• 제목/요약/키워드: Transient characteristics

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Mixde-mode simulation을 이용한 4H-SiC DMOSFETs의 계면상태에서 포획된 전하에 따른 transient 특성 분석 (Mixed-mode simulation of transient characteristics of 4H-SiC DMOSFETs - Impact off the interface changes)

  • 강민석;최창용;방욱;김상철;김남균;구상모
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2009년도 추계학술대회 논문집
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    • pp.55-55
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    • 2009
  • Silicon Carbide (SiC) is a material with a wide bandgap (3.26eV), a high critical electric field (~2.3MV/cm), a and a high bulk electron mobility (${\sim}900cm^2/Vs$). These electronic properties allow high breakdown voltage, high frequency, and high temperature operation compared to Silicon devices. Although various SiC DMOSFET structures have been reported so far for optimizing performances. the effect of channel dimension on the switching performance of SiC DMOSFETs has not been extensively examined. In this paper, we report the effect of the interface states ($Q_s$) on the transient characteristics of SiC DMOSFETs. The key design parameters for SiC DMOSFETs have been optimized and a physics-based two-dimensional (2-D) mixed device and circuit simulator by Silvaco Inc. has been used to understand the relationship with the switching characteristics. To investigate transient characteristic of the device, mixed-mode simulation has been performed, where the solution of the basic transport equations for the 2-D device structures is directly embedded into the solution procedure for the circuit equations. The result is a low-loss transient characteristic at low $Q_s$. Based on the simulation results, the DMOSFETs exhibit the turn-on time of 10ns at short channel and 9ns at without the interface charges. By reducing $SiO_2/SiC$ interface charge, power losses and switching time also decreases, primarily due to the lowered channel mobilities. As high density interface states can result in increased carrier trapping, or recombination centers or scattering sites. Therefore, the quality of $SiO_2/SiC$ interfaces is important for both static and transient properties of SiC MOSFET devices.

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A-Si 박막의 반사율변화에 따른 열전달계수 결정 (DETERMINATION OF THERMAL CONDUCTIVITY FROM TRANSIENT REFLECTIVITY MEASUREMENTS OF AMOPHOUS SILICON THIN FILMS)

  • 류지형;김향정;문승재
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2453-2458
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    • 2007
  • The performance of polysilicon thin film transistor (p-Si TFT) has an important role in the operation of active matrix liquid crystal displays. To fabricate the p-Si TFTs that have uniform characteristics, understanding of the recrystallization mechanism of silicon is crucial. Especially, the analysis of the transient temperature variation and the liquid-solid interface motion is required to find the mechanism. The thermal conductivity is one of the most important parameters to understand the mechanism. In this work, a KrF eximer laser beam was irradiated to amorphous silicon thin films. We measured the transient reflectivity at the wavelength of 633 nm. We carried out the numerical simulation of one dimension conduction equation so that we determined the most well-fitted thermal conductivity by comparing the numerically obtained transient reflectivity with the experimentally measured one. The experimentally determined thermal conductivity of amorphous silicon thin films is 1.5 W/mK.

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위성 추진시스템의 추력제어밸브 작동에 따른 추진제 비정상 유동 특성 (Transient Flow Behavior of Propellant with Actuation of Thrust Control Valve in Satellite Propulsion System)

  • 김정수;한조영;최진철
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.294-298
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    • 2001
  • Satellite propulsion system is employed for orbit transfer, orbit correction, and attitude control. The monopropellant feeding system in the low-earth-orbit satellite blowdowns fuel to the thrust chamber. The thrust produced by the thruster depends on fuel amount flowed into the combustion chamber. If the thruster valve be given on-off signal from on-board commander in the satellite, valve will be opened or closed. When the thrusters fire fuel flows through opened thruster valve. Instantaneous stoppage of flow in according to valve actuation produces transient pressure due to pressure wave. This paper describes transient pressure predictions of the KOMPSAT2 propulsion system resulting from latching valve and thrust control valve operations. The time-dependent set of the fluid mass and momentum equations are calculated by Method of Characteristics (MOC).

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광-마이크로파 기반 유도플라즈마의 과도응답 특성에 관한 연구 (Study of Transient Response in Non-uniform Plasma Layer with Optically-Controlled Microwave Pulses)

  • 왕설;최유순;박종구;김용갑
    • 전기학회논문지
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    • 제58권6호
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    • pp.1174-1179
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    • 2009
  • In this paper we develop the characteristic of density on non-uniform plasma in different layer of the semiconductor with optically controlled microwave pulses. The transient response of the microwave pulses in different plasma layer has been evaluated by calculating the variation of the reflection function of dielectric microstrip lines. The lines has used under open-ended termination containing optically induced plasma region, which has illuminated a laser source. The characteristics impedances resulting from the presence of plasma are evaluated by the transmission line model. The analyzes the variation of transient response in a 0.01cm layer near the surface for frequency range from 1GHz to 128GHz. The diffusion length LD is larger than compared to the absorption depth $l/_{\alpha}l$. The variation of characteristic response in plasma layer with microwave pulses which has in deferentially localized has been evaluated analytically.

