A Study on the Strength of Metal-Composite Hybrid Joints

금속-복합재 하이브리드 체결부의 강도 특성 연구

  • 정재우 (경상대학교 대학원 항공공학과) ;
  • 송민환 (한국항공우주산업(주)) ;
  • 권진회 (경상대학교 기계항공공학부 항공기부품기술연구소) ;
  • 최진호 (경상대학교 기계항공공학부 항공기부품기술연구소)
  • Published : 2005.04.29

Abstract

The strength of aluminum 7075 and carbon composite hybrid joints was studied for adhesive, bolt, and the adhesive-bolt combined joints. Several hybrid joint specimens were tested to get the failure load and modes for three types of the joints. Adhesive Cytec EA9394S was used for aluminum and carbon bonding. Failure load of the adhesive-bolt combined joint was 94 % of the sum of the failure load of the separately bonded and bolted joints. Hybrid joint also showed more stable failure behavior than the simple adhesive or bolted joint.

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