• Nuclear Engineering and Technology
• /
• v.26 no.3
• /
• pp.411-419
• /
• 1994

The containment failure probability due to hydrogen burning during severe accidents proceeding in a low pressure sequence is calculated using Monte Carlo method. The probability distribution functions for this Monte Carlo calculation is obtained from the statistical method. The calculations are performed for Kori unit 2, and the sensitivity studies on the input variables-the amount of hydrogen generated at SFD, cerium diameter, cerium length, oxidation rate at FCI, and the amount of hydrogen generated during MCCI-are also performed. It is revealed that SFD is the main factor in hydrogen generation, but the other sources also cannot be neglected. The containment failure probability due to the hydrogen burning lies within 6% in case of Kori unit 2.

• Proceedings of the KSME Conference
• /
• 2000.11b
• /
• pp.142-149
• /
• 2000

The results of stand and field testing of a combustion chamber for a heavy-duty 150 MW gas turbine are discussed. The model represented one of 14 identical segments of a tubular multican combustor constructed in the scale 1:1. The model experiments were executed at a pressure smaller than in the real gas turbine. The combustion efficiency, pressure loss factor, pattern factor, liner wall temperature, flame radiation, fluctuating pressure, and NOx emission were measured at partial and full load for both model and on-site testing. The comparison of these items of information, received on similar modes in the stand and field tests, has allowed the development of a method of calculation and the improvement of gas turbine combustors.

• Transactions of the Korean Society of Mechanical Engineers
• /
• v.12 no.6
• /
• pp.1372-1380
• /
• 1988

A heat transfer model for a pulse combustion water heater is developed, and an associated computer simulation is conducted to determine the temperature distribution as well as heat transfer rate. Parametric studies are performed to examine the effects of the operating and design variables on the thermal performance and heat transfer rate. They are found to be influenced mainly by energy input rate, the amount of excess air, the volume of combustion chamber, and the diameter of flue tube.

• 한국연소학회:학술대회논문집
• /
• 2000.12a
• /
• pp.236-245
• /
• 2000

A laboratory scale fluidized bed reactor was developed to treat the combustion characteristics of some fuels (wood, paper sludge, refuse derived fuel). The aims were to introduce the means of experiment and interpretation of the results and finally determine the particle characteristics on the pyrolysis and combustion process of the fuel. A single particle combustion process in the fluidized bed was closely observed. Understanding experimental facility characteristics and determining parameters were also carried out. The fuel combustion processes were observed by carbon conversion rate, recovery and mean carbon conversion time. They were estimated with the CO, $CO_2$ gas concentration monitored at the exit of the combustor. Fuel drying and pyrolysis process were governed by temperature distribution in the fuel particle. There was a significant overlap of the drying and devolatilization. However, transition process from devolatilization to char combustion seemed to be determined by mechanical solidity of the fuel particle after devolatilization process.

• 한국연소학회:학술대회논문집
• /
• 2012.04a
• /
• pp.41-42
• /
• 2012

Circulating fludized bed(CFB) furnace which can use a variety of low-grade fuels because of high heat capacity and good mixing characteristic in its furnace have turned out to be effective system. There is no many research to design CFB boiler in korea. thus, we feel necessity to research design method. So far accurate hydrodynamics and combustion mechanism information in CFB furnace has been lacked. Therefore, design method that derives design parameter is being made. so, this study is aimed to derive design parameters of CFB furnace from heat and mass balance by using existing plant data.

• Journal of the korean Society of Automotive Engineers
• /
• v.6 no.4
• /
• pp.18-28
• /
• 1984

디이젤 엔진은 피스톤이 실린더 내를 왕복 운동하면서 압축행정에서 연료의 연소에 의해 발생된 고열을 받아 고온에서 작동되기 때문에 피스톤 헤드에서 받은 열은 속히 아래부분으로 전달시 키고 동시에 실린더 벽으로 전달되게 하여야 한다. 여기서 열이 문제가 되는 요소를 생각해 보면, (1) 고압 : 연소 최고폭발압력이 높기 때문에 압력상승률도 커져 격렬한 연소상태가 된다. (2) 고온 : 격심한 가스 유동과 실린더 직경이 크기 때문에 피스톤 헤드부의 온도가 높아진다. (3) 연소생성물 중에 엔진 및 윤활유에 악 영향을 주는 성분이 많다. (4) 경량, 저가격 구조 때문에 열적 및 역학적 변형이 일어나기 쉽다. (5) 사용조건이 가혹해 연료가 이상 현상을 가져온다. 위의 요소들을 가지고 온도의 분포, 열의 전달과정, 피스톤 냉각 등에 대해서 알아본다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2017.05a
• /
• pp.1088-1092
• /
• 2017

In this study, a comparison of dynamic pressure data measured in hot-firing tests of liquid rocket engine gas generators with different types of dynamic pressure sensors is presented. The dynamic pressure sensors of different types and manufacturers have exhibited different dynamic pressure due to the influence of thermal shock. However, for the characteristic frequencies and RMS(root mean square) values which are important factors for the analysis of combustion instability, the differences between sensors have been found to be negligible.

• Proceedings of the Korea Institute of Fire Science and Engineering Conference
• /
• 2009.04a
• /
• pp.385-388
• /
• 2009

건축물의 적재가연물 특성은 성능위주 화재안전설계를 수행함에 있어 중요한 인자이다. 본 연구에서는 서점의 성능위주 화재안전설계에 이용할 목적으로 적재가연물을 대상으로 연소발열성상을 측정하기 위한 화재실험을 행하였다. 실험에서는 서적과 서가의 일부분을 재현한 시험체를 내화로에 넣고 ISO834 표준가열곡선에 따라 가열하여 화재 최성기에서의 연소성상을 파악하였다. 그 결과, 서적은 외부 가열을 받으면 표면연소 후에 탄화하여 주위에 고온이 형성되어도 열분해가스의 방출량이 증가하지 않는 것으로 파악되었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.32 no.4
• /
• pp.61-66
• /
• 2004

The objective of the present study is to develop methodology for the assessment of combustion stability of liquid rocket injectors. To simulate actual combustion occurring inside of a thrust chamber, a fullscale injector has been employed in the study, which bums gaseous oxygen and mixture of methane and propane. The main idea of the experiment is that the mixing mechanism is considered as a dominant factor significantly affecting combustion instability in a fullscale thrust chamber. A single split triplet injector has been used with an open-end cylindrical combustion chamber. The characteristics revealed by excited dynamic pressures in gaseous combustion show degrees of relative acoustic damping depending on operating conditions. Upon test results, the direct comparison between various types of injectors can be realized for the selection of the best design among prospective injectors.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2007.11a
• /
• pp.17-20
• /
• 2007

Effect of radial position of half-wave resonator is investigated experimentally for acoustic damping of tangential mode in a combustion chamber by adopting acoustic cold test. When resonator with optimal tuning length is installed， damping is enhanced as its radial location is away from the center of the faceplate. And, radial profile of damping factor is similar to that of the amplitude of the acoustic mode to be damped. As the location is close to the center, acoustic damping is mitigated and independent on the resonator length. on the other hand， the resonator with non-optimal length dose not show any effect of its radial position.