• Title/Summary/Keyword: liquefied butane spray

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Measurements of Droplet Sizes and Velocities with Optimum Probability Density Function in a Transient Liquefied Butane Spray (액상부탄 간헐분무의 액적 크기 및 속도 측정과 최적 확률분포 연구)

  • Kim, J.H.;Kim, J.W.;Koo, J.Y.
    • Journal of ILASS-Korea
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    • v.5 no.1
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    • pp.30-40
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    • 2000
  • The characteristics of liquefied butane spray are expected to be different from conventional diesel fuel spray, because a kind of flash boiling spray is expected when the back pressure is below the saturated vapor pressure of the butane(0.23MPa at 298K). The ambient pressure was held at a pressure above(0.37MPa) and below(0.15MPa) the fuel vapor pressure. The axial velocities, radial velocities, and size distributions in butane sprays were measured with PDPA(Phase Doppler Particle Analyzer) system. The PDPA measurement showed a smaller SMD at the 0.15MPa chamber pressure, compared to the 0.37MPa case. Log-hyperbolic density function for the droplets size distribution can be fitted to the experimental results of a liquefied butane spray.

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Simulation of Fuel Injection System and Model of Spray Behavior in Liquefied Butane (액상부탄 분사시스템의 수치시뮬레이션 및 분무특성 예측)

  • Kim, J.H.;Koo, J.Y.
    • Journal of ILASS-Korea
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    • v.3 no.2
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    • pp.24-33
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    • 1998
  • The characteristics of liquefied butane spray are expected to be different from conventional diesel fuel spray, because a kind of flash boiling spray is expected when the back pressure is below the saturation vapor pressure of the butane(0.23MPa at $25^{\circ}C$). An accumulator type pintle injector and its fuel delivery system has been simulated in ruder to give injection pressure, needle lift and rate of fuel injected. The governing equation were solved by finite difference metho. The injection duration was controlled by solenoid valve. Spray behaviors such as a transient spray tip penetration, spray angle and SMD were calculated based on the empirical correlations in case that the back pressure is both above the vapor pressure of the butane and below that of butane. When the back preassure is below the vapor pressure of the fuel, conventional correlation is modified to represent the effect of flash boiling.

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The Characteristics of a Transient Liquefied Butane Spray using PDPA and High Speed Camera (PDPA와 고속카메라에 의한 액상부탄 간헐분무 특성 연구)

  • 윤준규;임종한;김종현
    • Journal of Advanced Marine Engineering and Technology
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    • v.28 no.3
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    • pp.466-474
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    • 2004
  • The characteristics of liquefied butane spray are expected to be different from conventional diesel fuel spray, because a flash boiling spray is expected when the surround pressure is below the saturated vapor pressure of the butane(0.23MPa 98K). The axial velocities. radial velocities. and size distributions in butane sprays were measured with PDPA(Phase Doppler Particle Analyzer) system. Sprays were macroscopically observed by using the high speed camera in case that the surround pressure is 0.37MPa and 0.15MPa. respectively. Compared with the conventional spray. the reversed results were investigated when the surround pressure is below the saturated vapor pressure of the butane.

LPG Spray Characteristics in a Multi-hole Injector for Gasoline Direct Injection (분사조건에 따른 가솔린 직접분사용 다공 분사기에서의 LPG 분무특성)

  • Jung, Jinyoung;Oh, Heechang;Bae, Choongsik
    • Journal of ILASS-Korea
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    • v.19 no.1
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    • pp.1-8
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    • 2014
  • Liquefied petroleum gas (LPG) is regarded as an alternative fuel for spark ignition engine due to similar or even higher octane number. In addition, LPG has better fuel characteristics including high vaporization characteristic and low carbon/hydrogen ratio leading to a reduction in carbon dioxide emission. Recently, development of LPG direct injection system started to improve performance of vehicles fuelled with LPG. However, spray characteristics of LPG were not well understood, which is should be known to develop injector for LPG direct injection engines. In this study, effects of operation condition including ambient pressure, temperature, and injection pressure on spray properties of n-butane were evaluated and compared to gasoline in a multi-hole injector. As general characteristics of both fuels, spray penetration becomes smaller with an increase of ambient pressure as well as a reduction in the injection pressure. However, it is found that evaporation of n-butane was faster compared to gasoline under all experimental condition. As a result, spray penetration of n-butane was shorter than that of gasoline. This result was due to higher vapor pressure and lower boiling point of n-butane. On the other hand, spray angle of both fuels do not vary much except under high ambient temperature conditions. Furthermore, spray shape of n-butane spray becomes completely different from that of gasoline at high ambient temperature conditions due to flash boiling of n-butane.

A study on Behavior of Turbulent Transient Jets with Butane and Propane (Butane 및 propane의 비정상 난류 제트 특성에 관한 연구)

  • Lee, Beom-Ho;Song, Hak-Hyun;Cho, Seung-Hwan;Hong, Sung-Tae;Lee, Dae-Yup;Lee, Tae-Woo
    • Journal of ILASS-Korea
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    • v.15 no.2
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    • pp.74-82
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    • 2010
  • In order to understand the behavior of transient gaseous injection used in an LPG (Liquefied Petroleum Gas) engine, turbulent incompressible transient jets with butane and propane were measured and analyzed at pressures of 1.5 bar and 2.0 bar with injector diameters of 3 mm and 5 mm. Mie-scattering method with a tracer was used, and images were processed to investigate the behavior of butane and propane jets. Distances from the nozzle to transition region were measured as $L_e/d_{inj}$=4.35~19.4, where $L_e$ and $d_{inj}$ indicate respectively a distance from nozzle to transition point and nozzle diameter. Slits and tubes around jet at near-field were introduced to measure the effect of entrainment and the diameter of jet, which revealed that the entrainment of surrounding air is significant for developing jet diameter. When the entrainment is restricted, the behavior of jet became deviating from the baseline. It was found that the virtual origin located outside of a nozzle towards jet tip within the conditions of this work, and its location was estimated as $x_o/d_{inj}$=0.56~7.25, where $x_o$ is a distance from nozzle to virtual origin.