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Applicability of the Ti6Al4V Alloy to the Roller Arm for Aircraft Parts Made Using the DMLS Method
김종건,신도훈,장성화,김태규,Kim Gun-He,정경환,Kim Hyung Giun,박재현 한국항공우주학회 2022 International Journal of Aeronautical and Space Sc Vol.23 No.5
Additive manufacturing (also called 3D printing) technology is so well known that it is inaccurate to call it a new technology anymore, and it is being applied in many industrial fields. In the aviation industry, the influence of process variables and post-treatment processes on additive manufacturing technology has been studied extensively. In this study, the mechanical properties of aircraft parts made of Ti6Al4V powder and their suitability for applications involving aircraft were reviewed. A specimen was prepared and tested; then its microstructure was analyzed and compared with Ti6Al4V plate material. Selected mechanical properties were reviewed. The target product was fabricated using the same process parameters under the same conditions as used for the specimen. The influence analyses of the build orientation and post-processing were performed by dividing the build orientation of the target product into three parts. The shape deformation that occurred after post-processing was reviewed. In addition, the adequacy of the target product to resist the required loads was determined through a functional test of the product.
시차주사열량계를 이용한 진공백 성형 프리프레그의 경화 거동 연구
현동근,이병언,신도훈,김지훈 한국복합재료학회 2020 Composites research Vol.33 No.2
The cure kinetics of carbon fiber-reinforced prepreg for Vacuum Bag Only(VBO) process was studied by differential scanning calorimetry (DSC). The total heat of reaction (ΔHtotal = 537.1 J/g) was defined by the dynamic scanning test using prepregs and isothermal scanning tests were performed at 130oC~180oC. The test results of isothermal scanning were observed that the heat of reaction was increased as the temperature elevated. The Kratz model was applied to analyze the cure kinetics of resin based on the test results. To verify the simulation model, the degree of cure from panels using different cure cycles were compared with the measurement. The simulation model showed that the error against the experimental value was less than 3.4%. 본 연구에서는 시차주사 열량계(differential scanning calorimetry, DSC)를 이용하여 진공백 성형 공정에 사용되는 탄소 섬유 프리프레그의 경화 거동을 연구하였다. 프리프레그를 이용한 동적주사 시험을 통해 전체 발열량(ΔHtotal = 537.1 J/g)을 측정하였고, 130oC~180oC에서 등온주사 시험을 실시하였다. 등온주사 시험의 결과는 온도가 올라감에 따라 발열 반응이 증가되는 것을 확인하였다. 시험 결과를 토대로 수지의 경화 거동을 분석하기 위하여 Kratz 모델을 적용하였다. 서로 다른 경화 사이클로 제작된 평판의 경화도를 경화 예측 모델과 실험값을 비교하였다. 경화 예측 모델은 실험값 대비 3.4% 이하의 오차율을 보여 결과가 잘 부합하는 것을 확인하였다.
경화공정에 따른 복합재 부품 외부와 내부의 경화 거동 차이에 대한 연구
현동근,이동승,신도훈,김지훈 한국복합재료학회 2020 Composites research Vol.33 No.5
We measured the thermal conductivity of composite materials manufactured by the autoclave and vacuum bag only processes and predicted the cure behavior of the external and internal of composite parts with a cure kinetics model. The temperature difference between the external and internal depends on the processes because of the change of thermal conductivity. In the autoclave process, the temperature and cure behavior of the internal were similar to those of the external because of the high thermal conductivity. However, the temperature of the internal of the vacuum bag only process was different from that of the external. The difference can influence the part quality and evacuation of air. Compression tests were performed to find the mechanical property using 0o unidirectional specimens. The composite of the vacuum bag only process was found to have a lower compressive strength than that of the autoclave process. 본 연구는 탄소 복합소재를 이용하여 오토클레이브와 진공백(Vacuum Bag Only) 공정으로 소재의 열전도계수를구하고 경화 거동 모델을 통해 표면부와 내부의 경화 거동을 예측 및 비교하였다. 공정에 따른 열전도 계수의 변화로 인해 내부 온도가 표면부와 차이를 보였다. 오토클레이브 공정의 경우 높은 열전도 계수를 통하여 표면부와 내부의 온도는 거의 일치를 하였으며, 경화 거동 역시 유사하게 진행이 되었다. 하지만, 진공백 공정의 경우 표면부와 내부의 경화 거동이 많은 차이를 보였다. 이 차이는 부품 내부의 품질 및 공기 배출에 영향을 준다. 기계적 물성 차이를 확인하고자 0도 단방향 시편으로 압축시험을 수행하였고, 그 결과 진공백 성형이 조금 낮은 물성을 갖는다는 것을 확인하였다.
