• Applied Chemistry for Engineering
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• v.22 no.4
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• pp.439-443
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• 2011

It was performed to test the combustive properties of low density polyethylene and ethylene vinyl acetate (LDPE-EVA) mixture by the addition of magnesium hydroxide. Flame retardant of natural magnesium hydroxide was added to the mixture of LDPE-EVA in 40 to 80 wt% concentration. The composite was compounded to prepare specimen for combustive analysis by cone calorimeter (ISO 5660-1). Comparing with virgin LDPE-EVA, the specimens including the magnesium hydroxide had lower combustive properties. It is supposed that the combustion-retardation properties in the composites improved due to the endothermic decomposition of magnesium hydroxide. The specimens with magnesium hydroxide showed both the lower peak heat release rate (PHRR) and lower effective heat of combustion (EHC) than those of virgin polymer. As the magnesium hydroxide content increases, time to ignition increased and the peak heat release rate decreased.

• Aerospace Engineering and Technology
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• v.3 no.1
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• pp.188-196
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• 2004

To optimize and limit the axial length of baffle in KSR-III engine, stability rating tests using pulse gun as one of artificial disturbance devices have been done. Decay time and other parameters for the evaluation of stabilization ability of engine to external perturbation have been analyzed to quantify stabilization capacity of engine, in other words, dynamic stability margin. If baffle does not cover flame zone enough which can be considered as collision region of injector, it wasn't be able to suppress external perturbation sufficiently. The limit of combustion stability margin of engine is assumed to be 50 mm length baffle.

• Journal of Nuclear Fuel Cycle and Waste Technology(JNFCWT)
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• v.9 no.4
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• pp.237-245
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• 2011

As necessity of safety re-evaluation for spent fuel storage facility has emphasized after the Fukushima accident, accuracy improvement of heat load evaluation has become more important to acquire reliable thermal-hydraulic evaluation results. As groundwork, parametric and sensitivity analyses of various storage conditions for Kori Unit 4 spent fuel storage pool and spent fuel depletion parameters such as axial burnup effect, operation history, and specific heat are conducted using ORIGEN2 code. According to heat load evaluation and parametric sensitivity analyses, decay heat of last discharged fuel comprises maximum 80.42% of total heat load of storage facility and there is a negative correlation between effect of depletion parameters and cooling period. It is determined that specific heat is most influential parameter and operation history is secondly influential parameter. And decay heat of just discharged fuel is varied from 0.34 to 1.66 times of average value and decay heat of 1 year cooled fuel is varied from 0.55 to 1.37 times of average value in accordance with change of specific power. Namely depletion parameters can cause large variation in decay heat calculation of short-term cooled fuel. Therefore application of real operation data instead of user selection value is needed to improve evaluation accuracy. It is expected that these results could be used to improve accuracy of heat load assessment and evaluate uncertainty of calculated heat load.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.245-250
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• 2004

The objective of the present study is to conduct model combustion tests for various injectors to identify their combustion stability characteristics. Three different double swirl coaxial injectors with variation of a recess number have been tested for the comparative study of stability characteristic and flame structure. Gaseous oxygen and mixture of gaseous methane and propane have been employed for simulating actual propellants used for a fullscale thrust chamber. 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
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• 2004.10a
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• pp.278-281
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• 2004

The purpose of this paper is to show a reliable analytical method to predict the deflections of F/W Composite Motor Case. Structural analysis and testing of a Carbon/Epoxy Composites Motor Case for Pressure Loadings were performed. This paper presents the development of 3-D layered axi-symmetric solid element for finite element analysis. Finite element analyses were preformed considering fiber angle variation in longitudinal and thickness direction by ANSYS. The analytical results agree well with experimental results.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1997.04a
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• pp.3-10
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• 1997

본 연구에서는 추력 500 Kgf의 액체 추진기관을 설계, 제작 및 연소시험을 수행하여 연소 특성을 살펴보았다. 추진제로는 우주발사체 Booster용으로 폭넓게 사용되는 탄화수소계 연료인 kerosene과 산화제로 취급이 용이하고 저장 특성을 지닌 98 % White Fuming Nitric Acid(WFNA)를 사용하였고, 엔진 점화를 위해 WFNA와 접촉 발화성 (Hypergolic)을 갖는 Furfuryl Alcohol/Aniline 혼합액을 사용하였다. 로켓엔진은 20 Kgf/$cm^2$의 연소실 압력으로 500 Kgf의 평균 추력을 내도록 설계되었고, 연소실벽을 고온 연소가스로 부터 보호하기 위해 Film Cooling 방식을 적용하였다.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1998.05a
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• pp.31-36
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• 1998

가압유동층 복합발전(Pressurized Fluidized Bed Combustion Combined Cycle 또는 PFBC-CC)은 고효율 및 공해물질 배출이 적은 석탄이용 차세대 발전기술이다. 석탄을 연소하면서 발생되는 열은 스팀으로 회수하여 스팀터빈을 구동하고, 고온, 고압의 연소가스로 가스터빈을 구동하여 복합 발전함으로서 효율을 42- 45%까지 얻을 수 있으며, 유동층연소의 장점인 연소중 탈황과 낮은 질소산화물 배출특성으로 환경친화적이며 경제성이 우수한 청정석탄 이용기술이다. (중략)

• Journal of Energy Engineering
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• v.8 no.1
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• pp.174-180
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• 1999

본 연구는 여러 종류의 연소가스들의 연소 특성변수를 판단하여 각 가스들 간의 교체 가능성을 조사하는 것을 목적으로 하고 있다. 천연가스, 메탄가스, IGCC 생성가스의 연소특성, 즉 역화, 비화, 및 황염형성을 분제 버너를 이용하여 판단하였고, 실험 데이터는 연소 다이어그램 상에서 이론 공기량 분률과 입열로 표현하였다. 실험 결과, 메탄은 천연가스와 아무런 운전조건의 변화없이 호환가능하나, 천연가스를 IGCC 생성가스로 치환하고자 할 경우는 화염 안정으로 인하여 버너의 운전변수를 조절하여야만 한다. 이러한 연구결과는 다양한 산지에 따른 각종 천연가스들의 교체가능성 및 타 연료와의 호환가능성을 판단하는 기초자료로 사용될 수 있다.

• Proceedings of the Korean Institute of Industrial Safety Conference
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• 2003.05a
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• pp.428-433
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• 2003

화재 및 폭발 특성치로 인화점, 최소발화온도, 폭발한계, 최소발화에너지, 연소열 등을 들 수 있다. 연소특성은 인화성용제들(석유류 및 알코올류 등)의 취급, 저장, 수송에서 포함되어 있는 잠재 위험성을 평가할 때 고려된다. 여러 연소특성 가운데 폭발한계(explosive limits)는 가연성물질(가스 및 증기)을 다루는 공정 설계 시 고려해야 할 중요한 변수로써, 발화원이 존재할 때 가연성가스와 공기가 혼합하여 일정 농도범위 내에서만 연소가 이루어지는 혼합범위를 말한다.(중략)

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 2003.05a
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• pp.621-625
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• 2003

최근 지구온난화 문제와 관련하여 국제적으로 이슈가 되고 있는 $CO_2$ 저감 및 처리기술 중에서 연소 후 처리가 아닌 신개념 연소기술로서 NO$_{x}$가 배출되지 않고 $CO_2$의 고농도 원천분리가 가능하여 새로운 연소 및 발전기술로 부상하고 있는 매체순환식 가스연소기술(Chemical-Looping Combustion Technology, CLC)에 대한 연구가 국내외적으로 활발하게 진행되고 있다.(중략)