• Proceedings of the Materials Research Society of Korea Conference
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• 2009.05a
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• pp.36.1-36.1
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• 2009

OLED(organic light emitting diode)는 차세대 평판 디스플레이로 전자종이, 입는 디스플레이 등 flexible한 디스플레이로도 주목받고 있다. 하지만, OLED의 가장 큰 단점 중의 하나가 수분과 산소에 매우 민감하다는 것으로 이것은 OLED의 lifetime과 연결된다. 따라서 이에 대한 mechanism의 확립이 필요하다. 따라서 본 연구에서는, flexible한 OLED에 적용되는 금속 코팅막의 적층구조 및 기판의 노출온도에 따른 금속 코팅막의 수분침투 특성에 대해 MOCON의 weight gain test (WGT)를 통해 barrier layer에 대해 평가하고 이에 대한 mechanism을 확립하는데 그 목적이 있다. 금속 코팅막은 OLED의 cathode와 anode 재료로 많이 사용되는 Al과 ITO를 sputter장비를 이용해 single layer와 multi-layer의 두 가지 구조로 PET기판에 증착하였다. 또한, 노출온도에 따른 특성을 알아보고자 bare PET / ITO coated PET(single layer $50{\mu}m$) / Al coated PET(single layer $200{\mu}m$)의 세 가지 시편을 제작하였다. 이 시편을 각각 $25^{\circ}C$, $37.8^{\circ}C$, $50^{\circ}C$의 온도에서 test를 진행하였고 이 과정을 100%RH, 70%RH, 40%RH조건의 수분조건에서 진행하여 각각의 수분조건에서 각각의 온도에 따른 금속 코팅막의 수분침투 특성에 대한 mechanism을 확립하였다. 적층구조에 따른 수분침투 특성 평가 결과 multi-layer가 single layer보다 더 우수한 수분침투의 barrier 특성을 나타냈었다. 그리고 각 온도에 따른 test결과 온도가 증가할수록 barrier의 특성이 나빠짐이 보였다.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.02a
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• pp.351-351
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• 2010

OLED(organic light emitting diode)는 액정디스플레이를 대체할 차세대 평판디스플레이로 많은 주목을 받고 있다. 현재 많이 사용되고 있는 OLED의 기판재료는 Glass기판이지만 차세대 Flexible한 display에서의 적용을 위해서는 가볍고 유연한 plastic을 기판 재료로 사용 할 것으로 보인다. 하지만 plastic이 기판재료로 된 OLED의 가장 큰 단점중의 하나가 수분과 산소에 민감하여 열화를 초래한다는 것이다. 이런 수분침투와 열화 과정으로 인해 OLED의 발광효과가 약해져 OLED의 수명과 직접적으로 연결된다. 하여 외부에서 OLED내부로 유입되는 산소, 수분으로 부터 발광재료와 전극의 산화를 방지하며 외부의 충격으로부터 소자를 보호하기 위한 봉지기술은 반드시 필요하다. 따라서 본 연구에서는, flexible한 OLED에 적용되는 금속 코팅한 막의 적층구조 및 기판의 노출온도에 따른 금속 코팅막의 수분침투 특성에 대해 MOCON의 weight gain test (WGT)를 통해 barrier layer에 대해 평가하고 이에 대한 mechanism을 확립하는데 그 목적이 있다. 금속을 코팅한 막은 OLED의 cathode와 anode 재료로 많이 사용되는 Al과 ITO를 sputter장비를 이용해 single layer와 double-layer의 두 가지 구조로 PET기판에 증착하였다. 증착한 Al막의 두께는 각각 50 nm, 100 nm, 200 nm, 400 nm 등 4가지로 하였다. double-layer의 경우에는 총 두께를 절반씩 기판의 양쪽에 증착하였다. 적층구조에 따른 수분침투 특성 평가 결과로 보면 같은 두께일 때 double-layer는 single layer에 비해서 모든 시편에서 수분의 투습율이 낮음으로써 더 좋은 수분침투의 barrier 특성을 나타내었다. 특히 100 nm이상인 경우 투습율은 예상한 값보다 50%이상 낮게 나타났다.

• Composites Research
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• v.20 no.4
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• pp.25-30
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• 2007

The advanced fiber-reinforced laminated composites are widely used in a variety of engineering applications such as aerospace, marine, mechanical and civil engineering for weight savings because of their high specific strength and stiffness. The material properties of ply is known to have larger variations than that of conventional materials and very sensitive to the loading direction. Therefore, it is important to consider the variations on designing the laminated composite. This paper demonstrates the importance of considering uncertainties through examining the effect of material properties variations on various design requirements such as tip deflection, natural frequency and buckling stress using COMSOL-MATLAB interface.

• Journal of the Korean Society for Nondestructive Testing
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• v.29 no.4
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• pp.323-330
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• 2009

The objective of this research was to develop a practical integrated approach using extracted features from electrical resistance measurements and coupled electromechanical models of damage, for in-situ damage detection and sensing in carbon fiber reinforced plastic(CFRP) composites. To achieve this objective, we introduced specific known damage (in terms of type, size, and location) into CFRP laminates and established quantitative relationships with the electrical resistance measurements. For processing of numerous measurement data, an autonomous data acquisition system was devised. We also established a specimen preparation procedure and a method for electrode setup. Coupon and panel CFRP laminate specimens with several known damage were tested. Coupon specimens with various sizes of artificial delaminations obtained by inserting Teflon film were manufactured and the resistance was measured. The measurement results showed that increase of delamination size led to increase of resistance implying that it is possible to sense the existence and size of delamination. A quasi-isotropic panel was manufactured and electrical resistance was measured. Then three different sizes of holes were drilled at a chosen location. The panel was prepared using the established procedures with six electrode connections on each side making a total of twenty-four electrodes. Vertical, horizontal, and diagonal pairs of electrodes were chosen and the resistance was measured. The measurement results showed the possibility of the established measurement system for an in-situ damage detection method for CFRP composite structures.

