• Title/Summary/Keyword: 분무 평균 속도

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Spray Characteristics of Spray Nozzles Used for Greenhouse Cooling (온실 냉방용 분무노즐의 분무 특성)

  • 서원명;이종열;윤용철
    • Journal of Bio-Environment Control
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    • v.7 no.4
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    • pp.298-310
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    • 1998
  • This research was carried out to find out spray characteristics of 3 types of spray nozzle to be used for greenhouse cooling. Following results were obtained from this experimental study. Water amounts sprayed with each nozzle were increased with the spraying pressure. However the increment of sprayed amount with the increase of spraying pressure were not consistent regardless of nozzle types. For the whole tested spraying pressures of nozzle-type I, II, III, the minimum droplet sizes were about 1.7~2.5$\mu$m, 1.7~2.2$\mu$m and 1.7~2.2$\mu$m, respectively, and the maximum droplet sizes were about 44~60$\mu$m, 52~71$\mu$m and 45~61$\mu$m, respectively, and the average droplet sizes were about 23~38$\mu$m, 19~24$\mu$m and 17~25$\mu$m, respectively The most appropriate spraying pressures of nozzle-type I, II, III were analyzed to be 70kgf/$\textrm{cm}^2$, 30kgf/$\textrm{cm}^2$ and 30kgf/$\textrm{cm}^2$, respectively, and their sprayed amounts were about 124mL/min, 103mL/min and 84mL/min, respectively, and average droplet sizes were 22.6$\mu$m, 21.8$\mu$m and 20.6$\mu$m, respectively. Also, with the order of nozzle-type I, II, III, droplet size distributions less than 30$\mu$m were 95.4%, 85.7% and 79.0%, respectively, and the distributions larger than 40$\mu$m were 0.2%, 1.28% and 1.67%, respectively. However most all of the droplet size were less than 50$\mu$m.

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Spray Characteristics of Fuel Injector in DI Diesel Engine (직접 분사식 디젤 기관 인젝터의 연료 분무 특성)

  • 이창식;김민규;전원식;진다시앙
    • Transactions of the Korean Society of Automotive Engineers
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    • v.9 no.5
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    • pp.75-81
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    • 2001
  • This paper presents the atomization characteristics of single hole injector in the direct injection type diesel engine. The spray characteristics of fuel injector such as the droplet size and velocity were measured by phase Doppler particle analyzer. In this paper, the atomization characteristics of fuel spray are investigated for the experimental analysis of the measuring data by the results of mean diameter and mean velocity of droplet. The effect of fuel injection pressure on the droplet size shows that the higher injection pressure results in the decrease of mean droplet diameter in the fuel spray. The minimum size of fuel spray droplet appears on the location of 40mm axial distance from nozzle exit of diesel injector. Based on the experimental results, the correlation between the droplet diameter and mean velocity of the diesel spray due to the change of axial and radial distance from the nozzle tip were investigated.

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Spray Angle and Break-up Characteristics of Supersonic Liquid Jets by an Impinging Methods with High Speed Projectile (초고속 발사체의 액체 저장부 충돌에 의한 초음속 액체 제트의 분무 속도 및 분열 특성)

  • Lee, In-Chul;Shin, Jeung-Hwan;Kim, Heuy-Dong;Koo, Ja-Ye
    • Journal of the Korean Society of Visualization
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    • v.9 no.1
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    • pp.55-60
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    • 2011
  • Pulsed supersonic liquid jets injected into an ambient air are empirically studied by using a high pressure ballistic range system. Ballistic range systems which are configured with high-pressure tube, pump tube, launch tube and liquid storage nozzle. Experimental studies are conducted to use with various impact nozzle geometry. Supersonic liquid jets are generated by an impact of high speed of the projectile. High speed liquid jets are injected with M = 3.2 which pressure is 1.19 GPa. Multiple jets which accompany with shock wave and pressure wave in front of the jet were observed. The shock-wave affects significantly atomization process for each spray droplets. As decreasing orifice diameter, the averaged SMD of spray jets had the decreasing tendency.

