ABSTRACT A method of monitoring a power drive unit installed on an aircraft is provided. The method includes causing, by a controller, sensors to measure an angular position at corresponding locations along at least one wing of the aircraft. The controller, as part of the method, receives the angular position from the one or more sensors and analyzes the angular position to generate feedback information to implement the monitoring of the power drive unit. CA 3064625 2019-12-10


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    Title :

    DRIVELINE TORQUE MONITORING FOR LONG-TERM HEALTH ASSESSMENT


    Contributors:

    Publication date :

    2021-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / 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 / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein



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