The aircraft tire pressure resonant loop link assembly electromagnetically couples a magnetic field between a wheel axle electromagnetic adapter transformer primary coil and a tire pressure sensor receiver coil for powering a tire pressure sensor, and includes a pair of spaced apart electrically conductive connecting arms, a single electrically conductive primary loop electrically connected to first ends of the connecting arms mounted adjacent to a secondary tire pressure sensor coil, and a circuit including a resonant tuning capacitor and a secondary coil with one or more electrically conductive loops at second ends of the connecting arms. The tire pressure sensor coil pair includes a transformer core, and secondary resonant coil pair also includes a transformer core.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT TIRE PRESSURE SENSOR RESONANT LOOP LINK


    Weitere Titelangaben:

    FLUGZEUGREIFENDRUCKSENSORRESONANZKREISVERBINDUNG
    LIAISON DE BOUCLES RÉSONANTES DE CAPTEUR DE PRESSION DE PNEU D'AÉRONEF


    Beteiligte:
    LAMPING JEFF (Autor:in) / GONIODSKY IGAL (Autor:in)

    Erscheinungsdatum :

    20.06.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60C VEHICLE TYRES , Fahrzeugreifen



    Aircraft tire pressure sensor resonant loop link

    LAMPING JEFF / GONIODSKY IGAL | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT TIRE PRESSURE SENSOR RESONANT LOOP LINK

    LAMPING JEFF / GONIODSKY IGAL | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRCRAFT TIRE PRESSURE SENSOR RESONANT LOOP LINK

    LAMPING JEFF / GONIODSKY IGAL | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft tire pressure loop link

    LAMPING JEFF / GONIODSKY IGAL | Europäisches Patentamt | 2015

    Freier Zugriff

    AIRCRAFT TIRE PRESSURE LOOP LINK

    LAMPING JEFF / GONIODSKY IGAL | Europäisches Patentamt | 2020

    Freier Zugriff