• 제목/요약/키워드: Wall-injection

검색결과 446건 처리시간 0.023초

마이크로 패턴을 가진 초박육 사출성형의 성형성 개선 (Improvement of Moldability for Ultra Thin-Wall Molding with Micro-Patterns)

  • 윤재호;박근;권오경
    • 대한기계학회논문집A
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    • 제31권5호
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    • pp.556-561
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    • 2007
  • The rapid thermal response(RTR) molding is a novel process developed to raise the temperature of mold surface rapidly in the injection stage and then cool rapidly to the ejection temperature by air or water. The objectives of this paper are to investigate the effect of mold temperature, pressure and thickness of micro pattern molding and to provide a optimization of RTR injection molding for micro pattern from Moldflow simulation. Optimal minimum temperature and pressure was found without shortcut according to thickness. Filling percentage was influenced by glass transition temperature with the kinds of resin. Optimal temperature is slightly higher than glass transition temperature irrespectively of pressure, thickness, the kinds of resin in the micro pattern molding.

희박연소를 위한 혼합기의 성층급기와 유동에 관한 연구 (A Study on the Effects of Induced Mixture Flows and the Stratified Charge for a Lean Burn)

  • 전대수;이태원;윤수한;하종률
    • 한국자동차공학회논문집
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    • 제8권1호
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    • pp.1-9
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    • 2000
  • In the present study, the IDI-type constant volume chamber, which utilizes the indirect injection stratified charge method, is used to solve several problems including misfires and cycle-variations caused by unstable initial ignitions. A subchamber has been used to make an ignitable mixture under the low mean equivalence ratio. After burned in the subchamber, the flame jet getting through the passage hode enters the main chamber and burns the lean charge. There are many factors which affect the combustion characteristics of the indirect injection stratified engine. The passage hole angle is the most important since it determines the direction of flame flows into the main chamber. In the present study, we measured the combustion pressure, and the wall temperature, and computed the heat flux through the cylinder wall in order to understand the combustion characteristics depending on passage hole angle and the equivalence ratio.

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초음속 유동내 원형 2차분사 제트 주변에서의 표면 열전달 현상 연구 (Study on the Surface Heat Transfer Around a Circular Secondary Jet in the Supersonic Flow)

  • 이종주;유만선;조형희
    • 한국추진공학회지
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    • 제11권2호
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    • pp.47-53
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    • 2007
  • 본 논문에서는 초음속유동장 내에 분사된 2차 분사유동과 주유동의 상호작용에 의한 2차 분사노즐 주변에서의 열전달 현상을 관찰하였다. 벽면에는 등열유속조건을 주었다. 제트 자유유동간 운동량비(Jet to Freestream Momentum Ratio, J)에 따라 2차 분사를 초음속 유동장에 분사시켰으며, 적외선 카메라를 이용하여 2차 분사노즐 주변 벽면온도를 측정하였고, 이를 통하여 대류 열전달계수를 제시하였다.

미소중력 환경내의 벽면 근방 확산 화염 특성에 관한 수치 해석 (Numerical Simulation on Characteristics of Laminar Diffusion Flame Placed Near Wall in Microgravity Environment)

  • 최재혁;후지타 오사무
    • Journal of Advanced Marine Engineering and Technology
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    • 제30권1호
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    • pp.140-149
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    • 2006
  • Characteristics of a laminar diffusion flame placed near wall in microgravity have been numerically analyzed in a two-dimension. The fuel for the flame is $C_2H_4$. The flame is initiated by imposing a high temperature ignition source. The flow field, temperature field, and flame shape in microgravity diffusion flame are detailed. Especially, effects of surrounding air velocity and fuel injection velocity on the microgravity diffusion flame have been discussed accounting for standoff distance. And, the effect of curvature rate has been also studied. The results showed that velocities in a diffusion flame were overshoot because of volumetric expansion and distribution of temperature showed regularity by free-buoyancy This means that the diffusion flame in microgravity is very stable, while the flame in normal gravity is not regular and unstable due to buoyancy. Standoff distance decreases with increase in surrounding air velocity and with decrease in fuel injection velocity. With increasing curvature rate, the position of reaction rate moves away the wall.

충돌벽면이 직분식 LPG의 분무 및 연소 특성에 미치는 영향에 관한 실험 연구 (A Experimental Study on the Effects of the Impingement-wall on the Spray and Combustion Characteristics of Direct-Injection LPG)

  • 황성일;정성식;염정국
    • 동력기계공학회지
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    • 제19권2호
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    • pp.49-56
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    • 2015
  • As an alternative fuel that can be used in SI engine, LPG is one of clean fuels with larger H/C ratio compared to gasoline, low $CO_2$ emission, and small amount of pollutants such as sulfur compounds. When LPG is used in spark ignition engine, volumetric efficiency of the engine can be improved and pumping loss can be reduced by performing direct injection into the combustion chamber instead of port fuel injection. LPG-DI engine allows for lean combustion and stratified combustion under low load. In case of stratified combustion, air fuel ratio can be greatly increased compared to theoretic mixture ratio combustion. Improved thermal efficiency of the engine and reduced pumping loss can be expected from stratified combustion. Accordingly in this study, an experimental apparatus for visualization was designed and manufactured to study the combustion process of LPG after injection and ignition, intended to examine ignition probability and combustion characteristics of spark ignition direct injection(SIDI) LPG fuel. Ambient pressure, ambient temperature and fuel injection pressure were found as important variables that affect ignition probability and flame propagation characteristics of LPG-air mixture. Also, it was verified that the injected LPG fuel can be directly ignited by spark plug under appropriate ambient conditions.

