Working reinforcement (2) of airplane tire (1) is radially inside tread (3) and radially outside carcass reinforcement (4), comprising carcass layer (41). Working reinforcement (2) comprises working biply (21) of greatest axial width (LT) and two axial ends (E). Hoop reinforcement (7) comprises hooping layer (71) radially inside working biply (21), and having axial width (LF) at least equal to 0.8 times LT. Distance D between axial end (E) of greatest axial width (LT) and its orthogonal projection (I) onto the radially outermost carcass layer (41) is at least equal to 7 mm and the distance D′ between point (F) of working biply (21) of greatest axial width (LT), axially inside axial end (E) at a distance L equal to 25 mm, and its orthogonal projection (J) onto the radially outermost carcass layer (41) is at least equal to 4 mm and at most equal to the distance D.


    Access

    Download


    Export, share and cite



    Title :

    Crown Reinforcement For An Airplane Tire


    Contributors:

    Publication date :

    2017-03-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60C VEHICLE TYRES , Fahrzeugreifen



    Crown Reinforcement For An Airplane Tire

    ESTENNE VINCENT / JOULIN EMMANUEL | European Patent Office | 2017

    Free access

    Top Reinforcement of Airplane Tire

    ROMERO DE LA OSA MARC | European Patent Office | 2018

    Free access

    Aircraft Tire Crown Reinforcement

    ROMERO DE LA OSA MARC / MALIN DIDIER | European Patent Office | 2019

    Free access

    Carcass reinforcement for an airplane tire

    COGNE MICHAEL / DENDIEVEL JEAN-LUC | European Patent Office | 2015

    Free access

    Aircraft Tire Crown Reinforcement

    ROMERO DE LA OSA MARC | European Patent Office | 2016

    Free access