• 제목/요약/키워드: 김정수

검색결과 2,812건 처리시간 0.031초

저압 유기금속 기상화학증착법에 의한 1.3$\mu$m InGaAsP/InP uncooled-LD의 제작 (Fabrication of 1.3$\mu$m InGaAsP/InP uncooled-LD using low pressure MOVPE)

  • 조호성;김정수;이중기;장동훈;박경현;이승원;박기성;김홍만;박형무
    • 전자공학회논문지A
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    • 제32A권6호
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    • pp.75-81
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    • 1995
  • InGaAsP/InP uncooled LDs emitting at 1.3$\mu$m wavelength are of interest for several application of fiber-to-the-home, optical interconnection, long-haul high-bit-rate optical transmission systems, etc. The strain compensated PBH-MQW-LD employing 1.4% compressive strained well (${\lambda}=1.3{\mu}m$) and 0.7% tensile strained barrier (${\lambda}=1.12{\mu}m$) layers grown by low pressure metallicorganic vapor phase epitaxy was found to be low threshold current and stable temperature characteristics. The average threshold current of 5.6mA and average slope efficiency of 0.27mW/mA at room temperature were obtained for uncoated uncooled-LD.

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비고전적 감쇠시스템에서 주파수분리의 모드연관에 대한 영향 (Influence of Frequency Separation on Modal Coupling in Nonclassically Damped Systems)

  • 김정수;최기흥;최기상
    • 대한기계학회논문집
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    • 제18권9호
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    • pp.2245-2250
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    • 1994
  • The normal coordinates of a nonclassically damped systems are coupled by nonzero off-diagonal elements of modal damping matrix. The relationship between modal coupling and the frequency separation of the natural modes is presented in this paper. Contrary to widely accepted beliefs, increasing the frequency separation of the natural modes does not neccessarily diminish the effect of modal coupling. Consequently, in the pratical engineering applications, wide frequency separation of the natural modes would not be sufficient for neglecting modal coupling.

인공위성 추진기관 설계변수 도출을 위한 Hydrazine 액체 추진제의 비정상 유동해석 (Unsteady Flow Analysis of Liquid Hydrazine Propellant for the Design Parameter Derivation of Satellite Propulsion System)

  • 최진철;김정수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.497-501
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    • 2000
  • One of the way to derive design parameters of the fuel feeding system in satellite is to analyze unsteady flow of liquid propellant (hydrazine) in the propulsion system. During steady thruster firing the flow rate is constant: if a thruster valve is abruptly shut down among a sets of thrusters, pressure spikes much higher than the initial tank pressure occur. This renders the fuel flow unsteady, and the fluid pressure and flow rate to oscillate. If the pressure spikes are high enough, there are possibilities that propellant explosively decomposes, thruster valves are damaged, and adiabatic detonation of the hydrazine propellant is potentially incurred. Reflected shockwaves could also affect the calibration and operation of the pressure transducers. These necessitate the analysis of unsteady flow in the propulsion system design, and the calculation results obtained through some governing parameter variation are presented in this work.

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원형공간내 열분해 연료의 공간배치가 연소현상에 미치는 영향 (Influence of Pyrolyzing Fuel Disposition on Combustion Phenomena in a Cylindrical Enclosure)

  • 한조영;김정수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.680-685
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    • 2000
  • Investigation on ignition and flame propagation of pyrolyzing fuel in a cylindrical enclosure is accomplished. The pyrolyzing fuel of cylindrical shape is located in an outer cylinder sustained at high-temperature. Due to gravity, the buoyancy motion is inevitably incurred in the enclosure and this affects the flame initiation and propagation behavior. The radiative heat transfer plays an important role since a high temperature difference is involved in the problem. Numerical studies have been performed over overheat ratio, and vertical fuel eccentricity. The location of flame onset is affected by the vertical eccentricity of inner pyrolyzing fuel as well as thermal conditions applied.

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인공위성 추진시스템용 추력기 열차폐막의 구조해석 (Structural Analysis of Thruster Heat Shield for Satellite Propulsion System)

  • 이균호;김정수;한조영
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.468-472
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    • 2003
  • MRE-1 dual thruster module(DTM) which will be installed to the present under development KOMPSAT(Korea Multi-Purpose Satellite) can provide reliable and cost-effective means of propulsive control for attitude and maneuvering control system. Thruster heat shield, one of the main components of DTM, is designed to intercept the radiative heat exchange between thruster and satellite during firing. The inside diameter of the current configuration will be decreased a little compared with that of the previous one due to manufacturing method change. Therefore, the possibility of interference between thruster and heat shield due to configuration change is investigated through structural analysis and their results are described in this paper.

