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Manufacturing method of sandwich honeycomb structure based on carbon fiber reinforced carbon composite material

机译:基于碳纤维增强碳复合材料的夹心蜂窝结构的制造方法

摘要

The present invention relates to a method for manufacturing a sandwich honeycomb structure.;It is an object of the present invention to provide a lightweight honeycomb type carbon fiber reinforced composite material that can be used even at an ultra-high temperature.;The manufacturing method of the present invention is characterized in that the core portion of the honeycomb structural member and the outer surface portion of the sheet are made of a carbon fiber-reinforced composite material.;The sandwich honeycomb structural member according to the present invention is very light, but has excellent non-strength and shape stability and excellent energy absorption ability, and therefore can be used as an inner wall material for an aircraft and the like.
机译:本发明涉及一种夹层蜂窝结构的制造方法。本发明的目的是提供一种即使在超高温下也可使用的轻质蜂窝状碳纤维增强复合材料。本发明的特征在于,蜂窝状结构构件的芯部和片的外表面部由碳纤维增强复合材料制成。根据本发明的夹层蜂窝状结构构件非常轻,但是具有优异的非强度和形状稳定性以及优异的能量吸收能力,因此可以用作飞机等的内壁材料。

著录项

  • 公开/公告号KR960010234A

    专利类型

  • 公开/公告日1996-04-20

    原文格式PDF

  • 申请/专利权人 유현식;

    申请/专利号KR19940024029

  • 发明设计人 권익환;서휘원;성기범;

    申请日1994-09-23

  • 分类号B32B3/12;

  • 国家 KR

  • 入库时间 2022-08-22 03:45:19

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