Systems and methods for determining aircraft component phase position are provided. In one embodiment, a method can include receiving a set of data (200, fig 2) from a data acquisition system 119 associated with a component 122. The method can include identifying a plurality of phase reference points (510A-C, fig 6) based, at least in part, on the set of data (200). Each phase reference point (510A-C) can be indicative of a phase position of the component 122 relative to the data acquisition system 119 at a respective point in time. The method can include generating a model (602, fig 6) based, at least in part, on the plurality of phase reference points (510A-C). The model (602) can be indicative of the phase position of the component 122 relative to the data acquisition system 119 at a plurality of times. The method can include determining the phase position of the component 122 at one or more points in time based, at least in part, on the model (602).


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    Title :

    Aircraft component monitoring system


    Contributors:

    Publication date :

    2017-12-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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