• 제목/요약/키워드: Gas release

검색결과 661건 처리시간 0.023초

모델 가스터빈 연소기내의 자발 불안정성에 관한 실험적 연구 (An Experimental Study on the Self-excited Instabilities in Model Gas Turbine Combustor)

  • 이민철;홍정구;신현동
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2004년도 제29회 KOSCI SYMPOSIUM 논문집
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    • pp.197-205
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    • 2004
  • Most of gas turbines is operated by the type of dry premixed combustion to reduce NOx emission and economize fuel consumption. However this type operation, combustion induced instability brought failure problems cause by high pressure and heat release fluctuations. Though there has been lots of studies since Lord Rayleigh to understand this instability mechanism and control the instabilities, none of them made matters clear. In order to understand the instability phenomena, a simple experimental study with dump combustor was conducted at the moderate pressure and ambient temperature conditions. From this model gas turbine combustor self-excited instabilities at the resonance mode(200Hz) and bulk mode(10Hz) were occurred and observed at the three points of view; pressure, heat release and equivalence ratio which are acquired by peizo-electric transducer, HICCD camera and acetone LIF respectively. From this results we could see the instability mechanism clear with the account of time scale analysis which explained by the propagation of pressure wave to the upward of mixture stream and convectional transfer of the equivalence ratio fluctuation by this pressure fluctuation.

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연료 과농 가스발생기의 연소 안정성 특성 연구 (Combustion Stability Characteristics of Fuel-Rich Gas Generators)

  • 서성현;한영민;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제29회 추계학술대회논문집
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    • pp.119-122
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    • 2007
  • 본 연구에서는 가스발생기의 연소 안정 특성을 파악하기 위해 실험적 방법을 적용하였다. 액체산소와 Jet A-1을 추진제로 사용하며 연료 과농 상태에서 작동하는 실험 가스발생기는 연소실 축 방향 공진 모드에 결합된 1200 Hz 대역의 고주파 연소불안정을 겪었다. 이 연소불안정의 발생 유무는 연소실 출구부의 음향 경계 조건과 화염의 열 발생 축 방향 위치에 매우 민감하게 반응하였다. 결과적으로 단일 분사기 노즐 크기 증가에 의한 화염의 축 방향 길이 증가는 연소안정성을 확연하게 향상시켰다.

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에어백 인플레이터의 수중폭발 특성에 대한 실험 연구 (An Experimental Study on UNDEX Characteristics of Airbag Inflators)

  • 김형준;최걸기;나양섭;박경훈;정현
    • 대한조선학회논문집
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    • 제54권5호
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    • pp.439-446
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    • 2017
  • This paper deals with an experimental study of the dynamics of an underwater bubbles and shock waves, generated by rapid underwater release of highly compressed gas. Aribag inflators, which are used for automobile's airbag system, are used to generate the extremely-rapid underwater gas release. Experimental studies of the complex underwater bubble dynamics as well as underwater shock wave were carried out in a specifically designed cylindrical water tank. The water tank is equipped with a high-speed camera and pressure sensors. The high-speed camera was used to capture the expansion and collapse of the gas bubble created by inflators, while pressure sensors was used to measure the underwater shock propagation and magnitudes. The experimental results were compared against the results of explosion of pentolite explosive. Several physical phenomena that has been observed and discussed, which are different from the explosive underwater explosion.

연소실 길이에 따른 이중선회 가스터빈 모델 연소기에서 연소불안정 모드 연구 (A Study of Combustion Instability Mode according to the Variation of Combustor Length in Dual Swirl Gas Turbine Model Combustor)

  • 장문석;이기만
    • 한국연소학회지
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    • 제21권2호
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    • pp.29-37
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    • 2016
  • This study described the experimental investigations of combustion instability in a model gas turbine combustor. Strong coupling between pressure oscillations and unsteady heat release excites a self-sustained acoustic wave, which results in a loud and annoyed sound, and may also lead to a structural damage to the combustion system. In this study, in order to examine the combustion instability phenomenon of a dual swirling combustor configuration, the information of heat release and pressure fluctuation period with respect to the variation in both thermal power and combustor length was collected experimentally. As a result, the fundamental acoustic frequency turned out to increase with the increasing thermal power without respect to the combustor length. The frequency response to the combustor length was found to have two distinct regimes. In a higher power regime the frequency significantly decreases with the combustor length, as it is expected from the resonance of gas column. However, in a lower power regime it is almost insensitive to the combustor length. This insensitive response might be a result of the beating phenomenon between the interacting pilot and main flames with different periods.

