• 상하수도학회지
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• 제26권3호
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• pp.343-354
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• 2012

A electro-foaming fusion wrap fitting for polyethylene sewer pipe was built and foaming mechanism has been studied. A foaming sheet, supporting sheet and clamping band is assembled into a all-in-one structured electro-foaming fusion wrap fitting. To specify foaming and fusion of electro-foaming fusion wrap for PE sewer pipe, series of fusion tests were performed in various conditions. A parallel plate compression test up to 50 % of inner diameter deflection has been performed to check integrity of fusion quality and it was found that there were no visible signs of crack in wrapped area of fitting. Also air tightness test based on KS M 3511-2 has been performed to evaluate perfectness of wrap fusion quality and we found there were no pressure drop up to 10 times higher value than KS standard regulation.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2010년도 하계학술대회 논문집
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• pp.68-68
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• 2010

To reduce PV manufacturing costs, the thickness of solar cell is getting thinner. Bow is shown after cooling down the temperature of solder cell. It happens because of different thermal expansion coefficients of different metals. Bowed cell can make micro crack while module processing and it can drop off efficiency of PV module. As thinner solar cell is produced, the thickness of ribbon should be concerned to prevent extra bow. In this paper we investigate the contrast of deflection when we solder different thickness of ribbons on same solar cell. This approach would help to find out the optical thickness of ribbon for particular thickness of solar cell later on.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2007년도 춘계학술대회 논문집
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• pp.144-150
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• 2007

In this paper, the low velocity response of four different sandwich panels with metal and laminate composite facesheets has been investigated by conducting drop-weight impact tests using an instrumented falling-weight impact tower. Square samples of 100mm sides were subjected low-velocity impact loading using an instrumented testing machine at six energy levels. Impact parameters like maximum force, time to maximum force, deflection at maximum force and absorbed energy were evaluated and compared for four different types of sandwich panels. The impact test results show that sandwich panel with composite laminate facesheet could not observe damage mode of a permanent visible indentation after impact and has a good impact damage resistance in comparison with sandwich panel with metal aluminum facesheet.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.162-167
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• 2004

The low velocity impact characteristics of composite laminate curved beams are investigated to increase damage tolerance and reduce the deflection. Drop weight impact tests of the composite curved beam were performed with respect to pre-load, then the damage after impact was measured by macrography. Also, finite element analyses were performed using ABAQUS to investigate the stress state of composite curved beam with respect to pre-load and impact. From the investigation, it was found that pre-load of the composite curved beams had much influence on impact damage of the curved beam, which showed good agreement with the experiment results.

• 대한의용생체공학회:학술대회논문집
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• 대한의용생체공학회 1993년도 추계학술대회
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• pp.99-103
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• 1993

A monoleaflet polymer artificial heart valve which showed the remarkable improvement in pressure drop compared with other types of artificial valve was designed to decrease the deflection in vertical direction and the displacement or the valve tip in horizontal direction. Stress distribution change was studied as the location of the supporting members or the valve frame changed. And it was found that using the valve tip horizontal displacement the minimum valve thickness could be obtained in order to prevent the gap between the valve tip and the frame wall.

• 한국정밀공학회지
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• 제14권6호
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• pp.135-141
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• 1997

Low velocity impact test and compressive residual strength test after impact were performed by using Hercules AS4/3501-6[45/0/-45/90]$_{2s}$ laminated plate to investigate the low velocity impact damage behavior and the post-impact strength degradation on orthotropic composite laminate plate. Due to the lateral impact losd, the load path showed "" shape according to the laminate central deflection. Damage in a laminate occurs by inclined matrix crack at the damage initiation load stage and vertical matrix crack, occurs on the outer surface. Evaluating the compressive residual strength after the low velocty impact test, it could be found that there is a transient range where the compressive residual strength drop suddenly in the initial damage which is in the matrix crack range and the initial delamination area. is in the matrix crack range and the initial delamination area.

• 한국지반공학회논문집
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• 제15권6호
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• pp.29-44
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• 1999

