• Title/Summary/Keyword: 전기체

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All-solid-state electrochromic devices on flexible substrate (Flexible 기판 위의 전고상 전기변색 소자 제작)

  • 나윤채;심희상;조인화;성영은
    • Proceedings of the Materials Research Society of Korea Conference
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    • 2003.11a
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    • pp.129-129
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    • 2003
  • 전기변색(electrochromism)은 전기화학적 산화, 환원 과정을 통해 가역적인 광학특성의 변화를 갖는 현상을 말하며, 이를 이용한 전기변색소자(electrochromic device)는 전력 소모가 적고 변색효율이 크다는 장점으로 인해 smart window, display, mirror 등에 응용될 수 있다. 전기변색소자는 구조상 투명 기판, 투명 전도체, 환원 착색 물질 (cathodic coloration material), 산화 착색 물질(anodic coloration material), 그리고 투명 이온 전도체로 구성된다. 일반적으로 투명 기판으로는 열적 안정성이 좋은 유리기판을 사용하여 window에 응용할 수 있는 장점이 있는 반면 다양한 형태를 갖는 소자를 제작하기에는 그 한계가 있다.

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Analysis on Reactions of Full-Scale Airframe Static Structural Test (항공기 전기체 정적구조시험의 반력 분석)

  • Shim, Jae-yeul
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.3
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    • pp.195-205
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    • 2020
  • This study addresses analysis on reactions which are induced in restraint system for airframe full-scale static structural test. This system restraints 6 degrees of freedom of a test article. It is valuable to study evaluating test error through analysis on the reactions which include all errors in a test. It is required to calculate fistly right reactions for the evaluation. This study focuses on calculation of the right reactions. The reaction is represented by sum of nominal reaction(Rn) and testing error reactions(Rce, Rerr) and is analyzed by two steps (inital vs relative reaction) in this study. It would evaluate intrinsic error at 0%DLL and error induced from applying test load, separately. Based on analysis using test data of a full-scale static test(canard type aircraft), resultant force of Rces and Rce_rs are distributed within 82.8N while resultant force of Rerr_rs shows to increase upto max. 808N as load level increment. Such well distribution of the Rce within the small range is caused from TMF values characteristics which are well distributed within -30N~40N. Additionally, it is shown through qualitative analysis on three components(X0, Y0, Z0) of the relative reaction(Rerr_r) that the reactions must be calculated with considering deformation of test article to calculate correctly reactions. This study shows also that equations characterizing deformation of components of test article are required to calculate the correct reactions, the equations must include information which will be used to calculate movement of all loading points.

The analysis of E-field produced by satellite S-band under fairing of launcher (인공위성 S-band가 형성한 발사체 패어링내의 전기장 해석)

  • Kim, Eui-Chan;Lee, Sang-Kon
    • Aerospace Engineering and Technology
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    • v.10 no.2
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    • pp.82-86
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    • 2011
  • This paper presents an RF Electric field assessment at 2.290 [GHz] inside launcher PROTON M/Breeze M long fairings, produced by COMS TM. COMS intentional RE due to TM ON under fairing has been assessed considering PROTON M / BREEZE M fairing characteristics. As fairings of all launchers present similar sizes, a similar E-field level under fairing is expected for the other launchers. As a result, the RE level under faring is compliant with COMS RS limits, but is not compliant with RS requirements of the launcher PROTON M/Breeze M.

Research of Synthetic Resonance Characteristics for Electrohydraulic Thrust Vector Control Actuation System (전기-유압식 추력벡터제어 구동장치시스템의 합성공진 특성 연구)

  • Min, Byeong-Joo;Choi, Hyung-Don;Kang, E-Sok
    • Aerospace Engineering and Technology
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    • v.7 no.1
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    • pp.151-160
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    • 2008
  • In this paper, the analysis results of synthetic resonance characteristics are described for the electrohydraulic thrust vector control actuation system. The synthetic resonance is induced by integration of position servo actuation system on the flexible launch vehicle mounting structure. The new resonance mode is synthesized due to composition of hydraulic resonance for electrohydraulic position servo system with inertia load condition and structural resonance for flexible mounting structure. This synthetic resonance can make stability of control system worse by feedback and amplification of control system. The exact nonlinear analysis model of this phenomenon is developed to predict and design a control algorithm for improvement characteristics. The DPF (Dynamic Pressure Feedback) control algorithm has been designed and has excellent resonance suppression capability.

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PDP용 Ag 전극과 유전체의 동시소결

  • Kim, Jeong-Hun;Sin, Hyo-Sun;Yeo, Dong-Hun;Hong, Yeon-U;Yun, Ho-Gyu
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2009.11a
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    • pp.200-200
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    • 2009
  • 상용의 디스플레이로 널리 사용되고 있는 PDP(Plasma Display Panel)는 LCD와의 시장 경쟁으로 인하여 극한의 원가 경쟁 하에 있다. 따라서 각 공정에 대한 공정단가를 낮추기 위한 다양한 공정 및 소재 연구가 진행되고 있다. 그 가운데 하나가 Address와 Bus 전극으로 사용되고 있는 Ag 전극의 저온 소결이다. 이 공정은 저온소결 소재의 개발과 전극에 접촉하는 유전체 층과 matching이 중요하기 때문에 이들 소재의 동시 개발이 필요한 실정이다. 본 연구에서는 Ag 전극의 저온 소성을 위한 다양한 가능성을 검토하였다. 또한, 유전체와 동시 소결 가능한 소재의 특성 향상 및 저온 소성 연구를 동시에 수행하였다. Glass에 대한 유전체 층의 인쇄와 유전체 위에 전극 입자의 크기제어를 통한 기본 조성의 matching 특성을 비교하고 입자 크기가 전극의 소결 온도에 미치는 영향을 비교 평가 하였다. 유전체 층과의 matching 특성을 향상하기 위하여 유전체 조성의 일부를 전극에 첨가하여 두 소재간의 결합력을 증대시키기 위한 실험을 진행하였다. 그 결과를 바탕으로 저온 동시소성이 가능한 전극 소재의 최적화 실험을 실시하고 그 결과 최적의 전극 소재를 제시하였다.