Controlled synthesis of silica nanoparticles by a two-fluid nozzle flame reactor (이류체 노즐형 화염 반응기에 의한 실리카 나노분말 제조)

  • Chang, Han-Kwon;Jang, Hee-Dong;Chang, Won-Chul
    • Proceedings of the Korean Institute of Resources Recycling Conference
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    • 2005.10a
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    • pp.308-313
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    • 2005
  • 실리콘 잉고트의 절단공정에서 발생하는 폐실리콘 슬러지는 실리콘과 실리콘카바이드 등의 유가자원이 함유되어 있으며, 이 중 실리콘 분말은 실리콘 화합물인 알콕시실란 등을 제조하는데 원료로 사용이 가능하다. 본 연구에서는 폐실리콘 슬러지로부터 분리, 합성된 사에 톡시실란(TEOS)을 원료로 이용하여 실리카 나노분말을 합성하였다. TEOS 원료물질을 외부 혼합형 이류체 노즐을 이용하여 미세액적으로 분무하고 화염 속으로 도입시키고 화염열분해 반응을 진행시켜 실리카 나노분말을 합성하였다. 합성된 실리카 나노입자의 특성은 투과형 전자현미경 및 BET에 의하여 입자형상 및 평균 입자크기가 분석되었다. 주요 공정변수인 분산공기의 압력, 반응가스의 조성을 변화시켜 실험한 결과 평균크기가 $9{\sim}68nm$인 실리카 나노분말을 제조하였다.

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Preparation of Nano-Sized Indium Oxide Powder by Spray Pyrolysis Process (噴霧熱分解 工程에 의한 인듐 酸化物 나노 粉末 製造)

  • Yu, Jae-Keun;Park, Si-Hyun;Sohn, Jin-Gun
    • Resources Recycling
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    • v.13 no.6
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    • pp.16-25
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    • 2004
  • In this study, nano-sized indium oxide powder with the average particle size below 100 nm is prepared from the indium chloride solution by the spray pyrolysis process. The effects of the concentration of raw material solution, the nozzle tip size and the air pressure on the properties of powder were studied. As the indium concentration of the raw material solution increased from 40 g/l to 350 g/l, the average particle size of the powder gradually increased from 20 nm to 60 nm, yet the particle size distribution appeared more irregular, the intensity of a XRD peak increased and specific surface area decreased. As the nozzle tip size increased from 1 nm to 5 nm, the average particle size of the powder increased from 40 nm to 100 nm, the particle size distribution was much more irregular, the intensity of a XRD peak increased and specific surface area decreased. As the air pressure increased from 0.1 kg/cm$^2$ to 0.5 kg/cm$^2$, the average particle size of the powder varies slightly upto 90~100 nm. As the air pressure increased from 1 kg/cm$^2$ to 3 kg/cm$^2$, the average particle size decreased upto 50~60 nm, the intensity of a XRD peak decreased and the specific surface area increased.

A Study of Spray Characteristic with Orifice Diameter for Single Column Rotating Fuel Nozzle (단열식 회전연료 노즐의 오리피스 직경에 따른 분무특성 연구)

  • Jang, Seong-Ho;Choi, Seong-Man
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.253-256
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    • 2009
  • In the micro turbojet engine less than 350kw power class, it is not easy to find out the good atomization fuel injector with good spray quality. However conceptually, rotating fuel injection system can give high atomization quality by only the centrifugal force of a high speed rotating shaft of the engine without high-pressure fuel pump. With this motivation, we manufactured very small rotating fuel injector of 40 mm diameter and performed under a variety of injection orifices. We measured droplet size, velocity and spray distribution by the PDPA(Phase Doppler Particle Analyzer) system. Also spray was visualized by using high speed camera. From the test results, we could understand that the length of liquid column from the injection orifice is mainly controlled by the rotational speeds. Furthermore, droplet size(SMD) is decreased with the rotational speeds and is influenced by the diameter of the injection orifice and liquid film thickness.

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Study on Improvement of Tungsten Alloy Granular Powder in Defense Industry (방산 분야 텅스텐 합금 과립분말 개선 연구)

  • Ji, Sangyong
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.10
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    • pp.206-211
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    • 2020
  • Tungsten alloys are used widely in general industrial fields, but they are difficult to cast, so products are manufactured using powder metallurgy. In this study, a mixed powder of tungsten, nickel, and iron homogenized using a ball mill was added to pure water as a solvent, and PVA as a binder was added to prepare a spray drying mixture. The mixed liquid was prepared using a spraying machine. A study was carried out to produce a granular powder that can reduce the variations between products during the molding and sintering process of the powder metallurgy method. A preliminary experiment was conducted to confirm the influence of the variables in the granulation process. Through the preliminary test results, this experiment was performed with the volume of solvent of the spray drying the mixture as an independent variable, and granular powder having a mean particle size similar to that of the existing mass-production conditions and an increased apparent density was prepared. In addition, a pilot test was conducted for the molding and sintering process. The improved granular powder reduced the characteristic variation (weight variation) of the mass-produced product.

