• Title/Summary/Keyword: 오리피스 직경

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Optimum Design of Dual Orifice Fuel Nozzle (이중 오리피스 연료 노즐 최적설계)

  • Lim, O-Kaung;Choi, Eun-Ho;Kim, Sung-Sub
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.20 no.4
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    • pp.407-416
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    • 2007
  • Fuel spray nozzle has a critical effect on combustion characteristics. Mass flow rate and SMD(sauter mean diameter) were selected as design variables by using the experiment data of various types of duplex fuel nozzles for the swirl atomizers. The sensitivity of each design variable on the mass flow rate and SMD was analyzed and the uniformity of mass flow rate was investigated through the shape optimization of duel-orifice-type swirl atomizers. The design variables that have a little effect on the optimum design were excluded using the DOE(design of experiments) method, which enabled the optimization of sensitive design variables on mass flow rate and limit tolerance. The SMD of the research spray nozzle that was used in this study was found to be most similar to that of the calculation results using the Jasuja's SMD relationship. This study showed the specific characteristics of duel orifice type swirl atomizers and the optimization of these kinds of nozzle. This study provided the optimization design of mass flow rate and its allowable tolerance.

Development of the Vortex Tube for Automotive Exhaust System (자동차 배기계 적용을 위한 와류 튜브의 개발)

  • Lee, Jun-Sun;Park, Sung-Young
    • Proceedings of the KAIS Fall Conference
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    • 2010.11b
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    • pp.925-928
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    • 2010
  • 볼텍스 튜브는 고압의 가스를 이용하여 고온 가스와 저온 가스를 분리하거나 입자상 물질의 분리에 사용 할 수 있는 장치이다. 본 연구에서는 직경 10mm의 볼텍스 튜브의 기본 설계 자료를 구축하기 위하여 에너지 분리 성능 실험을 수행하였다. 설계를 위한 기초 자료를 확보하기 위하여, 공급압력, 볼텍스 발생기의 오리피스 직경 및 튜브의 길이가 에너지 분리 특성에 미치는 영향력을 실험을 통하여 분석하였다. 결과적으로 오리피스 직경과 공급압력이 볼텍스 튜브의 성능의 지배적인 성능인자임을 확인하였다. 튜브길이가 성능에 미치는 영향은 미미하였다.

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Acoustic Effect of an Orifice on Suppression of Pressure Oscillation in a Fluid Feeding Line (유체 공급 배관내 압력진동 감쇠에 미치는 오리피스의 음향학적 효과)

  • Son, Chae-Hun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.4
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    • pp.11-16
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    • 2006
  • Effects of an orifice on suppression of pressure oscillation in a fluid feeding line are investigated numerically through the installation of an orifice inside the feeding line. Based on linear acoustic theory, acoustic-damping effect of an orifice is emphasized in this study. When an orifice is installed at the node of pressure oscillation corresponding to the anti-node of velocity oscillation, damping capacity is maximized. On the other hand, the orifice installed at the anti-node of pressure oscillation has little damping capacity. As the blockage ratio and thickness of an orifice increase in the feeding line, damping factor increases. The feeding line with smaller diameter has more damping capacity, but damping factor increases more appreciably with blockage ratio in the feeding line with larger diameter.

A Combination Study on the Elevation Motion Friction Compensation Parameters in Gas Spring (1) (가스 스프링 Elevation 동작 마찰력 보상 변수 조합 연구 (1))

  • Lee, Jeong-Ick
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.5
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    • pp.657-666
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    • 2017
  • In this study, factor analysis was performed to reduce the friction in the elevation motion of a stand for a 50-inchtelevision. Pipe type cross-section control was used for accurate positioning control of the piston rod. The pipe type was also compared with a labyrinth-type crosssection for the orifice. The frictional force was then reduced using gas seal lip technology. Specifications were chosen, and a volume compensation experiment was carried out using an apparatus for compensating the volume of the cylinder, which is compressed by the volume of the piston rod. Based on CAE and experimental considerations, the labyrinth-type orifice is preferred for reducing friction. For the gas seal lip technology, outer and inner diameters of ${\Phi}20$ and ${\Phi}8$ for the hollow rod were more appropriate when assuming the weight of a 50-inch television to be 30kgf. The third is that the result of total consideration in stability problem and performance of volume compensation for specification decision and volume compensation experiment is determined the final speculation of hollow rod ?8x?4 and riveting system. The last is that the labyrinth orifice is not founded that of the ${\O}0.4{\sim}0.6$ orifice both tests on 300 mm intervals.

