• 제목/요약/키워드: planar type

검색결과 552건 처리시간 0.029초

모노폴 쌍으로 구성된 U자형 평면 UWB 안테나 설계 (Design of a U-Type Planar UWB Antenna Composed of Monopole Pair)

  • 이호상;장재삼;정영호;김철복;김재훈;박승배;이문수
    • 대한전자공학회논문지TC
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    • 제45권9호
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    • pp.60-66
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    • 2008
  • 본 논문에서는 UWB(Ultra-wideband) 통신시스템용 CPW(Coplanar Waveguide) 급전 구조의 안테나를 설계 및 제작한다. 초광대역 특성을 구현하기 위하여 두개의 평면형 모노폴 안테나의 상호결합을 이용한다. 안타나의 파라미터(평면형 모노폴의 폭과 두 모노폴 간의 간격) 조정을 통한 모노폴 쌍의 상호결합을 최적화하여 초 광대역 특성을 갖도록 한다. 그리고, 모노폴 쌍 안테나의 상호결합 효과를 확인하기 위해 모노폴 방사소자 사이의 수평부분 길이를 조정한 2개의 UWB 안테나를 제작하여 측정한다. 측정결과, 2개의 안테나 모두 UWB 전대역$(3.1\sim10.6GHz)$뿐 아니라 훨씬 넓은 주파수 대역에서 양호한 결과를 보인다.

Planar-Jet형 연소기 내 난류유동의 LES (Large-Eddy Simulation of Turbulent Flows in a Planar Combustor)

  • 김도형;양경수;신동신
    • 대한기계학회논문집B
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    • 제24권10호
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    • pp.1409-1416
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    • 2000
  • In this study, turbulent flows in a planar combustor which has a square rib-type flame holder are numerically investigated by Large Eddy Simulation(LES). Firstly, the flow fields with or without jet injection downstream of the flame-holder are examined using uniform inlet velocity. Comparison of the present LES results with experimental one shows a good agreement. Secondly, to investigate mixing of oxidizer(air) and fuel injected behind the flame holder, the scalar-transport equation is introduced and solved. From the instantaneous flow and scalar fields, complex and intense mixing phenomena between fuel and jet are observed. It is shown that the ratio of jet to blocked air velocity is an important factor to determine the flow structure. Especially, when the ratio is large enough, the fuel jet penetrates the main vortices shed from the flame holder, resulting in significant changes in the flow and scalar fields.

결합 선로를 이용한 평판 구조의 Marchand 발룬의 합성 (Synthesis of Marchand Balun Using Planar Coupled-Line)

  • 이종환;염경환
    • 한국전자파학회논문지
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    • 제16권2호
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    • pp.161-166
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    • 2005
  • 평판형 결합 선로를 이용한 Marchand 발룬의 합성 기법을 제시하였다. 이러한 형태의 발룬이 갖추어야할 설계 조건에 대해서 살펴보고, 설계 조건에 부합하는 발룬의 합성을 전송선 등가회로를 통해 간편하게 모델링 할 수 있음을 보였다. 합성된 발룬은 equi-ripple 대역 통과 특성을 나타내고, 일반적 인 평판 구조에서 구현하기 어려운 평형 선로 없이도 크기가 같고 위상이 반대인 평형 신호를 얻을 수 있다. 결합 선로를 이용한 Marchand 발룬의 구현에 많이 사용되는 다중 결합 선로의 물리적 구조와 발룬의 합성에 필요한 요소값들 사이의 관계를 해석하는 방법도 소개하였다. 이상의 방법들을 이용하면 평판 구조의 다중 결합 선로를 갖는 Marchand 발룬의 체계적인 설계가 가능하다.

22.9kV급 지중전력케이블의 부분방전 측정을 위한 평면루프센서 설계 및 제작 연구 (A Study on the Design and Fabrication for Partial Discharge Measurment in 22.9kV Underground Power Cable using Planar Loop Sensor)

  • 신동훈;임광진;;박노준;박대희
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2007년도 추계학술대회 논문집
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    • pp.210-211
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    • 2007
  • The objective of this paper is to effectively detect partial discharges in underground power cables. In this field, we have been usually applied several sensors for such partial discharges. This study used a type of beyond compare antenna based on the influence of background noises. Also, we designed a new structure that is able to easily apply in the adhesion of planar loop types for underground power cables in measurement sensitiveness elevation. A high frequency simulation tool (CST-MWS) was applied to the antenna used in this study, and it was used to evaluate certain characteristics. We fabricated an antenna using the simulation data obtained from a specific test. After checking the sensitivity of this Planar Loop Sensor in the Lab, it was tested in an actual site. This paper analyzed the data as a part of time and frequency domain using an oscilloscope and spectrum analyzer, respectively.

