首页> 外国专利> CARBON FIBER REINFORCED PLASTIC (CFRP) STRINGER TERMINATION SOFTENING WITH STACKED CFRP NOODLE

CARBON FIBER REINFORCED PLASTIC (CFRP) STRINGER TERMINATION SOFTENING WITH STACKED CFRP NOODLE

机译:碳纤维增强的叠层碳纤维增强塑料(CFRP)绞线机端接软化

摘要

PROBLEM TO BE SOLVED: To provide a method for enhancing productivity by reducing the number of components of a stringer used for improving stiffness in a vehicle such as an aircraft.SOLUTION: A stringer 100 includes a base flange 104, a web 102, and a noodle 114. The noodle includes a unidirectional fiber top portion 210 and a stacked laminate bottom portion coupled to the top portion. The bottom portion includes a predetermined number of stacks 220, each stack including three plies having three corresponding fiber orientations within an acreage region of the stringer. In a transition region 204 of the stringer, the stacked laminate bottom portion includes a predetermined number of stacks, each stack including the first and third plies of the acreage region.SELECTED DRAWING: Figure 2
机译:解决的问题:提供一种通过减少用于改善诸如飞机之类的车辆中的刚度的桁条部件的数量来提高生产率的方法。解决方案:桁条100包括基础凸缘104,腹板102和支撑条。面条114。面条包括单向纤维顶部210和连接到顶部的叠层层压底部。底部包括预定数量的叠层220,每个叠层包括三层,该三层在纵梁的面积内具有三个对应的纤维取向。在纵梁的过渡区域204中,堆叠的层压板底部包括预定数量的堆叠,每个堆叠均包括面积区域的第一层和第三层。

著录项

  • 公开/公告号JP2017114115A

    专利类型

  • 公开/公告日2017-06-29

    原文格式PDF

  • 申请/专利权人 BOEING CO;

    申请/专利号JP20160223759

  • 申请日2016-11-17

  • 分类号B29C70/06;B64C1;B64C1/06;B29K105/08;B29L31/30;

  • 国家 JP

  • 入库时间 2022-08-21 13:58:55

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