• Title/Summary/Keyword: Large chamber

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Double Outlet Left Atrium: A rare form of the atrioventricular septal defect with malposition of the atrial septum (좌심방 양심실 연결증 [DOLA])

  • Lee, Jae-Won;Seo, Gyeong-Pil
    • Journal of Chest Surgery
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    • v.18 no.2
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    • pp.273-278
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    • 1985
  • The case of a patient with abnormal position of the atrial septum resulting in a left atrium with two atrioventricular valves and a disconnected right atrium is presented with review of related articles. Anatomic details showed atrial situs solitus and a left sided cardiac apex. The right atrium received both venae cavae and a coronary sinus. No AV valve was found in the right atrium, and the floor of this chamber was placed above the posterior wall of right ventricular chamber. The atrial septum with secundum ASD was displaced to right anteriorly at its lower portion and inserted to right of tricuspid annulus. The tricuspid and mitral valve configuration was that of so-called partial ECD, i.e. mitral cleft with large anterior mitral leaflets. The ventricular septum was intact and both ventricular chambers were equally well developed with normal relationships. Surgical repair of this anomaly was performed by resecting the abnormally positioned lower part of the atrial septum, repairing the cleft of the anterior mitral leaflet, and septating the atrium for diverting the systemic and pulmonary venous blood to RV and LV, respectively.

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Concept Design of Hydro Reactive Solid Propellant for Underwater High Speed Ramjet Engine System (수(水)반응성 고체추진제를 이용한 수중고속램제트엔진 시스템 개념 설계)

  • Chae Jae-Ou;Sim Ju-Hyen;Kwak Yong-Whan;Koo Hyung-Joon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.121-131
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    • 2005
  • For thrust motion of high speed underwater torpedo the special hydro reactive fuels that burns in vapor water and water supply from aboard is used. The main component of this hydro reactive fuel is the powder of active metal (Mg, Al) that can burn in water vapor with large heat generation in the rocket combustion chamber. The thermodynamic analysis of combustion properties of the burning of the particles of these active metal in the vapor water have been carried out. The conception for the possible content variants of the hydro reactive fuels have been discussed using the geometrical and thermodynamic combustion conditions with the basic recommendation for contents of designed hydro reactive fuels in future.

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A Study of ${{\sigma}_v}'-D_r-N$ Correlation using Large Calibration Chamber System (대형 Calibration Chamber System을 이용한 ${{\sigma}_v}'-D_r-N$ 상관관계 연구)

  • Choi, Sung-Kun;Kim, Sang-In;Lee, Chung-Ho;Kim, Dong-Hoo;Lee, Woo-Jin
    • Proceedings of the Korean Geotechical Society Conference
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    • 2005.03a
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    • pp.1175-1182
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    • 2005
  • Using KUCCS, which enables real-time monitoring and controlling, the various boundary condition and in-situ field stress condition was simulated, to derive the correlation among ${{\sigma}_v}'-Dr-N$in domestic sandy soils. Soil specimens, having various relative density and confined stress, were formulated to evaluate N-value from the SPT. and Pile Driving Analyzer, PDA, was employed as a measuring device for the energy transfer efficiency in the rod. From the quantitative analysis of N-value, the correlating equation, $N_{60}/{D_r}^2=16.35+14.45{{\sigma}_v}'$ was obtained on the basis of Skempton's method(1986). More reliable soil parameters can be obtained from the N-value by using this study which considered regional characters and the correlation among ${{\sigma}_v}'-Dr-N$.

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Flow Visualizations and Hot-Wire Measurements on Air Flow in Two Different Neonate Incubators

  • Kim, Young-Ho;Yoo, Seoung-Chool;Kwon, Chi-Ho
    • Journal of Mechanical Science and Technology
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    • v.15 no.7
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    • pp.1051-1060
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    • 2001
  • Flow visualizations and hot-wire measurements on the inside flows of two different incubators are presented in this paper. An anatomically-correct neonate model was fabricated using the rapid prototyping machine, based on the 3-D scanned data. The result showed that air flow in the incubator was affected not only by the air circulation system but also by the design of incubator chamber. Large rotating motions were located around the corners of free space. A number of small eddies were found in regions of high shear flow, in areas such as that between the air inlet and the neonate. But, these small eddies were found to be stationary at that locations. Those small eddies might interfere with convective and evaporative heat transfers from the neonate. This study has led to a better understanding of flow mechanism in an incubator chamber and provided the guidance needed for the advancement of improved computational fluid dynamic models.

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The Separation of Colloid Particles of Different Sizes by Dielectrophoresis (유전이동을 이용한 콜로이드 입자의 크기에 따른 분리)

  • Hwang, Yeon
    • Korean Journal of Materials Research
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    • v.17 no.3
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    • pp.167-172
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    • 2007
  • The separation of the small colloidal particles from the mixture of two different sized particles using AC dielectrophoresis phenomenon was studied. The spherical mono-dispersed polystyrene particles dispersed in pure water were put into a perfusion chamber on a substrate, and AC electric fold was applied to the glass substrate with Au electrodes in 4 mm distance. The AC frequency was fixed at 1 kHz and the intensity of the field was varied from 25 V/cm to 160 V/cm. After applying the AC field, the degree of the chain formation that resulted from the particle movements by dielectrophoresis was observed by optical microscope. The mixture of the $1\;{\mu}m\;and\;5\;{\mu}m$ sized polystyrene particles at 0.5 vol% concentrations for each size was set in the dielectrophoresis conditions of 1 kHz and 100 V/cm. At this condition large $5\;{\mu}m$ sized polystyrene particles formed chains, on the contrary the $1\;{\mu}m$ sized polystyrene particles formed no chains. After water flowing for 20 min, it was found that small particles that were floating in the chamber had been removed by the water flowing.