노형진,안성재,김민석,조준우,신도훈,박혜성,김성환 한국냄새환경학회 2021 실내환경 및 냄새 학회지 Vol.20 No.4
Airborne bacteria are expected to float in the mushroom cultivation house, as it is a special environment with high humidity and high temperatures. Their concentration and diversity in the indoor air of the cultivation house could effect the health of farmers and the quality of mushrooms. To examine whether microbiota of airborne bacteria change from year to year, we measured the indoor temperature, humidity, and airborne bacterial concentration from mushroom cultivation houses located in six regions in Korea from 2020 to 2021, and isolated and identified airborne bacteria. The surveyed data were compared and the bacterial diversity of the 1st year and the 2nd year were determined. Based on the average temperature and humidity data surveyed, it can be seen that the temperature and humidity environment in the cultivation houses is such that bacteria can easily reproduce. It was observed that the temperature inside the cultivation houses tends to be higher or lower depending on the season and correlates with the temperature outside the cultivation houses. In the first year survey, 32 species of 20 genera were identified, and in the second year survey, bacteria belonging to 29 species of 22 genera were identified. Among them, the most detected species were all species belonging to the genus Bacillus. There were only three species (Bacillus altitudinis, Brevibacterium frigoritolerans, and Staphylococcus epidermidis) that were continuously isolated in common. Our results showed that the species of floating bacteria greatly vary from year to year even for the same cultivation houses.
박동철,김태곤,김승혁,신도훈,김현우,한중원 한국복합재료학회 2018 Composites research Vol.31 No.6
오토클레이브 (Autoclave) 성형 공정은 항공산업분야의 복합재 부품 제작에 있어서 매우 안정적이고 중요한 제조방법으로서 자리매김 해왔었지만 오토클레이브가 가진 많은 장점과 함께 단점 또는 제약 사항들을 보여주고 있다. 최근에는 이러한 한계를 극복하기 위하여 다양한 탈 오토클레이브 (OoA, Out-of-Autoclave) 공정들이연구 개발되고 있는데, 본 연구에서는 탈 오토클레이브 공정 중 하나로서 많은 관심을 받고 있는 액상성형공정 (Liquid Composite Molding)을 사용하여 시편들을 제작하고 이를 오토클레이브 공정으로 제작된 시편과 실험적으로 비교평가하였다. 액상성형공정 중 DB (Double Bagging), CAPRI (Controlled Atmospheric Pressure Resin Infusion) 및 VAP (Vacuum Assisted Process) 공정을 사용하여 시편 제작을 수행하고 내부 기공 함유량, 두께, 유리전이온도, 층간전단강도 및 굽힘강도 시험 평가를 통하여 각 제작 공정에 따른 차이를 확인할 수 있었다. 전체적으로 오토클레이브 성형 시편이 우수한 두께 균일도, 낮은 기공 함유량 및 양호한 기계적 강도 특성을 보였으며, 액상성형공정 중에서는 CAPRI 성형 시편이 DB 및 VAP 성형 시편에 비하여 상대적으로 우수한 특성을 가짐을 확인하였다. Autoclave process has been remaining as one of the most robust and stable process in fabricating structural composite part of aerospace industry. It has lots of advantages, however exhibits some disadvantages or limitations in capital investment and operation. Recently, there have been various Out-of-Autoclave process being researched and developed to overcome those limitations. In this study, laminate specimens were fabricated using LCM (Liquid Composite Molding) process, regarded as one of potential OoA process. DB (Double bagging), CAPRI (Controlled Atmospheric Pressure Resin Infusion), VAP (Vacuum Assisted Process) and Autoclave process were used for laminate specimens. Void content, Thickness, Tg (Glass Transition Temperature), ILSS (Interlaminar Shear Strength) and Flexural strength properties were evaluated for comparison. It is verified that Autoclave based specimen has uniform thickness distribution, the lowest void content and outstanding mechanical properties. And, CAPRI based specimen exhibits relatively good physical and mechanical properties over DB and VAP based specimen and comparable mechanical properties with autoclave based specimen.