Systems, computer-implemented methods and/or computer program products that facilitate automating fault isolation of flight control surfaces and damage detection of aircraft are provided. In one embodiment, a system (100) utilizes a processor (102) that executes computer implemented components stored in memory (104). One or more sensors (106) monitor wing and flight control surface from one or more vantage points to obtain full coverage of the wing. A machine vision component (108) assesses condition of the wing and the flight control surface based on results of the one or more sensors (106). A spectrographic component (110) detects leaks by monitoring airflow for traces of fuel or hydraulic fluid.
AUTOMATED FAULT ISOLATION OF FLIGHT CONTROL SURFACES AND DAMAGE DETECTION OF AIRCRAFT THROUGH NON-CONTACT MEASUREMENT
AUTOMATISIERTE FEHLERISOLIERUNG VON FLUGKONTROLLFLÄCHEN UND SCHADENSERKENNUNG VON FLUGZEUGEN DURCH EINE BERÜHRUNGSLOSE MESSUNG
ISOLATION AUTOMATISÉE DES DÉFAILLANCES DES SURFACES DE COMMANDE DE VOL ET DÉTECTION DE DOMMAGES DE L'AVION PAR UNE MESURE SANS CONTACT
2022-05-11
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 |
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