• Title/Summary/Keyword: 고연소도

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A Study on Characteristics of Emissions in GDI Engine with Intake Swirl Variation (흡기스월 변화에 따른 GDI 기관의 배기특성에 관한 연구)

  • 채재우;차민혁;이상만
    • Proceedings of the Korea Air Pollution Research Association Conference
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    • 2000.11a
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    • pp.207-209
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    • 2000
  • GDI(Gasoline Direct Injection) 기관은 전체적으로 희박한 영역에서 작동되기 때문에 저연비, 고출력화 및 배기유해가스 저감에 매우 유리하다. GDI 기관에 있어서 희박연소를 실현하고자 한 연구는 공기유동 강화방식, 연소실 형상의 최적화, 부실식 연소, 분사된 연료의 미립화, 흡기포트의 형상 변화, 운전조건 변화에 따른 분사전략의 변화 등 그 방식도 다양하며,$^{<1-5>}$ 최근엔 이러한 각 방식들의 장점들을 적절히 활용하고 이에 따라 각기 고유한 모델을 채택하여 접근하려는 시도를 하고 있다$^{<6>}$ . (중략)

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Combustion Performance Tests of High Pressure Subscale Liquid Rocket Combustors (고압 축소형 연소기의 연소 성능 시험)

  • Kim, Jong-Gyu;Lee, Kwang-Jin;Seo, Seong-Hyeon;Lim, Byoung-Jik;Ahn, Kyu-Bok;Han, Yeoung-Min;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.128-134
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    • 2007
  • Combustion performance and characteristics of high-pressure subscale liquid rocket combustors were studied experimentally. Four different models of combustor were considered in this paper. The high-pressure subscale combustor is composed of the mixing head, the water cooling cylinder and the nozzle. One model of the combustors employed regenerative cooling combustor in that the kerosene used for the chamber cooling is burned. This combustor was damaged due to a high frequency combustion instability occurred during a firing test. The results of the firing tests, comparison of performance, and characteristics of static and dynamic pressures of the combustors are described.

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A Study on Cyclone Combustion System for Efficient Thermal Oxidation of VOC (휘발성 유기물질의 효율적 열산화를 위한 사이클론 연소시스템 연구)

  • 현주수;이시훈;임영준;민병무
    • Journal of Energy Engineering
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    • v.13 no.2
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    • pp.112-117
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    • 2004
  • Volatile organic compounds (VOCs) are low calorific value gases (LCVG) emitted from chemical processes such as painting booth, dye works and drying processes etc. Characteristics of VOCs are low calorific values less than 150kcal/㎥, high activation energy for ignition and low energy output. These characteristics usually make combustion unstable and its treatment processes needs high-energy consumption. The cyclone combustion system is suitable for LCVG burning because it can recirculate energy through a high swirling flow to supply the activation energy for ignition, increases energy density In make a combustion temperature higher than usual swirl combustor and also increases mixing intensity. This research was conducted to develop optimized cyclone combustion system for thermal oxidation of VOCs. This research was executed to establish the effect of swirl number with respect to the combustion temperature and composition of exhausted gas in the specific combustor design.

A Parametric Study on Combustion Stability Characteristics of Fuel-rich Gas Generators (설계 인자에 따른 연료 과농 가스발생기의 연소 안정성 특성 연구)

  • Ahn Kyu-Bok;Moon Il-Yoon;Seo Seong-Hyeon;Han Yeoung-Min;Choi Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.171-176
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    • 2006
  • An experimental study on a fuel-rich gas generator was carried out. Thirty seven double-swirl injectors with recess number of 1.5 were distributed and installed in the injector head, which significantly influences the combustion performance. In the paper, the characteristics of combustion stability are inspected by the parametric varations such as changing length and diameter of a combustion chamber and installing a turbulence ring. The experimental results show that as a resonant frequency took place in a high region, the amplitude of the dynamic pressure generally diminished, however, the combustion instability could not be suppressed perfectly.

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