• 한국자동차공학회논문집
• /
• 제11권1호
• /
• pp.55-63
• /
• 2003

In a diesel engine, air-fuel mixture formation and ignition delay period have great influence on the performance of engine. Their main factors are combustion chamber shape, fuel injection system. air volume, air flow and so on. So, the combustion process in the cylinder is complex because of many factors which have direct and indirect effects on it. In this study, we take into consideration of scavenging pressure and scavenging temperature that are hewn as the main factor to the combustion process of two-stroke D.1. diesel engine. It is taken a picture of the combustion flame process for combustion chamber of re-entrant type and cylindrical type. So, it is applied to the basis data of combustion chamber design from an image analysis.

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 2001년도 제22회 KOSCI SYMPOSIUM 논문집
• /
• pp.67-74
• /
• 2001

The annular-reverse combustor was designed for APU combustor and a three dimensional analysis for reactive flow in the combustor was performed. At the same time, the experimental work was performed in KARl combustor test facility. In this study we found out that tangential swirl type combustor is good for flame holding than single vortex type combustor. The flame tube main hole size and relative position are very important parameters for combustor general performance. The ignition characteristics are strongly depend on the air fuel ratio with combustor inlet volume flow ratio.

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 2002년도 제25회 KOSCI SYMPOSIUM 논문집
• /
• pp.231-235
• /
• 2002

A theoretical and experimental study on the combustion process in a constant volume micro combustor is described. Unlike in a macro scale constant volume combustor, the heat loss to the wall plays a major role in flame propagation in a micro micro combustor. In order to analyze the effect of heat loss on combustion phenomena, pressure transition from ignition was measured. A number of cylindrical micro combustors with different diameter and depth were used for experiment to study the effect of length scales and shape factor. The diameter of combustor ranged from 7.5mm to 22.5 mm and the height of cylinder was from 1mm to 4mm. Initial pressure was also varied for the experiment. The diagnostic methods were severely limited due to the size of the apparatus and uncertainties of certain quantities to be measured in a small-scale environment. An analytical method to derive physical quantities that are essential for performance prediction from the pressure measurements is described.

• 오토저널
• /
• 제10권5호
• /
• pp.69-82
• /
• 1988

Heat transfer experiment is carried out during the performance test of the 4-cylinder 4-stroke cycle turbo-charged gasoline engine. Cycle simulation employing the measured pressure in cylinder, the cooling water temperature and flow rate and others is carried out in order to calculate the gas temperature in cylinder. In this simulation combustion process was simulated by Annand's two zone model and suction, compression, and other processes are calculated completely. From this simulation, we can obtain not only the heat transfer coefficient but also the flame speed, turbulent burning velocity, flame factor and the boiling condition of cooling passage. The results are investigated with engine speed, equivalence ratio and spark advance.

• 한국자동차공학회논문집
• /
• 제7권7호
• /
• pp.1-14
• /
• 1999

In the present study, the flame factor which primarily influence the simulation accuracy of the combustion process in a gasoline engine was modeled as a nonlinear function of turbulent intensity to laminar flame speed ratio. Multi-length-scale production rate model for turbulent kinetic energy equation was introduced to consider the different length scales of the swirling and tumbling motions in cylinder on the production rte of turbulent kinetic energy. By7 introducing the multi-length-scale production rate model for the turbulent kinetic energy equation, the predictions of turbulent burning velocity , cylinder pressure, mass burning rate and engine performance of a gasoline engine can much be improved.

• 한국표면공학회지
• /
• 제29권3호
• /
• pp.163-175
• /
• 1996

Flame-sprayed Ni-based coatings are investigated in order to improve the thermal fatigue properties of gray cast iron in the presence of water spraying. The results of thermal cycling tests from room temperature to $1100^{\circ}C$ indicate that thermal fatigue endurance is increased in the order of Ni-20%Cr, NiCr-6%Al, and Ni-5%Al. The thermal fatigue failure is caused by the formation of iron oxides between the coating and the substrate and then the thermal fatigue cracks have propagated either along the brittle iron oxide layer resulting in the spatting of the coatings in case of Ni-5%Al and NiCr-6%Al coatings or to the substrate resulting in the whole specimen fracture in case of Ni-20%Cr coating. It seems that the most governing factor for thermal fatigue resistance is the thermal expansion coefficient difference between the coating and the substrate. Microstructural variations before and after the tests are also discussed.

