• Title/Summary/Keyword: Evaporation efficiency

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Effects of Laser Parameters and Workpiece Conditions on Cutting Characteristics of Solid Wood and Wood-based Panel(II) - Specific Cutting Energy and Surface Qualities - (레이저변수(變數)와 피삭재조건(被削材條件)이 목재(木材) 및 목질(木質)보드의 절삭특성(切削特性)에 미치는 영향(影響)(II) - 비절삭(比切削)에너지와 절삭면(切削面)의 품질(品質) -)

  • Sim, Jae-Hyeon;Jung, Hee-Suk
    • Journal of the Korean Wood Science and Technology
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    • v.26 no.1
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    • pp.38-50
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    • 1998
  • Laser cutting tests were conducted to investigate the laser cutting characteristics of solid woods such as 25mm-thick white oak(Quercus acutissima) and maple(Acer mono), and wood-based panels such as 15mm-thick medium density fiberboard and particleboard. Test variables were laser power, cutting speed, grain direction, and moisture content. Specific cutting energy was measured and the qualities of cut surface were estimated in constant laser power. Specific cutting energy of white oak was larger than that of maple, and specific cutting energy of medium density fiberboard was smaller than that of particleboard. For both white oak and maple, specific cutting energy of green wood was smaller than that of air-dried wood because weight loss of moisture evaporation in green wood was larger than that in air-dried wood. In laser-cut surface, wood cells were not deformed and damaged, but in circular saw-cut surface fibers were pushed out and cut, and wood cells were deformed severely. However, mechanical surface roughness of saw-cut surface was smoother than that of laser-cut surface because of the existence of undeformed cell cavity in laser-cut surface.

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Spray Characteristics of a Liquid-fueled Ramjet Engine under High Pressure Air Condition (고압 유동조건에서의 액체 램제트 엔진의 분무특성)

  • Youn, H.J.;Lee, C.W.
    • Journal of ILASS-Korea
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    • v.9 no.2
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    • pp.34-40
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    • 2004
  • In a liquid-fueled ramjet engine, the insufficient mixing and evaporation result in the low combustion efficiency and combustion instability. Improving its characteristics and devising a means of fuel droplets with air may compensate these disadvantages of liquid fuel ramjet engine. The jet penetrations of various fuel injectors were measured to investigate the spray characteristics of a liquid-fueled ramjet engine under high pressure air-stream conditions. The penetrations in high pressure conditions are smaller than the values calculated from Inamura's or Lee's equations, and the jet penetrations in the high pressure conditions have a similar tendency. In the dual orifice injectors, the jet penetrations of rare orifice is rapidly increased due to the reduction of the drag, which is created by the jet column of front orifice. The jet penetration of rare orifice is increased because of the drag reduction created by the jet column of the front orifice. Because of the drag reduction formed by the column of jet, the jet penetration in the rear orifice of dual orifice injector is much larger than the jet penetrations of single orifice injector. As the distances of the orifice are increased, the jet penetrations of the rear orifice decrease.

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Development of environmentally sound technology for the wafer drying system (반도체 제조산업중 웨이퍼 건조공정의 청정기술 적용을 위한 연구)

  • Chang, In-Soung;Kim, Jae-Hyung
    • Clean Technology
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    • v.4 no.1
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    • pp.68-75
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    • 1998
  • An innovative wafer drying system was developed using Isopropyl alcohol (IPA) and nitrogen carrier gas in order to replace the commercial conventional drying system which was a non-environmentally friendly system. This system was designed as following ; the IPA evaporation chamber and the process chamber were separated to increase drying efficiency, and the carrier gas with the IPA vapor was delivered into the process chamber. It was investigated that the IPA concentration was the most important factor to operate the system. The optimum concentration was found to be 2.4 ml IPA/N2 1. In addition, the optimum flow rate of the nitrogen gas were maintained more than 60 l/min.

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Phagocytic Uptake of Surface modified PLGA Microspheres Using Dendritic Cell

  • Kim, Ji-Seon;Lee, Young-Sung;Lee, Jung-Gil;Park, Jeong-Sook;Lee, Jong-Kil;Chung, Youn-Bok;Han, Kun
    • Journal of Pharmaceutical Investigation
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    • v.41 no.3
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    • pp.185-190
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    • 2011
  • The purpose of this study was to evaluate the phagocytic uptake of surface modified PLGA microspheres containing ovalbumin (OVA) into dendritic cell. In order to find the most suitable formulation for targeted delivery to antigen presenting cells (APC), OVA was encapsulated by a double emulsion solvent evaporation method with three PLGA microspheres (PLGA 50:50, PLGA 75:25 and PLGA 85:15) and two surface modified microspheres by chitosan and sodium dodecyl sulfate (SDS). Physicochemical properties were evaluated in terms of size, zeta potential, encapsulation efficiency, different scanning calorimeter (DSC), x-ray diffraction, morphology, and OVA release test from microspheres. Phagocytic activity was estimated using dendritic cells and analyzed by fluorescence activated cell sorter (FACS). The result showed that zeta potential of PLGA particles was changed to positive by the chitosan modification. The release profile of chitosan modified PLGA microspheres exhibited sustained release after initial burst. The chitosan modified microspheres had higher phagocytic uptake than the other microspheres. Such physicochemical properties and phagocytic uptake studies lead us to conclude that chitosan modified microspheres is more suitable formulation for the targeted delivery of antigens to APC compared with the other microspheres.

