Protective Crown Reinforcement For Aircraft Tire

    公开(公告)号:US20170361657A1

    公开(公告)日:2017-12-21

    申请号:US15534411

    申请日:2015-12-02

    IPC分类号: B60C9/26 B60C9/18

    摘要: Protective reinforcement (3) for a tire has mean radial thickness T at least equal to two times diameter D of reinforcer (4), and comprises respectively on its radially interior face (31) and on its radially exterior face (32) parts (7) made of elastomeric compound having axial width W at least equal to diameter D of reinforcer (4). The path of any reinforcer (4), in circumferential direction (XX′), varies radially between radially interior first face (31) and radially exterior second face (32), in such a way that the set of paths of reinforcers (4) of protective reinforcement (3) constitutes a three-dimensional lattice. Furthermore, protective reinforcement (3) comprises a first family of reinforcers (41) each having a path, in the circumferential direction (XX′), contained in circumferential plane (XZ) and a second family of reinforcers (42) each having a path, in the circumferential direction (XX′), that follows a zigzag curve.

    Method and apparatus for producing three-dimensional objects

    公开(公告)号:US09844913B2

    公开(公告)日:2017-12-19

    申请号:US14367619

    申请日:2012-12-21

    摘要: An apparatus and a process for manufacturing a three-dimensional object by successive layer-by-layer consolidation of selected zones of a powder stratum, the consolidated zones corresponding to successive sections of the three-dimensional object, each layer being divided into a central internal portion and an external border, said process comprising the following steps in order: a—depositing a powder layer on a holder; b—fusing the external border of said powder layer by means of a laser beam originating from a first energy source by moving the laser beam of said first energy source relative to the object along a preset path that follows the contour of said external border corresponding to the contour of the cross section of the object so as to selectively fuse said layer; and c—fusing the central internal portion of the powder layer by means of an electron beam originating from a second energy source, by moving the electron beam of said second energy source relative to the object so as to sweep it over said central internal portion along a preset path corresponding to the central internal portion of the cross section of the object so as to selectively fuse said layer; or d—repeating steps a and b N times so as to form a plurality of superposed layers of fused material forming a portion of the external border of said object and then carrying out step c so as to fuse the central internal portion of the object corresponding to the N powder layers; and e—repeating steps a to c or a, b and d until all the layers of the object have been consolidated.