본 논문은 균질 및 비균질의 사질토 지반에서 항타 시공된 단일 강성말뚝의 수평거동에 대한 모형실험 결과들을 고찰하였다. 본 연구의 목적은 말뚝의 수평거동 특성에 대한 말뚝 시공상태 (Driven & Embedded), 말뚝 근입길이에 대한 하부지반의 두께비 (H/L),그리고 지반의 상대밀도의 영향에 관하여 실험적인 연구를 수행하고 이러한 영향들을 정량화 할 수 있는 실험결과를 얻었다. 모형 실험 결과들에 의하면, 수평거동은 느슨한 균질지반에서 시공방법에 상당히 의존하는 것으로 나타났다. 말뚝시공시 항타방법에 의존할 경우 균질지반에서는 느슨한 지반일수록 그리고 비균질 지반 $(E_{h1}/E_{h2}/=0.18)$에서는 상부층 두께가 클수록 수평변위 감소에 상당한 효과를 얻을 수 있으나, 최대 휨모멘트 감소는 수평변위 감소와 정반대의 결과를 나타냈다. 수평변위 측면에서, 매입말뚝에 대한 항타말뚝의 변위비 $(y_{Driven}y_{Embedded})$는 균질지반의 각 상대 밀도에 대하여 0.65-0.88 $(D_r=90%)$와 0.38-0.65 (D$_{r}$=61.8%)의 범위로 그리고 비균질지반에서 0.6-0.88 의 범위로 나타났다. 또한, 본 연구에서는 $y_D/y_E \;와\; NBM_D/MBM_E$에 대한 항타고와 H/L의 영향들을 모형실험 결과들로부터 실험식으로 제안하였다.

• Structural Engineering and Mechanics
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• 제65권5호
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• pp.573-585
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• 2018

This article presents strain gradient elasticity-based procedures for static bending, free vibration and buckling analyses of functionally graded rectangular micro-plates. The developed method allows consideration of smooth spatial variations of length scale parameters of strain gradient elasticity. Governing partial differential equations and boundary conditions are derived by following the variational approach and applying Hamilton's principle. Displacement field is expressed in a unified way to produce numerical results in accordance with Kirchhoff, Mindlin, and third order shear deformation theories. All material properties, including the length scale parameters, are assumed to be functions of the plate thickness coordinate in the derivations. Developed equations are solved numerically by means of differential quadrature method. Proposed procedures are verified through comparisons made to the results available in the literature for certain limiting cases. Further numerical results are provided to illustrate the effects of material and geometric parameters on bending, free vibrations, and buckling. The results generated by Kirchhoff and third order shear deformation theories are in very good agreement, whereas Mindlin plate theory slightly overestimates static deflection and underestimates natural frequency. A rise in the length scale parameter ratio, which identifies the degree of spatial variations, leads to a drop in dimensionless maximum deflection, and increases in dimensionless vibration frequency and buckling load. Size effect is shown to play a more significant role as the plate thickness becomes smaller compared to the length scale parameter. Numerical results indicate that consideration of length scale parameter variation is required for accurate modelling of graded rectangular micro-plates.

• 대한의용생체공학회:의공학회지
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• 제17권1호
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• pp.85-92
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• 1996

병변이 있는 판막을 대체하기 위하여 사용되는 인공판막으로는 기계식 판막, 고분자 판막 등이 있는데 고분자 판막이 기계식보다 항혈전성이 우수하므로 폴리우레탄을 이용하여 많이 연구되고 있다. 고분자 판막에는 단엽식, 삼엽식, 젤리피쉬식 등으로 제작되어 연구되고 있는데 이중 단엽식 판막은 제작이 가장 간편하고 심실내 씻김현상이 실제와 유사하며 혈류의 소용돌이 현상을 감소시킨다고 보고되고 있다. 혈압 강하를 감소시키기 위하여 고분자 판막의 두께를 얇게 할때 판막이 프레임 위 정상접촉 위치로 부터 탈구현상이 발생한다. 이것을 방지하기 위하여 2개의 지지대를 설치하여 판막의 수직변위를 최소로 하는 지지대 최적위치를 구하고, 그때 판막 끝의 수평 변위 및 판막에서의 응력분포상태를 구한 결과 최적위치는 지지대에 의해 나눠지는 3영역의 폭이 각각 6.2mm, 4.7mm, 5.1mm 일때 이고, 그때 최대 처짐이 0.19mm, 수평 최대변위가 0.047mm 이고 최대 주응력이나 등가응력의 최대치는 판막이 지지대가 접착되는 부위와 비접착 부위의 불연속점에서 발생하여 이 값들은 판막 각 영역의 폭이 커지면 증가함을 알았다.

• 한국해양공학회지
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• 제30권4호
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• pp.277-286
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• 2016

The first part of this study found the tendencies of the mechanical properties of two arctic structural steels (EH32 and FH32). In the second part, the crashworthiness of stiffened panels scaled down from the side frame structure of a Korean research icebreaker was determined. A procedure for designing the shapes and sizes of the stiffened panels, mass and shape of a drop striker, and a large temperature chamber, and then manufacturing these, is introduced in detail. From impact bending tests for the stiffened panels, the residual permanent deformations and deformation histories over time were captured using manual measurement and video image analyses. Numerical simulations of the impact bending tests were carried out for three different finite element models, which were mainly composed of shell elements, solid elements, and solid elements, with welding beads. It was proven from a comparison of the test results and numerical simulation results that the solid element model with the welding bead consideration approached the test results in terms of the residual deformations as long as the strain rate effect was taken into account.