Spray Structure and Cross-section Characteristics of Pulsed Liquid Jet Injected into a Cross-flow (횡단 유동장으로 펄스 분사된 액체 제트의 분무 구조 및 단면 분포 특성)

  • Lee, In-Chul;Koo, Ja-Ye
    • Journal of the Korean Society of Propulsion Engineers
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    • v.13 no.2
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    • pp.1-8
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    • 2009
  • Present studies of these experiments was conducted to using water, over a range of cross-flow velocities from 42 to 136 m/s, with injection frequencies from 35.7 to 166.2 Hz. In cross-flow field, main parameters of liquid jet for secondary breakup were cross-flow drag rather than pressure pulse frequency. As oscillation of the periodic pressure, liquid jet was moved up and down. Also, a bulk of liquid jet puff was detected at upper field of liquid surface. Because of pressure pulsation frequency, an inclination of SMD for the structured layer was evanescent. Cross-sectional characteristics of SMD at downstream area were non-structured distributions. The tendency of volume flux value for various frequency of pressure pulse was same distribution. And volume flux was decreased when the frequency of pressure pulse increasing.

Preparation of Mesoporous and Spherical-shaped Silica Particles by Spray Pyrolysis (분무열분해 공정을 이용한 메조기공을 가지는 실리카 구형입자의 제조)

  • Baek, Chul-Min;Jung, Kyeong Youl;Park, Kyun Young;Park, Seung Bin;Cho, Sung Baek
    • Korean Chemical Engineering Research
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    • v.46 no.5
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    • pp.880-885
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    • 2008
  • Spray pyrolysis was applied to prepare spherical silica particles with mesopores of a regular structure. The physical properties such as surface area, pore size, pore structure, particle size, and morphology were studied by BET, SEM, SAXS, and DLS analysis. At a fixed gas flow rate, the BET surface area changed from 200 to $1,290m^2/g$ as changing the CTAB/TEOS molar ratio from 0.05 to 0.3. At a fixed CTAB/TEOS ratio, the surface area of silica particles was varied from 1,062 to $1,305m^2/g$ with changing the gas flow rate from 10 to 40 l/min. The average pore size measured by BJH desorption was about $21{\sim}23{\AA}$ and not significantly influenced by the CTAB/TEOS ratio and the gas flow rate. Finally, the highest surface area which was $1,305m^2/g$ were obtained when the CTAB/TEOS ratio and the gas flow rate were 0.2 and 20 l/min, respectively. According to SAXS analysis, the prepared silica particles showed a strong peak at $2{\theta}=2.6^{\circ}$ and two minor peaks around $2{\theta}=4.4^{\circ}$ and $5.1^{\circ}$, which are due to regular mesopores of hexagonal structure. The morphology of silica particles prepared were spherical shape and the average particle size was $1.0{\mu}m$.

Disintegration Mechanism of a Coaxial Porous Injector (동축형 다공성재 분사기의 분열 메커니즘)

  • Lee, Keonwoong;Kim, Dohun;Son, Min;Koo, Jaye
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.2
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    • pp.39-45
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    • 2016
  • In a coaxial porous injector, a gas propellant is injected through the porous cylinder surface to the liquid jet which is encircled by a porous cylinder. In this study, to observe the differences in disintegration mechanisms between a shear coaxial injector and a coaxial porous injector, cold-flow tests and 2-D axisymmetric numerical analysis have been carried out. The shadowgraph images and Sauter mean diameters were compared in similar experimental conditions, and the effects of velocity distributions at the inner injector region on the disintegration of liquid jet were investigated through the numerical calculations. As a result, in high air mass flow rate condition, the disintegration performance of coaxial porous injector is better than shear coaxial injector, in spite of a lower velocity at the inner injector region.