首页> 外国专利> Low temperature, vacuum cure fabrication process for large, honeycomb core stiffened composite structures

Low temperature, vacuum cure fabrication process for large, honeycomb core stiffened composite structures

机译:大型蜂窝芯增强复合结构的低温真空固化制造工艺

摘要

A method for making a honeycomb composite structure wherein the method allows for fluid flow from cells of a honeycomb core during a cure process. More specifically, the method involves forming one or more vents in a skin of the structure, which are preferably filled with venting wicks, to allow for fluid flow before being sealed by the polymer matrix during a skin bonding process. Additionally, the structure preferably comprises a scrim that allows for fluid flow between multiple cells of the honeycomb core. The honeycomb composite structure produced according to this process comprises, among other things, a sealed venting region that comprises a polymer matrix and fibers that are transverse to the skin.
机译:一种制造蜂窝复合结构的方法,其中该方法允许在固化过程中流体从蜂窝芯的孔中流出。更具体地,该方法包括在结构的表皮中形成一个或多个排气孔,该排气孔优选地填充有排气芯,以允许流体在表皮粘合过程中被聚合物基质密封之前流动。另外,该结构优选地包括稀松布,该稀松布允许流体在蜂窝状芯的多个单元之间流动。根据该方法生产的蜂窝复合结构尤其包括密封的排气区域,该密封的排气区域包括聚合物基质和横向于皮肤的纤维。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号