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Spray characteristics of liquid-swirl/gas-jet coaxial injectors (액체스월-기체제트 동축 분사기의 분무특성)

  • Jeon, Jae-Hyoung;Hong, Moon-Guen;Kim, Jong-Gyou;Han, Yeoung-Min;Lee, Soo-Yong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.82-85
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    • 2009
  • In the development of Liquid Rocket Engine(LRE) systems, it is essential to understand the spray characteristics which influence mainly the performance and the stability of combustion. The injectors for this study have a recessed Liquid-swirl/Gas-centered jet coaxial type. For the similarity with actual conditions, the experimental conditions are calculated by using the momentum ratio as a matching parameter, and the stimulants of fuel and oxidizer are gaseous nitrogen and water respectively. The spray fields were measured by means of a photographic technique. Moreover, an effect of the momentum ratio has been investigated.

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Plasma Jet Devices for the Doping Process in Solar Cell

  • Lee, Won-Yeong;Kim, Jung-Gil;Kim, Yun-Jung;Han, Guk-Hui;Yu, Hong-Geun;Kim, Hyeon-Cheol;Jo, Gwang-Seop
    • Proceedings of the Korean Vacuum Society Conference
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    • 2013.02a
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    • pp.548-548
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    • 2013
  • 태양전지 제작에서 도핑 공정은 실리콘 웨이퍼에 불순물 원자를 주입시켜 p-n 접합을 형성시키는 과정이다. 도핑 공정은 주로 3족 혹은 5족 원소를 사용한다. 기존의 도핑 공정 장치는 소성로 및 레이저 장비를 사용하여 생산단가가 높고, 웨이퍼의 전면 도핑이 힘들다는 단점이 있다. 하지만 플라즈마 제트를 사용한 도핑장치는 저가의 장비를 개발할 수 있고, 전면 도핑이 쉽다는 장점을 가진다. 또한 도핑 농도 및 깊이 조절, 높은 농도의 도핑이 가능하다는 기존 장비의 장점을 유지한다. 플라즈마 제트를 솔라셀 웨이퍼 위에 도포된 dopant material layer에 조사하면 주로 플라즈마와 dopant간의 열적인 반응에 의하여 doping이 된다. 도핑을 위한 플라즈마 제트는 전류량의 조절 및 조사하는 양에 따라서 도핑 온도를 쉽게 조절 가능하다. 본 연구에서는 챔버 내 Ar 가스를 채운 후 플라즈마를 생성시켜 방전 특성을 조사한다. 챔버 내 가스의 압력, 전극과의 거리, 전극의 형태 등 장치의 조건을 변화시켜 특성을 확인하고, 안정적인 플라즈마의 물성을 유지하기 위한 조건을 찾는다. 또한 일반 대기압에서 가스 유량변화, 전극과의 거리, 전극의 형태 등 조건에 따른 방전 특성 및 플라즈마 방출 특성을 조사한다.

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Synthesis of Manganese Hydrogen Phosphate Hydrate by Controlled Double-jet Precipitation (더블제트 침전법에 의한 제이인산망간염 수화물의 새로운 합성 방법)

  • Kim, Won-Seok;Kang, Yong;Kim, Yeong-Cheol
    • Applied Chemistry for Engineering
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    • v.19 no.1
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    • pp.66-72
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    • 2008
  • Manganese hydrogen phosphate hydrate, $MnHPO_4{\cdot}2.25H_2O$, is a major constituent of the pre-conditioning compositions for the manganese phosphate coating treatment over carbon steel substrate. This compound is conventionally produced by the synthesis in the aqueous solution process followed by the filtration and drying processes and a series of size reduction and classification processes in dry state. However, it is evident that the conventional process is neither environment-friendly nor cost-effective. In this work, a new process principle was examined based on the controlled double-jet precipitation technology to produce the manganese chemical product of fairly uniform particle size distribution in an aqueous solution media. The effects of stabilizing agents were comparatively studied by the scanning electron microscope analysis in a uniformity point of view of the resulting particle size. Polyvinylpyrrolidone and Gum Arabic were excellent in controlling the crystal growth step, resulting in fairly uniform size distributions of the particles from the controlled double-jet process.

