• 오토저널
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• 제10권3호
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• pp.60-65
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• 1988

The ignition characteristics of repetitive electric sparks into a quiescent acetylene-air premixture and LPG-argon-air premixture was investigated by using a home-made Repetitive-Spark-Generator(RSG) to elucidate the effect of fuel burning velocity to ignition ability of RSG. Results show that the optimum spark delay time interval is strongly related with fuel burning velocity, or implicitly with characteristic reaction time scale of each fuel.

• Bulletin of the Korean Chemical Society
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• 제18권10호
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• pp.1071-1075
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• 1997

Detonation characteristics of acetylene were studied behind reflected shock waves in the temperature range 800-1350 K by monitoring OH emission and pressure profiles. For a comprehensive measurement of ignition delay time, the mixture composition was varied in a wide range of Ar mole % was varied from 0.625 to 2.5 in stoichiometric ratio of C2H2-O2-Ar. A computer simulation study was also performed to elucidate the important elementary steps determining ignition behavior. The 33-reaction mechanism provides a good agreement in delay time between the observed and the calculated ones.

• 한국가스학회지
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• 제17권2호
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• pp.21-27
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• 2013

화재 및 폭발 방호를 위해서 문헌에서의 최소자연발화온도 값을 사용하는 것이 일반적이다. 본 연구에서, n-Propanol+n-Octane 계의 최소자연발화온도는 ASTM E659 장치를 이용하여 발화지연시간으로부터 측정하였다. 2성분계를 구성하는 n-Propanol과 n-Octane의 측정된 최소자연발화온도는 각 각 $435^{\circ}C$와 $218^{\circ}C$ 였다. 그리고 두 개의 2성분계에서 측정된 발화지연시간은 제시된 식에 의한 예측된 발화지연시간과 적은 평균절대오차에서 일치하였다.

• 한국화재소방학회논문지
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• 제21권3호
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• pp.33-40
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• 2007

화재 및 폭발을 방호하기 위해서 최소자연발화온도는 제시된 낮은 값을 사용하는 것이 일반적이다. 본 연구에서는 ASTM E659-78 장치를 이용하여 가연성 혼합물인 ethylbenzene+n-hexanol 계와 ethylbenzene+n-propionic acid 계의 발화지연시간과 AIT 관계를 측정하였다. 2성분계를 구성하는 순수물질인 ethylbenzene, n-hexanol, n-propionic acid의 측정된 최소자연발화온도는 각각 $475^{\circ}C,\;275^{\circ}C\;and\;511^{\circ}C$였다. 그리고 두 개의 2성분계에서 측정된 발화지연시간은 제시된 식에 의한 예측된 발화지연시간과 적은 평균절대오차에서 일치하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제27권1호
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• pp.117-123
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• 2003

In a bi-fuel engine using gasoline and LPG fuel, with the current ignition timing for gasoline being used, the effective performance could not be taken in LPG fuel supply mode. The ignition timing in LPG fuel mode must be advanced much more than that of gasoline mode for the compensation of its lower flame speed, due to engine torque drop. This study aims to develop the control system for ignition spark timing conversion which is composed of hardwares and control algorithm for gasoline/LPG engine. We propose the control system which can advance the ignition spark timing in LPG fuel mode more than used in gasoline fuel mode. The advance of ignition timing is achieved by change of the ignition dwell time of coil igniter. The engine torque and F/E(Fuel-Economy) in LPG fuel mode are measured to evaluate the difference of engine performance between before and alter changing ignition spark timings. The engine torque and F/E are increased respectively, which proves the developed control system is effective so much for gasoline and LPG bi-fuel engine.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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• pp.215-218
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• 2014

High combustion efficiency of hydrogen could make it an ideal source of green energy in the future. At this time, high pressure vessel is the most reasonable method of storing hydrogen. However, such a high pressurized vessel could pose a critical threat if ruptured. For this reason, it is important to understand the mechanism of hydrogen's self-ignition when a high-pressure hydrogen released into air. This paper presents several visualization images as experimental results using high-speed camera. From the visualization images, the ignition is initiated near rupture disk immediately after failure of disk. And the initial ignition and flame is stronger as a rupture pressure increases. However, this ignition region do not affect the general self-ignition mechanism when a high-pressure hydrogen is released into air through tue after failure of disk.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2012년도 제44회 KOSCO SYMPOSIUM 초록집
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• pp.213-215
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• 2012

