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    Method of manufacturing a composite part, and resulting part
    2.
    发明授权
    Method of manufacturing a composite part, and resulting part 有权

    公开(公告)号：US09757909B2

    公开(公告)日：2017-09-12

    申请号：US13145158

    申请日：2010-01-21

    申请人： Guy Valembois

    发明人： Guy Valembois

    IPC分类号： B29C70/72 ,  B29C70/86 ,  F16C7/02 ,  B29L31/06

    CPC分类号： B29C70/86 ,  B29C70/72 ,  B29L2031/06 ,  F16C7/026 ,  F16C2220/28 ,  F16C2300/02

    摘要： The invention relates to a method for manufacturing a composite part intended for being subjected, via at least one attachment point, to pulling and/or compression forces. The method includes: winding fibers on a hub so as to form a portion of the wall of the part, and creating an externally convex rounded area at the location intended to form the area for applying the pulling and/or compression forces. The forces are radial thereto. The method also includes placing an insert on the convex rounded area, the insert including the attachment point or a mechanism for rigidly connecting the attachment point, and continuing to wind fibers so as to form the rest of the wall, while covering a portion of the insert and leaving the attachment point or the mechanism for rigidly connecting the attachment point accessible.

    COMPOSITE LINK FITTING
    4.
    发明申请
    COMPOSITE LINK FITTING 有权
    复合链接配件

    公开(公告)号：US20140014256A1

    公开(公告)日：2014-01-16

    申请号：US14028650

    申请日：2013-09-17

    申请人： Blair HSM Composites LLC

    发明人： Vincent PADDEN

    IPC分类号： B32B37/12 ,  B32B37/14

    CPC分类号： B32B37/12 ,  B29C70/86 ,  B29L2031/06 ,  B32B37/142 ,  F16C7/026 ,  F16C2208/04 ,  F16C2208/82 ,  F16C2208/86 ,  F16C2220/28 ,  Y02T50/43 ,  Y10T29/49288 ,  Y10T29/49622 ,  Y10T29/49787 ,  Y10T29/49826 ,  Y10T29/49915 ,  Y10T29/49924 ,  Y10T29/49947 ,  Y10T74/2142 ,  Y10T74/2162 ,  Y10T156/1052 ,  Y10T156/1075 ,  Y10T156/1724

    摘要： A method of forming a composite link fitting including joining two opposed bearing supports with an inner laminate core having a longitudinal axis extending there between. Each bearing support including a bearing bore formed as an aperture, a first stepped portion, a separate second stepped portion and a recess formed therein. The recess extending toward the bearing bore between an extent of the first and second stepped portions to a recess bottom. The inner laminate core including a central elongate layer, a first outer layer and a second outer layer, with the first and second outer layers disposed on opposed first and second sides of the central elongate layer. First and second ends of the central elongate layer disposed within respective recesses. Also, the method including wrapping an outer band around the two bearing supports and the inner laminate core to form the composite link fitting.

    摘要翻译： 一种形成复合连杆配件的方法，包括将两个相对的轴承支撑件与内部层压芯体相接合，所述内层压芯片具有在其间延伸的纵向轴线 每个轴承支撑件包括形成为孔的轴承孔，第一台阶部分，分离的第二台阶部分和形成在其中的凹部。 凹部在第一和第二阶梯部分的范围之间朝向轴承孔延伸到凹部底部。 内部层压芯包括中心细长层，第一外层和第二外层，其中第一外层和第二外层设置在中心细长层的相对的第一和第二侧上。 中央细长层的第一和第二端设置在相应的凹槽内。 此外，该方法包括将外带缠绕在两个轴承支撑件和内部层叠铁芯上以形成复合连杆配件。