Characteristics and Development Trends of Heat-Resistant Composites for Flight Propulsion System (비행체 추진기관용 내열 복합재의 특성 및 개발 동향)

  • Hwang, Ki-Young;Park, Jong Kyoo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.9
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    • pp.629-641
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    • 2019
  • In order to limit the temperature rise of the structure to a certain level or less while maintaining the aerodynamic shape of solid rocket nozzle by effectively blocking a large amount of heat introduced by the combustion gas of high temperature and high pressure, the heat-resistant materials such as C/C composite having excellent ablation resistance are applied to a position in contact with the combustion gas, and the heat-insulating materials having a low thermal diffusivity are applied to the backside thereof. SiC/SiC composite, which has excellent oxidation resistance, is applied to gas turbine engines and contributes to increase engine performance due to light weight and heat-resistant improvement. Scramjet, flying at hypersonic speed, has been studying the development of C/SiC structures using the endothermic fuel as a coolant because the intake air temperature is very high. In this paper, characteristics, application examples, and development trends of various heat-resistant composites used in solid rocket nozzles, gas turbine engines, and ramjet/scramjet propulsions were discussed.

분쟁사례를 통해서 본 DC 법률문제 1

  • Son, Seung-U
    • Digital Contents
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    • no.1 s.140
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    • pp.116-121
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    • 2005
  • 인간이 자신의 사상과 감정을 표현하고 그것을 기록할 수 있는 도구 즉, 커뮤티케이션 미디어를 사용한 이래 인류가 누적해온 표현물에 접근함으로써 그것을 이용하고 향유하는 것이 인간 모두가 누려야 할 보편적인 권리, 즉 인강의 기본권에 속하는 것인가? 아니면 특정의 조건을 갖춘 특히 그것을 이용할 지불능력이 있는 사람에게만 주어진 특권적인 것일까? 표현물들은 어떻게 하면 보다 가치있는 것들이 더 많이 생산되고 이용되 사회 구성원들의 표현을 더욱 풍요롭게 할 수 있을 것인가? 표현의 생산과 이용이라는 순환고리에서 과연 어느쪽에 무게 중심을 두어야 사회가 표현의 풍요를 누릴수 있을 것인가? 이러한 논란은 취근 문제된 제트스트림(Z!Stream)분쟁에서도 여실히 나타났다. 이러한 분쟁사례를 바탕으로 디지털콘텐츠 관련 법적 문제를 살펴보자

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Application Study on FMEA(Failure Mode and Effect Analysis) for Waterjet-lifter of Deep-Sea Manganese Nodule Miner (심해저 망간단괴 집광시스템의 물제트부양장치에 대한 FMEA 적용 연구)

  • Choi, Jong-Su;Hong, Sup;Lee, Tae-Hee;Kim, Hyung-Woo;Yeu, Tae-Kyeong
    • Journal of Ocean Engineering and Technology
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    • v.23 no.6
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    • pp.32-38
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    • 2009
  • An FMEA for the waterjet-lifter of a DSNM is performed to prevent the occurrence of device failure. A waterjet-lifter raises and transports manganese nodules from the deep-sea floor up to a somewhat elevated place, from which a pin-scraper transports the lifted nodules to the inner space of the DSNM. A concept design for a device using the axiomatic design methodology is shown as the mapping between the functional domain and physical domain. The FMEA for a DSNM is introduced briefly and the rating criteria of severity, occurrence, and detection for the DSNM are defined. The FMEA of the functional requirements of a DSNM device is accomplished. Three kinds of failure modes, as well as their effects and causes, are predicted. Current design control methods for detecting potential failures, such as physical or computational experiments, design confirmation, and mathematical calculation, are described and the recommended actions for several significant causes are suggested.

