• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2017.04a
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• pp.15-15
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• 2017

본 연구는 필드 작업 시 작업조건에 따른 정식기의 PTO 부하를 측정하고, 이를 이용하여 작업조건에 따른 안전율 시뮬레이션을 목적으로 수행하였다. 부하 계측 시스템은 PTO 축의 부하를 측정하기 위한 토크 센서, 토크 센서에서 발생한 신호를 수집하기 위한 데이터 수집장치, 노트북에 전원을 공급하기 위한 파워 컨트롤러로 구성하였다. 토크센서에서 입력된 부하 데이터를 처리하기 위한 소프트웨어는 Labview(Version 2011, National Instrument, USA)를 사용하였다. 포장시험은 유사한 토양 조건에서 4회 반복 시험을 수행하였으며, 작업속도 고속 조건에서 4개의 주간거리(26, 35, 43, 80cm)와 3개의 식부깊이 (85, 105, 136mm)에 대하여 수행하였다. 안전율 시뮬레이션을 위한 소프트웨어는 KISSsoft(Version 2016, Kissling & Co. AG, Switzerland)를 사용하였다. 식부깊이 85mm에서 주간거리 26, 35, 43, 80cm일 때 작업시 각각 굽힘 안전율은 2.2874, 2.4507, 2.7139, 2.8064로 나타났으며 접촉 안전율은 1.1787, 1.2799, 1.3205, 1.3275로 나타났다. 식부깊이 105mm에서 주간거리 26, 35, 43, 80cm일 때 작업 시 각각 굽힘 안전율은 2.1261, 2.2781, 2.4879, 2.5866로 나타났으며 접촉 안전율은 1.1296, 1.1425, 1.2710, 1.2507로 나타났다. 식부깊이 136mm에서 주간거리 26, 35, 43, 80cm일 때 작업 시 각각 굽힘 안전율은 1.6587, 1.6651, 1.7824, 2.2198로 나타났으며 접촉 안전율은 1.0030, 1.0104, 1.0450, 1.1931로 나타났다. 주간거리에 따른 식부깊이의 굽힘 안전율과 접촉 안전율은 가장 차이가 큰 주간거리 80cm에서 식부깊이가 85, 105, 136mm일 때 작업 시 각각 굽힘 안전율은 2.8064, 2.5866, 2.2198로 나타났으며 접촉 안전율은 1.3275, 1.2507, 1.1931로 나타났다. 시뮬레이션 결과 정식기 베벨기어의 안전율은 주간거리가 짧을수록, 식부깊이가 깊을수록 더 낮게 나타났다. 그러므로 정식 작업 시 정식기의 부하와 내구성을 고려하여 적절한 작업조건을 선정해야 함을 알 수 있다. 또한 향후 다양한 토양 조건 및 작업 단수 등에 따른 포장시험을 추가로 진행하여 여러 조건에서의 안전율 시뮬레이션을 수행할 예정이다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.6 no.3
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• pp.282-288
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• 1982

크랙탄성평판의 굽힘문제가 경계적분방정식으로 구성되었다. 자연변수인 변위, 수직기울기, 굽힘 모우멘트, 등가전단적과 크랙끝에서 응력의 성장율로 정의되는 응력확대계수들이 주변수로 포함 된다. 이 적분방정식들은 가역에너지 적분이론(Green-Rayleigh)을 기초로 크랙응력분포특성에 맞 게 발전되었으며 해당되는 핵함수들이 유도되었다. 등분석 모우멘트를 받는 중앙크랙이 있는 정 4각형 모형에 대한 응력확대계수가 계산되어 기존의 유한요소법의 해와 비교되었다.

• Composites Research
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• v.12 no.6
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• pp.53-64
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• 1999

Microstructural morphology and bending strengths of moulded composites of thermotropic liquid crystalline polymer(LCP) and polyamide 6 (PA6) have been studied as a function of epoxy fraction. Injection-moulding of a composite plaque at a temperature below the melting point of the LCP fibrils generated a multi-layered structure: the surface skin layer with thickness of $65\;-\;120{\mu\textrm{m}}$ exhibiting a transverse orientation; the sub-skin layer with an orientation in the flow direction; the core layer with arc-curved flow patterns. The plaques containing epoxy 4.8vol% exhibited superior bending strength and large fracture strain. With an increase of epoxy fraction equal to and beyond 4.8vol%, geometry of LCP domains was changed from fibrillar shape to lamella-like one, which caused a shear-mode fracture. An analysis of the bending strength of the composite plaques by using a symmetric layered model beam suggested that addition of epoxy component altered not only the microstructural geometry but also the elastic moduli and strengths of the respective layers.

• Journal of Aerospace System Engineering
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• v.13 no.4
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• pp.37-42
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• 2019

The objective of this study was to study the bending characteristics of Ag nano ink using EHD (Electrohydrodynamics) inkjet printing technology for flexibility and miniaturization of devices. The optimal conditions for the technology were derived, and bending characteristics of the Ag nano circuit obtained. For the EHD printing, it is essential to find the optimal point for each parameter such as material characteristics, density, flow rate, voltage, discharge height etc. Therefore, it was derived as the point from the working height and the applied voltage. Also, bending characteristics are confirmed by measuring resistance with each radius of curvature using a fabricated bending module. It was confirmed that rate of resistance change increases rapidly as the radius of curvature increases.

