• International Journal of Automotive Technology
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• 제5권3호
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• pp.181-188
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• 2004

A cylindrical constant-volume combustion chamber was used to investigate the flow characteristics at the spark electrode gap and the combustion characteristics of an inhomogeneous charge methane-air mixture under several parameters such as stratified pattern, initial charge pressure, ignition time and the excess air ratio of the initial charge mixture. Flow characteristics including mean velocity and turbulence intensity were analyzed by a hot-wire anemometer. The combustion pressure development, measured by a piezo-electric pressure transducer, was used to investigate the effect of initial charge pressure, excess air ratio and ignition times on combustion pressure and combustion duration. It was found that the mean velocity and turbulence intensity had the maximum value around 200-300 ms and then decreased gradually to near-zero value at 3000 ms. For the stratified patterns, the combustion rate under the rich injection (RI) condition was the fastest. Under the initial charge conditions, the second mixture was accompanied by an increase in the combustion rate, and that the higher the mass which is added in the second stage injection, the faster the combustion rate.

• 오토저널
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• 제9권4호
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• pp.50-60
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• 1987

Combustion characteristics of opposed-jet-flames spouting out from dual prechambers of a divided combustion chamber were investigated by using high speed schilieren photography and chamber pressure measurement. Result shows that opposed-jet-flames are characterized by the parameter ( $A_{ori}$/ $V_{p}$) and there exists a certain critical value of ( $A_{ori}$/ $V_{p}$)c which distinguishes flame propagation patterns in the main chamber. Also higher chamber pressure and shorter total burning time can be derived by adopting this dual prechamber divided combustion chamber, which would lead a possibility of an appropriate combustion method of high load and low emissions.ons.ons.

• 한국초등과학교육학회지:초등과학교육
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• 제28권4호
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• pp.467-475
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• 2009

This study is to enquire about ideals on combustion and to propose of teaching program using the history a science in '5. Combustion and Extinguishing' unit of elementary school science textbook in 6th grade. For this purpose, investigation questionnaires based on preceding research and science textbook are developed. The reliability of the questionnaires is .784, and the questionnaires are applied to 247 students in T elementary school in Busan. Through the results of the investigation, scientific conceptions existed in some parts. But some misconceptions still existed especially (question 1), substance's changes (question 7), formation process of product (question 13), combustibles among requirements of combustion. The patterns of the misconception are similar to historical misconceptions about combustion. Besides, the discoveries and inventions of combustion have some points about correcting misconceptions. Thus the five step teaching programs on combustion which were applied to history of the science are suggested. The confidence of the developed programs was verified as being 'excellent' by specialists. This program will be applied to think deeply about combustion in elementary school lesson and useful to introduce the history of science.

• 한국화재소방학회논문지
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• 제34권4호
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• pp.101-106
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• 2020

자체 제작된 니들 플레임을 이용하여 바닥재를 수직 연소시켰을 때의 화염의 성장 특성 및 탄화 패턴을 해석하였다. PVC 장판은 난연성이 있는 것으로 확인되었고, 직사 화염을 받은 곳은 안쪽으로 수축되는 패턴을 나타냈다. 수직 연소가 진행되면 하부에 망울 형태의 고형화가 발생하며, 그을음은 상부로 성장하는 패턴이 형성된다. 강화마루는 난연성이 없는 것으로 확인되었으며, 상부 표면인 라미네이트층의 소실과 불규칙적인 박리가 형성되는 것을 알 수 있다. 좌측면과 우측면의 탄화의 범위는 대칭적 구조를 나타내는 것으로 해석된다. 강화마루와 마찬가지로 카펫은 수직 연소 실험에서 난연성이 없는 것이 확인되었다. 카펫에 축열이 형성되면 화염은 상승기류를 형성하고, 주변에 가연성 물질이 있을 때 화염의 확산은 더욱 촉진하는 것을 알 수 있었다. 직사화염을 받은 카펫 표면의 탄화 패턴은 표면이 용융되어 흘러내렸을 뿐만 아니라 작은 구멍이 다수 발생되는 것을 알 수 있다.

• Journal of Mechanical Science and Technology
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• 제20권6호
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• pp.874-881
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• 2006

Combustion stability characteristics in actual full-scale combustion chamber of a rocket engine are investigated by experimental tests with the model (sub-scale) chamber. The present hot-fire tests adopt the combustion chamber with three configurations of triplet impinging-jet injectors such as F-O-O-F, F-O-F, and O-F-O configurations. Combustion stability bound-aries are obtained and presented by the parameters of combustion-chamber pressure and mixture (oxidizer/fuel) ratio. From the experimental tests, two instability regions are observed and the pressure oscillations have the similar patterns irrespective of injector configuration. But, the O-F-O injector configuration shows broader upper-instability region than the other configurations. To verify the instability mechanism for the lower and upper instability regions, air-purge acoustic test is conducted and the photograph or the flames is taken. As a result, it is found that the pressure oscillations in the two regions can be characterized by the first impinging point of hydraulic jets and pre-blowout combustion, respectively.

