• Title/Summary/Keyword: 전압불안정성

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Performance of Zn-based oxide thin film transistors with buried layers grown by atomic layer deposition

  • An, Cheol-Hyeon;Lee, Sang-Ryeol;Jo, Hyeong-Gyun
    • Proceedings of the Materials Research Society of Korea Conference
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    • 2012.05a
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    • pp.77.1-77.1
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    • 2012
  • Zn 기반 산화물 반도체는 기존의 비정질 Si에 비해 저온공정에도 불구하고 높은 이동도, 투명하다는 장점으로 인해 차세대 디스플레이용 백플레인 소자로 주목받고 있다. 산화물 트랜지스터는 우수한 소자특성을 보여주고 있지만, 온도, 빛, 그리고 게이트 바이어스 스트레스에 의한 문턱전압의 불안정성이 문제의 문제를 해결해야한다. 산화물 반도체의 문턱전압의 불안정성은 유전체와 채널층의 계면 혹은 채널에서의 charge trap, photo-generated carrier, ads-/desorption of molecular 등의 원인으로 보고되고 있어, 고신뢰성의 산화물 채널층을 성장하기 위한 노력이 이루어지고 있다. 최근, 산화물 트랜지스터의 다양한 조건에서의 문턱전압의 불안정성을 해결하기 위해 산화물의 주된 결함으로 일컬어지고 있는 산소결핍을 억제하기 위해 성장공정의 제어 그리고, 산소와의 높은 binding energy를 같은 Al, Hf, Si 등과 같은 원소를 첨가하여 향상된 소자의 특성이 보고되고 있지만, 줄어든 산소공공으로 인해 이동도가 저하되는 문제점이 야기되고 있다. 이러한 문제점을 해결하기 위해, 최근에는 Buried layer의 삽입 혹은 bi-channel 등과 같은 방안들이 제안되고 있다. 본 연구는 atomic layer deposition을 이용하여 AZO bureid layer가 적용된 ZnO 트랜지스터의 특성과 안정성에 대한 연구를 하였다. 다결정 ZnO 채널은 유전체와의 계면에 많은 interface trap density로 인해 positive gate bias stress에 의한 문턱전압의 불안정성을 보였지만, AZO층이 적용된 ZnO 트랜지스터는 줄어든 interface trap density로 인해 향산된 stability를 보였다.

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Dynamics Transition of Electroconvective Instability Depending on Confinement Effect (공간 제약 효과에 따른 전기와류 불안정성의 동역학 전이)

  • Lee, Seungha;Hyun, Cheol Heon;Lee, Hyomin
    • Korean Chemical Engineering Research
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    • v.59 no.4
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    • pp.626-631
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    • 2021
  • One of the nonlinear electrokinetic phenomena around ion exchange membrane is electroconvective instability which can be found in various electrokinetic applications such as electrodialysis, electrochemical battery, microfluidic analysis platform, etc. Such instability acts as a positive transport mechanism for the electrodialysis via amplifying mass transport rate. On the other hands, in the electrochemical battery and the microfluidic applications, the instability provokes unwanted mass transport. In this research, to control the electroconvective instability, the onset of the instability was analyzed as a function of confinement effect as well as applied voltage. As a result, we figured out that the dynamic behavior of electroconvective instability transited as a sequence of stable regime - static regime - chaotic regime depending on the applied voltage and confinement effect. Furthermore, stability curves about the dynamic transition were numerically determined as well. Conclusively, the confinement effect on electroconvective instability can be applied for effective means to control the electrokinetic chaos.

Various Considerations in Designing Stable Electrooptic Voltage and Magnetooptic Current Sensors (결정형 光전압/전류센서의 高안정성을 위한 고찰)

  • 이경식
    • Proceedings of the Optical Society of Korea Conference
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    • 1991.07a
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    • pp.103-108
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    • 1991
  • 결정형 光 전압/전류 센서에 있어서 내부다중반사(Multiple internal Reflection), 북굴절 및 물성의 온도의존성이 어떻게 불안정성 요인으로 작용할 수 있는지를 알아보았으며, 이들 요인들을 피해서 센서의 안정성을 높힐 수 있는 방법들을 소개하였다. 구성된 光 전압/전류센서의 간단한 동작도 보았다.

