• Title/Summary/Keyword: (D/C) ratio

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Performance of Gas Electron Multiplier (GEM) detector

  • Han, S.H.;Moon, B.S.;Kim, Y.K.;Chung, C.E.;Kang, H.D.;Cho, H.S.
    • Journal of Radiation Protection and Research
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    • v.28 no.4
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    • pp.343-348
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    • 2003
  • We have investigated in detail the operating properties of Gas Electron Multiplier (GEM) detectors with a double conical and a cylindrical structure in a wide range of external fields and GEM voltages. With the double conical GEM, the gain gradually increased with time by 10%; whereas this surface charging was eliminated with the cylindrical GEM. Effective gains above 1000 were easily observed over a wide range of collection field strengths in a gas mixture of $Ar/CO_2(70/30)$. The transparency and electron collection efficiency were found to depend on the ratio of external field and the applied GEM voltage; the mutual influence of both drift and collection fields was found to be trivial.

Analysis on Pressure and Temperature wave of Self Oscillating Heat Pipe (자려 진동 히트파이프의 압력 및 온도 파형 해석)

  • Choi, J.H.;Yoon, D.H.;Oh, C.;Kim, M.H.;Yoon, S.H.
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2000.11a
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    • pp.43-49
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    • 2000
  • Heat transfer characteristics of self oscillating heat pipe were experimentally investigated for the effect of fill charge ratios and heat loads. The heat pipe used for this study is made of copper capillary, has 0.002m internal diameter, a 0.34m length in one turn and consists of 19 turns. Heating and cooling section each have a length of 70mm. Water was used as working fluid inside heat pipe. As the experimental results, the self oscillating heat pipe was operated by self-exited oscillation and circulation of working fluid and the oscillation within the self oscillating heat pipe assumed chaotic behavior.

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An Analysis of Supersonic Jet Noise with a Converging-Diverging Nozzle (C-D 노즐을 고려한 초음속 제트 소음 해석)

  • Kim Yong Seok;Lee Duck Joo
    • Proceedings of the Acoustical Society of Korea Conference
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    • autumn
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    • pp.389-392
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    • 2001
  • To investigate the generation mechanism of the shock-associated noise, an underexpanded supersonic jet from an axisymmetic nozzle is simulated under the conditions of the Nozzle exit Mach number of 2 and the exit pressure ratio of Pe/Pe =1.5. The present simulation is performed based on the high-order accuracy and high-resolution ENO (Essentially Non-Oscillatory) scheme to capture the time-dependent flow structure representing the sound source. It was found that the shock-associated noise is generated by the weak interaction between the downstream propagating large turbulence structures of the jet flow and the quasi-periodic shock cell structure during the one is passing through the other. The directivity of propagating waves to the upstream is clearly shown in the visualization of pressure field. It is shown that the present calculation of the centerline pressure distribution is in fare agreement with the experimental data at the location of first shock cell.

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Structural Analysis of Boiler Module for Sea-Transportation (해상 운송을 위한 보일러 모듈의 구조 해석)

  • Jeon, Y.C.;Kim, T.W.;Jeong, D.G.
    • Proceedings of the KSME Conference
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    • 2001.06a
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    • pp.788-793
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    • 2001
  • Finite element analysis was carried out to investigate the integrity and reliability of boiler module during sea transportation. The boiler module was supported by steel structure to relieve the instantaneous shock from oceanic wave and its primary parts were strengthened with several reinforcements. Finned tube walls which were used in the furnace wall were assumed as orthotropic plates having equivalent material properties. The bank tubes were also equivalently modeled in accordance with ASME B31.1 for the convenience of finite element modeling. The calculation results were compared with the yield stress of the material. In particular, the bank tube stress, which was evaluated by converting the calculated stresses in equivalent tubes into those in original tubes by using the ratio of diameter, was also examined with yield stress.

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An Analysis of Optimal Link Voltage of VS-SVPWM for Current Harmonics Reduction

  • Lee Dong-Hee;Park Han-Woong;Ahn Jin-Woo;Kwon Young-Ahn
    • Proceedings of the KIPE Conference
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    • 2002.07a
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    • pp.343-346
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    • 2002
  • In recent, complex SVPWM (Space Vector PWM) algorithm can be easily implemented by high performance microprocessor and DSP. Various SVPWM techniques are widely studied due to the advantages of low harmonic distortion and high use ratio of D.C. link voltage. Most of various studies for improving of VS-PWM inverter performance are concentrated about switching pattern and zero pulse pattern split algorithms. However, dc link voltage that is determined at rated load and speed conditions is not proper in the low speed and under rated load. In this paper, analysis of current ripple with digitally implemented SVPWM inverter is introduced according to link voltage. The optimal link voltage in the designed inverter system and load condition is provided in order to suppress output voltage error and current ripple. As remaining the effective voltage vector interval per sampling period sufficiently, additional voltage error and current ripple are suppressed. The proposed algorithm is verified through digital simulation and experimental results.

