• Title/Summary/Keyword: 초기압력

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RF magnetron sputtering으로 제작된 ITO 박막의 공정압력 변화에 따른 특성

  • Jeong, Seong-Jin;Kim, Deok-Gyu;Kim, Hong-Bae
    • Proceedings of the Korean Vacuum Society Conference
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    • 2010.02a
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    • pp.203-203
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    • 2010
  • 본 연구에서는 RF magnetron sputtering을 이용하여 공정압력에 따라 증착된 ITO 박막의 투명 전극 특성을 연구하였다. ITO 박막은 $In_2O_3$ : $SnO_2$ 비율이 9:1로 소결된 3in 직경의 타겟을 사용하여 corning 1737을 유리기판 위에 증착하였다. 증착조건으로 초기압력은 $1.7{\times}10^{-6}torr$로, 가스 유량은 Ar 50 sccm으로, RF power는 25W로 각각 고정하였으며, 증착 공정압력을 $2.0{\times}10^{-2}$, $7.0{\times}10^{-3}$, $2.0{\times}10^{-3}torr$로 변화하면서 200nm 두께의 ITO 박막시편을 제작하였다. 제작된 시편의 AFM 분석결과 박막의 거칠기는 0.33nm 이었으며, 광투과도 및 비저항은 공정압력이 낮은 경우 상대적으로 양호한 결과를 보였다. 높은 공정압력에서 광투과도는 60% 정도로 나타났으나, 낮은 공정압력에서 RF power를 증가시킴에 따라 가시광선의 광투과도는 85% 이상으로, Hall측정을 통한 Mobility는 $37.6\;cm^2V^{-1}s^{-1}$로 각각 증가하였으며, 비저항은 $0.346{\times}10^{-3}{\Omega}cm$이었으며, 이동도는 $4.788{\times}10^{20}cm^{-3}$로써 양호한 투명전극 특성을 보였다.

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Biosparging 공법을 이용한 석유계탄화수소화합물 오염토양에 대한 현장적용성 평가

  • 신정엽;오경철;공준;이승우;전기식
    • Proceedings of the Korean Society of Soil and Groundwater Environment Conference
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    • 2004.04a
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    • pp.35-38
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    • 2004
  • 부틸알데히드로 오염된 대상 부지에 Biosparging 공법의 현장 적용을 위해 적정 공기 주입 압력 조건을 도출한 결과, 주 오염층인 자갈질 모래층에 공기주입 가능 파괴압력(Pe)는 약 300mmAq로 측정되었으며 4,500mmAq 압력 조건에서는 용존 산소농도의 영향 반경이 약 3 m로 나타났다. 위의 조건을 적용하여 약 150일간 운전한 결과, 영양물질을 투입하지 않은 초기 90일 동안 최고농도 대비 약 90%가 저감되었으며 그 이후에 영양물질을 투입하여 초기 최고 농도 대비 96%가 저감되어 복원목표치인 50ppm을 모든 지역에서 만족시켰다. 또한 생분해 반응속도가 k=0.03/day로 나타나 휘발성이 낮고 생분 해도가 뛰어난 부틸알데히드로 오염된 자갈질 모래층에 Biosparging공법이 성공적으로 적용된 사례이다.

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Quality Changes during Storage of Low Salt Fermented Anchovy treated with High Hydrostatic Pressure (초고압 처리한 멸치젓의 저장 중 품질 변화)

  • Lim, Sang-Bin;Jwa, Mi-Kyung;Mok, Chul-Kyoon;Woo, Gun-Jo
    • Korean Journal of Food Science and Technology
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    • v.32 no.2
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    • pp.373-379
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    • 2000
  • Low salt fermented anchovy was stored at $25^{\circ}C$ for a period of 20 days from the time of ultra-high pressure treatment under different operating conditions, such as magnitude of pressure($(200{\sim}500\;MPa)$, temperature$(20{\sim}50^{\circ}C)$ and treatment time$(5{\sim}20\;min)$ with viable cell count(VCC) and quality assessments conducted at regular intervals. VCC decreased logarithmically during storage. Lower values of VCC in the treated samples were observed compared to the untreated. A gradual increase in peroxide value was noticed during storage, compared to those of the untreated which showed a sudden rise. Thiobarbituric acid value decreased initially and remained at that level before rising almost exponentially between 12 and 20 days. Volatile basic nitrogen increased gradually during storage. Amino nitrogen remained almost constant up to 20 days, regardless of any conditions investigated. High pressure treatment maintained better quality during storage at $25^{\circ}C$ by reducing the viable cell count in low salt fermented anchovy.