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Effects of thin-film thickness on device instability of amorphous InGaZnO junctionless transistors (박막의 두께가 비정질 InGaZnO 무접합 트랜지스터의 소자 불안정성에 미치는 영향)

  • Jeon, Jong Seok;Jo, Seong Ho;Choi, Hye Ji;Park, Jong Tae
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.21 no.9
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    • pp.1627-1634
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    • 2017
  • In this work, a junctionless transistor with different film thickness of amorphous InGaZnO has been fabricated and it's instability has been analyzed with different film thickness under positive and negative gate stress as well as light illumination. It was found that the threshold voltage shift and the variation of drain current have been increased with decrease of film thickness under the condition of gate stress and light illumination. The reasons for the observed results have been explained by stretched-exponential model and device simulation. Due to the reduced carrier trapping time with decrease of film thickness, electrons and holes can be activated easily. Due to the increase of vertical channel electric field reaching the back interface with decrease of film thickness, more electrons and holes can be accumulated in back interface. When one decides the film thickness for the fabrication of junctionless transistor, the more significant device instability with decrease of film thickness should be consdered.

Electroconvective Instability on Undulated Ion-selective Surface (파상형 이온 선택 표면상의 전기와류 불안정성)

  • Lee, Hyomin
    • Korean Chemical Engineering Research
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    • v.57 no.5
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    • pp.735-742
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    • 2019
  • In this work, the electrokinetic interactions between the undulated structure of an ion-selective membrane and electroconvective instability has been studied using numerical analysis. Using finite element method, electric field-ionic species transport-flow field were analyzed by fully-coupled manner. Through the numerical study, the Dukhin's mode as the mechanism of undulated surface for the electroconvective instability were proven. The Dukhin's mode which competes with Rubinstein's mode has roles of (i) decreasing transition voltage to overlimiting regime and (ii) non-linearly increasing of overlimiting current. Also, (iii) the mixing efficiency is enhanced by removal mechanism of high-frequency Fourier mode of the electroconvective instability. Conclusively, the undulated ion-selective surface would provide energy-efficient mechanism for ion-selective transport systems such as electrodialysis, electrochemical battery, etc.

Experimental Observation of Instability of Supersonic Submerged Jets (수중초음속제트의 불안정성에 대한 실험적 고찰)

  • 정재권;이대훈;차홍석;박승오;권세진
    • Journal of the Korean Society of Propulsion Engineers
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    • v.6 no.2
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    • pp.45-52
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    • 2002
  • An experimental investigation on the structure and dynamic behavior of two dimensional over-expanded air jets exiting into water was carried out. The hish speed digital video imaging and static pressure distribution measurement were made to characterize the structure and time-dependant behavior of the jets. Mach number at the jet exit was 2.0 and was slightly less than the value predicted by the ideal nozzle calculation. Variance of jet spreading angle at different stagnation condition was measured as a function of mass flow rate. Periodic nature of the air jet distortion in water was observed and the frequency of the repetition was approximately 5-6 Hz for all cases tested. Three characteristic length scales were defined to characterize jet structure. $L_1$, maximum width of the plume when the periodic instability occurs, $L_2$, width of the jet where secondary reverse flow entrained jet flow and $L_3$, distance from the jet exit to the location where entrainment of the secondary reverse flow occurs. The ratio of $L_1$ and $L_2$ decreased with increasing stagnation pressure, i.e. mass flow rate. $L_3$ increased with increasing stagnation pressure. The temporal behavior of static pressure measurements also showed peak around frequency of 5, which corresponds the frequency obtained by visual measurements

Investment method of FACTS for improvement of stability for KEPCO System (안정도 향상을 위한 한전계통에서의 FACTS 투입 방안 모색)

  • Kang, Sang-Gyun;Lee, Byoung-Jun;Kwon, Sae-Hyuk;Song, Hwa-Chang;Yoon, Jong-Soo;Jang, Byung-Hoon
    • Proceedings of the KIEE Conference
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    • 2005.07a
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    • pp.208-210
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    • 2005
  • 본 논문에서는 전압 불안정성을 해소시키기 위한 방안으로 FACTS를 투입하기 위한 방안에 대하여 논의 하였다. 우선적으로 전압안정도 기준을 수립하고 상정사고에 대하여 PV 해석을 실시하고 전압안정도 기준을 만족시키지 못하는 사고를 스크리닝 한다. 각 상정 사고에 대하여 선정된 전압안정도 기준을 만족하도록 하기 위한 FACTS 투입 방안에 대하여 논의하였다. 일반적으로 전압안정도 측면에서 취약위치를 선정하는 방법으로 VQ해석이나 Tangent vector에 의한 Bus sensitivity를 구하여 부하변화에 대한 전압 감도(dV/$dP_{TOTAL}$)가 큰 모선을 취약 위치로 선정하는 방법, 또는 Modal Analysis를 통해 구한 참여인수값이 큰 모선을 취약 모선으로 선정하는 방법이 있다. 이 논문에서는 VQ해석과 Tangent vector를 이용한 해석 방법을 이용하여 전압안정도 측면에서 취약 위치 및 전압안정도 향상을 위한 FACTS 투입 후보지를 선정하였고 전압안정도 기준을 만족시키기 위해 각 후보지에 투입해야할 FACTS 용량을 산정하였다. 마지막으로 실질적으로 수도권 주요 모선에 모두 FACTS를 투입한 결과와 논문에서 사용한 방법과의 결과를 비교하여 적절한 절차를 사용하여 FACTS가 투입되었음을 확인하였다.