• 청정기술
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• 제25권4호
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• pp.331-335
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• 2019

전 세계적으로 환경오염에 대한 관심이 높아지고 있으며, 이를 해결하기 위한 기술개발 또한 활발하게 이루어지고 있다. 특히 열을 사용하는 분야에서는 연소로 인해 대기환경 오염물질이 많이 발생하고 있는 상황이다. 연소 촉매는 완전 연소와 연소온도를 낮춰 NOx와 CO를 줄이는 기술이다. 기존 연소 촉매는 귀금속 촉매를 사용하여 값이 비싸고 합성공정이 복잡하다. 본 연구는 요소를 이용하여 고온 연소촉매인 헥사알루미네이트를 제조하였으며, 합성시간에 따른 물성을 조사하였다. 그리고 이 촉매를 이용하여 연소 성능 및 특성을 평가하였다. 온도가 증가하면서 변화하는 메탄 전환율은 두 가지 패턴으로 나타났다. 1 h, 9 h, 12 h의 전환율이 비슷하게 나타났고, 3 h, 6 h의 전환율이 유사한 패턴을 나타내었다. 합성시간이 6 h에서 9 h으로 증가하면서 메탄 연소 성능이 급격하게 증가하였으며, T50이 되는 온도는 약 745 ℃로 나타났다. 9 h 합성된 연소촉매의 성능이 가장 우수하게 나타났으며, 이 연소촉매의 NOx 배출은 없었고, CO의 최대 배출량은 72 ppm으로 나타났다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.649-652
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• 2011

산화제 유동 변화를 위한 디스크를 예혼합실에 장착하여, 디스크의 직경과 길이를 변경하며 PMMA/GOx를 이용한 하이브리드 로켓 모터의 지상연소시험을 수행하였다. 디스크에 의해 산화제 유동의 와류유출(vortex shedding)이 발생하여, 연소율과 압력 진동 등의 연소 특성이 변화하였다. 연소실험 후 PMMA를 축방향으로 잘라내어 연소면을 관찰하여, PMMA의 연소면 전체에서 딤플 형태의 패턴이 발견하었다. 이는 연소 과정 중 연소면 근처에서 발생하는 blowing 효과에 의해 변화된 산화제 유동의 경계층 특성에 기인한 것으로 보이며, LES 기법을 이용하여 수행한 수치적 연구 결과와 일치한다. 이는 하이브리드 로켓 모터의 연소불안정 현상을 이해하는데 중요한 자료로 판단된다.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2006년도 추계학술대회 논문집 Vol.19
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• pp.322-323
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• 2006

The nano-sized Ce-doped YAG(Yttrium Aluminum Garnet, $Y_3Al_5O_{12}$) phosphor powders were prepared by combustion method from a mixed aqueous solution of metal nitrates, using citric acid as a fuel. The luminescence formation process and structure of phosphor powders were investigated by means of XRD, SEM and PL. The XRD patterns show that YAG phase can form at all of the $Ce^{3+}$ concentration. However, when $Ce^{3+}$ concentration is over 2.0mol%, XRD patterns show $CeO_2$ peak between (321) peak and (400) peak. The pure crystalline YAG:Ce with uniform size of 30nm was obtained at 0.6mol% of the $Ce^{3+}$ concentration. The crystalline YAG:Ce powders showed broad emission peaks in the range 475~630nm and had maximum intensity at 526nm.

• 한국연소학회지
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• 제21권1호
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• pp.31-37
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• 2016

Swirler generates the overall swirling flow in the combustion chamber and this swirling flow governs the flame stability and enhances fuel atomization. This paper deals with the flare angle effects on flow streamlines, recirculation zone, Central Toroidal Recirculation Zone(CTRZ) and Corner Recirculation Zone(CRZ) in the model combustion chamber using counter-rotating swirler. 2D PIV system was employed to obtain the velocity components and test condition was obtained using Reynolds Analogy equivalent to air test. We observed transitional flow patterns of flare angle increased. The obtained results show that the flare angle controls the behavior of Recirculation zone, Central Toroidal Recirculation Zone and Corner Recirculation Zone.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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• pp.193-196
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• 2015

Combustion of low concentration VOC in inert gas around the flammability limit has been experimentally studied. Streams of nitrogen and propane mixture with various compositions and flow conditions were treated by a turbulent partially-premixed pilot flame. HC and CO contents in exhaust gas measured and the flow patterns were visualized. The results suggested that there exists an optimal mixture velocity range for efficient combustion treatment for each flow condition and composition of the mixture.