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Papers : Application of Cavitating Venturi for Stable propellant feed system (논문 : 안정적인 액체연료 공급을 위한 Cavitating Venturi 의 응용)

  • Park,Hui-Ho;Kim,Yu;Jang,Eun-Yeong;Lee,Su-Yong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.1
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    • pp.88-94
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    • 2002
  • For the pressurized propellant supply system of liquid rocket, feed pressure is determined with respect to the chamber pressure of normal combustion state. However, during ignition period the initial chamber pressure is atmosopheric. This may cause overflow, hard-start and even critical damage for the engine. This paper proposes an improved propellant feed system for the stable combustion of liquid rocket. The proposed system utilizes the cavitating venturi to provide stable mass flow rate. Cavitating venturi offers unique flow control capabilities at normal and abnormal combustion state, because flow rate is soley dependent on the upstream absolute pressure and fluid properties, but independent on th downstream condition. Experimental variables are propellant feed pressure and chamber pressure. The effectiveness of cavitating venturi increased when the ratio of actual feed pressure to the cavitating venturi design pressure is increased. It is also found that Kerosene if more effective to supply stable mass flow rate than LOx.

도시가스 - 공기혼합기체의 폭발특성에 관한 연구

  • 박승호;임우섭;목연수;최재욱
    • Proceedings of the Korean Institute of Industrial Safety Conference
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    • 2000.06a
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    • pp.136-139
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    • 2000
  • 현대산업사회의 급속한 발전으로 사용이 편리하고, 깨끗한 연료인 도시가스의 사용량은 점점 더 증대될 뿐만 아니라 사용형태 또한 다양화되고 있어, 이에 따른 사고도 증가하고 있으며 사고의 규모도 대형화 되어가고 있다. 일반적으로 가스폭발의 경우 개방된 영역에서 보다 밀폐된 영역에서 발생할 경우 폭발압력에 의한 파괴효과는 더욱 증가한다. 이러한 부분에 대해 많은 학자들은 단일가스와 산화제를 혼합시킨 형태의 가스 폭발에 대한 특성을 연구하여 왔다. 그러나 산소농도의 변화에 따른 가연성가스의 폭발범위, 폭발시 초기압력의 변화, 최소점화에너지에 관한 연구는 거의 없는 실정이다. (중략)

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Numerical Simulation of The Pressure-Flow Control Characteristics of Shunt Valves Used to Treat Patients with Hydrocephalus (수두층 치료용 션트밸브의 압력-유량 제어특성 수치해석)

  • 장종윤;이종선;서창민
    • Journal of Biomedical Engineering Research
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    • v.22 no.5
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    • pp.403-412
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    • 2001
  • The Present study analyzed the pressure-flow characteristics of a Korean shunt valve. Changes in the characteristic currie depending on the design parameters were also investigated. The Korean shunt valve used in the present study was constant pressure type and our analyses were validated through experiments. We applied fluid-structure interaction to solve the flow dynamic Problem because the small diaphragm in the valve was made from flexible silicone elastomers. Considering the material nonlinearity of the hyper-elastic material. the Mooney-Rivlin approximation was employed. The results of the numerical analyses were close to the experimental results The major Pressure drop was observed to happen in the small diaphragm. The slope of the pressure-flow characteristic curve was computed to be 0.37mm$H_2O$.hr/cc, which was similar to the average value of commercial shunt valves. 0.40mm$H_2O$.hr/cc. Therefore. our valves analyzed in the Present study showed a Proper Pressure control characteristics of the constant pressure type shunt valves. The opening pressure could be controlled by adjusting the amount of predeflection of the valve diaphragm. In order to obtain opening pressures of 25mm$H_2O$ and 80mm$H_2O$, respectively, and the required predeflection was found to be 10.2$\mu$m and 35.3$\mu$m. The flow orifice size was found to be within 10$\mu$m during valve operation Therefore, Precision design and manufacturing techniques are necessary for successful operations of the shunt valve. The study indicated the amount of predeflection as well as the magnitude of corner rounding of the diaphragm edge are important design parameters to influence the slope of the pressure-flow characteristic curve.