• Journal of the Institute of Electronics Engineers of Korea SD
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• v.41 no.6
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• pp.91-98
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• 2004

This paper proposes a PCB plane model for generic SPICE circuit simulators. The proposed model reflects two frequency-dependent losses, namely skin and dielectric losses. After power/ground plane pair is divided into arrays of unit-cells, each unit-cell is modeled using a transmission line and two loss models. The loss model is composed of a resistor for DC loss, series HL ladder circuit for skin loss and series RC ladder circuit for dielectric loss. To verify the validity of the proposed model, it is compared with SPICE ac analysis using frequency-dependent resistors. Also, we show that the estimation results using the proposed model have a good correlation with that of VNA measurement for the typical PCB stack-up structure of general desktop PCs. With the proposed model, not only ac analysis but also transient analysis can be easily done for circuits including various non-linear/linear devices since the model consists of passive elements onl.

• Composites Research
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• v.26 no.2
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• pp.85-90
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• 2013

This paper presents the fabrication and 3-point flexion testing of carbon fiber reinforced polymer (CFRP) composite face/aluminum honeycomb core sandwich panels. Specimen sandwich panels were fabricated with three honeycomb types (3.18 mm, 4.76 mm, and 6.35 mm cell size) and three panel radii (flat, r = 1.6 m, r = 1.3 m). The curved sandwiches were fabricated normally with the core in the W-direction. The tensile mechanical properties of the CFRP $2{\times}2$ twill fabric face laminate were evaluated (modulus, strength, Poisson's ratio). The measured values are comparable to other CFRP fabric laminates. The flat sandwich 3-point flexion test core shear strength results were 11-30% lower than the manufacturer published data; the test set-up used may be the cause. With a limited sample size, the 1.3 meter panel curvature appeared to cause a 0.8-3.8% reduction in ultimate core shear strength compared to a flat panel.

• Journal of the Korean Society for Nondestructive Testing
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• v.26 no.4
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• pp.220-230
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• 2006

Fracture behavior of a monolithic PZT and a plate-type piezoelectric composite actuator (PCA) has been investigated under a bending load at three points by an acoustic emission (AE) monitoring. AE signal from a monolithic PZT at the maximum bending load shows the characteristics of high amplitude and long duration with a low frequency band of $100{\sim}230kHz$ which is confirmed by fast Fourier transform (FFT). For a PCA, it is concluded that AE signals with high amplitude over 80dB and low dominant frequency band of $170{\sim}223kHz$ emitted in the stage I are due to the brittle fracture in the PZT layer and the delamination between the PZT layer and the adjacent fiber composite layer. Based on the above analysis of AE behavior and damage observations with an optical microscopy and a scanning electron microscopy, AE characteristics related to fracture behavior of asymmetrically laminated PCA have been elucidated.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.37 no.4
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• pp.461-466
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• 2013

Advanced fiber-reinforced laminated composites are widely used in various fields of engineering to reduce weight. The material property of each ply is well known; specifically, it is known that ply is less reliable than metallic materials and very sensitive to the loading direction. Therefore, it is important to consider this uncertainty in the design of laminated composites. In this study, reliability analysis is conducted using COMSOL and MATLAB interactions for a laminated composite plate for the case in which the tip deflection is the design requirement and the material property is a random variable. Furthermore, the efficiency and accuracy of the approximation method is identified, and a probabilistic sensitivity analysis is conducted. As a result, we can prove the applicability of the advanced design method for the stabilizer of an underwater vehicle.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.26 no.6
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• pp.475-481
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• 2013

The residual stresses occur in the Frequency Selective Surface(FSS) embedded hybrid composite structures after co-curing due to mismatch among the coefficient of thermal expansions and stiffness values between the FSS and composite materials. The spring backs occur due to these residual stresses. Therefore, in this paper, the spring-backs caused by residual stresses in FSS embedded composite structures were studied with considering effect of symmetric and unsymmetric stacking sequence of composite laminates.

• Transactions of the Korean Society of Mechanical Engineers
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• v.17 no.1
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• pp.90-100
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• 1993

A finite element formulation of vibration control of a laminated plate with piezoelectric sensor/ actuators is presented. Classical lamination theory with the induced strain actuation and Hamilton's principle are used to formulate the equations of motion of the system. The total charge developed on the sensor layer is calculated from the direct piezoelectric equation. The equations of motion and the total charge are discretized with 4 node, 12 degrees of freedom quadrilateral plate bending elements with one electrical degree of freedom. The mass and stiffness of the piezoelectric layer are introduced by treating them as another layer in laminated plate. Piezoelectric sensor/actuators are distributed, but discrete due to the geometry of electrodes. By defining an i.d. number of electrode for each element, modelling of electrodes with variable geometry can be achieved. The static response of a piezoelectric bimorph beam to electrical loading and sensor voltage to given displacement are calculated. For a laminated plate under the negative velocity feedback control, the direct time response by the Newmark-.betha. method and damped frequencies and modal damping ratios by modal state space analysis are derived.