A control stick extending outward from a body located at an air vehicle enables the pilot to control tasks such as position and speed of the air vehicle. A strain gauge arm located on a control line in connection with the control stick measures a strain transferred to the control stick. A trim actuator located on the related strain gauge arm on the control line measures positional changes of the air vehicle. A sensor located on the strain gauge arm generates force data at a rate predetermined by the user upon a force exerted on the control stick. A control unit receives force data from sensors and positional percentage values from the trim actuator.


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    Titel :

    A FORCE MEASUREMENT SYSTEM


    Beteiligte:
    TURAN OZCAN (Autor:in) / SAMET KAMRAN (Autor:in) / KUTMARAL DILAN (Autor:in) / DIRIK ERDEM (Autor:in)

    Erscheinungsdatum :

    09.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE / B64C AEROPLANES , Flugzeuge



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