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A Study on the Safe Gap for Explosion-proof (내압방폭을 위한 Safe Gap의 측정에 관한 연구)

  • Oh Kyu-hyung
    • Journal of the Korean Institute of Gas
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    • v.1 no.1
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    • pp.1-6
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    • 1997
  • In case of using the electrical apparatus in the hazardous atmosphere which exist flammable gas mixtures, There is a dangerosity of gas explosion accident by the electrical spark. The most general method to prevent the explosion by the spark is to use the flame-proof type electrical apparatus to isolate the ignition source. from the flammable atmosphere. But actualy it is impossible to isolate the ignition sources from the atmosphere. So it was needed to find the safe gap which prevent ignition of flammable atmosphere by transmission of flame or heat when a flammable gas mixture exploded inside the apparatus. In this study we tried to find the maximum experimental safe gap(MESG) of $H_2$-air, and $CH_4$-air mixtures by using the 8 litre spherical vessel with 25mm flange. The experiment parameter were ignition position, concentration and initial pressure before explosion. From the experiment the ignition position was affected to the MESG. MESG value was minimum near the stoichiometric concentration of gas mixtures, and according to the increase of initial pressure MESG was decreased.

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Extinction Characteristic of AP/HTPB Composite Solid Propellant by Rapid Depressurization (급감압에 의한 AP/HTPB 복합고체추진제의 소화 특성)

  • Kim, Daeyu;Yoon, Jisang;Lee, Kukjin;Yoon, Woongsup
    • Journal of the Korean Society of Propulsion Engineers
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    • v.23 no.2
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    • pp.21-26
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    • 2019
  • Exposure to a rapidly depressurized environment causes extinction of a burning solid propellant. Experiments have been conducted to determine the rate of depressurization required to extinguish a burning solid propellant. For this purpose, a depressurization combustor was designed and fabricated. The results of this experiment were used to determine the boundary between extinction and non-extinction of AP/HTPB solid propellants under different propellant compositions. Experimental results show that the initial and final pressures have a considerable effect on the critical depressurization rate.

Controlling Factors of Open-Loop Combustion Response to Acoustic Pressures in Liquid Propellant Rocket Engine (강한 압력파동에 구속된 액체 추진제 연소응답의 지배인자)

  • Yoon Woongsup;Lee Gilyong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.267-273
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    • 2004
  • This paper targets to define controlling factors of pressure-coupled combustion response and estimate their effects on droplet evaporation process. Dynamic characteristics of hydrocarbon propellant vaporization perturbed by acoustic pressure are numerically simulated and analyzed. 1-D droplet model including phase equilibrium between two phases is applied and acoustic wave is expressed by harmonic function. Effects of various design factors and acoustic pressure on combustion response are investigated with parametric studies. Results show that driving frequency of acoustic perturbation and ambient pressure have important roles in determining magnitude and phase of combustion response. On the other hand, other parameters such as gas temperature, initial droplet size and temperature, and amplitude of acoustic wave cause only minor changes to magnitude of combustion response. Resultant changes in phase of heat of vaporization and thermal wave in droplet highly influence magnitude and phase of combustion response.

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A Study on Parameters of Soft Recoil Mechanism for Reduction of Recoil Force (주퇴력 저감을 위한 연식 주퇴 메커니즘의 매개변수에 관한 연구)

  • Yang, Tae-Ho;Lee, Young-Shin;Lee, Kyu-Sub;Jun, Sang-Bae;Kang, Kuk-Jeong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.36 no.7
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    • pp.823-828
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    • 2012
  • The soft recoil mechanism was an effective mechanism for reducing the recoil force by forwarding momentum. There were some parameters such as the fire angle, firing position, and initial pressure of the recuperator, which influenced the forwarding momentum. These parameters affected the generation of the forwarding momentum in the soft recoil mechanism. To design for the mechanism, the parameters affecting momentum were studied to consider some reasonable conditions. Among the various parameters, the initial pressure of the recuperator and firing position was confirmed as a key factor to have affected the momentum. It was determined that the recoil force had a minimum value when the initial pressure of the recuperator was 180.