The Combustion and Emission Characteristics with Increased Fuel Injection Pressure in a Gasoline Direct Injection Engine (가솔린 직접 분사식 엔진에서 연료 분사 압력 증가에 따른 연소 및 배기 배출물 특성)

  • Lee, Junsun;Lee, Yonggyu
    • Journal of ILASS-Korea
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    • v.22 no.1
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    • pp.1-7
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    • 2017
  • Recently, Performance and fuel efficiency of gasoline engines have been improved by adopting direct injection (DI) system instead of port fuel injection (PFI) system. However, injecting gasoline fuel directly into the cylinder significantly reduces the time available for mixing and evaporation. Consequently, particulate matters(PM) emissions increase. Moreover, as the emission regulations are getting more stringent, not only the mass but also the total number of PM should be reduced to satisfy the Euro VI regulations. Increasing the fuel injection pressure is one of the methods to meet this challenge. In this study, the effects of increased fuel injection pressures on combustion and emission characteristics were experimentally examined at several part load conditions in a 1.6 liter commercial gasoline direct injection engine. The main combustion durations decreased about $2{\sim}3^{\circ}$ in crank angle base by increasing the fuel injection pressure due to enhanced air-fuel mixing characteristics. The exhaust emissions and number concentration distributions of PM with particle sizes were also compared. Due to enhanced combustion characteristics, THC emissions decreased, whereas NOx emissions increased. Also, the number concentrations of PM, larger than 10 nm, also significantly decreased.

Electrical Properties of Rosen Type piezoelectric transformers using Low Temperature Sintering PMN-PNN-PZT ceramics (저온소결 PMN-PNN-PZT계 세라믹스를 이용한 Rosen형 압전변압기의 전기적 특성)

  • Lee, Sang-Ho;Yoo, Ju-Hyun;Kim, In-Sung;Song, Jae-Sung
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2008.06a
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    • pp.53-53
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    • 2008
  • Piezoelectric transformers have been widely used such as DC-DC convertor, invertor, Ballast, etc. Because, the y have some merits compared with electro-magnetic transformers such as step-up ratio, high efficiency, small size and lg hit weight, etc. Piezoelectric transformer require high electromechanical coupling factor kp in order to induce a large out put power in proportional to applied electric field. And also, high mechanical quality factor Qm is required to prevent mechanical loss and heat generation. In general, PZT system ceramics should be sintered at high temperatures between 1200 and $1300^{\circ}C$ in order to obtain complete densification. Accordingly, environmental pollution due to its PbO evaporation. Hence, to reduce its sintering temperature, various kinds of material processing methods such as hot pressing, high energy mill, liquid phase sintering, and using ultra fine powder have been performed. Among these methods, liquid phase sintering is basically an effective method for aiding densification at low temperature. In this study, In order to comparis on low temperature sintering and solid state sintering piezoelectric transformers, rosen type transformers were fabricated u sing two PZT ceramics compositions and their electrical properties were investigated.

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Fabrication and Characterization of Red Emitting OLEDs using the Alg3:Rubrene-GDI4234 Phosphor System (Alg3:Rubrene-GDI4234 형광 시스템을 이용한 적색 OLED의 제작과 특성 평가)

  • Jang Ji-Geun
    • Journal of the Korean Institute of Electrical and Electronic Material Engineers
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    • v.19 no.5
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    • pp.437-441
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    • 2006
  • The red emitting OLEDs using $Alq_3$:Rubrene-GDI4234 phosphors have been fabricated and characterized . In the device fabrication, 2- TNATA [4,4',4' - tris (2- naphthylphenyl - phenylamino ) - tripheny lamine] as the hole injection material and NPB [N,N'-bis (1-naphthyl)-N,N'-diphenyl-1,1'-biphenyl-4,4'-diamine] as the hole transport material were deposited on the ITO(indium tin oxide)/glass substrate by vacuum evaporation. And then, red color emissive layer was deposited using $Alq_3$ as the host material and Rubrene(5,6,11,12-tetraphenylnaphthacene)-GDI4234 as the dopants. finally, small molecule OLEDs with structure of ITO/2-TNATA/NPB/$Alq_3$:Rubrene-GDI4234/$Alq_3$/LiF/Al were obtained by in-situ deposition of $Alq_3$, LiF and Al as the electron transport material, electron injection material and cathode, respectively. Red OLEDs fabricated in our experiments showed the color coordinate of CIE(0.65, 0.35) and the maximum power efficiency of 2.1 lm/W at 7 V with the peak emission wavelength of 632 nm.

