Landing gear tire pressure sensing systems, methods and apparatuses are provided. In various embodiments, a tire pressure sensing system may be mounting to a landing gear. The system may comprise a rotating portion and a stationary portion. The rotating portion and stationary portion may be in electronic communication. The stationary portion may be configured to communicate an indication of tire pressure to a control unit.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    NOSE WHEEL TIRE PRESSURE SENSING SYSTEM AND APPARATUS


    Beteiligte:
    KELLER STEVEN (Autor:in) / SUMMERS PAUL L (Autor:in)

    Erscheinungsdatum :

    08.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    NOSE WHEEL TIRE PRESSURE SENSING SYSTEM AND APPARATUS

    KELLER STEVEN / SUMMERS PAUL L | Europäisches Patentamt | 2015

    Freier Zugriff

    Nose wheel steering system

    ACKS JAMES / REBER KOREY MICHAEL / KUCERA RONALD | Europäisches Patentamt | 2023

    Freier Zugriff

    NOSE WHEEL STEERING SYSTEM

    ACKS JAMES P / REBER KOREY M / KUCERA RONALD | Europäisches Patentamt | 2024

    Freier Zugriff

    Nose-wheel steering system

    ALLEN JASON BRADLEY | Europäisches Patentamt | 2023

    Freier Zugriff

    NOSE-WHEEL STEERING SYSTEM

    ALLEN JASON BRADLEY | Europäisches Patentamt | 2022

    Freier Zugriff