Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Internet-based Repair for Aircraft Composites

인터넷 기반의 항공기용 복합재의 보수

  • 추원식 (경상대학교 기계항공공학부 대학원) ;
  • 안성훈 (경상대학교 기계항공공학부)
  • Published : 2002.08.01
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Abstract

An Internet-based software called the Repair Advisory Service (RAS) was developed to assist aircraft composite repair. The RAS takes advantage of the web user interface and provides estimation of the failure loads of repaired composite laminates and Structural Repair Manual (SRM) with search capability. In this paper, a failure model of lap repair is discussed as an example of the modules in the RAS. The model takes into account anisotropy of each ply in the laminate and in the repair ply, and non-elastic behavior of the interlayer between the laminate and the repair patch. Failure loads calculated by the model were compared with test data, and a good agreement was found between the results of the model and the test.

항공기용 복합재의 보수를 보조하는, 보수 제안 서비스 (Repair Advisory Service, RAS)라는 인터넷 기반의 소프트웨어가 개발되었다. 웹 브라우저를 유저인터페이스로 하는 RAS는 보수된 복합재의 파괴하중 계산, 구조 보수 지시서 (SRM) 제공 및 검색 등을 보수 엔지니어에게 거리에 제약을 받지 않고 제공한다. 본 논문에서는 RAS의 기능을 겹치기 기술(lap repair)에 의해 보수된 복합재의 파괴하중을 계산하는 모델을 예로 보여준다. 이 모델은 기초복합재와 보수층에 있는 각 복합재 층의 이방성을 고려하여 개발되었고, 기초복합재와 보수복합재 사이의 경계층의 비탄성을 고려하였다. 모델에 의한 파괴하중은 실험결과와 유사한 결과를 보여준다.

Keywords

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