Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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A Study on Design of Type IV Hydrogen Pressure Vessels with Filament Winding Method

필라멘트 와인딩 공법을 적용한 타입 IV 수소 압력용기 설계 연구

  • Sungjin Ahn (School of Mechanical Engineering, Kunsan National University) ;
  • Hyunbum Park (School of Mechanical Engineering, Kunsan National University)
  • 안성진 (군산대학교 기계공학부) ;
  • 박현범 (군산대학교 기계공학부)
  • Received : 2023.10.11
  • Accepted : 2023.11.17
  • Published : 2023.12.31
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Abstract

In this study, designing of a Type 4 pressure vessel using the filament winding method was conducted. In order to prevent leakage in consideration of the design of the hydrogen storage tank, a liner was designed by applying high-density polyethylene (HDPE), and the composite structure was designed by stacking carbon/epoxy in the hoop and helical directions. As a theoretical approach, the angle of the helical fiber and fiber thickness of each hoop and helix were designed. The safety of the design was verified using the commercial software ANSYS.

본 연구에서는 필라멘트 와인딩 공법을 적용한 Type 4 압력용기의 설계를 수행하였다. 수소저장용 탱크의 설계인 점을 고려하여 누설을 방지하기 위해 라이너는 고분자 고밀도 폴리에틸렌(HDPE)을 적용하였고 복합재 구조는 카본/에폭시를 Hoop 방향과 Helical 방향으로 적층하여 설계하였다. 이론적 접근으로 Helical 섬유의 각도와 Hoop, Helical 각각의 섬유 두께를 결정하여 설계하였다. 설계에 대한 안전성은 상용소프트웨어인 ANSYS를 활용하여 유한요소 해석으로 검증하였다.

Keywords

Acknowledgement

본 연구는 2023년도 교육부의 재원으로 한국기초과학지원연구원 국가연구시설장비진흥센터의 지원을 받아 수행된 연구임.(2023R1A6C101B042) / 이 논문은 2022년도 정부(산업통상자원부)의 재원으로 한국에너지기술평가원의 지원을 받아 수행된 연구임(20224000000040).

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