• Journal of the Korean Institute of Electrical and Electronic Material Engineers
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• v.11 no.11
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• pp.1028-1034
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• 1998

Bi-2223 superconductor is known as one of the candidates for practical superconducting wires. Ag-sheathed Bi-2223 superconducting wires were fabricated using the powder-in-tube(PIT) method. When the 19-filaments wire was immersed in liquid nitrogen(77K), maximum critical current density Jc of 62 A/$mm_2$ at 0T was achieved. The critical current density has been shown to depend on the mechanical properties such as tensile stress and bending strain in Ag-sheathed Bi-2223 superconducting wires. The tensile strain for Jc degradation onset was in the range of 0.12~0.3%. In the case of 19-filaments wire, the bending strain is estimated to be smaller than 0.3% for the reasonable Jc value. The observed degradation of the critical current density due to strain effect is inevitable and can be attributed to the formation of microcracks within the superconducting core.

• Composites Research
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• v.12 no.3
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• pp.66-74
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• 1999

A modified mixed mode bending test was performed to investigate the mixed mode delamination for carbon/epoxy composite material. Various mixed mode ratios could be produced by changing the applied load position on the loading lever and the bending load position on the specimen. The modified mixed mode bending test was analyzed to obtain strain energy release rates using beam theory, compliance method and finite element method, This results were in good agreement with the experimental result, which confirmed the validity of this test.

• Composites Research
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• v.13 no.2
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• pp.72-80
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• 2000

Effect of graphite powder addition on the mechanical properties of carbon fiber reinforced carbon composites (C/C composites) was investigated. Greenbody (G/B) with 0~30wt.% graphite powder addition to phenol resin was prepared and carbonized at $1000^{\circ}C$ to make C/C composites. Flexural strengths of 20wt.% graphite powder additions showed maximum values in the both case of G/B and C/C composites. But, at the graphite addition over 20wt.%, there was negative effect due to the matrix inhomogeneity. Flexural strength of cured resin without graphite Powder was higher than that with graphite. However, flexural strength of carbonized resin with graphite increased three times as much as that of carbonized resin without graphite. Because the addition of graphite powder effects the restraint of shrinkage after carbonization and the deflection of crack path. In Mode II ENF test, energy release rates($G_{II}$) of G/B and C/C composites with the 20w1.% addition of graphite were both increased. But, the addition of graphite was more effective to the increase of $G_{II}$ in C/C composites than that in G/B.

• Journal of the Society of Naval Architects of Korea
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• v.33 no.4
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• pp.142-149
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• 1996

Pyramid type three roll bending machines are widely used in roll-bending process to produce singly curved plate. In forming singly curved plate, controlling the vertical displacement of the center roller is most important to acquire the shape required and automation system of the process. In this paper roller bending process is modeled as an elastic-plastic phenomenon and analyzed using beam theory and finite element method. In finite element analysis the workpiece is modeled by using beam elements and plane strain elements respectively. Through the analyses vertical center roller displacement is obtained to get constant curvature distribution along arc length. The relationship between center roller displacement and curvature in steady state as well as residual stress and strain along plate thickness direction are calculated through finite element analysis.

• Journal of the Microelectronics and Packaging Society
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• v.31 no.1
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• pp.23-28
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• 2024

Electronic products utilizing flexible devices experience harsh mechanical deformations in real-use environments. As a result, researches on the mechanical reliability of these flexible devices have attracted considerable interest among researchers. This study employed previous bending strain models and finite element analysis to predict the maximum bending strain of metal films deposited on flexible substrates. Bending experiments were simulated using finite element analysis with variations in the material and thickness of the thin films, and the substrate thickness. The results were compared with the strains predicted by existing models. The distribution of strain on the surface of film was observed, and the error rate of the existing model was analyzed during bending. Additionally, a modified model was proposed, providing mathematical constants for each case.

• Composites Research
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• v.18 no.2
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• pp.20-29
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• 2005

To evaluate the flexural deformation and strength of composite motor case above the glass transition temperature$(T_g),\;170^{\circ}C$, of resin material, a finite element analysis(FEA) model in which material non-linearity and progressive failure mode were considered was proposed. The laminated flexural specimens which have the same lay-up and thickness as the composite motor case were tested by 4-point bending test to verify the validity of FEA model. Also. mechanical properties in high temperature were evaluated to obtain the input values for FEA. Because the material properties related to resin material were highly deteriorated in the temperature range beyond $T_g$, the flexural stiffness and strength of laminated flexural specimen in $200^{\circ}C$ were degraded by also $70\%\;and\;80\%$ in comparison with normal temperature results. Above $T_g$, the failure mode was changed from progressive failure mode initiated by matrix cracking at $90^{\circ}$ ply in bottom side and terminated by delamination at the center line of specimen to fiber compressive breakage mode at top side. From stress analysis, the progressive failure mechanism was well verified and the predicted bending stiffness and strength showed a good agreement with the test results.