• 한국분무공학회지
• /
• 제3권1호
• /
• pp.19-26
• /
• 1998

The effect of mixture component makes a nelay time and a long total combustion period $\tau_{p\;max}$. The flame propagation delay $\tau_{df}$ was determined by the record of current ion. The pressure release delay $\tau_{dp}$ and $\tau_{p\;max}$ were determined by the indicated pressure diagram in constant volume of the combustion chamber. The results are as follows: 1) The ignition delay $\tau_t$ time takes the minimum value around $\Phi=1.15$. 2) $\tau_{df}$ and $\tau_t$ time increased according to the increases of the concentrated dilution gases, because the adiabatic flame temperature decreased due to the increases of the heat capacity. But dilution gases have little effect on flame nucleus formation delay 3) The relation between $\tau_t$ time and reciprocal laminar burning velocity is almost linear. 4) The increase of the propagation length is accompanied with increased ratio of the $\tau_{df},\;\tau_{dp},\;\tau_{t},\;\tau_{p\;max}$.

• International Journal of Automotive Technology
• /
• 제6권4호
• /
• pp.323-332
• /
• 2005

A cylindrical constant volume combustion chamber was used to investigate the flow characteristics at the spark electrode gap and the combustion characteristics of a homogeneous charged methane-air mixture under various overall charge pressures, excess air ratios and ignition times. The flow characteristics, including the mean velocity and turbulence intensity, were analyzed with a hot wire anemometer. Combustion pressure development measured by piezoelectric pressure transducer, a flame propagation image acquired by ICCD camera and exhaust emissions measured by 2-valve gas chromatography were used to investigate effects of initial pressures, excess air ratios and ignition times on the combustion characteristics. It was found that the mean velocity and turbulence intensity had the maximum value around 200-300 ms and then decreased gradually to a near-zero value after 3000 ms and that the combustion duration was shorten and the flame speed and laminar burning velocity had the highest value under the condition of an excess air ratio of 1.1, an overall charge pressure of 0.15 MPa and an ignition time of 300 ms in the present study. The $CO_2$ concentration was proportional to the ignition time and overall charge pressure, the $CO_2$ concentration was proportional to the excess air ratio, and the UHC concentration was inversely proportional to the ignition time and overall charge pressure.

• 대한기계학회논문집B
• /
• 제29권2호
• /
• pp.180-188
• /
• 2005

It is well known that a lean burn engine caused by stratified mixture formation has many kinds of advantages to combustion characteristics, such as higher thermal efficiency and lower CO, NOx levels than conventional homogeneous mixture combustion. Although this combustion can achieve low fuel consumption technology, it produces much unburned hydrocarbon and soot because of heterogeneous equivalence ratio in the combustion chamber. Therefore, the stratified mixture formation technology is very important to obtain the stable lean combustion. In this paper, fundamental studies for stratified combustion were carried out using a constant volume combustion chamber. The local effect of mixture formation according to control air-fuel distribution in the chamber was examined experimentally. In addition, the effect of turbulence on stratified charge combustion process was observed by schlieren photography. From this study, we found that the flame propagation speed increase with swirl flow and the swirl promotes the formation of fuel and air mixture.

• 한국추진공학회지
• /
• 제22권3호
• /
• pp.28-39
• /
• 2018

본 연구에서는 추력조절용 핀틀 노즐의 길이비에 따른 정상상태와 비정상상태 특성을 파악하기 위해 수치해석을 수행하였다. 노즐과 핀틀의 영역은 분리하여 격자를 생성하고 중첩격자기법을 사용하였다. 핀틀 형상은 길이비에 따라 5가지로 선택하였고, 정상상태 해석결과 핀틀의 길이가 길수록 추력과 추력계수가 높게 나타났다. 비정상상태 해석의 경우 핀틀의 속도에 따라서 연소실 압력 경향이 달라지며 추력과 유동구조에 영향을 미친다. 노즐 출구에서의 추력은 노즐목 단면적 변화에 빠른 응답특성을 보이며, 추력과 추력계수 등 성능 주요 인자들의 예측시 핀틀의 구동 속도와 핀틀 거동에 의한 연소실 압력파의 전달속도를 고려해야 한다.

• 한국군사과학기술학회지
• /
• 제19권3호
• /
• pp.302-310
• /
• 2016

An underground ammunition facility requires less quantity distances than the aboveground counterpart. However, chamber blast doors which resist the high blast-pressures are necessary for prevention of the consecutive explosions when an accident explosion occurs at any chamber. This paper aims to propose an procedure for calculation of the design loads for the chamber blast doors. Modeling considerations are drawn through analyzing the influences of the geometrical shapes and mechanical properties of rocks on the propagation of pressure wave along with the tunnels. Additionally, the design loads for the chamber blast doors in a newly-built underground ammunition facility are calculated based on the proposed procedure.