ISO 규격에서 규정한 표준용기 기체도입 도관의 직경에 대한 고찰

  • In, Sang-Ryeol
    • Proceedings of the Korean Vacuum Society Conference
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    • 2010.02a
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    • pp.332-332
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    • 2010
  • 진공펌프의 배기성능 지표들을 정량적으로 측정하기 위해서 사용하는 표준용기에 관한 규격들은 대체로 일치하는 사양들을 제시하지만 유독 기체도입 도관의 굵기에 대해서는 다양한 방식으로 규정하고 있어서 혼란스럽다. 현재 제정중인 ISO 규격에서는 도관 굵기를 용기 내경의 10분의 1로 규정하고 있는데 대형 펌프 용 표준용기에 맞춘다면 도관의 굵기가 지나치게 커질 수 있다. 과연 이렇게 굵은 도관이 정밀한 측정을 위해 꼭 필요한지 또는 오히려 방해가 되는 것은 아닌지 검토해 보기 위해 도관 굵기에 따라 도관출구를 빠져나오는 입자들과 오리피스 및 펌프 흡기구에 입사하는 입자들의 등방성에 대해 살펴보았다 계산 결과에 의하면 도관의 굵기는 오리피스 및 펌프 흡기구에 입사하는 입자들의 평균 방향 여현 값에 전혀 영향을 미치지 않는 것으로 나타났으며 반면에 도관이 오리피스나 흡기구 면에 국부적으로 그림자를 드리우거나 입자 분포와 평균 방향여현 분포를 왜곡시키지도 않았다. 즉 기체 도입 도관을 가늘게 해도 빔효과가 계속 전파되어서 측정에 악영향을 미치지 않으므로 별 문제가 안 되고, 도관이 규정되어 있는 범위 안에서 어느 정도 굵어져도 입자의 흐름을 방해한다는 증거는 없다는 뜻이다. 그렇다면 도관의 굵기를 한 값으로 못 박기보다 넓은 범위를 주어 가공 능력에 따라 사용자가 적절히 크기를 선택할 수 있도록 하는 것이 합리적이라고 판단된다.

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Evolutionary Feature of Spray Droplets Exiting from a Direct-Injection Type Thruster Nozzle-Orifice (직접분사방식 추력기 노즐오리피스로부터 발생하는 분무입자의 발달특성)

  • Kim, Jin-Seok;Jung, Hun;Kim, Jeong-Soo;Park, Jeong;Kim, Sung-Cho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.149-152
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    • 2009
  • Spray characteristic parameters such as droplet mean velocity, diameter, and volume flux are measured at various locations of spray in order to investigate the evolutionary feature of droplets exiting from a direct-injection type thruster nozzle-orifice. The experimental results indicate that the large droplets with high velocity at the center of upstream are broken-up into smaller droplets with low velocity due to their continuous momentum loss to surrounding air along with spray evolution toward downstream. Also it is found that the high volume flux expands its distribution in radial direction as a results of spray spreading and dispersion.

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Damping Characteristics of a Helmholtz Resonator Under the Flow Area (튜브(모사 챔버)내의 유동특성이 음향공 감쇠 능력에 미치는 영향)

  • Song, Jae-Gang;Kim, Young-Mun;Ko, Young-Sung;Kim, Sun-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.82-85
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    • 2008
  • A Helmholtz resonator is applied to control high frequency combustion instability in liquid rocket engine. Damping characteristics of the Helmholtz resonator are investigated by the flow characteristic and its design. To simulate combustion instability, resonance in a test section(with fixed volume) is made by a pressure pulsator, and then damping characteristics are investigated. Its orifice length and diameter are selected as the design parameters and flow rates are varied to reveal the effect on damping characteristics. The experimental results show that a Helmholtz resonator is also working with flows. When length and diameter of an orifice are small, the tuning frequency increases as the flow velocity increases.

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Combustion Characteristics of Landfill Gas in Constant Volume Combustion Chamber for Large Displacement Volume Engine (IV) -Torch Ignition (2) - (대형기관 모사 정적연소실에서 매립지 가스의 연소특성에 대한 연구 (IV) -토치 점화 (2)-)

  • Ko, Ansu;Ohm, Inyong;Kwon, Soon Tae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.39 no.2
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    • pp.135-146
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    • 2015
  • This paper is the fourth on the combustion characteristics of the landfill gas in a constant volume combustion chamber for a large displacement volume commercial engine and the second dealing with torch ignition. It discusses the combustion characteristics of torch ignition on the basis of the heat release and visualization. The results show that the jet and/or spout from the torch promote combustion by accelerating the flame front in the main combustion chamber. In addition, a hot gas jet exists when the orifice diameter is 4 mm, whereas the flame passes directly through the orifice if the diameter is 6 mm or greater. In addition, the effect of torch ignition differs according to the combination of the methane fraction, torch volume, and orifice size because various combustion processes occur as a result of the interaction of these parameters. Finally, it was found that the most suitable torch should have an orifice diameter of not less than 6 mm and an area ratio of not more than 0.15 to secure a consistent combustion process in a real engine.

Ground Ejection Tests for the Safe Separation Analysis of a Gliding Bomb (활공탄의 안전분리 해석을 위한 지상투하시험)

  • Lee, Kidu;Lee, Inwon;Park, Youngkun;Baek, Seungwoock;Jung, Nahyeon;Jung, Sangjun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.6
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    • pp.502-508
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    • 2013
  • Various combinations of cartridge and orifice were applied for ground ejection tests of a gliding bomb model equipped with a new guidance kit. Larger diameter of orifice made larger ejection force at each of bomb racks. Normal operations of the wing deploying mechanism and the devices inside of the bomb model were confirmed. Also high speed video data showed that pitch angle of the gliding bomb varied due to the ejection force.