• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2012년도 춘계학술대회 논문집
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• pp.349-350
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• 2012

• 한국안전학회지
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• 제23권6호
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• pp.34-37
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• 2008

The composite materials are widely used in the many applications of industry as well as aerospace field because of their high specific stiffness and strength which benefits the material and provides potential energy savings. However, composite materials also have a low property about external applied impact. In this paper, impact tests were conducted on different sample types(glass, carbon and kevlar composite) to obtain information such as absorbed energy and composite deformation using an instrumented impact test machine (DYNATUP 8250). 3 type samples were compared to experimental results. The data from impact test provided valuable information between the different type samples by wet lay up. This paper shows results of that kevlar composite has larger absorption energy and deformation than others.

• 한국정밀공학회지
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• 제18권11호
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• pp.34-41
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• 2001

This study is to investigate the energy absorption characteristics of CFRP(Carbon-Fiber Reinforced Plastics) tubes on static and dynamic tests. Axial static compression tests have been carried out using the static testing machine(Shin-gang buckling testing machine) and dynamic compression tests have been utilized using an vertical crushing testing machine. When such tubes are subjected to crushing loads, the response is complex and depends on the interaction between the different mechanisms that could control the crushing process. The collapse characteristics and energy absorption have been examined for various tubes. Energy absorption of the tubes are increased as changes in the lay-up which may increase the modulus of tubes. The results have been varied significantly as a function of ply orientation and interlaminar number.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2005년도 춘계학술대회 논문집
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• pp.168-173
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• 2005

Composite material is combined with two or more chemical ingredient and different components. FRP has been widely used for the structure of aircraft, ships, automobiles, sporting goods and other machines because of their high specific strength, high specific stiffness and excellent fatigue strength. Recently, the development of machine tool and cutting tool greatly relies on high speed process to satisfy high precision, high efficient machining, shortened process time to maximize material removal rate (MRR) through high cutting speed and feed speed. The research molded CFRP, GFRP as stacking sequence methods of two direction (orientation angle $0^{\circ}\;and\;0^{\circ}/9^{\circ}$) hand lay-up, drilled molded plates using cemented carbide drill and examined chip shapes, surface roughness properties.

• Composites Research
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• 제34권2호
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• pp.96-100
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• 2021

The lightweight industry continuously demands reliable near-net-shape fabrication where the preform just out-of-machine is close to the final shape. In this study, different half-finished preforms are made π-beams. Then the preforms are unfolded to make a 3D shape with integrated structure of fibers, providing easier handling in the further processing of composites. Several 3D textile preforms are made using weaving technique and are examined after resin infusion for mechanical properties such as inter-laminar shear strength, compressive strength and tensile strength. Considering that the time and labor are important parameters in modern production, 3D weaving technique reduces the manufacturing steps and therefore the costs, such as hand-lay up of textile layers, cutting, and converting into preform shape. Hence this 3D weaving technique offers many possibilities for new applications with efficient composite production.

• 한국안광학회지
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• 제16권2호
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• pp.107-115
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• 2011

목적: 안경렌즈 조제가공을 위한 보급형 전자동 옥습기 개발을 위해 설계하고 제작하고자 한다. 방법: 보급형 전자동 옥습기의 주요 설계도를 캐드로 그려서 제작에 필요한 정보를 얻었다. 이 데이터를 기본으로 보급형 자동옥습기 개발을 위해 시제품을 제작 하였다. 결과: 무패턴 모드는 외부 자동 취형기에서 안경테의 렌즈삽입부 정보를 RS232C 전송방식으로 형판 없이도 작동할 수 있었고, 패턴 모드는 형판을 이용해서 개발품의 좌측에 장착하여 작동할 수 있었다. 보급형 자동옥습기는 헤드부, 오토암부, 형판고정부 그리고 연삭부와 같은 주요 요소들로 구성되었다. 헤드부는 좌우모터와 상하모터의 작동을 이용하여 안경렌즈의 연삭을 제어하였다. 연삭부는 유리 재질, 플라스틱 재질, V-홈 그리고 광택을 낼 수 있는 연삭휠로 구성하였다. 슬라이드는 고정된 형판의 하부에 구비되었고, 고정 샤프트에 의해 회전되는 형판이 슬라이드부에 의해 지지할 수 있었다. 형판고정부는 안경사의 수동적인 조작에 의해 헤드파트를 승강 및 좌우 이동시킬 수 있게 하였다. 연삭휠의 분당 회전수를 3,600 rpm으로 최적화 하였다. 결론: 패턴리스와 패턴 렌즈 가공이 가능한 보급형 자동옥습기를 설계 및 제작하여 시제품 제작에 성공하였다. 최소의 비용으로 효율적이고 간편하게 조제가공이 가능하여 안경사들에게 큰 도움이 될 수 있을 것으로 예상된다.

