• Title/Summary/Keyword: Transient characteristics

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Modeling transient characteristics of NPT IGBT including trun-on condition (턴 온 상태를 고려한 NPT IGBT의 과도 특성 모델링)

  • Ryu, Se-Hwan;Lee, Yong-Kuk;Ahn, Hyoung-Keun;Han, Deuk-Young
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2003.07a
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    • pp.327-330
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    • 2003
  • In this work, current-voltage characteristics with time of NPT(Non-PunchThrough) IGBT is proposed during turn-on and turn-off by using analytical method. From the results, power loss at turn-off dominates the total electrical loss with respect to that at turn-on. The results have been compared with those of PSPICE and show the identical trend of power loss with each other.

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Characteristics of Vortex Shedding behind a Circular Cylinder with Serrated Fins (톱니형 핀이 부착된 튜브의 와유출특성 연구)

  • Bu, Jeong-Suk;Ryu, Byeong-Nam;Kim, Gyeong-Cheon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.8
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    • pp.1077-1086
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    • 2001
  • An experimental study is performed to investigate the characteristics of vortex shedding behind a circular cylinder with serrated fins using hot-wire anemometer. Strouhal numbers which are calculated using outer diameter of a circular cylinder with serrated fins are higher than that of a circular cylinder. Fin thickness and pitch are closely related with vortex shedding frequency and play increasing or decreasing vortex shedding after transient Reynolds number. Strouhal numbers using effective diameters which are proposed in this paper agree with that of a circular cylinder. After transient Reynolds number, a trend of Strouhal number can be estimated by checking the ratio of effective diameter to inner diameter.

A study on the transient characteristics in Single-phase Line-start Permanent Magnet (단상 유도동기 전동기(LSPM)의 과도 특성에 관한 연구)

  • Jung, Dae-Sung;Lee, Ju;Ree, Cheol-Jick
    • Proceedings of the KIEE Conference
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    • 2006.07b
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    • pp.631-632
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    • 2006
  • This paper is written by research for the transient characteristics of the Single-phase Line-start permanent Magnet. The Single-phase Line-start permanent Magnet is most likely to substitute for Single-phase Induction Motor which is used about many appliance currently, because that has good points. For example, It has a Line-start of ability and a High-efficiency. And it need not power convergence device. The rotor of The Single-phase Line-start permanent Magnet has cage-bar with permanent magnet. This motor is started by cage-bar. When it entered synchronous condition, the rotor is rotated by the permanent magnet. But the design of the permanent magnet is very important, because the breaking torque of the permanent magnet interrupt to start a rotor. Finally, if Flux Barrier is not concerned, we do not get result of our object. Therefore this thesis is concerned about Flux Barrier.

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Change of Insulation Properties of Stator Coil fed by Inverter Source on Traction Motor (인버터 전원에 의한 견인전동기 고정자 코일의 절연특성 변화)

  • Jang, Dong-Uk;Park, Hyun-June;Lee, Gil-Hun;Choi, Jong-Sun;Lee, Jung-Soo
    • Proceedings of the KIEE Conference
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    • 2003.04a
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    • pp.420-422
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    • 2003
  • Aging and failure of motor insulation depend on the stresses imposed on it. The insulation life time depends on the severity of the stresses. The electrical aging by transient surge is very important to traction motor in EMU(electric multiple unit). This paper Presents the insulation characteristics of stator coil by transient surge from inverter. There are several nondestructive tests available for checking the condition of motor insulation, the probable extent of aging,. and the rate of which aging is taking pace. So the insulation characteristics of stator coil were each analyzed by measurement of leakage current, dielectric loss($tan{\delta}$), capacitance, polarization index(PI) and partial discharge. The method of diagnosis is able to analyze the aging condition and Predict the life of the traction motor in EMU.

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Recognition of the Direct and Reflected Sounds in an Irregulary Formed Chamber (비정방형실내에서의 직접음과 반사음 식별에 관한 연구)

  • 차일환;박규태;임광호
    • The Journal of the Acoustical Society of Korea
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    • v.2 no.1
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    • pp.11-19
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    • 1983
  • An irregulary formed chamber was designed and constructed to recognize the direct sound radiated from the sound source and the reflected sound from the walls of the chamber. The sound signal used was tone burst in the frequency response characteristics with the signal detection after transient effect. The direct wave, transient phenomena and the primary reflected sound could be asiily distinguished each other by measurements of the arrival time of the time difference. And also noise could be easily distinguished by the same method. The result obtained can be used in industries for automatic measurement of the sound pressure reponse characteristics with respect to frequencies.

