According to one embodiment, an aircraft part environmental stress analysis system (200) includes a part failure repository (250), a part history repository (235), and a failure analysis engine (260). The part failure repository (250) is configured to store a plurality of failure records, each failure record (255) identifying a failed aircraft part. The part history repository (235) is configured to store a plurality of part records (300), each part record storing, for a failed aircraft part, at least one measurement of an aspect of a natural environment of which the failed aircraft part was subject to. The failure analysis engine (260) is operable to compare the plurality of failure records (255) to the plurality of part records (300) and identify at least one potential environmental cause of failure for a plurality of failed aircraft parts based on the comparison.
Aircraft comprising an aircraft part failure analysis system
Luftfahrzeug mit einem Fehleranalysesystem für Luftfahrzeugsteile
Aéronef comprenant un système d'analyse de défaillances de pièces
2017-07-19
Patent
Electronic Resource
English
IPC: | G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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