A braking system (4) for an aircraft wheel (2) comprises first and second brake rotor discs (20a, 20b) axially spaced along an axis (A) and rotationally coupled to the wheel (2), a stator disc (24) arranged axially between the first and second rotor discs (20a, 20b), and a heat shield (34) mounted to at least one of the first and second rotor discs (20a, 20b). Radially outer portions (30) of the first and second rotor discs (20a, 20b) extend radially outwardly of the stator disc (24) to define a gap (32) between the radially outer portions (30) of the first and second rotor discs (20a, 20b). The heat shield (34) extends at least partially over or into the gap (32).


    Access

    Download


    Export, share and cite



    Title :

    BRAKING SYSTEM FOR AN AIRCRAFT WHEEL


    Additional title:

    BREMSSYSTEM FÜR EIN FLUGZEUGRAD
    SYSTÈME DE FREINAGE POUR ROUE D'AÉRONEF


    Contributors:
    STRAS KAROL (author) / WYSZOWSKI ADAM (author) / PACAK PAWEL (author)

    Publication date :

    2023-02-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



    AIRCRAFT WHEEL BRAKING DEVICE

    MOLINE SYLVAIN / HEUDE SÉBASTIEN / MALADOT PIERRE | European Patent Office | 2024

    Free access

    Aircraft wheel braking device

    MERLIN SIMONE / HEAD STEVEN / MALADOT PHILIPPE | European Patent Office | 2023

    Free access

    BRAKING SYSTEM FOR AN AIRCRAFT WHEEL

    STRAS KAROL / WYSZOWSKI ADAM / PACAK PAWEL | European Patent Office | 2023

    Free access

    Method for managing braking of aircraft wheel

    JABER SYLVAIN / CEKIC RAFFI | European Patent Office | 2016

    Free access

    AIRCRAFT WHEEL BRAKING PERFORMANCE COMMUNICATIONS SYSTEMS AND METHODS

    GADZINSKI JOHN | European Patent Office | 2016

    Free access