• 제목/요약/키워드: Combustion Measurement

검색결과 541건 처리시간 0.027초

연소장내 화염계측 오차 평가 (Error Evaluation on Flame Measurement in Combustion Field)

  • 양영준;허태영
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2014년도 추계학술대회 논문집
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    • pp.167-169
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    • 2014
  • Spray combustion has been used in many industrial fields, for instance, such as diesel engines, gas turbines and industrial furnaces, and furthermore various measurement techniques have been applied to elucidate the phenomenon of spray combustion. In order to measure simultaneously the droplet velocity and the droplet size of spray, Phase Doppler Anemometry (PDA) was frequently used in spray combustion. However, the measurement error is occurred due to existence of flame, which is considered as influencing the precision of measurement. Therefore, the purpose of this study is experimentally to conduct the systematic evaluation on the measurement error when PDA measurement is applied to combustion field.

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이중관 구조 박막형 순간온도 프로브의 응답성에 관한 연구 (A Study on the Responsibility of Thin film instantaneous surface temperature probe of a Dual-pipe structure)

  • 최석렬;박경석
    • 한국연소학회:학술대회논문집
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    • 대한연소학회 2003년도 제27회 KOSCO SYMPOSIUM 논문집
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    • pp.237-242
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    • 2003
  • The measurement study of instantaneous temperature at combustion chamber wall and the temperature of combustion gas has been under lots of research and development to conclude the temperature process in internal combustion engine for combustion characteristics analysis. The measurement with fast responsibility should be used for temperature measurement inside combustion chamber wall since temperature of wall changes, due to the various gas temperature, irregularly during the combustion. Therefore, thin film instantaneous surface temperature probe, which characterizes the fastest and the most accurate responsibility among contact typed temperature measurement, was used for the experiments. This new thin film instantaneous surface temperature probe improved the problems of noise and durability. The optimal coating thickness of thin film instantaneous surface temperature probe was proven to be $10{\mu}m$ for the best responsibility and durability. It also allowed the stable temperature measurement be taken up to $1,200^{\circ}C$ and proven to be read possibly from the combustion chamber wall.

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위상도플러 유속계를 이용한 계측에 있어서의 화염에 기인한 오차의 평가 (The evaluation of error due to flame in the measurement using phase doppler anemometry)

  • 양영준
    • 센서학회지
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    • 제14권5호
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    • pp.313-321
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    • 2005
  • Spray combustion has been used in many industrial fields, for instance, such as diesel engines, gas turbines and industrial furnaces, and furthermore various measurement techniques have been applied to elucidate the phenomenon of spray combustion. In order to measure simultaneously the droplet velocity and the droplet size of spray, phase doppler anemometry (PDA) was frequently used in spray combustion. However, the measurement error is occurred due to existence of flame, which is considered as influencing the precision of measurement. Therefore, the purpose of this study is experimentally to conduct the systematic evaluation on the measurement error when PDA measurement is applied to combustion field.

건식 저 NOx 가스터빈의 연소동압 측정용 소프트웨어 시스템 개발 (Development of a Software System for Measurements of Combustion Dynamics of a Dry Low NOx Gas Turbine)

  • 장욱;서석빈;정재화;안달홍;김종진;차동진
    • 설비공학논문집
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    • 제14권11호
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    • pp.931-938
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    • 2002
  • Combustion dynamics of a dry low NOx gas turbine have been measured by utilizing a dynamic pressure measurement system. The software part of the measurement system, implemented with a commercial general-purpose DASYLab version 5.6 code, basically acquires combustion dynamics signals, performs the FFT analysis, and displays the results. The gas turbine often experiences momentary combustion instability, especially when its combustion mode changes. It is found that the measurement system developed in the study may outperform the other commercial dynamic pressure measurement system. The developed system currently serves to monitor the combustion dynamics of the gas turbine.

동시 시계열 계측에 의한 예혼합 분무화염 내 유적군 연소기구의 평가 (Evaluation of Combustion Mechanism of Droplet Cluster in Premixed Spray Flame by Simultaneous Time-Series Measurement)

