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고속 열 성형 유한요소해석을 활용한 CF/PEKK 열가소성 복합재 구조물 제작 공정 예측 및 검증
Evaluation of Stamp Forming Process Parameters for CF/PEKK Thermoplastic Composite Using Finite Element Method 원문보기

Composites research = 복합재료, v.34 no.5, 2021년, pp.296 - 304  

이경인 (School of Mechanical and Aerospace Engineering, Gyeongsang National University) ,  최현석 (School of Mechanical and Aerospace Engineering, Gyeongsang National University) ,  곽준우 (School of Mechanical and Aerospace Engineering, Gyeongsang National University) ,  이준성 (School of Mechanical and Aerospace Engineering, Gyeongsang National University) ,  주현우 (Korea Aerospace Industries, Ltd.) ,  권진회 (School of Mechanical and Aerospace Engineering, Gyeongsang National University) ,  남영우 (School of Mechanical and Aerospace Engineering, Gyeongsang National University)

초록
AI-Helper 아이콘AI-Helper

본 연구에서는 유한요소법(FEM)에 기반한 CF/PEKK 열가소성 복합재 고속 열 성형 해석을 수행하였고 제작 공정을 예측 및 검증하였다. 대표적인 L 형 구조물 모델에 대해 트리밍 여유에 따른 성형성을 응력, 두께, 주름분포를 분석하였다. 그 결과, 블랭크의 트리밍 여유가 증가할수록 구조물의 성형성이 향상하는 것을 확인하였다. 특히 두께 및 주름 분포 측면에서 해석 모델과 실험 결과를 비교하여서 고속 열 성형 모델의 타당성을 검증하였다. 제작된 구조물은 시차 주사 열량 분석법 및 이미지 분석법을 통해 결정화도와 기공률이 측정되었다. 제작된 열가소성 구조물의 전 영역 기공률은 평균 0.75%, 결정화도는 약 21%로 항공기에 적용 가능한 수치로 평가되었다. 따라서 본 연구를 토대로 열가소성 복합재 고속 열 성형 공정에 대해 효과적인 예측이 가능할 것으로 판단된다.

Abstract AI-Helper 아이콘AI-Helper

This study presented the evaluation of the stamp forming process for L-shape CF/PEKK thermoplastic composite using the finite element model. The formability of three different trimming allowances has been examined for representative product geometry. The results showed that those manufactured by hig...

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표/그림 (14)

참고문헌 (50)

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