• 한국군사과학기술학회지
• /
• 제17권6호
• /
• pp.725-732
• /
• 2014

The silencer for the medium caliber gun was studied to reduce the propagation of gun-generated noise from the firing test range to the community. Three types of silencer were made to compare the reduction of sound pressure level and the effect of chamber volume and the exit angle to the reduction of sound pressure was considered. The structural analysis and measurement of pressure in the silencer showed that the structure is safe in terms of strength. The increase of recoil force to buffer must be considered in the development of silencer. The hypothesis test on the muzzle velocity for the existence of silencer showed that there are no difference at the significance level of 0.05.

• 대한기계학회논문집B
• /
• 제32권7호
• /
• pp.513-517
• /
• 2008

A parametric study was made to understand the fundamentals of combustion of CNG fuel in a constant volume chamber in the respect of swirl effect, and the numbers of spark ignition. Optical devices were applied for the visualization of the physics of combustion, and combustion pressures and exhaust emission were measured at several equivalence ratios by controlling speeds of a swirling motor. When the speed of a swirling motor was raised the combustion conditions were improved. The corresponding maximum combustion pressure and heat release rate were increased and the speed of flame propagation was getting faster. This research may contribute to improve the performance of CNG engine and reduce emissions in future.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2004년도 추계학술대회논문집
• /
• pp.790-795
• /
• 2004

The characteristics of refrigerator noise recorded in anechoic chamber was investigated in condition of a the real living room and a kitchen. To predict the noise propagation in an apartment unit, room acoustic simulation software was used. It was found that the noise level in the real living room was $4\sim8dB$ higher than in the anechoic chamber. When a noise barrier and absorption materials were used on the rear wall and floor, the noise level reduced up to $3\sim4dB$. In addition, when the subjective evaluation of auralized refrigerator noise was undertaken using headphone, it was revealed that 21dB (A) is the allowable sound pressure level of 95% satisfaction.

• 한국가스학회지
• /
• 제12권3호
• /
• pp.68-74
• /
• 2008

폭발챔버에서 전파하는 화염과 장애물 위치 및 형태에 따른 상관관계를 조사하기 위해 폭발실험을 수행하였다. 챔버내에 장애물 설치 위치는 점화원으로부터 상부로 200 mm, 500 mm, 800 mm 높이로 변화를 주어 설치하였고, 장애물 형태는 삼각기둥, 사각기둥 및 원통형으로 변화시켰다. 전파하는 화염과 장애물 위치 및 형태에 따른 상관관계를 조사하기 위해 고속카메라를 사용하였다. 고속카메라로 얻어진 화염 이미지로부터 장애물 주위의 국부 화염속도 및 그 화염속도의 확률밀도함수가 계산되었다. 실험결과, 장애물이 800 mm에 위치하였을 때 화염속도 및 폭발압력이 가장 높게, 200 mm에서는 가장 낮게 나타났다. 이러한 결과는 폭발거동 특성이 장애물 위치에 큰 의존성을 가지는 것으로 해석될 수 있다. 또한, 장애물 형태가 삼각형이었을 때 화염속도 및 폭발압력이 가장 높게, 원형에서는 가장 낮게 나타났다.

• 대한기계학회논문집B
• /
• 제23권5호
• /
• pp.593-602
• /
• 1999

This paper presents combustion characteristics of LPG-air mixture ignited by the plasma jet in a cylindrical vessel with constant volume, in which our focus is placed on the multi-hole plug configuration. Four types of the plug configuration depending on the number of orifice and the arranged angle are considered, along with two cases of conventional spark ignition for comparison. Not only the flame propagation is photographed at intervals, but the pressure in the combustion chamber is also recorded through the entire combustion process. The results show that the plasma jet ignition enhances the overall combustion rate remarkably in comparison to the spark ignition by generating irregular flame front and penetrating through the unburned mixture. The combustion enhancement rate agrees favorably with the available data, which supports the validity of our experiment. Synthetically estimating, the two-hole sixty-degree plug appears to be the most desirable, in that the maximum pressure as well as the combustion duration is less affected by the sub-energy level than the others. It is also deduced that there may exist an optimal plug configuration capable of rapid combustion for a specific combustion chamber.