• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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• pp.184-188
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• 2001

The squeeze infiltration process is potentially of considerable industrial importance. The performance enhancements resulting from incorporation of short alumina fiber into aluminum are well documented. These are particularly significant for certain automobile components. But the solidification process gets complicated with manufacturing parameters and factors for porosity formation do not fully understand yet. In this study porosity defects were observed under several infiltrating conditions ; a kind of matrix, an initial temperature of melt, and a volume fraction of reinforcement. The desimetry and the microscopic image analysis were done to measure the amount of porosity. A correlation between manufacturing parameters and defects was investigated through these.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 1999년도 추계학술발표대회 논문집
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• pp.219-222
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• 1999

A method for numerical simulation of the carbonization process in manufacturing of a carbon-carbon composite is developed. A general theory, which consists of analyses of heat and mass transfer together with stress and displacement predictions, is constructed. A homogeneous, single phase, isotropic material is selected and a computer program is developed for an arbitrary 2-dimensional geometry using FEM. Material properties are obtained through experiments and references, and are modeled effectively to serve the simulation purpose. The validity of the simulation is verified through several comparisons with experimental data, where close agreements are observed. Finally, examples of actual applications are considered to exhibit the capability and utilization of the code in process optimization.

• 한국기계가공학회지
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• 제12권1호
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• pp.77-83
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• 2013

This paper presents the feasibility on the application of composite coil spring, which has great interest in the automobile industry. In order to obtain much lighter weight of the composite spring, it will be necessary to optimize the design variables such as fiber angles and diameter of coil, etc. First of all, mechanical properties were measured to consider the effects of FVR and ply angles for carbon fiber composite material. And the shear modulus with respect to ply angles were derived based on twisting angles calculated by torsional beam model. Next we determined the design parameters of composite coil spring, which has equivalent spring rate to the steel coil spring. In order to assess the proposed method, finite element model of the composite spring was developed and analysed to obtain the spring constant. The results showed that static spring rate of the composite spring was in a good agreement with that of steel spring.

• 한국기계가공학회지
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• 제18권1호
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• pp.65-71
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• 2019

The development of adsorbed natural gas (ANG) has emerged as one of potential solutions. It is desirable to reduce the weight of vessel by applying light-weighed a composite carbon fiber in order to response to a egulation of $CO_2$ emission. Through understanding of a composite carbon fiber, and material characteristic of a composite carbon fiber is required in order for better application of a reduction of weight and an analysis of material characteristic. Herein, this study suggest the composite carbon fiber vessel applied to the characteristic of carbon fiber, and it decides the preliminary shape based on the test of material characteristic for ANG vessel applied to a composite carbon fiber, and its basic shape calculate through on the netting theory. Moreover, the detail shape design is analyzed by a finite element analysis, and in the stage of detail sahp design and analysis of stress was performed on the typical shape using a finite element analysis, and the result of preliminary design was verified.

• Design & Manufacturing
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• 제15권3호
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• pp.39-44
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• 2021

In molding of continuous fiber-reinforced thermoplastic composites, it is very difficult to impregnate between the reinforcements and the matrix since the matrix has a high melting temperature and high viscosity. Therefore, most of composite molding processes are divided in the manufacturing processes of intermediate materials called prepreg and the forming of products from intermediate materials. The divided process requires additional facilities and thermoforming, and they increase the cycle time and cost of composite products. These problems can be resolved by combining the continuous fiber-reinforced composite molding process with injection molding. However, when a composite material is manufactured by inserting woven fabric into the injection mold, poor impregnation occurs on the surface of the molded product. It affects the properties of the composites. In this paper, through an impregnation experiment using cores with different heat transfer rates and pore densities, the reason for the poor impregnation was confirmed, and molding experiments were conducted to produce composite with improved surface impregnation by inserting the mesh. And also, the surface impregnation and deformation of composites molded using different types of mesh were compared with each other.