Specific Process Conditions for Non-Hazardous Classification of Hydrogen Handling Facilities

  • Choi, Jae-Young;Byeon, Sang-Hoon
    • Safety and Health at Work
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    • 제12권3호
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    • pp.416-420
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    • 2021
  • Hazardous area classification design is required to reduce the explosion risk in process plants. Among the international design guidelines, only IEC 60079-10-1 proposes a new type of zone, namely zone 2 NE, to prevent explosion hazards. We studied how to meet the zone 2 NE grade for a facility handling hydrogen gas, which is considered as most dangerous among explosive gases. Zone 2 NE can be achieved considering the grade of release, as well as the availability and effectiveness of ventilation, which are factors indicative of the facility condition and its surroundings. In the present study, we demonstrate that zone 2 NE can be achieved when the degree of ventilation is high by accessing temperature, pressure, and size of leak hole. The release characteristic can be derived by substituting the process condition of the hydrogen gas facility. The equations are summarized considering relation of the operating temperature, operating pressure, and size of leak hole. Through this relationship, the non-hazardous condition can be realized from the perspective of inherent safety by the combination of each parameter before the initial design of the hydrogen gas facility.

수소 폭발위험범위에 대한 IEC기준과 시뮬레이션 결과의 비교분석 (Comparative Analysis of IEC Standard and Simulation Results for Hydrogen Hazardous Distance)

  • 안승효;김은희;이선희;마병철
    • 한국가스학회지
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    • 제28권1호
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    • pp.19-26
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    • 2024
  • 수소 등 인화성 가스를 취급하는 사업장은 KS C IEC 60079-10-1 기준에 따라 취급시설 주변을 폭발위험장소로 구분하여 관리하여야 한다. 그렇지만 동 기준은 가스의 종류, 실내·외 여부, 대기조건 등의 구분없이 누출특성값을 기준으로 폭발위험범위를 산정하므로 실효성 등에 대한 의문이 제기되고 있다. 본 연구에서는 수소를 대상으로 누출특성과 실외대기 조건에서 시뮬레이션(PHAST 및 HyRAM)을 통해 폭발위험범위를 도출하고 IEC 기준의 log-log 그래프에서 비교하였으며, 각 결과에 대한 회귀분석을 수행하였다. 그 결과, 각 조건에서 시뮬레이션 결과가 IEC 기준보다 0.6~3.8배 이상 적게 나타났으며, 동일한 누출특성값에서 풍속 및 대기안정도에 따라 폭발위험범위가 상이한 것을 확인할 수 있었다. 또한, 간편하게 사용할 수 있는 누출특성과 폭발위험범위에 대한 선형회귀식을 도출하였다. 따라서, 수소 취급 사업장 등에서 폭발위험범위 산정 시 본 연구에서 제시한 그래프와 선형회귀식을 통하여 IEC 기준과 시뮬레이션 결과를 용이하게 비교 및 활용할 수 있을 것으로 판단된다. 이를 적용할 경우 합리적인 폭발위험장소 구분이 가능하여 경제적인 부담을 최소화할 수 있을 것으로 기대되며, 수소 폭발 등의 위험성을 크게 감소시킬 수 있을 것으로 전망한다.

Hypoxia-Induced EDNO Release is Further Augmented by Previous Hypoxia and Reoxygenation in Rabbit Aortic Endothelium