As one of the primary fuel sources, oxy-fuel combustion of coal is actively being investigated because of the climate changing problem such like the emission of green house gases. In this paper research about the pulverized coal technology, which is widely used in both power-generating and iron-making processes was studied to invesgate the ignition behaviour of pulverized coal particles during coal combustion as changing the ambient oxygen concentration of the particle. The ignition phenomenon of the coal particles fed into a laminar flow reactor was imaged with a Integrated charged-coupled device (ICCD) camera. The ignition points were determined throught the analysis of the images, and then the ignition delay times were able to be calculated. The experiment results show that a lower oxygen concentration increases the ignition delay time.

• 청정기술
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• 제26권3호
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• pp.204-210
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• 2020

본 연구에서는 F-T 공정을 통해 합성하여 제조한 바이오항공유(Bio-7629, Bio-5172)와 기존에 사용 중인 석유계항공유(Jet A-1)의 점화특성을 비교하여 분석하였다. Combustion research unit (CRU) 장비를 활용하여 각 항공유의 점화지연시간을 측정하였고, 그 결과를 연료의 물성 및 구성 화합물에 대한 분석을 통해 해석하고자 하였다. 점화지연시간은 Bio-5172가 가장 짧게 측정되었으며 Jet A-1이 가장 길게 측정되었다. 이는 물리적 점화지연시간에 영향을 줄 수 있는 연료의 물성 측면에서 Jet A-1이 가장 큰 표면장력을 가지며 Bio-5172가 가장 낮은 점도를 갖기 때문인 것으로 해석된다. 또한, 각 연료를 구성하는 화합물의 종류 및 비율에 대하여 분석한 결과, 실험 대상 바이오항공유에 없는 방향족화합물이 Jet A-1에는 약 22.8%의 비율로 존재함을 확인하였다. 이는 산화 과정 시에 비교적 반응성이 낮은 benzyl radical을 생성하여 점화지연시간이 길게 측정되는 데에 영향을 주는 것으로 판단된다. Bio-7629와 Bio-5172는 paraffin으로만 구성되어 있으며, n-/iso-의 값은 각각 0.06, 0.80으로 큰 차이를 보였다. 가지화 된 정도가 낮은 paraffin일수록 산화 시에 생성되는 peroxy radical의 이성질화가 빠르게 진행되어 점화의 전파속도 또한 빨라진다. 따라서 n-paraffin의 함량이 비교적 높은 Bio-5172의 경우에 점화지연시간 또한 짧게 측정된 것으로 해석된다.

• 한국연소학회지
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• 제5권1호
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• pp.43-53
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• 2000

Experimental studies on determination of the supply leading time of propellants to combustion chamber have been made to stably and efficiently guarantee the ignition process with liquid rocket engine. The propellant used is a Jet A-1 as fuel and a liquid oxygen as oxidizer. Unlike impinging FOOF type of injectors are arranged radially and the designed O/F ratio is 2.34. The present experiment program also includes the stability on the quadlet type of ignitor using the triethylalumimum as an ignition source and injector life tests. Experimental results clarifies that the propellant supply through LOx leading to combustion chamber is proper for stable ignition and combustion processes based on the fuel and oxidizer manifold pressures, combustion chamber pressure, and the variation of flame length from the nozzle exit with lapse time, and shows that the leading supply time of propellants affects the engine performance little. The effect of positioning cooling holes is remarkable to protect the injector face.

• KIEE International Transactions on Electrophysics and Applications
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• 제5C권4호
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• pp.145-151
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• 2005

The synthetic breaking test method was developed to evaluate the breaking performance of ultra high-voltage circuit breaker and made up of two independent circuits; current source circuit and voltage source circuit. In application of this test method, it is necessary to extend the arc of the test breaker. So, the new re-ignition system using VTGS (Vacuum Triggered Gap-Switch) was constructed to improve the efficiency and reliability of this test. In this re-ignition system, VTGS operates in high vacuum state of $5{\time}10^{17}$torr and control system consists of the triggering device and the air M-G (Motor-Generator). This re-ignition system showed the operating characteristics, such as delay time ($t_d$) and jitter time ($t_j$ not exceeding 5us and 1us respectively, and had the operating voltage of $25\~150kVdc$ at the gap distance of 24mm.