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An Optimal Efficiency Control of Reluctance Synchronous Motor using Direct Torque Control (직접 토크 제어를 이용한 리럭턴스 동기 전동기의 최대 효율제어)

  • Park Hong-il;Kim Nam-Hun;Choi Kyeong-Ho;Kim Dong-Hee;Kim Min-Huei
    • Proceedings of the KIPE Conference
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    • 2002.07a
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    • pp.431-434
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    • 2002
  • This paper presents an implementation of direct torque control(DTC) of Reluctance Synchronous Motor(RSM) with an efficiency optimization using the 32bit DSP TMS320C31. The influence of iron loss can not neglected as high speed and precision torque control of RSM, so the optimal current ration between torque current and exiting current analytically derived to drive RSM at maximum efficiency For RSM, torque dynamics can be maintained even with controlling the flux level because the generated torque is direct]y proportional to the stator current. The experimental results for an RSM are presented to validate the applicability of the proposed method. The developed control system is shown high efficiency features with 1.0Kw RSM having 2.57 ratio of d/q reluctance.

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Development of the Preventive Diagnostic Expert System of Gas in Oil for Power Transformer (변압기 예방진단을 위한 유중가스 전문가 시스템 구축 연구)

  • Choi, I.H.;Kweon, D.J.;Jung, G.J.;Sun, J.H.;Kim, C.G.;Kim, K.H.
    • Proceedings of the KIEE Conference
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    • 1999.11d
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    • pp.1019-1021
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    • 1999
  • In this paper, we describe the design and appliance of the preventive diagnostic expert system of gas in oil for power transformer. This expert system is developed to use expert system development tool; Element Expert (NEURON DATA Inc.) Analysis is developed by four diagnose methods. In first, the standard of KEPCO is applied. It classifies the state of transformer by four level: Normal, warning, abnormal and danger. And the others are gas pattern methods, IEC code method, and Dornen & Roger Ratio method and applied later. These latter methods analyse the cause of result. Inference engine was designed with Element Expert. In last, we operate the system with sample data and we can obtain the correctly inferred result for the state of transformer.

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Inclusion Complexation of Cyclodextrin with Prothionamide in Aqueous Solution

  • Kim, Shin-Tae;Kim, Shin-Keun
    • Journal of Pharmaceutical Investigation
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    • v.12 no.4
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    • pp.132-144
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    • 1982
  • The inclusion of ${\beta}-cyclodextrin$ $({\beta}-CyD)$ with prothionamide in aqueous phase was investigated by circular dichroism(CD), ultraviolet (UV) absorption, and solubility technique. The results suggested that a region of drug chromophore was located within the asymmetric center of ${\beta}-cyclodextrin$. Solubility and spectral changes were quantitatively treated to obtain stoichiometric ratio, which was found to be 1 : 1, and formation constants which were determined by solubility, CD, and UV method were 257, 367, and 389 $M^{-1}$, respectively. Also, the formation constant of the inclusion complex was determined by CD method at various pH. The result was that $K_c$ depended upon the pH of medium, and this fact also supported that thioamide moiety was accomodated in the cavity of ${\beta}-cyclodextrin$.

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Characteristics of transmission efficiency in power driveline of agricultural tractors

  • I. H. Ryu;Kim, D. C.;Kim, K. U.
    • Proceedings of the Korean Society for Agricultural Machinery Conference
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    • 2000.11b
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    • pp.132-138
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    • 2000
  • Complex gear shifting and high speed-reduction ratio reduce the transmission efficiency in power driveline of agricultural tractors. According to a field test, the power transmission efficiency of a tractor in transporting operations was estimated about 70%. However, the actual efficiency was found by the experiment to fluctuate in a range of 56 to 87%. Therefore, the constant efficiency model commonly used for a simulation of power drivelines is not likely to simulate its performance more accurately. In order to predict power transmission efficiency more accurately, a new model was proposed and the new concepts of the maximum efficiency and sticking torque were introduced. The error mean between the measured and the predicted efficiencies was about 2.3% in mean. The new model reflecting the transmission characteristics in the power driveline of tractors could be used to analyze and predict the power transmission performance of tractors more accurately.

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Optimization of Injection Molding of Bobbin Part based on CAE (CAE를 이용한 보빈 성형품의 사출성형 최적화)

  • Kwon, Y.S.;Cho, Y.S.;Kim, B.G.;Min, B.H.;Jeong, Y.D.
    • Journal of Power System Engineering
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    • v.6 no.2
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    • pp.68-72
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    • 2002
  • Design of experiment was applied to analyze the shrinkage characteristics of the bobbin molded by injection molding. Among lots of design and processing conditions, the thickness of a bobbin and cooling conditions of a mold were considered. The temperature difference between top and bottom parts of the bobbin was considered as the objective to minimize the shrinkage of a bobbin. Optimal thickness of a bobbin was 2.0mm at the part of body and 1.5mm at the part of wing, respectively. Optimal cooling conditions such as cooling time and coolant inlet temperature were 12 second and $12^{\circ}C$, respectively.

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