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중소기업을 위한 생산정보시스템의 개발

  • 정병호;소영섭;허은영;이해영;조영호;김정수
    • 한국경영과학회:학술대회논문집
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    • 대한산업공학회/한국경영과학회 1996년도 춘계공동학술대회논문집; 공군사관학교, 청주; 26-27 Apr. 1996
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    • pp.190-193
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    • 1996
  • In recent, most of automobile industries adopt the concept of Just In Time production. The paternal manufacturers require their suppliers to supply parts just in time. It is very important for a subcontractor to produce the parts in the appointed time of delivery. This study develops a production information system for Woosin Industry, which is one of such subcontractor of Hundai Motors Company(HNC). The system is developed on Client/Server system. Firstly, three modules are developed, i.e., scheduling module to make a schedule, the subsystem of sales management to deal with the information about order of HMC, delivery of parts, and bill collecting, and the module for supporting material requirement planning and purchace of material.

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자동차 후류에 대한 3차원 유동의 PIV 측정 (PIV Measurements of Three-Dimensional Wake Around a Road Vehicle)

  • 김진석;김성초;성재용;김정수;최종욱
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2004년도 추계학술대회 논문집
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    • pp.1-4
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    • 2004
  • The PIV measurements are performed to get the quantitative flow visualization around a road vehicle. The model scaled with 1/48 is located in the middle test section of the closed-loop water tunnel and the measuring system consists of CCD camera, diode laser, synchronizer, and computer. The experimental data are obtained at two Reynolds numbers of 50,000 and 100,000 based on the model length. The quasi-three-dimensional isovorticity surfaces, based on two-dimensional velocity field data, are generated. There is little difference between the results in part of the recirculation region and the vorticity contour according to the Reynolds number. Also a little bit complicated three dimensional flows are predicted behind the road vehicle.

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가열된 고체표면에 부착된 단일 액적의 증발냉각 (Evaporation Cooling of Single Droplet on a Heated Solid Surface)

  • 유갑종;방창훈;김정수
    • 대한기계학회논문집B
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    • 제25권6호
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    • pp.845-852
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    • 2001
  • The characteristics of evaporation cooling of single droplet on a heated surface were studied experimentally. The two kinds of heater modules were tested to measure cooling characteristics of metal surface (high conductivity) and Teflon surface (low-energy surface, low conductivity). The results showed that time averaged heat flux during droplet evaporation increased exponentially with initial surface temperatures of brass, copper and steel. The heat flux and evaporation time did not varied with metal conductivities. However, the temperature drop after the deposition of droplet was larger on Teflon than on the metals. Thus, the correlation of interface temperature between liquid droplet and metal surface was proposed as a function of the initial surface temperature of heating materials, which could be applied to both metal and non-metal ones.

다목적실용위성 2호 추진계의 열설계 (Thermal Design for KOMPSAT-2 Propulsion System)

  • 한조영;김정수;이균호
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.77-82
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    • 2001
  • Thermal design for KOMPSAT-2 propulsion system has been performed. Overall design requirements and the constitution for propulsion system is described. To meet the thermal design requirements, both a primary and a redundant heater circuit, each with two thermostats placed in series, will protect each hydrazine-wetted components, even if one heater circuit fails to operate. Heater power is turned off if any one of these thermostats is opened at its higher setpoint. Thus, even if one thermostat is failed closed, the second thermostat will turn off the heater. All such components shall be insulated with MLI. Propulsion heater sizing based on the constant worst cold case condition is conducted through thermal analysis. All heaters selected for propulsion components operate to prevent propellant freezing satisfying the thermal requirements for the propulsion subsystem over the worst case average voltage, i.e. 25 volts.

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대만에서 고추에 발생한 미보고 Potyvirus에 관한 연구 (An Unusual Potyvirus from Pepper in Taiwan)

  • 김정수
    • 한국식물병리학회지
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    • 제3권4호
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    • pp.261-269
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    • 1987
  • 포장에서 고추에 황화, 엽맥록대 그리고 엽맥주름을 일으키는 바이러스가 분리되었다. 이 바이러스는 PVY항혈청과 ELISA 검정에서 반응하였으나 CMV, TMV, TBRV, AMV, TSWV, TEV, PMV, TRSV와는 반응하지 않았다. 바이러스 입자의 전자현미경 검경 결과 길이가 750-760nm의 사상형 입자였다. 이 바이러스는 진딧물에 의해 쉽게 전염되었으며 기주범위는 PVY와 비슷하였으나 Chemopodium amaranticolor와 C. quinoa에 전신 감염을 일으켰다.

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