PROPAGATION PROCESSES OF NEWLY DEVELOPED PLASMA JET IGNITER

  • Ogawa, Masaya;Sasaki, Hisatoshi;Yosgida, Koji;Shoji, Hideo;Tanaka, Hidenori
    • International Journal of Automotive Technology
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    • v.3 no.1
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    • pp.9-16
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    • 2002
  • In plasma jet ignition, combustion enhancement effects occur toward the plasma jet issuing direction. Therefore, when the igniter is attached at the center of a cylindrically shaped combustion chamber, plasma jet should issue toward the round combustion chamber wall. The plasma jet igniter that had an annular circular orifice has been developed. The purpose of this study is to elucidate the relationship between the newly developed plasma Jet igniter configuration and combustion enhancement effects. In this newly developed plasma Jet igniter, flame front wrinkle appears on the flame front and flame propagates rapidly. Plasma Jet influences on the flame propagation far long period when the plasma jet igniter has issuing angle 90 degrees and large cavity volume, because the plasma jet only lasts several ms. However, in the early stage of combustion, flame front area of issuing angle 45 degrees is larger than that of 90 degrees, because the initial flame kernel is formed by the plasma jet.

Development of Mass Transfer Models for Ammonia Flux Estimation from Sewage Treatment Plants (하수처리장에서의 암모니아 플럭스 산정을 위한 물질전달모형 개발)

  • Sa, Jae-Hwan;Jeon, Eui-Chan;Jeong, Jae-Hak
    • Journal of Korean Society for Atmospheric Environment
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    • v.22 no.5
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    • pp.701-711
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    • 2006
  • Sewage treatment plants located near to large cities emit extremely higher concentration of odorous materials. This study evaluated flux profiles of ammonia emitted from the water surface of sewage treatment plants using a dynamic flux chamber. Also, an ammonia overall mass transfer coefficient and a mass transfer model was developed in order to estimate fluxes of ammonia using environment parameters and the flux from the sewage treatment plants. The developed mass transfer model was evaluated through a fitness analysis. Comparison modeled flux applying empirical overall mass transfer coefficients of ammonia and measured ammonia flux show a high linearity with 0.977. The flux ratio of 1.282 demonstrated highly statistical fitness, also. Modeled flux using the mass transfer model was compared with measured flux. In result, it indicated that empirical overall mass transfer coefficients were similar to measured flux. The mass transfer model using the empirical overall mass transfer coefficient developed in this study was proved to be an easy and effective method to make accurate and precise predictions for ammonia flux discharged from sewage treatment plants.

Waterhammer For In-line Booster Pump (직결식 펌프의 수격현상)

  • Kim, S C.;Lee, K. B.;Kim, K. Y.
    • 유체기계공업학회:학술대회논문집
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    • 2004.12a
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    • pp.208-216
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    • 2004
  • The waterhammer occured when the pumps are started or stopped for the operation or tripped due to the power failure, the hydraulic transients occur as a result of the sudden change in velocity. The field tests of the waterhammer were carried out for PanGyo booster pumping station. The PanGyo pumuing station was installed booster pump of 6 sets and in-line pump of 2 sets. The main surge suppression device was equipped with the pump control valve and the surge relief valve as auxiliary. However, the pump control valve had not early controlled in the planned closing mode, and the slamming occurred to the valve of which abruptly closed during the large reverse flow. Because the pressure wave caused by the pump failure was superposed on the slam surge, the upsurge increased so extremely that the shaft of the valve was damaged. After the addition surge suppression device was equipped with air chamber. Further more in-line pump is needed surge suppression device that the pumping station acquired the safety and reliability for the pressure surge.

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Material Trends of Nozzle Extension for Liquid Rocket Engine (액체로켓엔진 노즐확장부 소재기술 동향)

  • Lee, Keum-Oh;Ryu, Chul-Sung;Choi, Hwan-Seok
    • Current Industrial and Technological Trends in Aerospace
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    • v.9 no.1
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    • pp.139-149
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    • 2011
  • The combustion chamber and nozzle of a liquid rocket engine need thermal protection against the high temperature combustion gas. The nozzle extension of a high-altitude engine also has to be compatible with high temperature environment and several kinds of cooling methods including gas film cooling, ablative cooling and radiative cooling are used. Especially for an upper-stage nozzle extension having a large expansion ratio, the weight impact on the launcher performance is crucial and it necessitated the development of light-weight refractory material. The present survey on the nozzle extension materials employed in the liquid rocket engines of USA, Russia and European Union has revealed a trend that the heavier metals like stainless steels and titanium alloys are being substituted with light weight carbon fiber or ceramic matrix composite materials.

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Design & Development of KSLV-II Ullage Motor (KSLV-II 가속모터 설계 및 개발)

  • Oh, Jisung;Lee, Gwan Joo;Kim, Sujeong;Kim, Hanjoon;Park, Euiyong;Kwon, Hyukho;Cho, In-Hyun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.1122-1126
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    • 2017
  • KSLV-II ullage motor is a type of the separation motor of Korea Space Launch Vehicle. Simultaneously operates with the retro Motor to perform the stage separation. The internal ballistics design, application of propellant composition, and the design of the combustion chamber and the canted nozzle were performed in accordance with the target performance of the ullage motor. Ti-6Al-4V alloy was applied to the combustion as material of chamber and nozzle. The heat resistant material of the nozzle was selected to ensure the heat resistance of the propellant containing a large amount of aluminum. And the combustion performance of the ullage motor satisfying the KSLV-II requirements was secured by performing the ground combustion test.

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