• 대한기계학회논문집A
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• 제27권3호
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• pp.440-449
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• 2003

Residual strength of fiber metal laminates after impact was studied. 3/4 lay up FML was fabricated using 4 ply prepreg, 2 ply aluminum sheets, and 1 ply steel sheet. Quasi isotropic ([0/45/90/-45]s) and orthotropic ([0/90/0/90]s) FRP were also fabricated to compare with FML. Impact test were conducted by using instrumented drop weight impact machine (Dynatup, Model 8250). Penetration load and absorbed energy of FML were superior to those of FRPs. Tensile tests were conducted to evaluate the residual strength after impact. Strength degradation of FML was less than that of FRP. This means that the damage tolerance of FML is excellent than that of FRP. Residual strength of each specimen was predicted by using Whitney and Nuismer(WN) Model. Impact damage area is assumed as a circular notch in WN model. Damage width is defined as the average of back face and top face damage width of each specimen. Average stress and point stress criterions were used to calculate the characteristic length. It is supposing that a characteristic length is a constant. The distribution of characteristic length shows that the assumption is reasonable. Prediction was well matched with experiment under both stress criterions.

• 대한기계학회논문집A
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• 제34권7호
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• pp.867-872
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• 2010

자연계에 존재하지만 사용되지 못 하고 버려지는 에너지를 효과적으로 채집하여 배터리를 충전하거나 전기 장치에 전기 에너지를 공급하는 에너지 하베스팅에 대한 연구를 수행하였다. 압전재료는 물체의 움직임이나 진동으로부터 에너지를 채집하는 주요한 재료로 널리 연구되고 있다. 본 논문에서는 기존의 PZT 압전 특성을 개량하고자 압전-복합재료 발전소자(Piezo-Composite Generating Element, 이하 PCGE)를 도입하여 성능 예측모델을 제안하고 이를 실험적으로 검증하였다. PCGE는 탄소/에폭시, PZT, 유리/에폭시 층으로 구성된다. 제작 과정에서 적층된 PCGE는 오토클레이브 안에서 $177^{\circ}C$의 온도에서 성형되는데, 이때 PCGE 내부에 초기잔류응력이 발생하게 되어 압전재료의 성능이 변화하게 된다. 세 종류의 PCGE를 제작한 후 에너지 채집 실험을 수행하여 제안된 성능 예측모델의 타당성과 기계적 진동을 전기적 에너지로 변환되는 성능을 검증하였다. 실험 결과 이론적인 성능 예측모델이 실험 결과와 잘 일치함을 확인하였다.

• International Journal of Ocean System Engineering
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• 제2권3호
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• pp.185-194
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• 2012

A Macroscopic combination of two or more distinct materials is commonly referred to as a "Composite Material", having been designed mechanically and chemically superior in function and characteristic than its individual constituent materials. Composite materials are used not only for aerospace and military, but also heavily used in boat/ship building and general composite industries which we are seeing increasingly more. Regardless of the various applications for composite materials, the industry is still limited and requires better fabrication technology and methodology in order to expand and grow. An example of this is that the majority of fabrication facilities nearby still use an antiquated wet lay-up process where fabrication still requires manual hand labor in a 3D environment impeding productivity of composite product design advancement. As an expert in the advanced composites field, I have developed fabrication skills with the use of machinery based on my past composite experience. In autumn 2011, the Korea government confirmed to fund my project. It is the development of a composite sanding machine. I began development of this semi-robotic prototype beginning in 2009. It has possibilities of replacing or augmenting the exhaustive and difficult jobs performed by human hands, such as sanding, grinding, blasting, and polishing in most often, very awkward conditions, and is also will boost productivity, improve surface quality, cut abrasive costs, eliminate vibration injuries, and protect workers from exposure to dust and airborne contamination. Ease of control and operation of the equipment in or outside of the sanding room is a key benefit to end-users. It will prove to be much more economical than normal robotics and minimize errors that commonly occur in factories. The key components and their technologies are a 360 degree rotational shoulder and a wrist that is controlled under PLC controller and joystick manual mode. Development on both of the key modules is complete and are now operational. The Korean government fund boosted my development and I expect to complete full scale development no later than 3rd quarter 2012. Even with the advantages of composite materials, there is still the need to repair or to maintain composite products with a higher level of technology. I have learned many composite repair skills on composite airframe since many composite fabrication skills including repair, requires training for non aerospace applications. The wind energy market is now requiring much larger blades in order to generate more electrical energy for wind farms. One single blade is commonly 50 meters or longer now. When a wind blade becomes damaged from external forces, on-site repair is required on the columns even under strong wind and freezing temperature conditions. In order to correctly obtain polymerization, the repair must be performed on the damaged area within a very limited time. The use of pre-impregnated glass fabric and heating silicone pad and a hot bonder acting precise heating control are surely required.