• 한국복합재료학회:학술대회논문집
• /
• 한국복합재료학회 2000년도 춘계학술발표대회 논문집
• /
• pp.49-52
• /
• 2000

A new composite manufacturing technique which combines winding and curing together is studied and analyzed. This method is especially suited to the manufacture of thick composite materials in which thermal spiking is a common problem. An experimental apparatus was designed and built for use with a filament winder to continuously cure a thick composite cylinder. A hoop-wound composite cylinder with 152 mm wall thickness was manufactured and embedded thermocouples and strain gages were monitored throughout the cure process. The experimental data were compared with analytical results.

• 한국생산제조학회지
• /
• 제21권1호
• /
• pp.1-6
• /
• 2012

This paper presents a stress safety of a composite pressure cylinder for a hydrogen gas vehicle. The composite pressure cylinder in which is composed of an aluminum liner and carbon fiber wound layers contains 104 liter hydrogen gas, and is compressed by a filling pressure of 70 MPa. The FEM computed results are analyzed based on the US DOT-CFFC basic requirement for a hydrogen gas cylinder and KS B ISO specification. The FEM results indicate that the stress, 255.2 MPa of an aluminum liner is sufficiently low compared with that of 272 MPa, which is 95% level of a yield stress for aluminum. Also, the composite layers in which are wound on the surface of an aluminum cylinder are safe because the stress ratios from 3.46 to 3.57 in hoop and helical directions are above 2.4 for a minimum safety level. The proposed composite pressure cylinder wound by carbon fibers is useful for 70 MPa hydrogen gas vehicles.

• Advanced Composite Materials
• /
• 제18권3호
• /
• pp.233-249
• /
• 2009

Safe installation and operation of high-pressure composite cylinders for hydrogen storage are of primary concern. It is unavoidable for the cylinders to experience temperature variation and significant thermal input during service. The maximum failure pressure that the cylinder can sustain is affected due to the dependence of composite material properties on temperature and complexity of cylinder design. Most of the analysis reported for high-pressure composite cylinders is based on simplifying assumptions and does not account for complexities like thermo-mechanical behavior and temperature dependent material properties. In the present work, a comprehensive finite element simulation tool for the design of hydrogen storage cylinder system is developed. The structural response of the cylinder is analyzed using laminated shell theory accounting for transverse shear deformation and geometric nonlinearity. A composite failure model is used to evaluate the failure pressure under various thermo-mechanical loadings. A back-propagation neural network (NNk) model is developed to predict the maximum failure pressure using the analysis results. The failure pressures predicted from NNk model are compared with those from test cases. The developed NNk model is capable of predicting the failure pressure for any given loading condition.

• Composites Research
• /
• 제25권4호
• /
• pp.126-132
• /
• 2012

상용프로그램을 사용하여 복합재료 실린더를 설계할 때는 적층 각과 적층 수에 따른 node 수의 증가로 해석하는데 오랜 시간이 걸리기 때문에 본 논문은 LabVIEW를 사용하여 재료의 물성치, 적층각, 적층 수 등을 입력하여 빠른 시간에 응력분포를 구할 수 있는 GUI 프로그램을 개발하여 초기설계시 설계가능영역을 빠른 시간 내에 살펴볼 수 있도록 하였다. 자긴가공된 특수강 실린더의 응력분포와 내압을 받는 특수강/복합재 실린더의 응력분포는 MSC Nastrsn/Patran v.2010 사용하여 값을 비교하였고, 복합재료 실린더의 응력분포는 선행 연구된 값과 비교하여 검증하였다. 또한 프로그램을 사용하여 내압을 받는 자긴가공된 특수강/복합재 실린더의 응력분포를 살펴봄으로써 설계초기단계에서 경향성 검토를 쉽게 할 수 있어 초기설계에 유용하게 사용될 것으로 사료된다.

• 한국복합재료학회:학술대회논문집
• /
• 한국복합재료학회 2005년도 춘계학술발표대회 논문집
• /
• pp.203-206
• /
• 2005

The objective of study on composite cylinder for alternative fuel vehicle is to develop safe, efficient, and commercially viable, on-board fuel storage system for the fuel cell vehicle or natural gas vehicle that use highly compressed gaseous fuel such as hydrogen or natural gas. This study presents the whole procedure of development and certification of a type 3 composite cylinder of 207bar service pressure and 70 liter water capacity, which includes design/analysis, processing of filament winding, and validation through various testing and evaluation. Design methods of liner configuration and winding patterns are presented. Three dimensional, nonlinear finite element analysis techniques are used to predict burst pressure and failure mode. Design and analysis techniques are verified through burst and cycling tests. The full qualification test methods and results for validation and certification are presented.