2차 분사의 위치 변화에 따른 로켓노즐 출구에서의 추력 분포 변화 (The Variation of Thrust Distribution of the Rocket Nozzle Exit Plane with the Various Position of Secondary Injection)

  • 김성준;이진영;박명호
    • 산업기술연구
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    • 제20권B호
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    • pp.45-53
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    • 2000
  • A numerical study is done on the thrust vector control using gaseous secondary injection in the rocket nozzle. A commercial code, PHOENICS, is used to simulate the rocket nozzle flow. A $45^{\circ}-15^{\circ}$ conical nozzle is adopted to do numerical experiments. The flow in a rocket nozzle is assumed a steady, compressible, viscous flow. The exhaust gas of the rocket motor is used as an injectant to control the thrust vector of rocket at the constant rate of secondary injection flow. The injection location which is on the wall of rocket is chosen as a primary numerical variable. Computational results say that if the injection position is too close to nozzle throat, the reflected shock occurs. On the other hand, the more mass flow rate of injection is needed to get enough side thrust when the injection position is moved too far from the throat.

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초정밀 박육 플라스틱 제품 성형기술에 관한 연구 (A study on the injection molding technology for thin wall plastic part)

  • 허영무;신광호
    • Design & Manufacturing
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    • 제10권2호
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    • pp.50-54
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    • 2016
  • In the semiconductor industry the final products were checked for several environments before sell the products. The burning test of memory and chip was implemented in reliability for all of parts. The memory and chip were developed to high density memory and high performance chip, so circuit design was also high integrated and the test bed was needed to be thin and fine pitch socket. LGA(Land Grid Array) IC socket with thin wall thickness was designed to satisfy this requirement. The LGA IC socket plastic part was manufacture by injection molding process, it was needed accuracy, stiffness and suit resin with high flowability. In this study, injection molding process analysis was executed for 2 and 4 cavities moldings with runner, gate and sprue. The warpage analysis was also implemented for further gate removal process. Through the analyses the total deformations of the moldings were predicted within maximum 0.05mm deformation. Finally in consideration of these results, 2 and 4 cavities molds were designed and made and tested in injection molding process.

주입 위치에 따른 기포와 상변화물질의 유동 상호 작용에 관한 연구 (Study on Flow Interaction between Bubble and Phase Change Material according to Injection Location)

  • 김민혁;지윤영;손동기;고한서
    • 한국가시화정보학회지
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    • 제21권3호
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    • pp.75-84
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    • 2023
  • In this study, we conducted analysis of bubble dynamics and flow of liquid phase change material(PCM) using shadowgraphy and particle image velocimetry(PIV). Characteristics of internal flow varied depending on locations of injection when solid PCM was liquefied from heated vertical wall. When bubbles rose immediately, they exhibited elliptical shape and zigzag trajectory. In contrast, when bubbles rose after merging at the bottom of solid PCM, with equivalent diameter for the inter-wall distance of 0.64 or greater, they showed a jellyfish shape and strong rocking behavior. It was observed by the PIV that the small ellipse bubbles made most strong flow inside the liquid PCM. Furthermore, the flow velocity was highest in the case of front injection, as the directions of temperature gradients and bubble-driven flow were aligned. The results underscore the significant influence of injection location on various characteristics, including bubble size, shape, rising path of bubbles, and internal flow.

폴리머 수용액 주입에 의한 난류마찰저항 감소에 대한 실험 연구 (Experimental Study on Frictional Drag Reduction of Turbulent Flow by Polymer Solution Injection)

  • 김형태;김덕수;김우전
    • 대한조선학회논문집
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    • 제40권3호
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    • pp.9-15
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    • 2003
  • An experimental study has been carried out as a basic research for development of the friction drag reduction technology for ships by polymer injection. Experimental apparatus and procedures have been devised and prepared to measure the changes of the wall friction with injection of a polymer solution and basic experimental data on the friction drag reduction are obtained for a turbulent fiat-plate boundary layer and fully-developed channel flows. Variations of the friction drag reduction with some important parameters of polymer injection, such as the concentration of polymer solution, its injection flow rate and the measuring position downstream from the injection slot, are also investigated. Important experimental data and results obtained in the present study are presented. The amount of friction drag reduction up to 50% is observed.

Study on Effects of Pressure Ratio on the Wall-impingement Spray Characteristics of Nitrogen Gas using CNG Injector

  • Pham, Quangkhai;Chang, Mengzhao;Choi, Byungchul;Park, Suhan
    • 한국분무공학회지
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    • 제27권1호
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    • pp.1-10
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    • 2022
  • In this study, an experimental investigation on the effects of the pressure ratio on the wall-impingement spray characteristics of nitrogen gas using a compressed natural gas (CNG) injector was conducted. The transient development of the impingement spray was recorded by a high speed camera with Z-type Schlieren visualization method. The spray behavior under various pressure ratio conditions were analyzed. The experimental results showed that the pressure ratio has positive effect on the development of spray wall-impingement. The effects of the above factor were evaluated in a constant volume chamber at atmospheric conditions. The data from test showed that, with the increase of the pressure ratio, the spray tip penetration (STP) quickly increases before the impingement and gradually increases after the impingement. Additionally, the spray velocity first increases and then sharply decreases on regardless of the injection pressure level. As the spray spreading angle increases, spray area and volume increases rapidly with the increase in STP at the beginning of injection, and finally entered a stable range, has a great correlation with the increase of pressure ratios.