The invention provides a method of reducing the cooling time for disks of a brake (5) of an aircraft wheel (1) fitted with a heat screen (10) extending between the wheel and the disks of the brake, and mounted to rotate on aircraft landing gear about an axis of rotation, the method comprising making perforations (11, 12, 13) through the heat screen to allow air heated by the disks to pass through the heat screen towards the wheel, the perforations being provided with obstacles to block any radiation from passing directly from the disks towards the wheel.


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    Title :

    ECRAN THERMIQUE DE ROUE FREINEE D'AERONEF PERFORE


    Additional title:

    PERFORATED HEAT SHIELD FOR BRAKED WHEEL
    PERFORIERTES HITZESCHILD FÜR GEBREMSTES RAD EINES LUFTFAHRZEUGS


    Contributors:

    Publication date :

    2022-03-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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