Disclosed is a brake disc 210a for an aircraft wheel brake comprising: a temperature sensing device 300 comprising a surface acoustic wave, SAW, sensor element and a sensor antenna, wherein: the temperature sensing device 300 is attached to the brake disc 210a by means of a ceramic adhesive 602 and one or more ceramic bolts 604. The brake disc 210a may be annular in form and have a hole through the centre to receive a torque tube 218, and a notch 605 intended to receive a spline of the torque tube. The temperature sensing device 300 may be mounted in the notch 605. Also disclosed is a method of attaching a temperature sensing device to a brake disc of an aircraft wheel brake.


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    Titel :

    Wheel brake and temperature sensing device


    Beteiligte:
    MAURICIO PEREIRA DA CUNHA (Autor:in) / ROBERT L LAD (Autor:in) / IAN WHITE (Autor:in) / KURT BRÜGGEMANN (Autor:in) / RICHARD DOWNING (Autor:in) / MAUD CONSOLA (Autor:in)

    Erscheinungsdatum :

    2023-11-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01K MEASURING TEMPERATURE , Messen der Temperatur / B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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