• Title/Summary/Keyword: Combustion Performance

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Numerical Study of Premixed Combustion within a Porous Ceramic Burner of Different Ceramic Properties (서로 다른 물성치로 이루어진 다공 세라믹 연소기 속에서의 예혼합화염 연소에 대한 수치해석 연구)

  • Lim, In-Gweon
    • Journal of the Korean Society of Combustion
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    • v.2 no.1
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    • pp.1-8
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    • 1997
  • Premixed combustion within porous ceramic media is numerically studied to understand burning characteristics and to find best configurations for burner implementations. Among many parameters, critical to burner performance, flame location and extinction coefficient are selected as major parameters for this study. The flame structure and burner performance with respect to these two parameters are observed. In the study, it is found that the location of flame is the most important in porous burner operation since it affects the rate of heat transfer and flame structure. Stability of the flame within the porous ceramic burner is discussed with respect to the flame location. It is found that to obtain high radiative output, the flame should be located downstream section of the burner. But the flame is to be unstable at most of downstream section except near the exit plane. To overcome this problem, new porous ceramic burner, using different ceramic properties in one burner instead of single property ceramic, is made and tested. With a combination of ceramics of high extinction coefficient at upstream and another material of low extinction coefficient at downstream of the burner, the flame can be stabilized at wider region of the burner with higher radiative output compared to the original burner configuration.

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Performance Analysis of an Oxy-fuel Combustion Power Generation System Based on Waste Heat Recovery: Influence of CO2 Capture (배열회수형 순산소연소 발전시스템의 성능해석: CO2 포집의 영향)

  • Tak, Sang-Hyun;Park, Sung-Ku;Kim, Tong-Seop;Sohn, Jeong-Lak;Lee, Young-Duk
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.33 no.12
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    • pp.968-976
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    • 2009
  • As the global warming becomes a serious environmental problem, studies of reducing $CO_2$ emission in power generation area are in progress all over the world. One of the carbon capture and storage(CCS) technologies is known as oxy-fuel combustion power generation system. In the oxy-fuel combustion system, the exhaust gas is mainly composed of $CO_2$ and $H_2O$. Thus, high-purity $CO_2$ can be obtained after a proper $H_2O$ removal process. In this paper, an oxy-fuel combustion cycle that recovers the waste heat of a high-temperature fuel cell is analyzed thermodynamically. Variations of characteristics of $CO_2$ and $H_2O$ mixture which is extracted from the condenser and power consumption required to obtain highly-pure $CO_2$ gas were examined according to the variation of the condensing pressure. The influence of the number of compression stages on the power consumption of the $CO_2$ capture process was analyzed, and the overall system performance was also investigated.

An Optimization of the Combustion Parameters for Reducing Exhaust Emissions in a Direct Injection Diesel Engine (직접분사식 디젤기관 배기배출물 저감을 위한 연소인자의 최적화)

  • 주봉철;노병준;김규철;이삼구
    • Transactions of the Korean Society of Automotive Engineers
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    • v.8 no.5
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    • pp.78-85
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    • 2000
  • This study is to develop the diesel engine which has 6 cylinder natural aspiration direct injection type of 7.4$\ell$ with high performance, low emissions and low fuel consumption Finally the developed engine meets Korean `98 exhaust emission regulation for the city bus of heavy duty diesel engine by optimizing the various combustion parameters affecting performance and exhaust emissions. Combustion parameters are the swirl ratio of intake ports, the profile of injection pump`s cam affecting injection pressure, the design features of piston bowl of injection pump`s cam affecting injection pressure, the design features of piston bowl of combustion chamber and injector`s hole size. Through experimental analysis, various combustion parameters are optimized and the results are as follows; the swirl ratio is 2.20, the profile of injection pump`s cam is concave and re-entrant ratio, inner diameter of piston bowl and hole diameter of injector is 0.88,$\psi$64.0mm and $\psi$0.25mm respectively.

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Numerical Study on the Effect of Nozzle Geometry on the Small CRDI Engine Performance (노즐 형상 변경이 소형 CRDI 엔진의 성능에 미치는 영향에 대한 수치 해석적 연구)

  • Min, Se Hun;Suh, Hyun Kyu
    • Journal of ILASS-Korea
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    • v.20 no.4
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    • pp.254-260
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    • 2015
  • The objective of this study is to investigate the effect of multi-hole nozzle on the performance of small CRDI engine. Combustion and exhaust emission characteristics of engine were studied by using CFD simulation with ECFM-3Z combustion model. The conditions of simulation were varied with nozzle geometry, injection timing and injection quantity. In addition, the results were compared in terms of combustion pressure, rate of heat release, $NO_x$ and soot emissions. It was found that combustion pressure was increased when injection timing was advanced. The rate of heat release of 6 hole nozzle was higher than that of 12 hole nozzle since the quantity of fuel impinged at the bottom of piston rim was different under different injection timing conditions. In the case of $NO_x$ emission, 6 hole nozzle generated more $NO_x$ emission than 12 hole nozzle. On the other hand, in the case of soot emission, 12 hole nozzle showed higher value than 6 hole nozzle because injected fuel droplets from multi-hole nozzle were coalesced.

