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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Format: | Patent |
Sprache: | eng |
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Zusammenfassung: | 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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