• 한국철도학회논문집
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• 제5권4호
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• pp.231-236
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• 2002

Todays, crash safety requirements of the railway vehicle structures become important design criterion according to the increased driving speed and the lightweight construction. Although the crash analysis using computer simulation can be effectively applied to predict the crash performance of the railway vehicles in the early design stage, the optimized design w.r.t the crash safety could be realized by the crash tests with actual prototype vehicles. However, it is very expensive and time-consuming task to perform the crash test of the railway vehicles. As a measure to cope with the problem, in this paper, the scale modeling technique is suggested and experimentally verified to predict the impact energy absorption characteristics of full scale model of aluminum extrusions sub-structures and the high-speed railway vehicle structure.

• 한국기계가공학회지
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• 제8권4호
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• pp.136-142
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• 2009

The vehicle's light-weight technology is divided into optimization of structure geometric and material. Structure geometric optimization and improvement of materials has examined to be power-train and maintenance on the severe condition. The core technology of Special vehicle's light-weight is constitute by Drop box, Axle and Final reduction gear. Technology and product of the parts is high to overseas and import dependency. We will want to examine the possibility of light-weight for the Axle Case and Drop box-connections. In this research, conventional design of excess weight will inhibit the mobility and fuel efficiency. Through the improvement of Axle material, we saw the possibility reducing weight. If you use the results of these studies, it will be available to domestic production technology and reducing weight of RV car, Dump truck, Track crain, etc.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2009년도 춘계학술대회 논문집
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• pp.219-222
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• 2009

Green ocean is one of the main issues internationally. Most governments are leading the role in boosting the economy through creating new green market and establishing system of coping with increasing international environmental regulation. Green ocean, which is a solution for the environmental issue of global warming, is applied throughout the industry. Domestic transportation industry including railway is also developing technology for creating green ocean. Transportation must decrease energy consumption at running stages because it shows high environmental loads expecially on using stages during its life cycle. Therefore, There are some tries for developing technologies; new engine through alternative energies, hybrid and lightweight. Railway transportation can not be exception. it is intended for this paper to suggest the direction of manufacturing environmentally friendly railway vehicle through the global warming effect evaluation of several materials being applied to vehicle and comparison of the results.

• Composites Research
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• 제32권4호
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• pp.171-176
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• 2019

본 연구는 복합재를 사용한 휠체어 고정구의 구조 강도 특성에 대하여 평가하였다. 이를 위해 특별교통수단 내 휠체어 고정구의 시험 기준 ISO 10542에 의거하여 전방 충돌 슬레드 유한요소해석을 진행하였고, 이를 통해 얻은 고정구에 작용하는 하중데이터를 휠체어 고정구 유한요소해석의 초기 조건으로 사용하였다. 고정구는 블록, 가이드, 레일로 구성되어 있으며, 이 중에서 레일의 중량 비율이 가장 높기 때문에 탄소섬유 에폭시 복합재를 레일에 적용하는 것이 적합한 것으로 나타났다. 또한 기존의 레일에서 하단 부분을 복합재로 적용한 하이브리드 레일은 기존 SAPH 440으로 제작된 레일의 구조강도와 비슷하게 설계할 경우, 약 27% 정도 경량화를 달성할 수 있는 것으로 나타났다.

• Composites Research
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• 제36권3호
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• pp.230-240
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• 2023

전개형 반사판 안테나는 단위 구조물 형태의 반사판이 접힌 상태로 수납되어 발사체에 탑재된 후, 운용궤도에 도달 및 전개되어 임무를 수행하는 위성체이다. 전개형 반사판 안테나는 수납 부피를 줄일 수 있어 발사체의 제한적 수납공간에 대형 우주 구조물을 탑재시킬 수 있으며, 경량소재를 적용할 경우 발사 및 운용 성능 향상에 용이한 장점이 있다. 본 논문에서는 전개형 반사판 안테나를 구성하는 주반사판에 대해 강성 및 강도 등의 구조적 분석을 통해 초기 개념설계를 수행하였다. 탄소섬유 복합재 및 허니콤 코어를 적용하여 경량 복합재 주반사판을 설계하였으며, 적층 패턴 및 형상을 설계 변수로 운용조건에 적합한 주반사판 설계안을 도출하였다. 이후 모드(Modal analysis), 준정적(Quasi-static), 열 구배(Thermal gradient) 및 동적(Dynamic) 거동에 대한 상세 구조해석을 수행하여 경량 복합재 반사판 안테나의 성능을 분석하였다

