• 제목/요약/키워드: 예혼합

검색결과 854건 처리시간 0.027초

직교류 열교환기의 모듈수에 따른 열전달 및 압력강하 특성 (Heat Transfer and Pressure Drop of Cross-flow Heat Exchanger on Modules Variation)

  • 김종민;김진수;유병훈;금성민;이창언;이승로
    • 에너지공학
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    • 제22권2호
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    • pp.120-127
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    • 2013
  • 본 연구는 예혼합 연소시스템에 적용할 직교류 엇갈림 배열 열교환기의 열전달 및 압력강하 특성 검토를 목적으로 한다. 따라서 비예혼합화염보다 화염길이가 짧고 당량비 조절을 통해 NOx 및 CO 배출을 제어할 수 있는 예혼합방식의 버너 앞에 모듈로 구성된 열교환기를 설치한 후 당량비를 변화시킬 때 NOx와 CO의 배출특성을 검토하였다. 또한 열교환기의 모듈 변화에 대한 유용도, 엔트로피 생성량 및 압력강하를 계산하였고 엑서지 로스를 검토하여 열교환기의 성능을 분석하였다.

가솔린 균일 예혼합 압축착화 엔진의 착화시점 검출 (Start of Combustion Detection Method for Gasoline Homogeneous Charge Compression Ignition Engine)

  • 최두원;이민광;선우명호
    • 한국자동차공학회논문집
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    • 제16권4호
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    • pp.151-158
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    • 2008
  • Gasoline Homogeneous Charge Compression Ignition (HCCI) combustion is a new combustion concept. Unlike the conventional internal combustion engine, the premixed fuel mixture with high residual gas rate is auto-ignited and burned without flame propagation. There are several operating factors which affect HCCI combustion such as start of combustion (SOC), residual gas fraction, engine rpm, etc. Among these factors SOC is a critical factor in the combustion because it affects exhaust gas emissions, engine power, fuel economy and combustion characteristics. Therefore SOC of gasoline HCCI should be controlled precisely, and SOC detection should be preceded SOC control. This paper presents a control oriented SOC detection method using 50 percent normalized difference pressure. Normalized difference pressure is defined as the normalized value of difference pressure and difference pressure is difference between the in-cylinder firing pressure and the motoring pressure. These methods were verified through the HCCI combustion experiments. The SOC detection method using difference pressure provides a fast and precise SOC detection.

메탄-산소 층류화염전파속도 측정 (Determination of Laminar Burning Velocity in Premixed Oxy-Methane Flames)

  • 오정석;노동순;이은경;홍성국
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.258-262
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    • 2011
  • 실험용 분젠 연소기를 사용하여 예혼합된 메탄-산소 층류화염전파속도를 연구하였다. 이를 위해 $CH^*$ 자발광 측정기법과 슐리렌 사진술이 사용되었다. 실험결과는 CHEMKIN 3.7을 이용한 수치해석 결과와 비교하였다. 층류화염전파속도를 측정하기 위하여 층류여역 내에서 전체 당량비는 0.5에서 2.0까지 조절하였다. 동축 화염에서 화염전파속도는 각도측정법을 사용하였으며 슐리렌 사진에서는 3.1 m/s로 $CH^*$ 자발광 사진에서는 2.9 m/s로 측정되었다.

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냉시동시 압축착화 조건의 상관관계에 관한 수소 HCCI 기관의 실험적 연구 (An Experimental Study on Correlation of Compression Ignition Condition at Cold Start with Hydrogen HCCI Engine)

  • 이광주;이종구;안병호;이종태
    • 한국수소및신에너지학회논문집
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    • 제23권6호
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    • pp.628-633
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    • 2012
  • It was found that the pure hydrogen-air pre-mixture was self-ignited at a high compression ratio without any assisting method in room temperature, thus refuting the preconception that compression ignition of hydrogen engine was impossible. Therefore, in order to analyze the correlation of compression ignition condition at cold start with hydrogen HCCI engine clearly, the possibility of compression igniting compression ratio is investigated with the change of equivalence ratio and engine speed, experimentally. As the results, it is confirmed that the possibility of compression-igniting compression ratio at cold start was decreased by increasing equivalence ratio due to decreasing auto-ignition temperature. In addition, it is grasped that the possibility of compression-igniting compression ratio at cold start is decreased around 14.9% by increasing engine speed at same supply energy.