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

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 1999년도 추계학술발표대회 논문집
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• pp.139-142
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• 1999

Screw rotors are core parts of screw type air compressors, compressors in refrigerating machines and super chargers of automobiles etc. They are composed of a female and a male rotors which have complex section profiles and helically swept geometry. Screw type compressors have advantages of low noise, high efficiency, less needs in maintenance etc. Usually, machining process of screw rotors requires long machining time using CNC machine designed only for screw rotors, which increase the cost of production. In this work, the screw rotors for air-compressors were manufactured with fiber reinforced epoxy composite materials by resin transfer molding process. The mold for the RTM process was made of aluminum and silicon rubber and was designed for release of helical shape products. Composite screw rotors, manufactured by RTM process, have advantages of lightweight, less cost of production, good characteristics of vibration etc.

• 항공우주시스템공학회지
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• 제17권2호
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• pp.71-77
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• 2023

액상성형공정(LCM, Liquid Composite Molding) 은 복합재료 오토클레이브(Autoclave) 성형공정의 단점을 극복할 수 있는 탈 오토클레이브(OoA, Out of Autoclave) 공정의 하나로 매우 복잡한 형상이나 대형 구조물을 일체형으로 만들 수 있어 항공산업에서 큰 경쟁력을 가진 공법으로 알려져 있다. 이러한 장점 때문에 액상성형공정을 적용한 항공 부품제작 수요가 늘고 있으며 FAA에서는 액상성형공정을 적용한 복합재료에 대한 인증(Qualification) 방법을 제시한 바 있다. 국내에서도 액상성형공정 적용 복합재료에 대한 부품제작 수요 및 재료인증 수요가 꾸준히 제기되고 있다. 따라서 본 연구에서는 기존에 구축된 프리프레그 복합재료 인증방안 이외에 LCM 공정을 적용한 복합재료에 대한 인증방안을 수립하기 위한 연구를 진행하였다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 추계학술발표대회 논문집
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• pp.45-48
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• 2005

In manufacturing process of composite cylinders with metal liner, the autofrettage process which induces compressive residual stress on liner to improve cycling life can be applied. In this study, finite element analysis technique is presented, which can predict accurately the compressive residual stress on liner induced by autofrettage and stress behavior after. Material and geometry non-linearity is considered in finite element analysis, and the Von-Mises stress of a liner is introduced as a key parameter that determines pressure cycling life of composite cylinders. Presented methodology is verified through fatigue test of liner material and pressure cycling test of composite cylinders.

• Composites Research
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• 제37권3호
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• pp.219-225
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• 2024

정찰위성의 탑재체인 위성용 전개형 반사판 안테나는 발사 환경에 대한 구조안정성 및 궤도 환경에 대한 운용 성능을 고려하여 경량화, 고성능의 구조 개발이 필수적이다. 그 중, 복합재 주반사판은 전개형 반사판 안테나를 구성하는 핵심 구성품이며, 발사체 탑재 성능을 고려한 경량 설계 뿐만 아니라 위성체 임무 수행 중 민첩한 자세제어 기동 이후 높은 품질의 위성 영상을 획득하기 위해서는 높은 전개 시 강성을 갖는 고성능의 주반사판 개발이 요구된다. 주반사판 개발을 위해 전개형 반사판 안테나를 구성하는 복합재 주반사판의 적층 설계 및 재료 물성에 따른 구조적 성능을 분석하여 주반사판의 초기 설계안을 도출하였으며, 도출된 초기 설계안을 기준으로 제작 공정을 변수로 4가지 타입의 복합재 주반사판을 제작하였다. 공정 변수로는 복합재 구조의 성형 공정, 탄소 섬유 복합재 시트와 허니콤 코어 간 접착 필름의 적용 유/무, 샌드위치 복합재 내부의 벤팅 경로를 선정하였다. 제작된 4가지 종류의 주반사판에 대해 무게 측정, 비파괴 검사, 표면오차 측정 및 모드 시험을 통한 전개 시 강성 측정을 수행하였으며, 경량 및 구조적 성능을 향상시킬 수 있도록 접착 필름을 미적용하며 벤팅 경로를 포함하는 주반사판 제작 공정을 선정하여 SAR(합성 개구 안테나)를 포함한 위성체에 실 적용이 가능한 복합재 주반사판을 개발하였다.