A technique for comprising the compression fatigue rupture strength of the carcass reinforcement external layer (3) of an aeroplane tire in the region of bending on the rim (7). The distance (d) between a point (A) on the bead external face (6) and the carcass reinforcement external layer (3), measured along the straight line perpendicular at this point to the bead external face, is at a maximum at the point (M) on the bead external face that is the orthogonal projection of the radially external end (E) of the filling element (5) onto the bead external face, and the distance (dmax) between the orthogonal projection (M) of the radially external end (E) of the filling element (5) onto the bead external face (6) and the carcass reinforcement external layer (3) is at least equal to 1.3 times the distance (d1) between the orthogonal projection (L) of the center (O) of the bead wire core (4) onto the bead external face and the carcass reinforcement external layer.


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    Title :

    ARMATURE DE CARCASSE POUR PNEUMATIQUE D'AVION


    Additional title:

    CARCASS REINFORCEMENT FOR AN AIRPLANE TIRE
    UNTERBAUVERSTÄRKUNG FÜR FLUGZEUGREIFEN


    Contributors:

    Publication date :

    2018-02-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B60C VEHICLE TYRES , Fahrzeugreifen



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    ROMERO DE LA OSA MARC / DELACROIX SERGE | European Patent Office | 2017

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    ARMATURE DE SOMMET POUR PNEUMATIQUE D'AVION

    ROMERO DE LA OSA MARC / DELACROIX SERGE | European Patent Office | 2018

    Free access