희박 예혼합 모형 가스터빈 연소기의 화염구조와 배기특성에 관한 실험적 연구 (Experimental Investigation on Flame Structure and Emission Characteristics in a Lean Premixed Model Gas Turbine Combustor)

  • 문건필;이종호;전충환;장영준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.356-361
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    • 2003
  • The objective of this study is a qualitative comparison between line-integrated OH chemiluminescence ($OH{\ast}$) image and its Abel inversion image at different phase of the oscillating pressure field. PIV(Particle Image Velocimetry) measurements were conducted under non-reacting conditions to see the global flow structure. Also NOx emission was measured to investigate the effect of fuel-air premixing on combustion instability and emission characteristics. Experiments were carried out in an atmospheric pressure, laboratory-scale dump combustor operating on natural gas. Combustion instabilities in present study exhibited a longitudinal mode with a dominant frequency of ${\sim}341.8$ Hz, which corresponded to a quarter wave mode of combustor. Heat release and pressure waves were in-phase when instability occurred. Results gave an insight about the location where the strong coherence of pressure and heat release existed. Also an additional information on active control to suppress the combustion instabilities was obtained. For lean premixed combustion, strong correlation between $OH{\ast}$ and NOx emissions was expected largely due to the exponential dependence of thermal NOx mechanism on flame temperature.

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하이브리드/이중 선회제트 연소기에서 부분예혼합-예혼합 선회화염의 상호작용 (Interaction Between Partially Premixed and Premixed Swirl Flames in a Hybrid/Dual Swirl Jet Combustor)

  • 조준익;황철홍;이기만
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2012년도 제44회 KOSCO SYMPOSIUM 초록집
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    • pp.7-8
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    • 2012
  • The effects of interaction between partially premixed and premixed swirl flames on CO and NOx emissions were experimentally investigated using a hybrid/dual swirl jet combustor for a micro-gas turbine. Under the condition of constant angle ($45^{\circ}$) for outer swirl vane, the angle and direction of inner swirl vane installed for a partially premixed flame were varied as main parameters with a constant fuel flow rate for each nozzle. It was found that for all conditions, CO and NOx emissions were measured below 4 ppm and 15 ppm at 15% $O_2$, respectively, in a wide range of equivalence ratio (0.6~0.9). For co-swirl flows, CO emission increased dramatically as the angle of inner swirl vane increased from $15^{\circ}$ to $45^{\circ}$ near lean-flammability limit (i.e. equivalence ratio of 0.5). On the other hand, the case of swirl $angle=45^{\circ}$ provided the lowest NOx emission at higher equivalence ratios than 0.6. For counter-swirl flows, the case of swirl $angle=45^{\circ}$ extended the lean-flammability limit but higher NOx emissions were found compared to those of co-swirl flows. These results could be inferred by interaction between (inner) partially premixed and (outer) premixed swirl flames. However, these estimations were not clear yet because there was insufficient data on turbulent flow structure and fuel-air mixing in the present experimental approach.

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난류 예혼합 화염에서의 프랙탈 차원의 통계적 특성 (Statistical Characteristics of Fractal Dimension in Turbulent Prefixed Flame)

  • 이대훈;권세진
    • 대한기계학회논문집B
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    • 제26권1호
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    • pp.18-26
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    • 2002
  • With the introduction of Fractal notation, various fields of engineering adopted fractal notation to express characteristics of geometry involved and one of the most frequently applied areas was turbulence. With research on turbulence regarding the surface as fractal geometry, attempts to analyze turbulent premised flame as fractal geometry also attracted attention as a tool for modeling, for the flame surface can be viewed as fractal geometry. Experiments focused on disclosure of flame characteristics by measuring fractal parameters were done by researchers. But robust principle or theory can't be extracted. Only reported modeling efforts using fractal dimension is flame speed model by Gouldin. This model gives good predictions of flame speed in unstrained case but not in highly strained flame condition. In this research, approaches regarding fractal dimension of flame as one representative value is pointed out as a reason for the absence of robust model. And as an extort to establish robust modeling, Presents methods treating fractal dimension as statistical variable. From this approach flame characteristics reported by experiments such as Da effect on flame structure can be seen quantitatively and shows possibility of flame modeling using fractal parameters with statistical method. From this result more quantitative model can be derived.