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평면형 MMIC 공진기를 이용한 낮은 위상잡음을 갖는 X 대역 MMIC 발진기 (An X-band Low Phase Noise MMIC Oscillator Using a Planar-Type MMIC Resonator)

  • 이문규;조일현;최종원
    • 한국ITS학회 논문지
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    • 제6권1호
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    • pp.38-46
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    • 2007
  • 본 논문에서는 평면형 MMIC 공진기를 이용하여 X대역에서 동작하는 낮은 위상잡음 특성의 HBT 발진기를 설계하였다. 제안한 공진기는 기존의 분포소자를 이용한 헤어핀 공진기 면적의 1/4 수준으로 크기를 소형화를 하였다. 발진기의 측정결과 발진주파수는 8.295 GHz, 출력전력은 4.8 dBm, 위상잡음은 100 kHz 옵셋 주파수에서 -106.8 dBc/Hz와 1 MHz 옵셋 주파수에서 -121.7 dBc/Hz를 보였다.

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평판형 유전체 장벽 방전 반응기에서 Acetonitrile의 분해 특성 (Decomposition of Acetonitrile by Planar Type Dielectric Barrier Discharge Reactor)

  • 송영훈;김관태;류삼곤;이해완
    • 한국군사과학기술학회지
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    • 제5권3호
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    • pp.105-112
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    • 2002
  • A combined process of non-thermal plasma and catalytic techniques has been investigated to treat toxic gas compounds in air. The treated gas in the present study is $CH_3$CN that has been known to be a simulant of toxic chemical agent. A planar type dielectric barrier discharge(DBD) reactor has been used to generate non-thermal plasma that produces various chemically active species, O, N, OH, $O_3$, ion, electrons, etc. Several different types of adsorbents and catalysts, which are MS 5A, MS 13X, Pt/alumina, are packed into the plasma reactor, and have been tested to save power consumption and to treat by-products. Various aspects of the present techniques, which are decomposition efficiencies along with the power consumption, by-product analysis, reaction pathways modified by the adsorbents and catalysts, have been discussed in the present study.

채널 구조에 따른 1T-DRAM Cell의 메모리 특성 (Memory Characteristics of 1T-DRAM Cell by Channel Structure)

  • 장기현;정승민;박진권;조원주
    • 한국전기전자재료학회논문지
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    • 제25권2호
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    • pp.96-99
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    • 2012
  • We fabricated fully depleted (FD) SOI-based 1T-DRAM cells with planar channel or recessed channel and the electrical characteristics were investigated. In particular, the dependence of memory operating mode on the channel structure of 1T-DRAM cells was evaluated. As a result, the gate induced drain leakage current (GIDL) mode showed a better memory property for planar type 1T-DRAM. On the other hand, the impact ionization (II) mode is more effective for recessed type.

평면형 마이크로 가스센서 (Planar-Type Micro Gas Sensor)

  • 이상윤;정완영;이덕동
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 1998년도 추계학술대회 논문집
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    • pp.101-104
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    • 1998
  • A new planar-type micro gas sensor was designed and fabricated on silicon substrate and the operating characteristics of the sensor were investigated. The thin sensitive film of the sensor was fabricated by spin-coating of the SnO$_2$ sol solution which was synthesized by hydrothermal method. The spin-coating method for preparation of sensing layer was adopted to improve the long-term stability of the fabricated sensing film instead of physical methods such as rf sputtering and thermal evaporation. The fabricated microsensor showed a fairly good sensing performance for CO gas in air at 250$^{\circ}C$ The sensitivity(S=Ra/Rg) was shown to be about 5 to 2000ppm CO with heating power of 50mW.

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적층형 Crescent-Shaped Input Type 원형 압전변압기의 특성 (A Study on the Characteristics of Circular Piezoelectric Transformner which has Multi-layered Crescent-Shaped Input Electrode)

  • 정성수;박태곤
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2006년도 추계학술대회 논문집 Vol.19
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    • pp.223-224
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    • 2006
  • This paper present a new disk-type piezoelectric transformer. The input side of the transformer has a crescent-shaped electrode and the output side has a focused poling direction. This transformer has multi-layered structure. The piezoelectric transformers operated m each transformer's resonance vibration mode. The electrodes and poling directions on commercialy available piezoelectric ceramic disks were designed so that the planar or shear mode coupling factor ($k_p,\;k_{15}$) becomes effective rather than the transverse mode coupling factor ($k_{31}$). The Resonance frequency is 65.22[kHz] and maximum voltage step-up ratio is 149. Multi-layered transformer has better efficiency and step-up ratio than the single-layered transformer.

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MEMS 공정을 이용한 마이크로 액체 추력기 배열체 제작 (Fabrication of a liquid microthruster array by MEMS manufacturing process)

  • 허정무;권세진
    • 항공우주시스템공학회지
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    • 제9권2호
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    • pp.13-18
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    • 2015
  • Micro planar type liquid propellant thruster was fabricated by MEMS manufacturing process for micro/nano satellites applications. 90 wt.% hydrogen peroxide was used as propellant and for propellant decomposition, Pt/Al2O3 was used as catalyst. Micro thruster structure was made by 5 photosensitive glasses patterned with thruster component profiles. Objective thrust was 50 mN and required hydrogen peroxide mass flow was 2.1 ml/min, which was supplied by syringe pump and teflon tube in experimental test. Performance test said that average steady thrust was approximately 30 mN, around 60% of objective thrust, and transient time was about 5 sec. It is estimated that extended response time was due to high thermal energy loss of micro scale thruster and low enthalpy input by propellant mass flow.