An aircraft tire (1) comprises a working reinforcement (2) radially on the inside of a tread (3) and radially on the outside of a carcass reinforcement (4), comprising at least one working bi-ply (5) made up at least in part of two working layers (6, 7) and comprising, at each axial end, an axial-end additional thickness (51). Each working layer (6, 7) is made up of an axial juxtaposition of strips (8) of width W, a strip (8) having a mid-line (81) extending circumferentially along a periodic curve (9) forming, in the equatorial plane (XZ) and with the circumferential direction (XX′), a non-zero angle A and a radius of curvature R at its extrema (10). The ratio R/W is at most equal to N/(1−cosA)+½, such that each axial-end additional thickness (51) comprises at most (N+2) working layers.


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    Title :

    Aircraft Tire Crown Reinforcement


    Contributors:

    Publication date :

    2016-08-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand / B60C VEHICLE TYRES , Fahrzeugreifen



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