenance identifiers of the clique;
output the candidate part identifier; and
perform a maintenance task on the aircraft by replacing or servicing the part of the aircraft which is identified by the candidate part identifier.
12. The system of claim 11 , wherein the memory stores executable instructions which, when executed by the processor, cause the processor to:
perform a Bron-Kerbosch algorithm to extract the clique from the graph.
13. The system of claim 12 , wherein the memory stores executable instructions which, when executed by the processor, cause the processor to:
extract a monochromatic maximum clique in the graph.
14. The system of claim 11 , wherein the memory stores executable instructions which, when executed by the processor, cause the processor to:
extract a further clique from the graph, the further clique comprising a further plurality of the maintenance identifiers and a respective further plurality of edges of the graph; and
identify a further candidate part identifier which is common to at least two edges of the further clique, the further candidate part identifier identifying a further part of the aircraft which is a possible cause of the generation of at least some of the further maintenance identifiers of the further clique.
15. The system of claim 14 , wherein the memory stores executable instructions which, when executed by the processor, cause the processor to:
extract a further monochromatic maximum clique in the graph.
16. The system of claim 15 , wherein the memory stores executable instructions which, when executed by the processor, cause the processor to:
rank the clique and the further clique by monochromaticity.
17. A non-transitory computer-readable medium storing executable instructions which, when executed by a processor, cause the processor to:
receive an aircraft health dataset comprising a plurality of maintenance identifiers, each maintenance identifier of the plurality of maintenance identifiers identifying an aircraft fault;
store a diagnostics database storing a plurality of part identifiers, each part identifier of the plurality of part identifiers identifying a part of an aircraft which is a possible cause of the generation of at least one maintenance identifier;
generate a graph of the plurality of maintenance identifiers and a plurality of edges in which maintenance identifiers are connected to one another by an edge of the plurality of edges when the maintenance identifiers are identified by a common part identifier in the diagnostics database;
extract a clique from the graph by enumerating a maximal clique in the graph, the clique comprising a plurality of the maintenance identifiers and a respective plurality of edges of the graph;
identify a candidate part identifier which is common to at least two edges of the clique, the candidate part identifier identifying a part of the aircraft which is a possible cause of the generation of at least some of the maintenance identifiers of the clique;
output the candidate part identifier; and
perform a maintenance task on the aircraft by replacing or servicing the part of the aircraft which is identified by the candidate part identifier.