• 제목/요약/키워드: Rate of mass combustion

검색결과 337건 처리시간 0.024초

배치형 내부 사이클론식 순환유동층 연소로내 2차 공기 주입에 의한 슬러지 소각 유해 배가스 저감효과 (Effect of Secondary Air Injection on Emission from Sludge Incineration in a Batch-type Internally Cycloned Circulating Fluidized Bed Combustor)

  • 장석돈;신동훈;황정호
    • 한국연소학회지
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    • 제7권3호
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    • pp.16-22
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    • 2002
  • Combustion performance of an internally cycloned circulating fluidized bed for paper sludge was discussed through a series of batch type experiments. Operation parameters such as water content, feeding mass of sludge and secondary air injection rate were varied to find out the effect on the combustion performance, which was examined with carbon conversion rate and pollutant emission such as CO and NOx. A conventional solid fuel reaction was observed in the experiments of varying water content and feeding mass of the sludge, which is characterized with kinetic limited reaction zone, diffusion limited reaction zone and transition zone. Secondary air injection with swirl enhances the mixing of the gas phase as well as the solid phase, and improves combustion efficiency accompanied with higher carbon conversion rate and lower pollutant emission rate.

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모래에 함침시킨 알콜의 연소특성 (Combustion Characteristics of Immobilized Alcohols in Sands)

  • 우인성
    • 한국안전학회지
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    • 제11권3호
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    • pp.137-142
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    • 1996
  • Combustion characteristics of immobilized methyl, ethyl and propyl alcohols on sands were studied. Experiments were performed by burning methyl, ethyl and propyl alcohols Immobilized on sands (particle size 0.1~5mm) and ceramic balls(particle size 5mm) to measure mass burning rate, height burning rate and combustion temperature. It was concluded that the longer time from ignition to extinguishment was resulted from the larger particle size of sands and the smaller size of sands exhibited the higher mass burning rate. Of alcohols tested the relative magnitude of facilitation of combustion was methyl>ethyl>propyl alcohol. Combustion temperature of alcohols, without regard to the types of alcohols, was not increased with smaller sands. However, with larger sands, combustion temperatare of alcohols was increased with the larger particle.

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폐기물 소각로 베드에서의 연소현상 관찰을 위한 실험적 연구 (An Experimental Study on the Bed Combustion Phenomena in MSW(Municipal Solid Waste) Incinerator)

  • 민지현;신동훈;최상민
    • 대한기계학회논문집B
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    • 제23권2호
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    • pp.159-165
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    • 1999
  • Experimental studies have been performed to observe the basic phenomena of waste bed combustion in MSW incinerator. A reduced scale apparatus was utilized to simulate the combustion behavior in real plant with 1-dimensional transient behavior at the experimental setup, which uses wet cubic wood with ash content as simulated waste. LHV (lower heating value) of solid fuel, fuel particle size and flow rate of combustion air were taken as important parameters of the bed combustion. For the quantitative analysis, FPR (flame propagation rate), TBT (total burn-out time) and PBT (particle burn-out time) was defined. LHV represent the capability of heat release of the fuel, so that a higher LHV results in faster reaction rate of the fuel bed, which is shown by higher FPR. Fuel particle size is related with surface area per unit mass as well as heat and mass transfer coefficient. As the particle size increases the FPR decreases owing to decreasing specific surface area. Air injection supplies oxygen to the reaction zone. However oversupply of combustion air increases convection cooling of the bed and possibly extinguishes the flame.

실물형 액체로켓엔진 연소기 케로신냉각 연소시험 성능결과 (Combustion Performance of a Full-scale Liquid Rocket Thrust Chamber Using Kerosene as Coolant)

  • 한영민;김종규;문일윤;서성현;최환석;이수용
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제27회 추계학술대회논문집
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    • pp.163-168
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    • 2006
  • 본 논문에서는 추력 30톤급 액체로켓엔진의 실물형 연소기 물냉각 연소시험 성능결과에 대해 기술하였다. 연소기 연소압력은 53bara 그리고 추진제 유량은 90kg/s이다. 케로신을 이용한 첫 번째 시험인 관계로 설계유량보다 약 120%정도인 32kg/s을 공급하면서 시험을 수행하였다. 이후 설계 케로신 유량 25kg/s을 공급하면서 성공적으로 시험을 수행하였다. 각각의 연소시험 결과에 대해 기술하였으며, 채널 연소실에서 케로신 냉각 성능이 충분해 재생 냉각 연소시험이 가능하다는 것을 알 수 있었다.

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밀도에 따른 지표 연료의 연소실험 분석 (A Combustion Analysis of Surface Fuel Burning Experiment According to Density Variation)

  • 김응식;김장환;김동현;박형주;김정훈
    • 한국화재소방학회논문지
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    • 제24권1호
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    • pp.1-7
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    • 2010
  • 본 연구에서는 지표화의 대표적인 연소물질인 굴참나무(Quercus Variabilis: Q.V.)와 소나무(Pinus Densiflora: P.D.) 낙엽을 이용하여 연료의 밀도 변화에 따른 열 유체속도, 연소온도, 질량감소속도, 화염높이 및 연소시간 등의 연소특성을 분석하였다. 바스켓 높이는 10cm, 지름 20, 30, 40 그리고 50cm의 원통형 바스켓에 밀도별로 각각 채운 후 표면에 점화원을 인가하여 실험을 실시하였다. 침엽수종 낙엽의 경우 밀도와 지름의 증가함에 따라 질량감소속도, 화염지속시간, 화염의 높이 그리고 연소시간은 증가한 반면, 활엽수종 낙엽의 경우 질량감소속도와 화염높이는 증가하다가 감소하였으며 화염지속시간과 연소시간은 증가하였다. 또한, 기체유속 및 온도는 화염 높이가 커질수록 증가하는 경향을 나타내었다.