압력섭동에 따른 비정상 화염편 응답특성 해석 (Flamelet Analysis for Transient Response to Pressure Oscillations)

  • 배준경;김용모;김성구
    • 한국연소학회지
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    • 제16권1호
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    • pp.30-35
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    • 2011
  • This study has been mainly motivated to numerically investigate the transient flame response to pressure oscillations in the gaseous hydrogen - liquid oxygen flames at supercritical pressures. The present analysis is based on the real-fluid transient flamlet model and the flame field is acoustically perturbed only by the sinewave oscillations in the frequency range from 1,000 Hz to 5,000 Hz. Based on numerical results, the detailed discussions are made for the flame response characteristics and the transient flamelet response associated with the high-frequency combustion instability in the liquid propellant rocket engines.

직교이방성 속빈 원통에서 과도적 흡습열 응력에 관한 연구 (A Study on the Transient Hygrothermal Stresses in an Orthotropic Hollow Cylinder)

  • 조환기;신근용
    • 한국군사과학기술학회지
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    • 제2권1호
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    • pp.110-120
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    • 1999
  • 본 논문은 흡습환경에서 온도변화를 겪는 무한히 긴 속빈 실린더의 시간변화에 따른 흡습열 응력 변화에 관해서 연구한 것이다. 평면변형률 가정에 기초한 흡습열탄성론의 방정식이 열과 습기 사이의 연성효과를 고려하여 수립되었다. 시간경과에 따른 흡습열 응력을 구하기 위한 완전한 형태의 해가 연성분리기법과 변수분리방법을 이용하여 구하였으며, 온도와 습도 집중치의 분포를 포함한 수치적인 적용 예에 대한 결과를 분석하였다. 시간경과에 따른 흡습열 특성이 직교이방성 속빈원통벽에서 변위와 응력의 변화 및 분포에 미치는 영향을 함께 제시하였다.

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초전도 동기발전기의 댐퍼 과도상태 해석 (Analysis of Damper Transient in Superconducting Synghronous G)

  • 전연도;이형우;이주
    • 한국초전도저온공학회:학술대회논문집
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    • 한국초전도저온공학회 1999년도 제1회 학술대회논문집(KIASC 1st conference 99)
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    • pp.125-128
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    • 1999
  • This paper presents the 2-D analysis of damper transient in superconducting of damper transient in superconducting synchronous generator(SCG) using finite element method. Efficient 2-D analysis model which compensates the leakage flux is proposed for the savign of computation time and memory capacity required in 3-D finite element analysis. The characteristics of damper transient in SCG and the prime role of damper also have been evaluated.

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MEMS 설계를 위한 실리콘 산화막 특성 (The Characteristics of Silicon Oxides for Microelectromechanic System)

  • 강창수
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2010년도 하계학술대회 논문집
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    • pp.371-371
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    • 2010
  • In this paper, the stress induced leakage currents of thin silicon oxides is investigated in the MEMS implementation with nano structure. The stress and transient currents associated with the on and off time of applied voltage were used to measure the distribution of high voltage stress induced traps in thin silicon oxide films. The oxide current for the thickness dependence of stress current, transient current, and stress induced leakage currents has been measured in oxides with thicknesses between $41{\AA}$, which have the gate area $10^{-3}cm^2$. The stress current, transient current is used to estimate to fundamental limitations on oxide thicknesses.

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HVDC 송전망이 대형발전단지의 과도안정도에 미치는 영향 분석 (Analysis of Effect of HVDC Transmission System on the Transient Stability)

  • 전혁모;전영환
    • 전기학회논문지
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    • 제65권1호
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    • pp.1-8
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    • 2016
  • The characteristics of Korean power systems are large capacity of generation sites and concentrated load in Seoul metropolitan area. According to the national generation facility plan, more generation facilities are needed to be constructed as the electrical demands are forecasted to increase. Moreover, the size of generation sites are expected to increase, too. Therefore transient stability problems become worse and worse. Recently, the necessity of HVDC has been raised to overcome the difficulty of constructing HVAC transmission lines. This paper shows the analysis of transient stability when HVDC transmission system is added to the power system consisting of large generation sites.

보존적 중첩격자기법을 이용한 동적 플랩의 천이적 공력거동에 관한 수치적 연구 (Numerical Study on Transient Aerodynamics of Moving Flap Using Conservative Chimera Grid Method)

  • 최성욱;장근식;김인선
    • 한국전산유체공학회지
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    • 제5권2호
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    • pp.9-19
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    • 2000
  • Transient aerodynamic response of an airfoil to a moving plane-flap is numerically investigated using the two-dimensional Euler equations with conservative Chimera grid method. A body moving relative to a stationary grid is treated by an overset grid bounded by a 'Dynamic Domain Dividing Line' which has an advantage for constructing a well-defined hole-cutting boundary. A conservative Chimera grid method with the dynamic domain-dividing line technique is applied and validated by solving the flowfield around a circular cylinder moving supersonic speed. The unsteady and transient characteristics of the flow solver are also examined by computations of an oscillating airfoil and a ramp pitching airfoil respectively. The transient aerodynamic behavior of an airfoil with a moving plane-flap is analyzed for various flow conditions such as deflecting rate of flap and free stream Mach number.

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