A landing gear system includes a landing gear collar and a strut assembly supported by the landing gear collar. The strut assembly includes a piston that is adjustable between a fully extended position and a fully compress position. The landing gear system further includes a rotary encoder and a controller. The rotary encoder rotates in response adjusting the piston and to outputs a data value in response to its rotation. The controller is in signal communication with the rotary encoder and determines a stroke of the piston based on the data value output from the rotary encoder.


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    Titel :

    CONFIGURABLE ROTARY ENCODER INCLUDING TWO POINT INFLIGHT AUTO CALIBRATION AND ERROR ADJUSTMENT


    Weitere Titelangaben:

    KONFIGURIERBARER DREHGEBER MIT AUTOMATISCHER ZWEIPUNKTKALIBRIERUNG UND FEHLERANPASSUNG WÄHREND DES FLUGS
    ENCODEUR ROTATIF CONFIGURABLE COMPRENANT UN ÉTALONNAGE AUTOMATIQUE ET UN RÉGLAGE D'ERREUR EN VOL À DEUX POINTS


    Beteiligte:

    Erscheinungsdatum :

    2024-08-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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