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.


    Access

    Download


    Export, share and cite



    Title :

    A FORCE MEASUREMENT SYSTEM


    Contributors:
    TURAN OZCAN (author) / SAMET KAMRAN (author) / KUTMARAL DILAN (author) / DIRIK ERDEM (author)

    Publication date :

    2025-01-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



    A FORCE MEASUREMENT SYSTEM

    TURAN OZCAN / SAMET KAMRAN / KUTMARAL DILAN et al. | European Patent Office | 2023

    Free access

    measurement system of wave force or current force

    HONG JANG PYO / CHO SEOK KYU / SUNG HONG GUN et al. | European Patent Office | 2018

    Free access

    measurement system of wave force or current force

    European Patent Office | 2019

    Free access

    Force measurement

    Emerald Group Publishing | 1999


    Fluid wave and force measurement system

    Larks, J. | Tema Archive | 1978