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Grid Sensor Network for Vehicle Location Awareness in the Airport (공항 내 이동체 위치 인식을 위한 그리드 센서 네트워크)

  • Ryu, Won-Sang;Yang, Jung-Kyu;Roh, Hyoung-Hwan;Seo, Ki-Won;Kim, Jong-Cheol;Jeong, Myoung-Sub;Park, Jun-Seok;Oh, Ha-Ryoung;Seong, Yeong-Rak
    • Proceedings of the KIEE Conference
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    • 2008.07a
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    • pp.1418-1419
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    • 2008
  • 본 논문에서는 그리드 센서 네트워크를 이용한 공항 내 이동체 위치 인식 방법을 제안한다. 그리드 센서 네트워크는 공항에 격자형으로 다수의 센서를 설치하여 이동체의 위치를 인식하는 방법이다. 격자 형태로 설치된 센서들은 이동체에 부착된 센서로부터 이동체 식별정보 및 위치 측정에 필요한 정보를 수신하고 중앙 서버로 전송한다. 중앙 서버에서는 수집된 정보들을 이용하여 이동체들의 위치를 계산하고 추적하게 된다. 본 논문에서는 현재 공항 내 이동체 위치 인식과 관련된 몇 가지 기술들에 대하여 살펴보고, 제안하고자 하는 그리드 센서 네트워크를 이용한 위치 인식 방법에 대하여 살펴본다.

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Effect of Dynamic Electric Fields on Dielectric Reliability in Cu Damascene Interconnects (동적인 전기장이 다마신 구리 배선에서의 절연파괴에 미치는 영향)

  • Yeon, Han-Wool;Song, Jun-Young;Lim, Seung-Min;Bae, Jang-Yong;Hwang, Yuchul;Joo, Young-Chang
    • Journal of the Microelectronics and Packaging Society
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    • v.21 no.4
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    • pp.111-115
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    • 2014
  • Effect of dynamic electric fields on dielectric breakdown behavior in Cu damascene interconnects was investigated. Among the DC, unipolar, and bipolar pulse conditions, the longest dielectric lifetime is observed under the bipolar condition because backward Cu ion drift occurs when the direction of electric field is changed by 180 degrees and Cu contamination is prohibited as a results. Under the unipolar pulse condition, the dielectric lifetime increases as pulse frequency increases and it exceed the lifetime under DC condition. It suggests that the intrinsic breakdown of dielectrics significantly affect the dielectric breakdown in addition to Cu contamination. As the unipolar pulse width decreases, dielectric bond breakdown is more difficult to occur.

Comparison of Heating Characteristics of Electric Heating Element Heater and Oil Hot Air Heater in Single Span Greenhouses (전기발열체 난방기 및 유류온풍 난방기의 단동온실 난방 특성 비교)

  • Kwon, Jin Kyung;Kim, Seung Hee;Shin, Young An;Lee, Jae Han;Park, Kyeong Sub;Kang, Youn Koo
    • Journal of Bio-Environment Control
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    • v.26 no.4
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    • pp.324-332
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    • 2017
  • The comparative experiments were conducted for single span greenhouses where cucumbers were cultivated to analyze the effect of heating between a carbon fiber electric heating element heater and an oil hot air heater in terms of the inside climate, energy consumption and plant growth. In order to analyze the effect of heating capacity, 6, 9, and 16 kW of electric powers were supplied to the electric heating element for same setting temperature of 15?. As a result, as the heating capacity increased, the number of ON-OFF cycles of the electric heating element and the temperature inside the greenhouse increased proportionally. In the comparison of two heaters, it was shown that the temperature and relative humidity distributions of the electric heating element installed greenhouse was much uniform than those of the oil hot air heater installed greenhouse. The heating energy consumptions during the heating period of 79 days were 867L for the oil hot air heater and 8,959 kWh for the electric heating element heater, and the heating costs were 607 and 403 thousand won respectively. In the electric heating element installed greenhouse, the cucumber growth was slightly better and the yield was 4.3% higher than those of the oil hot air heater installed greenhouse, but there were no statically significant difference in the cucumber growth and yield between greenhouses.

Characteristic Research of Electromechanical Actuation System for Launch Vehicle Thrust Vector Control (발사체 추력벡터제어용 전기-기계식 구동장치시스템 특성 연구)

  • Min, Byeong-Joo;Choi, Hyung-Don;Kang, E-Sok
    • Aerospace Engineering and Technology
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    • v.6 no.2
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    • pp.164-170
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    • 2007
  • In this paper, the development results of electromechanical TVC actuation system is described in the aspect of design, analysis, manufacturing and test. The kinds of prime power for TVC actuation system is classified by the variety of propulsion system of launch vehicle. The electric power by battery is the sole candidate for prime power of TVC actuation system at the view point of feasible domestic infra technologies for the present. The characteristic analysis study is performed between electromechanical and electrohydraulic actuation system with respect to power efficiency, performance and weight efficiency. The electromechanical actuation system has superiority of power and weight efficiency according to less opportunity of power conversion process.

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