Energy Band Schemes in Organic Electroluminescent Devices Using Terbium Complexes Prepared by Vacuum Evaporation Method (진공 증착법에 의한 Terbium Comp1exes를 이용한 유기 전기 발광 소자의 에너지 밴드에 관한 연구)

  • 표상우;김옥병;이한성;최돈수;이승희
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 1999.05a
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    • pp.582-588
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    • 1999
  • 정보화 사회의 발전과 함께 멀티미디어에 대한 관심이 집중되고 있으며, 점유 공간이 작고 가벼우며 대면적이 가능한 정보 표시 디스플레이에 대한 기술은 고부가가치 산업으로 인식되어 지고 있다. 이러한 정보 표시 디스플레이들 중, 전기 발광 소자 (Electroluminescence Display : ELD), 액정 표시 디스플레이 (Liquid Crystal Display LCD), 플라즈마 디스플레이 (Plasma Display Panel) 등의 대한 연구가 세계적으로 매우 활발하게 진행되고 있다. 본 연구에서는 란탄 계열의 금속 착 화합물인 Tb(ACAC)$_3$(Phen)과 Tb(ACAC)$_3$(Phen-Cl)를 이용해 다비이스를 제작한후 광학적 및 전기적 특성을 조사하였다. 또한 luminous efficiency와 cyclic voltametric 방법을 이용해 에너지 밴드로 두 발광 물질인 Tb(ACAC)$_3$(Phen)과 Tb(ACAC)$_3$(Phen-Cl)을 비교.분석하였다. 본 연구의 디바이스 구조를 보면 anode/hole transporting layer (HTL)/emitting material layer (EML)/electron transporting layer (ETL)/cathode와 같고 ETL를 aluminum-tris- (8-hydroxyquinoline) (Alq$_3$)와 bis(10-hydroxybenzo(h)quinolinato)beryllium (Bebq$_2$)를 사용하였으며 HTL 로 N,N'-diphenyl-N,N'-bis(3-methylphenyl)-1,1'-biphenyl-4,4'-diamine (TPD)를 사용하였다.

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Spray Characteristics of a Liquid-fueled Ramjet Engine under High Pressure Air-stream Conditions

  • Lee, Choong-Won;Youn, Hyun-Jin;Lee, Tae-Hee;Lee, Geun-sun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.03a
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    • pp.749-752
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    • 2004
  • In a liquid-fueled ramjet engine, the insufficient mixing and evaporation result in the low combustion efficiency and combustion instability. Improving its spray characteristics and devising a means of mixing fuel droplets with air may compensate these disadvantages of liquid fuel ramjet engine. The jet penetrations of various fuel injectors were measured to investigate the spray characteristics of a liquid-fueled ramjet engine under high pressure air-stream conditions. The penetrations in high pressure conditions are smaller than the values calculated from Inamura's or Lee's equations, and, in the high pressure conditions, the jet penetrations are similar each other. In the dual hole injectors, the jet penetrations of rear orifice is rapidly increased due to the reduction of the drag, which is created by the jet column of front orifice. The jet penetration of rear orifice is increased because of the drag reduction created by the jet column of the front orifice. And, because of the drag reduction formed by the column of jet, the jet penetration in the rear orifice of dual hole injector is much larger than the jet penetration of single hole injector. As the distances of the orifice are increased, the jet penetrations of the rear orifice decrease.

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Prediction of Erosion Rate in Passages of a Turbine Cascade with Two-Phase flow (터빈익렬 유로에서 2상 유동에 따른 삭마량 예측)

  • Yu, Man Sun;Kim, Wan Sik;Cho, Hyung Hee
    • 유체기계공업학회:학술대회논문집
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    • 1999.12a
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    • pp.301-308
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    • 1999
  • The present study investigates numerically particle laden flow through compressor cascades and a rocket nozzle. Engines are affected by various particles which are suspending in the atmosphere. Especially in the case of aircraft aviating in volcanic, industrial and desert region including many particles, each components of engine system are damaged severely. That damage modes are erosion of compressor blading and rotor path components, partial or total blockage of cooling passage and engine control system degradation. Numerical prediction and experimental data, erosion rates are predicted for two materials - ceramic, soft metal - on compressor blade surface. Aluminum oxide ($Al_2O_3$) Particles included in solid rocket propelant make ablative the rocket motor nozzle and imped the expansion processes of propulsion. By the definition of particle deposition efficiency, characteristics of particles impaction are considered quantitatively Stoke number is defined over the various particle sizes and particle trajectories are treated by Lagrangian approach. Particle stability is considered by definition of Weber number in rocket nozzle and particle breakup and evaporation is simulated in a rocket nozzle.

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