METHOD OF MANUFACTURING COMPOSITE MATERIAL BEARING COMPONENT
    6.
    发明申请
    METHOD OF MANUFACTURING COMPOSITE MATERIAL BEARING COMPONENT 有权
    制造复合材料轴承组件的方法

    公开(公告)号:US20150000138A1

    公开(公告)日:2015-01-01

    申请号:US14010062

    申请日:2013-08-26

    IPC分类号: F16C43/00

    摘要: A method of manufacturing a composite material bearing component includes designing a pattern of a fabric combination including a PTFE film, a quartz fabric and a glass fabric, which are stacked, in consideration of a final shape of a bearing, and stacking the fabric combination on a fusion surface which is a steel surface of a bearing structure of a composite material bearing; and simultaneously performing molding and fusing under conditions of a thermal treatment temperature of 300˜400° C. and a pressure of 30˜100 kgf/cm2, thereby manufacturing the composite material bearing. This composite material bearing functions as a self-lubricating high performance bearing, thus satisfying high performance requirements of the driving friction surface of a B&S (Ball & Socket) nozzle which is a thrust vector control nozzle and satisfying a high load and low friction efficient required of guided weapon components.

    摘要翻译: 制造复合材料承载部件的方法包括:考虑到轴承的最终形状,并将织物组合层叠在一起,设计包括PTFE膜,石英织物和玻璃织物的织物组合的图案 作为复合材料轴承的轴承结构的钢表面的熔融面; 同时在热处理温度为300〜400℃,压力为30〜100kgf / cm2的条件下进行成型和熔融,由此制造复合材料轴承。 该复合材料轴承用作自润滑高性能轴承,从而满足作为推力矢量控制喷嘴的B&S(球窝套管)喷嘴的驱动摩擦面的高性能要求,并满足高负载和低摩擦效率要求 导弹武器组件。