  • Han, Jae-Jin;Suh, Suk-Hyo;Suh, Kyung-Phil;Kim, Ki-Whan
    • The Korean Journal of Physiology and Pharmacology
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    • 제2권2호
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    • pp.209-216
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    • 1998
  • The present study was designed: (1) to determine whether or not hypoxia stimulates the release of endothelium-derived relaxing factors (EDRFs) from endothelial cells, and (2) to examine whether or not the hypoxia-induced EDRFs release is further augmented by previous hypoxia-reoxygenation, using bioassay system. In the bioassay experiment, rabbit aorta with endothelium was used as EDRFs donor vessel and rabbit carotid artery without endothelium as a bioassay test ring. The test ring was contracted by prostaglandin $F_{2{\alpha}}$ $(3{\times}10^{-6}\;M/L)$, which was added to the solution perfusing through the aortic segment. Hypoxia was evoked by switching the solution aerated with 95% $O_2/5%\;CO_2$ mixed gas to one aerated with 95% $N_2/5%\;CO_2$ mixed gas. When the contraction induced by prostaglandin $F_{2{\alpha}}$ reached a steady state, the solution was exchanged for hypoxic one. And then, hypoxia and reoxygenation were interchanged at intervals of 2 minutes (intermittent hypoxia). The endothelial cells were also exposed to single 10-minute hypoxia (continuous hypoxia). When the bioassay ring was superfused with the perfusate through intact aorta, hypoxia relaxed the precontracted bioassay test ring markedly. Whereas, when bioassay ring was superfused with the perfusate through denuded aorta or polyethylene tubing, hypoxia relaxed the precontracted ring slightly. The relaxation was not inhibited by indomethacin but by nitro-L-arginine or methylene blue. The hypoxia-induced relaxation was further augmented by previous hypoxia-reoxygenation and the magnitude of the relaxation by intermittent hypoxia was significantly greater than that of the relaxation by continuous hypoxia. The results suggest that hypoxia stimulates EDNO release from endothelial cells and that the hypoxia-induced EDNO release is further augmented by previous hypoxia-reoxygenation.

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자료동화기술을 이용한 대기중 오염물질 확산평가 (Data Assimilation Techniques Applied to Estimate the Dispersion of the Pollutant in the Atmosphere)

  • 한문희;정효준;김은한;서경석;황원태;이선미
    • 한국방사성폐기물학회:학술대회논문집
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    • 한국방사성폐기물학회 2004년도 학술논문집
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    • pp.368-376
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    • 2004
  • 영광부지의 추적자 확산실험결과의 자료동화를 통하여 Gaussian plume 모형의 확산인자의 수정과 추적자 방출률 평가를 수행하였다. 부지 주변의 여러 지점에서 관측한 실험결과에 선형계획법을 적용하여 확산평가에 있어선 가장 불확실성이 크다고 알려진 확산인자를 수정하였다. 원자력 비상시 초기 대응평가에 사용되는 정보 가운데 가장 큰 불확실성을 포함한 선원항 정보를 추적자 농도 분포로부터 추정하였다. 실험 당시의 추적자 방출량을 모른다고 가정하고 Gaussina plume 모형의 예측치와 확산실험의 실측치를 이용한 최소자승법을 적용하여 방출률을 추정하였다. 확산인자를 수정한 후 Gaussian plume 모형의 예측력은 방출점으로 3km 및 8km 떨어진 포집선 두 경우 모두 증가하는 것으로 나타났다. 실험당시의 방출률을 모른다고 가정하고 관측지점의 농도에 최소자승법을 적용한 결과 24%이내에서 실제 방출률을 양호하게 추정하고 있음을 확인할 수 있었다.

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증기누출사고의 영향평가에서 제트화재에 미치는 매개변수의 영향 (The Effects of Parameters Affecting the Results in the Jet Fire for the Vapor Release Accident)

  • 조지훈;하정호;함병호;윤대건;김태옥
    • 한국화재소방학회:학술대회논문집
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    • 한국화재소방학회 1996년도 학술발표회
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    • pp.53-56
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    • 1996
  • In order to propose the method of the consequence analysis for fire accidents by the heavy gas release and to obtain optimum conditions of parameter selections, the consequence analysis for jet fire by the accident of xylene vapor release were performed. And the effect and the sensitivity analysis of parameters affecting the consequence were investigated. Simulation results showed that important parameters affecting results of the xylene vapor release accident were mainly hole diameter, interested distance, wind speed, and so on. For the jet fire, the accident result and the sensitivity of thermal radiation were increased with the decrease of interested distance and the increase of hole diameters, and the accidental result was increased as the increase wind speed, but the sensitivity of thermal radiation was decreased.

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