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A Study on Transient Characteristics of Flow Caused by Heat Addition in Supersonic Nozzle (초음속 노즐 내부 유동장의 가열에 의한 천이 특성에 대한 연구)

  • Chung, Jin-Do;Kim, Jang-Woo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.29 no.1 s.232
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    • pp.80-86
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    • 2005
  • This study presents numerical solutions of the two-dimensional Navier-Stokes equations for supersonic unsteady flow in a convergent-divergent nozzle with heat addition. The TVD scheme in generalized coordinates is employed in order to calculate the moving shock waves caused by thermal choking. We discuss on transient characteristics, start and unstart phenomena, fluctuations of specific thrust caused by thermal choking and viscous effects. We prove that the control of separation of boundary layer is the most important key problem to prevent the thermal choking.

One Dimensional Analysis for Dynamic Characteristics of Turbopump-fed Liquid Rocket Engine (1-D 모델링을 통한 터보펌프식 액체로켓 엔진의 동적 특성 해석)

  • Son, Min;Ku, Ja-Yeo
    • Journal of Aerospace System Engineering
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    • v.4 no.1
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    • pp.1-9
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    • 2010
  • As the rocket KSLV-1 called NARO was launched lately, development of domestic rocket technology has been accelerated elastically. Since the rocket technology needs a lot of empirical data, a variety of experiments should be done and lots of time have to be spent for accumulating the foundation of technology. However using a computer can be the solution to close a gap of technique because the simulation can be executed in short time against real experiments and calculate a multiplicity of cases easily. In this research, the transient analysis of turbopump-fed liquid rocket system was worked by the one dimensional modeling. The rocket system consists of the modulized components that are engine, turbopump and so on. For 70 ton class system, the rocket transient process of starting was studied and the performance analysis in steady condition was achieved. In addition, the estimation of nozzle internal flow was investigated by using a nozzle coefficient.

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Transient Liquid Phase Bonding of Gamma Prime Precipitation Strengthened Ni Based Superalloy (석출강화형 Ni 기 초내열합금의 천이액상확산접합)

  • Kim, Jeong Kil;Park, Hae Ji;Shim, Deog Nam
    • Journal of Welding and Joining
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    • v.35 no.3
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    • pp.52-61
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    • 2017
  • Transient liquid phase (TLP) bonding is essential technology to repair micro-cracking on the airfoil of blades and vanes for gas turbines. Understanding of the characteristics of TLP bonding of the superalloys is necessary in the application of the technology for repairing these components. In this study, the focus was on investigating TLP bonding characteristics of ${\gamma}^{\prime}$ precipitation strengthened Ni based superalloy. TLP bonding was carried out with an amorphous filler metal in various bonding conditions, and the microstructural characterization was investigated through optical microscopy (OM) and electron probe micro-analysis (EPMA). The experimantal results explained clearly that bonding temperatures had critical effects on the TLP bonding behaviors, and that isothermal solidication of the joints made at higher temperatures than $1170^{\circ}C$ was controlled by Ti diffusion instead of B.

Dynamic Response of the System for Vacuum Pump Performance Evaluation (진공 펌프 성능 평가 계통의 동적 응답)

  • Sim, Woo-Gun;Lim, Jong-Yeon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.11
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    • pp.1359-1367
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    • 2004
  • The demand of vacuum pump has been increased in the process of semi-conduct manufacturing, as a core component. The response of the system for vacuum pump performance test can be utilized to assess the system and to obtain the reliability of the apparatus for the test. The system consists of gas supply tank, pressure chamber, measurement chamber and transmission line. Transient analysis for compressible fluid has been conducted to evaluate the dynamic characteristic of the volume terminated transmission line. Numerical approach based on the method of characteristics is used for the analysis. The response is evaluated with the important parameters for the system: i.e., length and diameter of the line, volume of the terminal tank. Using the numerical results, pumping speeds are calculated and then compared to the experimental results.

Effects of dimple/protrusion array on heat transfer coefficients in rectangular wavy duct (주름진 덕트에서 딤플/돌출 형상이 열전달계수에 미치는 영향)

  • Kwon, Hyun-Goo;Hwang, Sang-Dong;Cho, Hyung-Hee
    • Proceedings of the KSME Conference
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    • 2008.11b
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    • pp.2352-2356
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    • 2008
  • Heat transfer and performance characteristics have been investigated for a rectangular wavy duct with dimple or protrusion arrays. The test duct was 15mm in height and 105mm wide. The print diameter of the dimple/protrusion wall was 12.99mm and the depth/height of the dimple/protrusion was 3.75mm. Local heat transfer coefficients on the dimple/protrusion wall were measured using a transient TLC technique. The Reynolds number was varied from 3,000 to 10,000. For the wavy duct tested in this study, adverse static pressure characteristics occurred at turning region of the wavy duct due to secondary flows. For the wavy duct with protrusion array, higher heat transfer enhancement level of 7.4 times than smooth straight case in maximum was obtained at low Reynolds number due to the high heat transfer enhancement by vortex flows. Also, the protrusion array increased the performance level of 3.0 at low Reynolds number of 3,000.

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