• 한국가스학회지
• /
• 제23권5호
• /
• pp.24-34
• /
• 2019

본 연구에서는 수관식 보일러의 열교환기를 모사하기 위하여 수관의 존재 유무에 따른 화염의 안정화와 연소 특성을 당량비와 유속에 따라 비교하였다. 버너는 화염이 존재하는 SiC foam과 역화 방지를 위한 세라믹 보드, 균일한 유동장을 형성하는 알루미나 볼로 구성되며, 반경 반향의 열 손실을 최소화하기 위하여 단열재로 밀폐되어 있다. 결과적으로 수관이 존재하는 경우 낮은 당량비 구간에서 역화 및 날림 현상의 경계가 넓어지는 것을 안정화 영역에서 확인할 수 있었다. 또한, 수관이 존재하는 경우 NOx 배출량이 수관이 없는 경우보다 증가하는 것을 확인하였다. 이는 수관이 존재함으로써 열 손실을 억제하여 화염의 온도가 증가하는 것으로 판단하였으며, O₂ 배출량과 화염의 온도를 예측하여 입증하였다.

• 대한기계학회논문집B
• /
• 제35권12호
• /
• pp.1375-1381
• /
• 2011

커먼레일 분사 시스템이 장착된 대형 단기통 가시화 엔진에서 디젤과 JP-8 의 연소 및 배기 특성을 분석하였다. 두 연료 적용 시, 배기 배출 경향을 분석하기 위해 직접 화염가시화와 이색법을 적용하였다. 연소 과정은 직접 화염 가시화로부터 화염 강도 분석을 통해 이루어 졌다. 이색법 결과는 화염 온도 및 KL 값을 도출하여 분석을 하였다. 직접 화염 가시화 결과, JP-8 연소 시, 점화 지연 기간이 길며, 디젤 연소에 비해 화염이 빠르게 소멸되는 것을 확인하였다. 화염 강도 분석을 통해 디젤 연소의 경우, 연소 전 기간에 걸쳐 높은 화염 강도 수준을 유지하며 화염 지속 기간이 긴 것을 알 수 있었다. 이색법 결과를 통해, JP-8 연소의 경우, 국부적으로 고온의 화염 면이 더 많이 분포하는 것을 확인하였으며, 이는 $NO_x$가 더 많이 배출된 경향을 설명해준다. 또한 KL 치 분석 결과, JP-8 연소 시 낮은 수준의 KL 값이 더 고르게 분포하는 것을 알 수 있었으며, 이는 JP-8 연소 시 스모크 가 덜 배출된 결과를 뒷받침 해준다.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2001년도 춘계학술대회논문집D
• /
• pp.840-845
• /
• 2001

Development of a small gas-turbine combustor for 100kW class APU(Auxiliary Power Unit) has been performed. This combustor is a reverse-annular type and has a tangential swirler in the liner head to improve the fuel/air mixing and flame stability. Three main and three pilot fuel injectors of the simplex pressure-swirl type are used. The performance target at the design condition includes a turbine inlet temperature of 1170K, a combustion efficiency of 99%, a pattern factor of 30%, and an engine durability of 3000 hours. Under developing the combustor, we conducted performance test of our first prototype(TS1) with some variants. As a result of the test, the performance targets of the combustor are satisfied except that the pattern factor is about 4% higher than target value. So, we redesigned the second prototype(TS2) and conduct performance test with the critical focus on pattern factor and exit mean temperature. We adopted TS2 four variant to check the improvement of pattern factor. As the result, the pattern factors of several variants were satisfied with the performance target. Finally, We chose the TS2A variant as a final combustor for our APU model.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 1999년도 하계학술대회 논문집 E
• /
• pp.2097-2100
• /
• 1999

Nondestructive and destructive tests were performed the stator windings of three high voltage motors prior to the rewind. Nondestructive tests included ac current increase rate($\Delta$I), dissipation factor(${\Delta}tan{\delta}$), and maximum partial discharge(Qm) The destructive tests included breakdown at three phases with ac voltage. Flashover occurred between the connected winding of endwinding and the stator flame. In two cases creeping discharge occurred between the individual phase windings and the wedges In the stator ends. The results of destructive tests could rarely be determined the breakdown voltage.