Pressure Control of Staged Combustion Liquid Rocket Engine (다단연소사이클 액체 로켓엔진의 압력제어에 대한 연구)

  • Hwang, Changhwan;Lee, Kwangjin;Woo, Seongphil;Im, Ji-Hyuk;Jeon, Junsu;Lee, Jungho;Yoo, Byungil;Han, Yeoungmin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.88-93
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    • 2017
  • For the control of pre-burner combustion pressure, the open angle of TTR(Throttle for Thrust Regulation) valve was varied from $143^{\circ}$ to $185^{\circ}$ while testing of cold flow, ignition, combustion. The major performance variables of rocket engine and hydraulic performance of TTR valve regarding the open angle was verified. However the controllability of pre-burner combustion pressure was not verified due to the limitations of test. The comprehensive research will be done after supplementing these problems.

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Durability Test of a Direct Injection Diesel Engine Using Biodiesel Fuel (바이오디젤유를 사용하는 직접분사식 디젤기관의 내구특성)

  • 유경현;오영택
    • Transactions of the Korean Society of Automotive Engineers
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    • v.12 no.1
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    • pp.32-38
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    • 2004
  • To evaluate the durability of direct injection diesel engine using biodiesel fuel, a small D. I. diesel engine was operated on a blend(BDF 20) of 20% biodiesel fuel and 80% diesel fuel for 200 hours. Engine dynamometer test was performed at a load of 90% and a speed of 1900 rpm to monitor the engine performance and exhaust emissions. Engine performance parameters and exhaust emissions were sampled at 1 hour interval for analysis. The combustion maximum pressure and the crank angle at this maximum pressure as a combustion variation factor were considered to study the combustion characteristics of BDF 20 in diesel engine during durability test. As the results, the standard deviations and errors of combustion variation factors on BDF 20 were very little and combustion characteristics were very stable during the durability test. BDF 20 resulted in lower emissions of carbon monoxide, carbon dioxide, and smoke emissions with special increase of nitrogen oxides compared to diesel fuel. There was no also unusual change in engine oil composition from using BDF 20. Most of engine parts were clean and showed little wear, but soots were detected around the hole of fuel injector when BDF 20 was used in direct injection diesel engine for 200 hours.

Combustion Performance Tests of Sub-scale Combustor for Liquid Rocket Engine (다종의 축소형 고압연소기 연소성능시험)

  • Kim Seung-Han;Seo Seonghyeon;Moon Il-Yoon;Seol Woo-Seok;Cho Gwang-Rae;Han Yeoung-Min
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.259-264
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    • 2004
  • The critical component of combustor having high combustion efficiency for high performance liquid rocket engine is injector. The results of design and hot firing tests of six sub-scale combustors which have respectively an impinging type injector(1ea.), an bi-propellant swirl closed injector(1ea.), and hi-propellant swirl mixed injector(4ea.) were described in this paper. The combustion test were successfully performed. The combustion efficiency have higher value than predicted value and high frequency combustion instability does not occur.

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Analysis on the Characteristics of RICEM for Researching Combustion Characteristics of Linear Hydrogen Power System (리니어 수소동력시스템의 연소연구용 급속흡입압축기의 특성 해석)

  • Lee, J.H.;Kim, K.M.;Jeong, D.Y.;Lee, Jong-T.
    • Journal of Hydrogen and New Energy
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    • v.16 no.1
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    • pp.66-73
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    • 2005
  • Hydrogen linear power system is estimated as the next generation power system which can obtain a performance as same as fuel cell. In order to develop Hydrogen combustion power system with high thermal efficiency, it is very important to understand the basic characteristics of hydrogen combustion and establish combustion stabilization technique of its system. In this study, RICEM(Rapid Intake Compression Expansion Machine) for researching of hydrogen combustion linear power system was manufactured and evaluated, and the basic characteristics of linear RICEM were analyzed.

The effects of oxygen-concentration increased by oxygen-enriching membrane on combustion of S.I. engines (기체분리막에 의해 상승된 산소농도가 스파크점화기관의 연소에 미치는 영향)

  • 권병철;김형섭
    • Journal of the korean Society of Automotive Engineers
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    • v.14 no.6
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    • pp.74-80
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    • 1992
  • The purpose of this study is to improve the performance of gasoline engine. Combustion-characteristics orignated from supplying cylinder with fuel-air mixture which was formed by the rise of oxygen-concentration in air with oxygen-enriching membrane have been investigated. The results showed that the poor-limit of oxygen-concentration was increased by shortening combustion-duration because the rise of oxygen-concentration in fuel-air mixture resulted in the promotion of combustion-velocity. Also, the generation of large output of power was expected from combustion in proportion as the amount of oxygen was increased.

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Effect of Reentrant Type Bowl Geometry on Combustion Characteristics in Diesel Engine -Effect of Reentrant Angle and Cupola Height of Bowl Center- (리엔트런트형 연소실 형상이 디젤기관의 연소특성에 미치는 영향 -리엔트런트 각도 및 중앙돌기부 높이의 효과-)

  • Kwon, S.I.
    • Transactions of the Korean Society of Automotive Engineers
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    • v.3 no.3
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    • pp.37-45
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    • 1995
  • Effect of reentrant type bowl geometry on combustion characteristics was investigated in a D.I. diesel engine. The main factor was the cupola height of bowl center and the reentrant angle of combustion chamber, and the cylinder pressure, engine performance and emissions of the engine using the total 11 kinds of the combustion chamber were measured by test. The results are as follows. The NOx decreases by increasing the cupola height of bowl center because it makes the decreasing of maximum combustion pressure by the heat loss and smooth combustion from good airflow. The smoke increases by increasing the reentrant angle at high speed range of the engine, but decrease at low and medium speed range until the reentrant angle becomes $15^{\circ}$.

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