Development of a 2-fluid Jet Mixer for Preventing the Sedimentation in Livestock Liquid Manure Storage Tank (가축분뇨액비저장조 침전물 퇴적 방지를 위한 2류체 제트노즐식 교반장치 개발에 관한 연구)

  • Yu, B.K.;Hong, J.T.;Kim, H.J.;Kweon, J.K.;Oh, K.Y.;Park, B.K.
    • Journal of Animal Environmental Science
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    • v.18 no.3
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    • pp.207-220
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    • 2012
  • There are around 7,500 manure tanks to treat the manures from pigs in Korea. In the tank, there are too much sediments deposited on the base and wall, which causes low efficiency of stock capacity and manure fermentation. In order to minimize sediments and to ferment manure effectively, we developed a 2-fluid jet mixer for mixing sediments in liquid livestock manure tank. For developing the prototype, we tested a factorial experimental system with various nozzles, and simulated CFD models with two kinds of nozzle arrangement. From the results of factorial experiment and CFD simulation, we concluded the dia. ratio of primary : secondary nozzle should be 1:2 and the nozzles should be arranged at the same distances toward to the circumferential direction. With this results, we manufactured a 2-fluid jet mixer which is consists of four 2-phase nozzles, centrifugal slurry pump and root's type air blower. And, we carried out the performance test of the prototype in the round shaped liquid manure tank in the farm. The performance test results showed that the uniformity of TS (Total Solid) and VS (Volatile Solid) was raised from 21.3 g/L, 13.3 g/L In steady state to TS and VS to 23.0 g/L, 14.1 g/L in the mixing operation. Therefore, we could conclude that the prototype of 2-fluid mixer could make the solid material which could be sediments in the tank not to be deposited in the tank and to be contacted to air bubbles which could enhance the efficiency of the fermentation of livestock manure.

A Study of Spray Characteristics for the Slinger Injector System of Micro Turbo Jet Engine (초소형 터보제트엔진 슬링거 인젝터의 분무특성)

  • Choi, Hyun-Kyung;Choi, Seong-Man;Lee, Dong-Hun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.354-358
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    • 2007
  • An experimental study was performed to understand spray characteristics of the slinger injector. system for the micro turbojet engine. In this fuel injection system, fuel is sprayed and atomized in the combustor by centrifugal forces of engine shaft. This experimental apparatus consist of a high speed rotating Spindle, slinger injector, pressure tank and acrylic case. The droplet size and velocity were measured by PDPA(Phase Doppler Particle Analyzer) and spray was visualized by using Nd-Yag laser-based flash photography. From the test results, the droplet size(SMD) is largely affected to rotational speed, mass flow rate and the number of injection orifice. From the this experimental study, we could understand the spray characteristics of the slinger injection system and obtain the optimum shape of the slinger injector nozzle which is suitable for the micro turbojet engine.

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Spray Characteristics of Jet According to Position of Injector Hole in Cross Flow (횡단유동내 인젝터 홀의 위치에 따른 제트의 분무 특성)

  • Choi, Myeung Hwan;Shin, DongSoo;Radhakrishna, Kanmaniraja;Son, Min;Koo, jaye
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.905-911
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    • 2017
  • Effects of injector position and momentum flux ratio on a vertical jet in a cross flow field were studied qualitatively and shown by using air and water. The experiment was carried out by fixing the momentum flux ratio and varying the position of the injector hole. Conversely, the injector hole position was fixed and the momentum flux ratio was varied. Image visualization was performed by a Shadowgraph technique using a high speed camera. The visualized images were compared for finding differences in spraying through Density Gradient Magnitude Image. It is observed that as the x/d of the apparatus increased the jet break up height decreases and the spray angle also decreases. When x/d is 0, the spray reaches the floor and ceiling at any momentum flux ratio.

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Cooling Performance of Air/Water Mist Jet Impinging for a Rapid Thermal Annealing System (급속 열처리 시스템을 위한 물/공기 액적류 충돌 제트의 냉각 특성에 관한 연구)

  • Lee, Jun Kyoung
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.14 no.5
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    • pp.68-74
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    • 2015
  • In the present work, a series of numerical calculations have been conducted on the cooling of a hot surface using an air/water mist jet. In some cooling processes, such as in the glass-tempering process, direct contact between the cold water drops and the hot surface should be avoided, because this may cause surface cracks due to the sharp temperature gradients. Thus, the main focus of this study is finding the appropriate operating conditions for maximum cooling without direct contact between the drops and the surface. A series of numerical experiments have been performed, and, at the same time, those results were compared with those of the previous experiments for verification purposes. The effects of droplet impinging velocity, hot plate temperature, and liquid loading ratio for mono-dispersed drops of various sizes were studied in detail.