• 한국기계가공학회지
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• 제17권3호
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• pp.141-147
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• 2018

Recently, interest in customers has shifted to the emotional quality of customers as the driving, handling, and collision stability of automobiles have been greatly improved. The NVH performance of a vehicle is quantified and evaluated from the DPDS. To improve the DPDS, we need to optimize the shape without considering the increases in thickness of the parts or additions to the parts. And at the same time, we need to establish design and analysis processes to satisfy the requirements of the DPDS.

• 항공우주시스템공학회지
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• 제7권2호
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• pp.8-14
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• 2013

When launch vehicles are manufactured, one of the key points is a design of lightweight structure for reducing costs. Isogrid structure was designed to solve this topic, and many researches were carried out about buckling load because compression load is mainly applied to them. Recently, many studies are also being carried out about FEM model geometry of isogrid structure. The reason is that isogrid structure depends on size of ribs so it is difficult to modify about small changes in rib pattern. In this study, 1/8 model of cylindrical isogrid structure model was developed to analyze buckling behavior. Through parameter study, buckling analysis were performed to analyze buckling load and buckling mode depending on size of ribs.

• Design & Manufacturing
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• 제13권3호
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• pp.24-28
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• 2019

In this study, a study was carried out that could effectively produce a heat dissipation effect on plastic materials. Using carbon nanotube (CNT), aluminum powder and plastic, the material properties were tested in 2 cases of compounding ratio. The test sample mold was designed and constructed prior to the experiment. The experiments include tensile strength, elongation rate, flexural strength, flexural elasticity rate, eye-jaw impact strength, gravity and thermal conductivity. Results from 60% and 70% mixture of aluminium to plastic were tested, and a 10% less combined result was a relatively good property. For research purposes, the heat dissipation effect and light weighting obtained a good measure when the combined amount of Al was 60%.

• Design & Manufacturing
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• 제13권3호
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• pp.6-10
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• 2019

In this study, a study was carried out that could effectively produce a heat dissipation effect on plastic materials. Using carbon nanotube (CNT), aluminum powder and plastic, the material properties were tested in 2 cases of compounding ratio. The test sample mold was designed and constructed prior to the experiment. The experiments include tensile strength, elongation rate, flexural strength, flexural elasticity rate, eye-jaw impact strength, gravity and thermal conductivity. Results from 60% and 70% mixture of aluminium to plastic were tested, and a 10% less combined result was a relatively good property. For research purposes, the heat dissipation effect and light weighting obtained a good measure when the combined amount of Al was 60%.

• International Journal of Aeronautical and Space Sciences
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• 제17권4호
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• pp.551-564
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• 2016

High-speed flight vehicles (HSFVs) such as space launch vehicles and missiles undergo severe dynamic loads which are generated during the launch and in in-flight environments. A typical vehicle is composed of thin plate skin structures with high-performance electronic units sensitive to such vibratory loads. Such lightweight structures are then exposed to external dynamic loads which consist of random vibration, shock, and acoustic loads created under the operating environment. Three types of dynamic loads (acoustic loads, rocket motor self-induced excitation loads and aerodynamic fluctuating pressure loads) are considered as major components in this study. The estimation results are compared to the design specification (MIL-STD-810) to check the appropriateness. The objective of this paper is to study an estimation methodology which helps to establish design specification for the dynamic loads acting on both vehicle and electronic units at arbitrary locations inside the vehicle.