Impact Property of S-2 Glass Woven Composites with Different Matrices and Stitching

S-2 유리섬유 평직복합재의 기지재료 및 스티칭에 따른 충격 특성 비교

  • 변준형 (한국기계연구원 소재성형연구센터 복합재료팀) ;
  • 황병선 (한국기계연구원 소재성형연구센터 복합재료팀) ;
  • 엄문광 (한국기계연구원 소재성형연구센터 복합재료팀) ;
  • 이정훈 (한국기계연구원 소재성형연구센터 복합재료팀) ;
  • 남원상 (한국기계연구원 소재성형연구센터 복합재료팀) ;
  • 송승욱 (대한항공 항공우주사업본부) ;
  • 이창훈 (대한항공 항공우주사업본부)
  • Published : 2005.11.18

Abstract

For the damage tolerance improvement of conventional laminated composites, stitching process has been utilized for providing through-thickness reinforcements. 2D prefonl1S were stacked with S-2 glass plain weave, and 3D preforms were fabricated using the stitching process. For the matrix system, epoxy and phenol resins were considered. To examine the damage resistance performance the low velocity drop weight impact test has been carried out, and the impact damage was examined by scanning image. CAI (Compressive After Ih1paet) tests were also conducted to evaluate residual compressive strength. Compared with 2D epoxy composites, 2D phenol composites showed drastic reduction in the compressive strength prior to impact because of the higher contents of voids. The damage area of 2D phenol composites were also larger than that of 2D epoxy composites. However, by introducing the stitching, the damage area of 3D phenol composites was reduced by 60%, while the CAI strength improvement was negligible.

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