• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.451-454
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• 2006

This paper describes the results of cold flow test and hot firing tests of an uni-element coaxial swirl injector and hot firing tests of a subscale combustor, as to the development effort of coaxial swirl injector for high performance liquid rocket engine combustor. A major design parameter for coaxial swirl injector is the recess number of a bi-swirl injector. The results of hot firing tests of the uni-element injector combustor and the sub-scale combustor are analyzed to investigate the effect of the recess number influencing on the combustion performance and pressure fluctuation. The test results of a cold flow test of the unielement combustor shows that it was shown that the change in recess number has significant effect on mixing characteristics and efficiency, while the effect of recess number on atomization characteristic is not The results of a series of firing tests using unielement and subscale combustor show that the recess length significantly affects the hydraulic characteristics, the combustion efficiency, and the dynamics of the liquid oxygen/kerosene bi-swirl injector. As a point of combustion performance, combustion efficiencies are 90% for unielement combustor and 95% for subscale combustor. The difference in the characteristic velocities between the unielement combustor and the subscale combustor may be caused by the difference in thermal loss to the combustor wall and the relative lengths of the combustion chamber. For a mixed type coaxial swirl combustor, the pressure drop across the injector increases as recess number becomes larger. The low frequency pressure fluctuation observed in unielement combustor can be related to the propellant mixing characteristics of the coaxial bi-swirl injector. The effect of the recess number on the pressure fluctuation inside the combustion chamber is more significant in un i-element combustor than the subscale combustor, of which the phenomena are also observed in time domain and frequency domain.

• 대한기계학회논문집B
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• 제31권3호
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• pp.292-299
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• 2007

In gas turbine technology, the flame stability is inherently greater in conventional diffusion type combustion over a wider range fuel to oxidizer ratio. However, premixed type combustion which has narrow flame stability region, is widely used due to environmental reason. It has been observed in experiments that combustion instability of low frequency (${\sim}10Hz$) results from the modulation of equivalence ratio at fuel injection hole when a pressure fluctuation propagates upwards along the channel of the burner under an unchoked fuel flow condition. In this study, a commercial program was used to determine how the fuel flow rate changed with respect to the pressure, velocity of the fuel flow and the mass fraction in a choked and an unchoked condition. The calculation focuses on the upstream of the dump plane to know how the forced pressure with the fuel injection conditions affects the modulation of the equivalence ratio. Therefore, it is found that pressure fluctuation leads to oscillation of mass flow rate and then results in equivalence ratio modulation under the unchoked fuel flow condition.

• 동력기계공학회지
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• 제11권1호
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• pp.51-55
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• 2007

A study on combustion characteristics using emulsified fuel in a diesel engine were performed experimentally. In this paper, the experiments were performed at engine speed 1800rpm, emulsion ratios were 0%, 10%, 20%, and main measured items were specific fuel consumption, cylinder pressure, rate of pressure rise, rate of heat release etc. The obtained conclusions were as follows. 1) Specific fuel consumption increased maximum by 19.8% at low load, but was not affected at full load. 2) Rate of pressure rise and rate of heat release were about the same in the case of 10% and 20% of emulsion ratio. 3) Cylinder Pressure increased 9.6%, rate of pressure rise increased 53.4% in case of emulsion ratio 20% at full load. 4) Rate of heat release increased 72.4% in case of emulsion ratio 20% at full load.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.134-137
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• 2009

본 연구에서는 친환경 추진제인 고농도 과산화수소와 케로신을 사용하는 저추력 이원추진제 로켓 엔진의 O/F ratio에 따른 연소 성능 특성을 파악하였다. 연소시험에 사용된 엔진은 6개의 동축 스월 인젝터로 구성된 멀티 인젝터와 연소실, 노즐로 구성되어있으며, 촉매 점화 방식을 사용하였다. 연소 시험은 O/F ratio 3.8에서 11.0까지 변화시켜가며 수행하였다. 연소 시험 결과를 이용하여 특성 속도($C^*$)와 압력 섭동 값을 계산한 결과, 연소 효율은 O/F ratio 5~6 구간에서 가장 좋았으며 모든 구간에서 연소실 압력대비 압력 섭동 값이 5% 미만으로 안정적임을 확인하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회B
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• pp.2946-2951
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• 2008

Combustion instability is a major issue in design of gas turbine combustors for efficient operation with low emissions. Combustion instability is induced by the interaction of the unsteady heat release of the combustion process and the change in the acoustic pressure in the combustion chamber. In an effort to develop a technique to predict self-excited combustion instability of gas turbine combustors, a new stability analysis method based on the transfer matrix method is developed. The method views the combustion system as a one-dimensional acoustic system with a side branch and describes the heat source as the input to the system. This approach makes it possible to use the advantages of not only the transfer matrix method but also well-established classic control theories. The approach is applied to a simple gas turbine combustion system to demonstrate the validity and effectiveness of the approach.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.86-90
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• 2012

본 연구에서는 '하이브리드 로켓 불안정성 I'에 이어 하이브리드 로켓에서 발생할 수 있는 연소불안 정성에 대해 연구하였다. 하이브리드 로켓 연소기 내부에 와류가 발생할 수 있도록 연소기를 설계하여 연소시험을 수행하였고, 연소실 압력 공진 주파수의 다이아프램 유 무에 따른 특성, 연료 길이에 따른 특성, 연료 포트 직경에 따른 특성, 다이아프램 직경에 따른 특성, 노즐목 직경에 따른 특성, 산화제 유량 변화에 따른 특성에 대한 연구를 수행하였다. 본 연구의 주요 연소실 압력 공진 주파수는 Vortex shedding으로 판단되며, Hybrid low frequency와 Helmholtz mode가 또다른 공진주파수 인 것으로 판단된다.