연소 불안정 예측을 위한 열음향 해석 모델 - Part 1 : 선형 안정성 해석 (Thermoacoustic Analysis Model for Combustion Instability Prediction - Part 1 : Linear Instability Analysis)

  • 김대식;김규태
    • 한국추진공학회지
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    • 제16권6호
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    • pp.32-40
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    • 2012
  • 가스터빈 희박 예혼합 연소기에서 발생하는 연소 불안정의 고유 주파수 및 초기 성장률의 예측을 위하여 선형 열음향 해석 모델이 소개되었다. 모델 검증을 위하여 입출구 조건이 잘 정의되고, 상대적으로 이전 연구 결과에서 적용된 연소기에 비하여 구조가 간단한 모델 연소기가 선정되었다. 정의된 연소기에서 음향 해석을 위한 선형 관계식이 유도되었고, 이를 통하여 선형 안정성 해석 방안이 제시되었다. 해석 결과 연소 불안정의 특성에 대한 전체적인 변화 경향은 성공적으로 예측하였으나, 주파수의 절대값에 있어서는 실제 실험 결과보다 다소 작은 값을 예측하는 것으로 나타났다. 이러한 주파수의 예측 오차는 짧은 화염보다는 긴 화염에서 더욱 두드러지는 것으로 나타났다.

모형 가스터빈 연소기에서 희박 예혼합 화염의 연소 특성 및 유동 해석에 관한 연구 (A Study on Combustion Characteristics and Flow Analysis of a Lean Premixed Flame in Lab-Scale Gas Turbine Combustor)

  • 유혜연;김규보;전충환;장영준
    • 대한기계학회논문집B
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    • 제32권8호
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    • pp.574-581
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    • 2008
  • The characteristics of combustion and flow for a lean premixed flame in lab-scale gas turbine combustor was studied through experiment and numerical analysis. From the experiment, flame structure and heat release rate were obtained from OH emission spectroscopy. Qualitative comparisons were made line-integrated OH chemiluminescence image and abel-transformed one. NOx analyzer was implemented to get the characteristic of NOx exhaust from the combustor. From the numerical analysis, the thermal distribution and characteristic of recirculation zone with the change of fuel-air mixing degree, the characteristic of methane distribution with equivalence ratio in the combustor respectively. Total heat release rate is increased with increasing equivalence ratio. Thermal Nox is reduced with increasing fuel-air mixing degree. Increasing equivalence ratio results in the decrease of the size of reaction zone and alteration of the position of the reaction zone into the entrance of the combustor.

디젤 예혼합 압축착화 엔진에서 배기가스 재순환과 과급의 영향 (Effect of EGR and Supercharging on the Diesel HCCI Combustion)

  • 박세익;국상훈;배충식;김장헌
    • 한국자동차공학회논문집
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    • 제14권5호
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    • pp.58-64
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    • 2006
  • Homogeneous charge compression ignition(HCCI) combustion is an advanced technique for reducing the hazardous nitrogen oxide(NOx) and particulate matter(PM) in a diesel engine. NOx could be reduced by achieving lean homogeneous mixture resulting in combustion temperature. PM could be also reduced by eliminating fuel-rich zones which exist in conventional diesel combustion. However previous researches have reported that power-output of HCCI engine is limited by the high intensive knock and misfiring. In an attempt to extend the upper load limit for HCCI operation, supercharging in combination with Exhaust Gas Recirculation(EGR) has been applied: supercharging to increase the power density and EGR to control the combustion phase. The test was performed in a single cylinder engine operated at 1200 rpm. Boost pressures of 1.1 and 1.2 bar were applied. High EGR rates up to 45% were supplied. Most of fuel was injected at early timing to make homogeneous mixture. Small amount of fuel injection was followed near TDC to assist ignition. Results showed increasing boost pressure resulted in much higher power-output. Optimal EGR rate influenced by longer ignition delay and charge dilution simultaneously was observed.