发明名称 Crown Reinforcement For Airplane Tire
摘要 Aeroplane tire (1) comprises a working reinforcement (2) radially between tread (3) and carcass reinforcement (4). Working reinforcement (2) includes a working biply (21) comprised of the zigzag circumferential winding of strip (5) of width W onto a cylindrical laying surface (6) of radius R, with its axis of revolution being axis of rotation (YY′) of the tire, in a periodic curve (7) with period P and forming angle A with circumferential direction (XX′) of the tire in equatorial plane (XZ) of the tire. The winding of strip (5) comprises N periods P of curve (7) over T circumferences 2ΠR of surface (6). N is a whole number which satisfies the following conditions: (a) N*(W/sin A)=2ΠR,(b) N*P=2ΠR*T, where T is a whole number,(c) N*T is the lowest common multiple of N and T, and the ratio T/N is at least equal to 1.8 and at most equal to 2.2.
申请公布号 US2017066287(A1) 申请公布日期 2017.03.09
申请号 US201515120856 申请日期 2015.02.23
申请人 COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN ;Michelin Recherche et Technique S.A. 发明人 ROMERO DE LA OSA Marc
分类号 B60C9/26;B29D30/30;B60C9/00;B29D30/70 主分类号 B60C9/26
代理机构 代理人
主权项 1. A tire for an aeroplane, comprising: a working reinforcement radially on the inside of a tread and radially on the outside of a carcass reinforcement; the working reinforcement comprising at least one working biply comprised of two radially superposed working layers; the at least one working biply comprised of a zigzag circumferential winding of a strip of width W onto a cylindrical laying surface of radius R, having as its axis of revolution the axis of rotation of the tire, in a periodic curve; the periodic curve having a period P and forming an angle A with the circumferential direction of the tire in the equatorial plane of the tire; the zigzag circumferential winding of the strip comprising N periods P of the periodic curve over a number T of circumferences 2ΠR of the cylindrical laying surface; the number N of periods P of the periodic curve is a whole number which satisfies the following conditions: (a) N*(W/sin A)=2ΠR, (b) N*P=2ΠR*T, where T is a whole number, (c) N*T is the lowest common multiple of N and T,and the ratio T/N between the whole number T of circumferences 2ΠR of the cylindrical laying surface and the whole number N of periods P of the periodic curve which are needed to make up the at least one working biply, is at least equal to 1.8 and at most equal to 2.2.
地址 Clermont-Ferrand FR