• Title/Summary/Keyword: 원추형화염

Search Result 5, Processing Time 0.02 seconds

An experimental study on the burning velocity measurement of natural gas (천연가스의 연소속도 측정에 관한 실험적 연구)

  • Yu, Hyeon-Seok;Han, Jeong-Ok;Bang, Hyo-Seon
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.21 no.2
    • /
    • pp.195-201
    • /
    • 1997
  • Static and non-static flame methods were used to measure the laminar burning velocity of methane, ethane and natural gas. The flame slot angle and velocity of unburned gas mixture were determined by Schlieren method and LDV, respectively, for static flame. The diameter of nozzle was selected as 11 mm. The experimental results containing the stretch effect showed that the maximum burning velocities were 41.5 for natural gas, 40.8 for methane and 43.4 cm/sec for ethane on equivalence ratio of 1.1. Constant volume combustion chamber was also used for non-static flame. The propagation process of flame front was visualized by high speed camera during constant pressure. The maximum burning velocity of natural gas was determined as 42.1 cm/sec on equivalence ratio of 1.15.

Experimental Study of Thermo-Flow Field in a Model Gas Turbine Combustor with Various Swirl Conditions (스월변화에 따른 모형 가스터빈 연소기의 열유동장의 실험적 연구)

  • Ryu, Song-Youl;Koo, Ja-Ye
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.30 no.4
    • /
    • pp.70-76
    • /
    • 2002
  • Characteristics of kerosine spray combustion were investigated at various swirl condition. PDPA(Phase Doppler Particle Analysis) was used to measure the droplet sizes and velocities. R-type(Platinum vs. Platinum-13%rhodium) thermocouple was used to measure the temperature of combustion flow field inside model combustor. A visualization of spray and flame was performed with still camera. As swirl number increases due to increase of swirl vane angle, the spray and the flame were developed to radial direction rapidly. When swirl number is small, the configuration of flame is cone type, but swirl number is large, the configuration of flame is cylindrical type due to enhanced mixing by the transport of swirl momentum.

Numerical study of a conical MILD combustor with varing the fuel flow rate (연료유량 변화에 따른 원추형 MILD 연소로의 수치적 해석)

  • Kim, Tae Kwon
    • Journal of the Korea Academia-Industrial cooperation Society
    • /
    • v.15 no.6
    • /
    • pp.3370-3375
    • /
    • 2014
  • MILD combustion is a highly favored technology for solving the trade-off relation between high thermal efficiency and low pollutant emissions. The system has low NOx concentration in high temperature combustion by recirculating the combustion gas, as well as improving the thermal efficiency by making the internal temperature in a combustion furnace uniform. This study describes the combustion characteristics of a conical MILD combustor in a laboratory-scale furnace by adjusting the equivalence ratio with the fuel gas flow rate while maintaining a constant air flow rate of the furnace. The MILD regime in the furnace is well characterized and the in-furnace temperature and emissions were predicted, respectively, for the range of equivalence of 0.69 - 0.83. For the range of equivalence ratios, this study confirmed the existence of a stable flame region that has an approximately $300^{\circ}C$ temperature difference between the maximum flame temperature region and main reaction region.

Effect of Pressure and Stoichiometric Air Ratio on NOx Emissions in Gas-Turbine Dump Combustor with Double Cone Burner (이중원추형 모형연소기에서 압력과 공기비에 따른 NOx 배출특성)

  • Nam, Dong-Hyun;Nam, Hyun-Su;Han, Dong-Sik;Kim, Gyu-Bo;Cho, Seung-Wan;Kim, Han-Suk;Jeon, Chung-Hwan
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.36 no.3
    • /
    • pp.251-257
    • /
    • 2012
  • This work presents an experimental investigation of NOx emissions according to inlet air temperature (550-660 K), stoichiometric air ratio (${\lambda}$, 1.4-2.1), and elevated pressure (2-5 bar) in a High Press Combustor (HPC) equipped with a double cone burner, which was designed by Pusan Clean Coal Center (PC3). The exhaust-gas temperature and NOx emissions were measured at the end of the combustion chamber. The NOx emissions generally decreased as a function of increasing ${\lambda}$. On the other hand, NOx emissions were influenced by ${\lambda}$, inlet air temperature and pressure of the combustion chamber. In particular, when the inlet air temperature increased, the flammability limit was extended to leaner conditions. As a result, a higher adiabatic temperature and lower NOx emissions could be achieved under these operation conditions. The NOx emissions that were governed by thermal NOx were greatly increased under elevated pressures, and slightly increased at sufficiently low fuel concentrations (${\lambda}$ >1.8).

Effect of pressure and stochiometric air ratio on flame structure and NOx emission in gas turbine dump combustor with double cone burner (이중원추형 모형연소기에서 압력과 공기비에 따른 화염 구조 및 NOx 배출특성)

  • Nam, Hyun Su;Han, Dong Sik;Kim, Gyu Bo;Jeo, Chung-Hwan
    • 한국연소학회:학술대회논문집
    • /
    • 2012.04a
    • /
    • pp.177-179
    • /
    • 2012
  • This work presents an experimental investigation to study $NO_x$ emissions under stoichiometric air ratio and elevated pressure (2~10bar) in a High Press Combustor(HPC) equiped with double cone burner which was designed by Pusan Clean Coal Center(PC3). Exaust gas temperature and $NO_x$ emissions were measured at the end of the combustion chamber. The $OH^*$ radical concentration and $NO_x$ emission were decreased as a function of increasing ${\lambda}$ generally. On the other hand, $OH^*$ radical concentration and $NO_x$ emission increased with ${\lambda}$ pressure of the combustion chamber. $NO_x$ emissions which were governed by thermal $NO_x$, were highly increased under the elevated pressure, but slightly increased at sufficiently low fuel concentrations (${\lambda}>2.0$).

  • PDF