3차원 방향으로 극소 열팽창계수를 갖는 탄소/에폭시 복합재료 격자 구조물

Carbon/Epoxy Grid Structure with Near Zero CTE in 3-D Direction

  • 이형주 (건국대학교 항공우주공학과) ;
  • 김창근 (건국대학교 항공우주공학) ;
  • 윤광준 (건국대학교 항공우주공학) ;
  • 박훈철 (건국대학교 항공우주공학과)
  • 발행 : 1999.11.01

초록

The present paper proposes design and manufacturing methods of the carbon/epoxy square grid structure with near zero-CTE in three geometrical principal directions. Bonding strength of the grid structure is examined for different bonding methods. Numerical examples show that maximum displacement of the composite grid structure is almost zero comparing with that of aluminum grid structure with same dimension under thermal loading.

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