  • 황승민
    • 대한환경공학회지
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    • 제31권6호
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    • pp.442-448
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    • 2009
  • 예혼합 분무화염의 유적군 연소 기구를 평가하기 위하여 레이저 가시화법, MICRO (multi-color integrated Cassegrain receiving optics) 및 PDA (phase Doppler anemometer) 광학계측 시스템을 이용하여 동시 시계열 계측을 실시하였다. 또한 유적군의 군연소수를 실험적으로 산출하여 이론해석에 적용하였을 경우 실제로 관찰되는 군연소 형태와 일치하는지에 대하여 검토하였다. 유적군 단면화상에 의해 확인된 모든 유적군에 대하여 실험적으로 군연소수 $G_c$를 산출한 결과 주로 내부 군연소와 외부 군연소로 분류되었으며 이론해석과 일치하였다. 또한 실제 관찰된 군연소 형태와 그 유적군의 군연소수를 이론해석에 적용한 경우에 군연소 형태가 일치하는 경우와 일치하지 않는 경우가 있었다. 일치하지 않는 원인은 군연소수를 유적의 기하학적 배치만으로 결정한 것이나 현상의 3차원성이 측정 결과에 영향을 미친 것이라고 생각되어진다.

고온 CO2 가스의 복사 파장을 이용한 부분별 온도 측정 (Temperature Measurement by Radiation Wavelength of High Temperature CO2 gas)

  • 맹새롬;유미연;김세원;이창엽
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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    • pp.315-316
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    • 2014
  • Combustion gases emit various radiation signals by chemical reaction and excited molecules in combustion system. Since temperature measurement of combustion system is very difficult, non-contact temperature measuring methods are being researched. In this paper, we propose optical system of simple structure and implement technique for measuring temperature partially in furnace using radiation wavelength signals of high temperature $CO_2$ gas generated during combustion.

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난류 화염 구조 규명을 위한 조건 평균 측정법 (Conditional Sampling Measurement to Identify Flame Structures in Turbulent Combustion)

  • 허강열
    • 한국가시화정보학회지
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    • 제2권1호
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    • pp.8-11
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    • 2004
  • Conditional sampling measurement is required for conditional averages as well as unconditional Favre averages to resolve different flame structures of turbulent combustion. A Favre average can be obtained as an integral of conditional average and Favre PDF in terms of the mixture fraction, which is a preferred choice as a sampling variable in diffusion controlled turbulent combustion. MILD combustion data are presented as an example for a conditionally averaged data set and comparison with CMC calculation results.

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동시계측에 의한 난류 미분탄 화염의 순간구조에 관한 연구 (Study on Instantaneous Structure of Turbulent Pulverized Coal Flame by Simultaneous Measurement)

  • 황승민
    • 한국환경과학회지
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    • 제27권5호
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    • pp.309-317
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    • 2018
  • In this study, a laser sheet technique and PLIF (Planar laser-induced fluorescence) are applied to a laboratory-scale pulverized coal burner of the open type, and the spatial relationship of the pulverized coal particle zone and the combustion reaction zone is examined by simultaneous measurement of Mie scattering and OH-LIF images. It is found that this technique can be used to investigate the spatial relationship of the combustion reaction zone and pulverized-coal particles in turbulent pulverized-coal flames without disturbing the combustion reaction field. In the upstream region, the combustion reaction occurs only in the periphery of the clusters where high-temperature burned gas of the methane pilot flame is entrained and oxygen supply is sufficient. In the downstream region, however, combustion reaction can be seen also within clusters of pulverized-coal particles, since the temperature of pulverized-coal particles rises, and the mixing with emitted volatile matter and ambient air is promoted.

보일러 연소해석시와 측정시의 연소가스 중량 및 체적비교 (Comparison of the Product Properties between Combustion Analysis and Measurement)

  • 장석원;임상규;정훈;이인철
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.368-372
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    • 2003
  • There arc two methods to evaluate the combustion product, that is analysis method and measurement method. Properties of the combustion products, constituents, and quanties, can be used to calculate boiler efficiency and beat losses. Using combustion evaluation methods combustion calculation were performed at certain condition and analyze the results. In this paper by comparing the results between two methods, deviation, correction and possibility of site application were confirmed

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하이브리드 로켓 모터에 대한 연소 실험 측정 불확도 (Combustion Experiment Measurement Uncertainty for Hybrid Rocket Motor)

  • 김수종;문희장;김진곤
    • 한국항공운항학회지
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    • 제19권1호
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    • pp.7-14
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    • 2011
  • In this study, the measurement uncertainty of combustion experimental system and experimental parameters for hybrid rocket were evaluated by B type evaluation method. The measurement uncertainty of all experimental parameters was lower than 3%. The highest value of expanded uncertainty was characteristic velocity efficiency with 2.83% and the expanded uncertainty of regression rate which is the design and performance parameter was indicated to 0.03%. These results shown that the reliability of hybrid combustion system was located within allowed limits.