• Proceedings of the Korean Society of Precision Engineering Conference
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• 2003.10a
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• pp.209-209
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• 2003

• Journal of the Korean Society of Propulsion Engineers
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• v.5 no.2
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• pp.59-64
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• 2001

The purpose of this work is to investigate the static strength, the stress distribution, and the failure process of quasi-isotropic composite laminates made of two different matrices when loading directions are changed. We carried out static tests of $[0/-60/+60]_s$ and $[+30/-30/90]_s$ laminates. Two types of matrices used are AS4/epoxy and AS4/PEEK. The damage mechanisms of the quasi-isotropic laminate, $[0/-60/+60]_s$, strongly depend on the load direction applied to the laminate.

• Proceedings of the Materials Research Society of Korea Conference
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• 2012.05a
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• pp.104.1-104.1
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• 2012

타이타늄(Ti)은 비강도가 높고, 내식성이 우수하여 항공기, 자동차 및 선박과 같은 수송기기의 소재로 사용되고 있다. 이러한 특성을 가진 타이타늄을 이종소재와 결합하여 더 우수한 기계적 특성을 얻을 수 있다면, 그 응용범위를 확대할 수 있을 것이다. 본 연구에서는 타이타늄과 알루미늄(Al) 판재를 적층한 후, 열간압연을 통해 타이타늄/알루미늄 적층재를 제조하였다. 이와 같은 적층재를 다양한 압하율로 냉간 압연한 후 미세조직을 관찰하였으며, 인장시험을 통해 기계적 특성을 조사하였다. 아울러 타이타늄 판재만으로도 유사한 실험을 실시하여 기계적 특성을 적층재와 비교 평가하였다.

• Journal of Institute of Control, Robotics and Systems
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• v.4 no.3
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• pp.329-333
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• 1998

본 논문에서는, LSI 적층 기술을 이용한 실시간 처리 마이크로 비젼의 개발을 소개하고 있다. 새롭게 개발된 LSI 적층기술을 이용하여, 영상신호의 증폭, 변환, 연산처리등의 기본기능을 가지는 다수의 LSI 웨이퍼를 적층한다. 각 층간의 고밀도 수직배선을 통하여 대량의 영상정보를 동시에 전달하므로써, 대규모 동시 병렬처리를 가능하게 하며, 다수의 층에 걸쳐 파이프 라인 처리가 이루어진다. VLSI 설계시스템을 이용하여, 윤곽 검출기능을 가지는 테스트 칩을 설계(2 .mu.m CMOS design rule)하고, 시뮬레이션을 통하여 양호한 동작(처리시간 10 .mu.s)을 확인하고 있다. 시험제작을 위해서는, 새롭게 개발된 LSI 적층기술이 이용된다. 영상처리의 기본회로가 실려있는 웨이퍼의 기반을 30 .mu.m 의 두께까지 연마하고, 개발된 웨이퍼 aligner를 이용하여 수직배선이 형성된 상하 두 개의 웨이퍼를 미세조정하면서 접착한다. 이상의 제작과정을 반복하여 두께 1mm이하의 인공망막과 같은 마이크로 비젼을 제작한다.

• Composites Research
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• v.23 no.5
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• pp.15-21
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• 2010

In this study, repair and maintenance schemes of the damaged composite structure was investigated, and a repair process of the carbon/epoxy laminate composite structure was investigated numerically and experimentally. The composite laminates were damaged by drop weight type impact test machine. The damaged composite structure was repaired using external patch repair method after removing damaged area. The compressive strength test and analysis results after repairing the impact damaged specimens were compared with the compressive strength test and analysis results of undamaged specimens and impact damaged specimens. Finally, the strength recovery capability by repairing were investigated.

• Composites Research
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• v.16 no.2
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• pp.9-17
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• 2003

We have implemented a system of falling weight impact tester in order to evaluate the impact energy absorbing characteristics and impact strength of CFRP laminate plates. The absorbed energy of T-300 orthotropic composites is higher than that of quasi-isotropic specimen over impact energy 7J, but in case of using T700 fiber, much difference does not show. Also, absorbed energy of T-300 orthotropic composites, which are composed of the same stacking number and orientation became more than that of T700 fiber specimen however there was no big difference in case of quasi-isotropic specimens. Delamination area of impacted specimens was measured with ultrasonic C-scanner to find correlation between impact energy and delamination area. Delamination area and frequency responses were evaluated between impacted and unimpacted specimens. There is a strong correlation between frequency responses and impact-induced delamination. The presence and scale of damages have been investigated based on the variations of frequency responses.

• Journal of the Korean Society of Propulsion Engineers
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• v.10 no.3
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• pp.48-52
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• 2006

Through-the-thickness properties of thick-walled cylindrical composites are required to determine structural performances because interlaminar tensile stress is primarily responsible for structural failure of the composites during their curing process. It is necessary for evaluating the tensile properties to find individual test methods to find appropriate methods because there are no recognised international standards(test methods and test specifications) available for generating reliable tensile properties in the direction. This paper has performed an experimental study to measure that properties of carbon fabric/phenolic composites which are produced by domestic company. Several test methods using an aluminum specimen were compared and evaluated. The best test method to measure transverse through-the-thickness properties of composite materials was developed by the experimental results that strain trends on all faces of composite specimen are the same.

• Asia-pacific Journal of Multimedia Services Convergent with Art, Humanities, and Sociology
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• v.8 no.3
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• pp.589-596
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• 2018

Transportation or structure has the important role at clothing, food, and housing at modern society. If even the small crack happens and propagates at transportation or structure, the parts are fractured and they can cause a disaster. CT specimen was used in order to investigate the damage trend due to the crack propagation at this study to prevent this situation. As the material of CT specimen, the unidirectional carbon fiber reinforced plastic of the composite material in the limelight nowadays. The laminate angle designated in order of [60/-60/60/-60] was applied to the specimen model with the unidirectional fiber. As the analysis condition, the forced displacement was applied to the hole of upper part after fixing the hole of lower part. At the result of this study, the equivalent stress and shear stress was shown to be higher in order of the structural steel, copper, titanium and aluminum. This study result is thought to be utilized usefully at verifying the damage of CT specimen made of inhomogeneous material.

• Journal of Korean Society of Steel Construction
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• v.26 no.6
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• pp.559-570
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• 2014

In this study, compression and shear characteristics of laminated rubber bearings and lead rubber bearings with various parameters are investigated by using material and geometric nonlinear three-dimensional finite element analysis. Rubber coupon tests are performed to make a model of the laminated rubber bearings. In addition, the material constants of the rubber are calculated by the curve fitting process of stress-strain relationship. The finite element analysis and experimental tests of the laminate rubber bearings are used to verify the validity of the rubber material constants. It is seen that the compression behavior of the laminated rubber bearings and lead rubber bearings mainly varies depending on the first shape factors and their shear behavior significantly varies depending on the second shape factors. In addition, the horizontal stiffness and energy dissipation capacity of lead rubber bearing are increased when the diameter of a lead bar is increased.

• Composites Research
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• v.17 no.1
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• pp.18-28
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• 2004

In order to evaluate the strength of carbody structures of railway rolling stock made of laminated fiber-reinforced composite materials, total laminate approach was introduced. Structural analyses were conducted to check the basic design of hybrid composite carbody structures of the Korean Tilting Train eXpress(TTX) with the service speed of 180km/h. The mechanical tests were also conducted to obtain strengths of composite laminates. The results show that all stress components of composite carbody structures are inside of failure envelopes and total laminate approach is recommended to predict the failure of hybrid composite carbody structures at the stage of the basic design.