• 한국가스학회지
• /
• 제16권1호
• /
• pp.46-50
• /
• 2012

본 연구에서는 수압반복시험 장비를 이용하여 70 MPa용 Type 3의 수소복합용기에 대한 거동과 용기내부에 압력이 가해졌을 때 용기 거동을 유한요소법으로 해석하였다. 그 결과, 안전성과 경량성으로 주목받고 있는 Type3 수소용기는 실린더부에서 파열이 먼저 시작되었으며, 유한요소해석 결과에서도 동일한 양상을 확인하였다. 시험결과로 용기내부에 압력이 가해짐에 따라 실린더 몸통부가 부풀어 올라 돔너클과 실린더 몸통부가 가장 취약함을 알 수 있었다.

• Composites Research
• /
• 제24권3호
• /
• pp.25-30
• /
• 2011

복합재료의 비파괴 검사 방법에 관한 연구는 복합재료의 신뢰성 및 안전성을 개선시키는데 매우 중요하다. AE기법은 소성변형, 섬유파손, 모재균열 또는 박리에 의해 생성되는 탄성파에서 감지되는 변형 에너지를 감지하여 결함을 평가하는 기법이다. 본 논문에서는 외부 수압을 받는 필라멘트 와인딩 복합재 원통과 샌드위치 원통의 수압시험이 수행되었고, PVDF센서로부터 측정된 AE 신호특성을 분석하였다. 또한, L-C 동조회로와 Band-pass filter 회로를 가진 AE 신호분석기를 설계, 제작 하였으며, 필라멘트 와인딩 원통과 샌드위치 원통에 대한 수압실험에서 제작된 AE 신호분석기의 균열 검출 능력을 평가하였다.

• 한국가스학회지
• /
• 제17권6호
• /
• pp.46-51
• /
• 2013

복합재 압력용기는 높은 비강성과 비강도 그리고 내피로성으로 수소연료전지자동차와 천연가스자동차에 사용된다. 이음매가 없는 일체형 라이너를 갖는 복합재 압력용기는 고강도 탄소섬유와 에폭시 레진으로 라이너 전체를 감싼다. 본 연구에서는 구조적으로 취약한 너클 부위와 압축잔류응력을 고려하여 필라멘트 와인딩 패턴과 자긴압력 설계 기법을 제시하였다. 복합재 압력용기 시제품에 대한 압력반복시험을 통해 제안된 방법을 검증한다.

• Journal of Mechanical Science and Technology
• /
• 제17권2호
• /
• pp.171-180
• /
• 2003

One of the most significant problems in the processing of composite materials is residual stress. The high residual stress may cause cracking in the matrix without external loads and degrade the integrity of composite structures. In this study, thermo-viscoelastic residual stresses occurred in an aluminum liner-inserted polymer composite cylinder are investigated. This type of the structure is used for rocket fuselage due to the convenience to attach payloads and equipment to the metal liner by machining. The time and degree of cure dependent thermo-viscoelastic constitutive equations are developed and coupled with a thermo-chemical process model. These equations are solved with the finite element method to predict the residual stresses in the composite cylinder and also in the interface between the liner and the composite during cure.

• Journal of Mechanical Science and Technology
• /
• 제16권6호
• /
• pp.757-761
• /
• 2002

When a layer of cylindrical composite component containing an axisymmetric residual stress state is removed from the inner or outer surface, the dimension of the remaining material changes to balance internal forces. Therefore, in order to machine cylindrical composite components within tolerances, it is important to know dimensional changes caused by residual stress redistribution in the body. In this study, analytical solutions for dimensional changes and the redistribution of residual stresses due to the layer removal from a residually stressed cylindrically orthotropic cylinder were developed. The cylinder was assumed to have axisymmetric radial, tangential and axial residual stresses. The result of this study is useful in cases where the initial residual stress distribution in the component has been measured by a non-destructive technique such as neutron diffraction with no information on the effect of layer removal operation on the dimensional changes.