An airborne platform includes a body and a sensor device. The body includes a first material having a first flexibility. The sensor device is positioned inside the body, and includes an electric conductor. The electric conductor includes a second material that has a second flexibility that is less than the first flexibility. The sensor device is configured to output an output signal indicating whether the sensor device has undergone mechanical failure in response to a load applied to the sensor device that is greater than a load threshold.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Systems and methods for conductive aircraft sensors


    Beteiligte:
    LUNIN STEPAN V (Autor:in)

    Erscheinungsdatum :

    2021-03-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    SYSTEMS AND METHODS FOR AIRCRAFT BRAKE SENSORS

    ZELL BRIAN KEITH | Europäisches Patentamt | 2019

    Freier Zugriff

    SYSTEMS AND METHODS FOR AIRCRAFT BRAKE SENSORS

    ZELL BRIAN KEITH | Europäisches Patentamt | 2016

    Freier Zugriff

    Systems and methods for aircraft brake sensors

    ZELL BRIAN KEITH | Europäisches Patentamt | 2016

    Freier Zugriff

    Unmanned Aircraft Systems Sensors

    D. D. Weatherington | NTIS | 2005


    METHODS AND SYSTEMS FOR THREAT AIRCRAFT DETECTION USING MULTIPLE SENSORS

    KARANTZA ALEXANDER / SOMANDEPALLI VIJAY | Europäisches Patentamt | 2022

    Freier Zugriff