• 제어로봇시스템학회논문지
• /
• 제22권4호
• /
• pp.247-252
• /
• 2016

In this paper, we propose a new defect detection technology for micro-defect on the surface of steel products. Due to depth and size of microscopic defect, slop of surface and vibration of strip, the conventional optical method cannot guarantee the detection performance. To solve the above-mentioned problems and increase signal to noise ratio, a novel retro-schlieren method that consists of retro reflector and knife edge is proposed. Moreover dual switching lighting method is also applied to distinguish uneven micro defects and surface noise. In proposed method, defective regions are represented by a black and white pattern. This pattern is detected by a defect detection algorithm with Gabor filter. Experimental results by simulator for sample defects of cold rolled steel show that the proposed method is effective.

• 한국소성가공학회:학술대회논문집
• /
• 한국소성가공학회 2002년도 금형가공 심포지엄
• /
• pp.266-273
• /
• 2002

Milli-structure components are classified as a component group whose size is between macro and micro scales, that is, about less than 20mm and larger than 1mm. The bending of these components of thin sheets has a typical phenomenon of bulk deformation because of the forming size. The recent trend towards miniaturization causes an increased demand for parts with very small dimensions. The conceptual miniature bending process enables the production of such parts with high productivity and accuracy. The stress values of the flow curve decrease with miniaturization, which means that coarse grained materials show a higher resistance against deformation, when the grain size is in the range of the sheet thickness. In this paper, a new numerical approach is proposed to simulate intergranular milli-structure in forming by the finite element method. The grain element and grain boundary element are introduced to simulate the milli-structure of strip in the bending. The grain element is used to analyze the deformation of individual grain while the grain boundary element is for the investigation on the movement of the grain boundary. Also, the result of the finite element analysis is confirmed by a series of milli-sized forming experiments.

• Design & Manufacturing
• /
• 제2권1호
• /
• pp.51-56
• /
• 2008

Recently, the demand of high-productivity injection mold increases since the consumption of packaging grows in the world. Stack mold is composed of more than two molds and it has very high productivity and economic efficiency. In this study, stack mold was developed to improve productivity of vehicle fixed weather strip with TPV materials and to investigate the characteristic of injection molding using CAE.

• 한국정보통신학회:학술대회논문집
• /
• 한국해양정보통신학회 2011년도 추계학술대회
• /
• pp.54-55
• /
• 2011

마이크로 스트립 안테나는 최근 소형화, 경량화 및 다층 구조를 통합 집적화 과정을 통하여 통신용 소자로서 그 활용도가 높다. 또한 통신 시스템의 소형화를 통하여 저전력 및 경비 절감이 기대된다. 본 연구에서는 장거리 통신이 가능한 마이크로 스트립 안테나를 설계를 목적으로 하며, 제작된 프로토타입 안테나를 대상으로 네트워크 어낼라이저를 이용하여 그 특성을 분석하였다.

• 우주기술과 응용
• /
• 제1권1호
• /
• pp.33-40
• /
• 2021

본 논문에서는 총 무게 42 kg 이내의 요구사항을 토대로 차세대소형위성 2호 영상 레이다 시스템을 개발한 결과를 보고한다. 차세대소형위성 2호는 소형급 인공위성으로, 탑재체의 무게 비중이 전체 무게 대비 약 40% 정도를 차지하도록 설계하였다. 영상 레이다 시스템은 안테나, RF송수신기, 기저대역 신호처리기, 전력부 등으로 구성되며, 이 중에서 특히 무게 비중이 큰 부품은 영상 레이다의 핵심인 안테나이다. 안테나 설계시 이득, 효율 등을 고려한 다양한 선택이 가능하지만, 차세대소형위성 2호 사업에서 요구하는 무게, 전력 및 해상도 등을 반영하여 Micro-strip Patch Array 안테나를 채택하여 설계하였다. 차세대소형위성 2호의 임무 요구 조건에 부합하도록 안테나의 주파수는 9.65 GHz, 이득은 42.7 dBi 그리고 반사손실은 -15 dB로 규정하여 개발하였으며, 차량에 탑재한 현장시험을 통하여 요구 성능의 충족 여부를 검증하였다.

• Journal of electromagnetic engineering and science
• /
• 제16권3호
• /
• pp.191-193
• /
• 2016

This paper proposes a voltage-controlled oscillator (VCO) that has broadband turning and low-level of phase noise characteristics. Due to the micro-strip line resonant circuit with a low Q value, which is applied to the broadband tuning range, the depreciated phase noise performance is compensated by restraining the harmonics of the oscillating frequency. The VCO was designed according to the proposed structure as well as the conventional structure, and the superiority of the proposed structure was verified through its simulation, fabrication, and measurement.

• 전자공학회논문지A
• /
• 제29A권10호
• /
• pp.24-28
• /
• 1992

A new design method of microstrip wide band VHF tunable bandpass filters using varacter diodes is presented. In the proposed filter both the input and output ports are coupled through capacitors, and an open micro-strip line is inserted between the coupled line in order to obtain the desired degree of coupling. The optimized filter responseses for the frequency range of 220-404MHz by TOUCH-STONE are compared with the measured ones.

• 전자통신동향분석
• /
• 제15권1호통권61호
• /
• pp.38-40
• /
• 2000

자동 요금 징수 시스템인 ETC(Electronic Toll Collection) 시스템에서 차량의 탑재장치와 비컨(Beacon) 간에 마이크로파가 전파되는 경로를 모델화하였으며 다중 경로에 따른 페이딩 효과를 분석하였다. 또한 환경 변화 즉 강우 시 마이크로파 전파도 고려하여 수치분석을 하였다. 분석결과 강우에 의한 반사면의 반사계수가 변하여 페이딩 효과가 크게 증가하였다. 이런 수치해석 결과를 탑재장치에서 수신된 전압의 크기와 비컨과 차량 사이의 거리로 도시하였다.

• 한국정보전자통신기술학회논문지
• /
• 제2권2호
• /
• pp.63-68
• /
• 2009

We study on the transient response in non-uniform microstrip lines with optically controlled microwave pulses. The transient response of the microwave pulses in plasma layer has been evaluated by reflection function of dielectric microstrip lines. The variation of characteristic response in plasma layer with localized pulses has been evaluated analytically. Reflection the change of the reflection amplitude has been observed.

• Smart Structures and Systems
• /
• 제6권7호
• /
• pp.867-887
• /
• 2010

An energy-based variational approach is used for structural dynamic modeling of the IPMC (Ionic Polymer Metal Composites) flapping wing. Dynamic characteristics of the wing are analyzed using numerical simulations. Starting with the initial design, critical parameters which have influence on the performance of the wing are identified through parametric studies. An optimization study is performed to obtain improved flapping actuation of the IPMC wing. It is shown that the optimization algorithm leads to a flapping wing with dimensions similar to the dragonfly Aeshna Multicolor wing. An unsteady aerodynamic model based on modified strip theory is used to obtain the aerodynamic forces. It is found that the IPMC wing generates sufficient lift to support its own weight and carry a small payload. It is therefore a potential candidate for flapping wing of micro air vehicles.