In one embodiment described herein is a mast moment sensor system for a rotorcraft comprising a rotor shaft bearing strain sensor. In some embodiments the mast moment sensor system is configured to compute a rotor mast moment using the rotor shaft bearing strain information. In one embodiment herein the rotor shaft bearing strain sensor comprises a fiber optic strain sensor.


    Access

    Download


    Export, share and cite



    Title :

    MAST MOMENT SENSING FOR AN AIRCRAFT


    Additional title:

    MASTMOMENTERFASSUNG FÜR EIN FLUGZEUG
    DÉTECTION DU MOMENT DE FLEXION DU MÂT POUR UN AÉRONEF


    Contributors:
    BUEHNE ALAN (author)

    Publication date :

    2025-06-25


    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



    MAST MOMENT SENSING FOR AN AIRCRAFT

    BUEHNE ALAN | European Patent Office | 2024

    Free access

    Mast torque sensing for aircraft

    BOONE ALLAN | European Patent Office | 2025

    Free access

    AIRCRAFT DRAIN MAST

    SCHRECK TOBIAS / NAPP CHRISTIAN | European Patent Office | 2024

    Free access

    Mast-mounted aircraft generator

    RAAD BERNARD ANTHONY | European Patent Office | 2019

    Free access

    MAST-MOUNTED AIRCRAFT GENERATOR

    RAAD BERNARD ANTHONY | European Patent Office | 2016

    Free access