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 240 and a stationary portion 250. 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.


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    Title :

    NOSE WHEEL TIRE PRESSURE SENSING SYSTEM AND APPARATUS


    Additional title:

    BUGRAD-REIFENDRUCKÜBERWACHUNGSSYSTEM UND VORRICHTUNG
    SYSTÈME ET APPAREIL DE DÉTECTION DE LA PRESSION D'UN PNEU DE ROUE AVANT


    Contributors:

    Publication date :

    2015-10-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60C VEHICLE TYRES , Fahrzeugreifen / B64C AEROPLANES , Flugzeuge



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