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Instability of Electric Characteristics in Hydrogenated Amorphous Carbon (수소화된 비정질 탄소박막에서 전기적 특성의 불안정성)

  • Kang, Sung Soo;Lee, Won Jin
    • Journal of Korean Ophthalmic Optics Society
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    • v.4 no.2
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    • pp.105-111
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    • 1999
  • This paper presents experimental results on the electrical properties of hydrogenated amorphous carbon films(a-C:H) prepared by PECVD. DC conductance of a-C:H was measured as a function of temperatures in the range of 100 to 423K. We studied two a-C:H films: one was well explained by the Mott's Variable Range Hopping(VRH) rule, but the other sample did not follow it. However, the conduction data of second sample were well fitted to Shimakawa's Multi-Phonon Hopping(MPH) model according to which conductivity is proportional to $T^M$ with m=15-17. but, in our samples, m was 10-12. Also a-C:H showed several bias effects like relaxation of conductance, bias-dependent conductance and the change of conductance slope in 1n(${\sigma}{\sqrt{T}}$) vs. $T^{1/4}$ plot. In this study we interpret these data by bias-dependent detrapping model.

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슬롯 각도에 따른 경계층 상호작용의 피동제어 성능 및 유동 구조 비교 연구

  • Lee, Hun-Sik;Lee, Jae-Hwan;Kim, Jong-In
    • Proceeding of EDISON Challenge
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    • 2016.11a
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    • pp.96-100
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    • 2016
  • 슬롯판을 이용한 경사충격파와 경계층 간섭유동 제어에서, 슬롯의 각도를 바꾸어 가며 제어 성능을 비교하는 수치적 연구가 수행되었다. 기준이 되는 수직 슬롯, 각도를 달리한 6개의 case를 선정하여 하여 충격파 뒤에서 전압손실 및 경계층 안정성을 기준으로 제어 성능을 평가하였다. 수치해석 결과 모든 형상에 대해 제어하지 않은 상태보다 좋은 성능을 얻었다. 공력성능이 뛰어난 그룹과 그렇지 않은 그룹을 구분하여 슬롯과 공동 유동 구조를 분석하면서 경계층 불안정성을 야기하고 전압손실 감소에 영향을 미치는 것은 경계층과 충격파가 상호작용하는 영역에서 Vortex를 얼마나 제어할 수 있는지 여부임을 알 수 있었고, 이러한 Vortex를 얼마나 제어할 수 있는지에 따라 공력 성능이 결정됨을 파악할 수 있었다.

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A Study on Subcritical Instability of Axisymmetric Supersonic inlet (축대칭 초음속 흡입구의 아임계 불안정성 연구)

  • Shin, Phil-Kwon;Park, Jong-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.8
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    • pp.29-36
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    • 2004
  • Supersonic inlet buzz can be defined as unstable subcritical operation associated with fluctuating internal pressures and a shock pattern oscillating about the inlet entrance. The flow pulsations could result in flameout in the combustor or even structural damage to the engine. An experimental study was conducted to investigate the phenomenon of supersonic inlet buzz on axisymmetric, external-compression inlet. An inlet model with a cowl lip diameter of 30mm was tested at a free stream Mach number of 2.0. Subcritical instability was investigated by considering the frequency of pressure pulsation and shock wave structure at the inlet entrance. The results obtained show that total pressure recovery ratios were varied from 0.42 to 0.78, and capture area ratio from 0.34 to 0.98. The frequency of the subcritical flow increased with decrease in capture area ratios. Frequency was measured at $224{\sim}240Hz$.