• 한국연소학회지
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• 제7권4호
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• pp.36-44
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• 2002

Carbon molecules with closed-cage structures are called fullerenes $(C_{60},\;C_{70})$, whose applications include super-conductors, sensors, catalysts, optical and electronic device, polymer composites, and biological and medical materials. The synthesis of fullerenes has been recently studied with low-pressure benzene/argon/oxygen flames. The formation of fullerene is known as molecular weight growth processes of PAHs (polycyclic aromatic hydrocarbon). This study presents results of PAHs and fullerene measurements performed in a low-pressure benzene/argon/oxygen normal co-flow laminar diffusion flame. Through the central tube of the burner, benzene vapors carried by argon are injected. The benzene vapors are made in a temperature-controlled bubbler. The burner is located in a chamber, equipped with a sampling system for direct collection of condensable species from the flame, and exhausted to a vacuum pump. Samples of the condensable are analyzed by HPLC (High Performance Liquid Chromatography) to determine the yields of PAHs and fullerene. Also, we computed mole fraction of fullerene and PAHs in a nearly sooting low pressure premixed, one-dimensional benzene/argon/oxygen flame (equivalence ratio ${\Phi}=2.4$, pressure=5.33kPa). The object of computation was to investigate the formation mechanism of fullerenes and PAHs. The computations were performed with CHEMKIN/PREMIX. As a result of this study, fullerenes were synthesized in a low pressure (20torr) $C_6H_6/Ar/O_2$ flames and the highest concentration of fullerene was detected just above the visible surface of a flame.

• 한국연소학회지
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• 제16권1호
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• pp.52-57
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• 2011

The present study describes the characteristics of combustion and exhaust emissions in compression ignition engines using diesel-gasoline dual fuel. For investigating combustion characteristics, diesel fuel was injected directly in a single-cylinder compression ignition engine with a common-rail injection system and gasoline fuel was injected into a premixed chamber installed in an intake port. In order to investigate exhaust emission characteristics, exhaust gas was measured by emission analyzer and smoke meter. The experimental results showed that cases of diesel-gasoline dual fuel combustion exhibited extended ignition delay and reduced peak combustion pressure compared to those of directly injected diesel fuel cases. Furthermore, premixed gasoline-air mixture reduced NOx emissions due to low peak of rate of heat release(ROHR).

• 한국산학기술학회논문지
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• 제22권6호
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• pp.75-82
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• 2021

디젤엔진의 열효율을 높이면서 NOx와 PM을 효과적으로 저감시키기 위해 HCCI(Homogeneous Charge Compression Ignition), PCCI(Premixed Charge Compression Ignition), RCCI(Reactivity Controlled Compression Ignition) 등의 저온연소(LTC: Low Temperature Combustion)전략이 개발되어 왔다. 본 연구에서는 저반응성 연료로는 가솔린을 사용하고 고반응성 연료로는 디젤을 사용하는 RCCI 엔진에서 고반응성 연료인 디젤연료의 분사 시기와 이단 분사비율이 성능 및 배출가스에 미치는 영향을 수치해석을 통하여 파악하고자 하였다. 이단 분사 시 첫 번째 분사시기가 너무 진각되면 연소가 느려지면서 연소온도가 낮아져 연소성능이 저하되고 HC, CO가 증가한다. 대략 -60°ATDC 의 분사시기가 연소성능, 배출가스 및 최대압력상승률을 고려하였을 때 가장 최적의 분사시기라고 판단된다. 이단 분사 시 두 번째 분사시기를 변경하였을 때 연소성능 및 배출가스, 최대압력상승률 등을 고려하면 대략 -30°ATDC 부근에서 최적인 것으로 판단된다. 이단 분사 시 분사량 비율은 첫 번째 분사량을 60% 정도로 하였을 때 최적의 결과를 얻었다. 마지막으로 단일 분사보다는 이단 분사한 경우 연소성능 및 배출가스 부분에서 더 효과적인 것으로 판단된다.

• 한국연소학회지
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• 제21권4호
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• pp.16-22
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• 2016

Pressure and temperature variations in a shock tube have been studied numerically by changing the diameter ratio of a driven part to a driver part. There are five cases where the adopted diameter ratios are 40%, 50%, 60%, 80%, and 100% respectively. The diameter of the driver part remains unchanged meanwhile the shock tube driven part diameter increases from 40% to 100% of the driver part. In the 100% ratio case, the driver part and driven parts have the same diameter of 66.9 mm. As the diameter ratio decreases, the pressure in the shock tube and available test time are increased.