A structural health monitoring system and method includes a plurality of sensors configured to collect sensed data, a first structural component, and a controller configured to receive the sensed data and detect a first condition based upon the sensed data. The controller is further configured to initiate a first structural interrogation of the first structural component upon detection of the condition.
AUTOMATED STRUCTURAL INTERROGATION OF AIRCRAFT COMPONENTS
INTERROGATION STRUCTURELLE AUTOMATISEE DE COMPOSANTES D'AERONEF
2018-03-19
Patent
Electronic Resource
English
IPC: | G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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 |
AUTOMATED STRUCTURAL INTERROGATION OF AIRCRAFT COMPONENTS
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