• Composites Research
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• v.17 no.4
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• pp.53-60
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• 2004

This paper describes a method for a falling weight impact test to estimate the impact energy absorbing characteristics and impact strength of CFRP laminate plates based on considerations of stress wave propagation theory. The absorbed energy of T300 orthotropic composites is higher than that of quasi-isotropic specimen over impact energy 6.8J, but in case of using T700 fiber, much difference does not show. Also, absorbed energy of T300 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. The delamination areas of the impacted specimen were measured with the ultrasonic C-scanner to find correlation between impact energy and delamination area. The fracture surfaces were observed by using the SEM (scanning electron microscope) through a low-velocity impact test in order to confirm the fracture mechanism.

• Proceedings of the Korean Vacuum Society Conference
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• 2011.08a
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• pp.239-239
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• 2011

최근에 감지막의 pH 감지특성을 평가하기 위해 electrolyte insulator semiconductor (EIS) 구조가 유용하게 이용되고 있다. EIS는 CMOS공정과 호환이 가능하고 구조가 간단하며 pH 변화에 반응속도가 빠르다는 장점을 가지고 있다. EIS 구조를 갖는 pH 센서의 동작 메커니즘은 pH 용액의 수소이온이 감지막의 표면에서 표면전위를 변화시키는 것에 기인한다. pH 감지막으로는 높은 유전율과 안정성이 뛰어난 high-k 물질이 많이 연구되고 있다. 그 중 high-k 물질인 ZrO2은 낮은 열전도도, 산성에서 알칼리성 영역까지의 넓은 화학안정성을 가지며 낮은 열 팽창성, 높은 유전상수 등 우수한 특성을 가지고 있다. 본 실험은 SiO2/ZrO2를 적층한 EIS 소자를 제작하여 열처리에 따른 전기적 특성과 pH 감지 특성을 평가해 보았다. EIS 적층막으로 사용된 SiO2는 실리콘과 high-k 감지막 사이의 계면상태를 양호하게 유지시키기 위한 완충막으로 성장되었다. 후속열처리는 rapid thermal annealing (RTA) 시스템을 이용하여 750$^{\circ}C$, 850$^{\circ}C$, 950$^{\circ}C$로 H2/N2 분위기에서 30초 동안 실시하였다. RTA 열처리 온도가 증가할수록 높은 pH 감지특성이 보였으며 hysteresis 현상과 drift 효과와 같은 non ideal 효과에 강한 immunity가 있는 것을 확인하였다. 결론적으로 SiO2/ZrO2 적층구조를 갖는 EIS는 RTA 950$^{\circ}C$ 열처리를 실시하였을 때 우수한 EIS pH 센서를 제작할 수 있을 것으로 기대된다.

• Composites Research
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• v.24 no.6
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• pp.49-55
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• 2011

The use of advanced composite materials in main structures of military and civil aircraft has been increased rapidly because of their considerable metals in high specific strength and stiffness. However, the mechanical properties of composite materials may severely degrade in the presence of damage. Especially, the high-velocity impact such as a hailstorm, and a small piece of tire or stone during high taxing, can cause considerable damage to the structures and sub-system in spite of a very small mass. However, it is not easy to detect the damage in composite plates using a single sensor or any conventional methods. In this paper, the PVDF sensors and AE sensors were used for monitoring high-velocity impact damage initiation and propagation in composite laminates. The WT(wavelet transform) is used to decompose the sensor signals. In the PVDF sensor and AE sensor signal analysis, amounts of high-frequency signals are increased when the impact energy is increased. PVDF sensor and AE sensor signal appeared similar results. This study shows how various sensing techniques can be used to characterize high-velocity impact damage of advanced composite laminates.

• Journal of the Korean Ceramic Society
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• v.40 no.11
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• pp.1090-1095
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• 2003

In this paper, the modeling and design of high-Q multilayer passives and multilayer diplexer for GSM/DCS applications designed and fabricated using these passives have been investigated.. To miniaturize the system, configurations of inductor and capacitor have involved a square spiral structure and a vertically-interdigitated capacitor similar to 3D interdigital structure, respectively. Multilayer diplexers for GSM/DCS applications were designed and fabricated to apply high-Q multilayer passives to practical systems, which were designed by the proposed structural and equivalent circuit model. LPF for GSM band had the passband insertion loss of less than 0.55 dB, the return loss of more than 12 dB, and the isolation level of more than 26 dB by locating attenuation pole at 1800 MHz. HPF for DCS band had the passband insertion loss of less than 0.82 dB, the return loss of more than 11 dB, and the isolation level of more than 38 dB by locating attenuation pole at 930 MHz.

• Journal of Aerospace System Engineering
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• v.14 no.3
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• pp.69-77
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• 2020

Airframe structure development of the 35 kg class 'Disaster and Public Safety Multicopter' UAV is described in this paper. To reduce the airframe weight, T-700 grade CFRP composite material was used, and the fuselage was designed with the semi-monocoque structure and plate installed with the control and communication devices designed in a sandwich structure. The specimen tests for the laminated plate and pipe were conducted to verify the strength and stiffness of the designed parts. The stacking sequence of composite materials was determined by the static strength and vibration analysis, and landing gear strut was designed by the nonlinear analysis with decent speed and ground clearance requirements. The static strength test was performed to evaluate the structural integrity and to verify the landing gear behavior.

• The Journal of The Korea Institute of Intelligent Transport Systems
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• v.20 no.2
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• pp.72-78
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• 2021

This paper proposes a wide-band dual-polarization stacked patch array antenna for satellite SAR system applications. The array antenna was designed for loss minimization and wide-band characteristics to enhance the performance of the SAR system and optimize it for active return loss in applications to active phased arrays. The fabricated array antenna showed a performance of 19.26%/19.79% fractional bandwidth within the -10 dB reference level of the active return loss and showed loss characteristics of 0.797 dB/0.799 dB averaged within the operational frequency for both H/V-polarization cases. The pattern performance was verified by comparing the measured patterns with the calculated patterns obtained by the array factor.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2012.10a
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• pp.161-162
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• 2012

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2012.10a
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• pp.571-572
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• 2012

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2008.06a
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• pp.103-104
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• 2008

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2011.06a
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• pp.1459-1460
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• 2011