정적연소기에서 점화장치가 열발생률과 잘량연소율에 미치는 영향에 관한 연구 (A Study on the Effects of Ignition Systems on the Heat Release Rate and Mass Fraction Burnt at a Constant Volume Combustion Chamber)

  • 송정훈;이기형;선우명호
    • 대한기계학회논문집B
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    • 제24권11호
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    • pp.1486-1496
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    • 2000
  • The initial flame kernel development and flame propagation in a constant volume combustion chamber is analyzed by the heat release rate and the mass fraction burnt. The combustion pressure is measured with a piezoelectric type pressure sensor. In order to evaluate the effects of ignition system and ignition energy on the flame propagation, four different ignition systems are designed and tested, and the ignition energy is varied by the dwell time. Several different spark plugs are also tested and examined to analysis the effects of electrodes on flame kernel development. The results show that the when the dwell time is increased, and when the spark plug gap is extended, heat release rate and the mass burnt fraction are increased. The materials and shapes of electrodes affect the flame development, because they change the energy transfer efficiency from electrical energy to chemical energy. The diameter of electrodes influences not only the heat release rate but also the mass burnt fraction as well.

액체로켓엔진의 2단 시동에 관한 연구 (A Study on the 2-Stage Startup of Liquid Rocket Engine)

  • 박순영;조원국
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.324-327
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    • 2008
  • Two stage startup of high thrust liquid rocket engine can reduce the abrupt impulse to the vehicle and engine by changing oxidizer flow rate to the combustion chamber. Also it ensures stable ignition of combustion chamber against hard start and to prevent pump stall by the sudden supply of large mass flow rate. However high discharge pressure of oxidizer pump or temperature rise in gas generator may be a problem in applying the preliminary stage. To solve this problem, we analyzed the effect of the slope of oxidizer pump's head curve and the oxidizer mass flow rate to combustion chamber during preliminary stage using the rocket engine startup analysis code. A moderate slope(${\circleddash}{\sim}$-3) of head curve and 80% mass flow rate during preliminary stage can reduce the oxidizer pump discharge pressure by 15 to 20% comparing with the condition of ${\circleddash}$=-4.37 head curve and 70% mass flow rate. Also it can maintain the turbine inlet temperature rise within 50K from the nominal value.

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수소 생산을 위한 수증기 개질기의 형상 변화와 작동 조건에 대한 수치해석 연구 (Numerical Study on Geometries and Operating Parameters of a Steam Reformer for Hydrogen Production)

  • 변강수;이재성;김호영
    • 한국연소학회지
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    • 제16권3호
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    • pp.1-11
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    • 2011
  • The main objective of this paper is to investigate characteristic of steam reformer at various geometries and operating conditions. In this paper, the steam reforming is studied by a numerical method and three dimensional simulations were used for effective analytical study. User - Defined Function (UDF) was used to simultaneously calculate reforming and combustion reaction. And the numerical model is validated with experimental results at the same operating conditions. In order to understand the relationship between operating conditions such as gas hourly space velocity(GHSV), mass flow rate of combustor inlet, various numerical investigations are carries out for various geometries. Numerical results show that cylindrical geometry is more effective than rectangular geometry for heat transfer to reactors and reforming efficiency. As mass flow rate of combustor inlet increase, reaction occurs more faster and temperature increase with each geometry. On the other hand, reaction and hydrogen conversion decrease as mass flow rate of reactor decreases.

PE-GOX 하이브리드 로켓에서의 과도 연소 특성 연구 (A Study on the Transient Combustion Characteristic in PE-GOX Hybrid Rocket)

  • 조성봉;이정표;송나영;김수종;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제27회 추계학술대회논문집
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    • pp.228-231
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    • 2006
  • 일반적으로 하이브리드 추진 연소 특성에서 연소 시간은 실험식의 인자로 고려되지 않는다. 따라서 실험의 변수로써 연소 시간이 하이브리드 연소 특성 및 추진 특성에 미치는 영향에 관하여 연구하였다. 후퇴율은 연소 시간에 따라 감소하나, 연료 질량 유속은 일정한 것으로 나타났다.

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모래에 침지시킨 방향족 유기용제의 연소특성 (Combustion Characteristics of Immobilized Aromatic Organic Solvent in Sands)

  • 우인성;황명환;정덕채
    • 한국안전학회지
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    • 제15권3호
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    • pp.83-87
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    • 2000
  • Combustion characteristics of immobilized benzene and toluene in sands were studied. Experiments were performed by burning benzene and toluene immobilized on sands(particle size 0.1~0.5mm) to measure combustion rate and combustion temperature. The longer time from ignition to extinguishment was resulted from the larger particle size exhibited the higher mass burning rate. Of aromatic compounds tested the relative magnitude of facilitation of combustion was benzene and toluene. Combustion temperature of benzene and toluene without regard to the types of benzene and toluene was not increased with smaller sand. However, with larger sands, combustion temperature of benzene and toluene were increased by 50~$100^{\circ}C$ and the highest combustion temperature was obtained with larger sands.

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