Aircraft Failure Diagnostic Method and System
The present invention relates to an aircraft failure diagnostic method and system. The method includes one configuration phase defining the possible correlations between the detectable faults. Each of these correlations are associated with data pertinently describing the circumstances of the malfunc...
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| creator | BAILLY CARINE ALBOUY CHRISTIAN |
| description | The present invention relates to an aircraft failure diagnostic method and system. The method includes one configuration phase defining the possible correlations between the detectable faults. Each of these correlations are associated with data pertinently describing the circumstances of the malfunction and appropriate failure-repair operations. A phase of correlating the detected fault is performed phase of recovering the data describing the circumstances of the malfunction and a phase of determining failure-repair operations is then performed. |
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The method includes one configuration phase defining the possible correlations between the detectable faults. Each of these correlations are associated with data pertinently describing the circumstances of the malfunction and appropriate failure-repair operations. A phase of correlating the detected fault is performed phase of recovering the data describing the circumstances of the malfunction and a phase of determining failure-repair operations is then performed.</description><language>eng</language><subject>CALCULATING ; COMPUTING ; COUNTING ; ELECTRIC DIGITAL DATA PROCESSING ; MEASURING ; PHYSICS ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><creationdate>2008</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20081009&DB=EPODOC&CC=US&NR=2008249678A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20081009&DB=EPODOC&CC=US&NR=2008249678A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BAILLY CARINE</creatorcontrib><creatorcontrib>ALBOUY CHRISTIAN</creatorcontrib><title>Aircraft Failure Diagnostic Method and System</title><description>The present invention relates to an aircraft failure diagnostic method and system. The method includes one configuration phase defining the possible correlations between the detectable faults. Each of these correlations are associated with data pertinently describing the circumstances of the malfunction and appropriate failure-repair operations. 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The method includes one configuration phase defining the possible correlations between the detectable faults. Each of these correlations are associated with data pertinently describing the circumstances of the malfunction and appropriate failure-repair operations. A phase of correlating the detected fault is performed phase of recovering the data describing the circumstances of the malfunction and a phase of determining failure-repair operations is then performed.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR |
| title | Aircraft Failure Diagnostic Method and System |
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