• 제목/요약/키워드: ignition temperature

검색결과 882건 처리시간 0.027초

CaO가 첨가된 Mg-3Al, Mg-6Al 및 Mg-9Al Eco-Mg 합금의 발화 저항성 평가 (Ignition resistance of CaO added Mg-3Al, Mg-6Al and Mg-9Al Eco-Mg alloys)

  • 이진규;김세광
    • 한국주조공학회지
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    • 제31권2호
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    • pp.60-65
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    • 2011
  • Molten magnesium alloys and magnesium products are easily oxidized and burned when they are exposed to high temperature for manufacturing process and by accident. In order to solve these problems, CaO addition in magnesium alloys has been developed. The ignition resistance of CaO added Mg-3Al, Mg-6Al, and Mg-9Al Eco-Mg alloys were investigated in comparison with those of magnesium alloys without CaO. The ignition resistance was examined by three methods : DTA, furnace chip ignition test, and torch ignition test. DTA was carried out for obtaining quantitative ignition temperature data with respect to specimen geometry and test environment; the furnace ignition test for burr and chip ignition temperature data; and the torch test for ignition temperature data for manufactured products. The ignition resistance of magnesium alloys under all conditions greatly increased by CaO addition.

우드펠릿의 저장량에 따른 발화온도 및 발화유도시간에 관한 연구 (A Study on the Ignition Temperature and Ignition Induction Time According to Storage Amount of Wood Pellets)

  • 김형석;최유정;김정훈;정필훈;최재욱
    • 한국화재소방학회논문지
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    • 제33권1호
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    • pp.7-14
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    • 2019
  • 우드펠릿은 화력발전소 및 화목 보일러의 연료로 많이 사용되고 있으나 발열량이 높은 우드펠릿을 장기간 보관 시 자연발화의 위험성이 있다. 본 연구에서는 시료 용기의 크기에 따라 유량의 변화에 따른 최소자연발화온도와 발화한계온도를 구하였으며, 발화한계온도를 이용하여 겉보기 활성화 에너지를 측정함으로써 우드펠릿의 발화 특성을 예측하였다. 겉보기 활성화 에너지는 190.224 kJ/mol을 구하였다. 용기에 저장된 시료량이 두꺼워질수록 시료 표면에서 중심까지의 열전달이 어려워 발화유도시간이 긴 것으로 나타났으며, 용기의 크기가 같을 경우 유량의 양이 많아 질수록 자연발화온도는 낮아졌다. 또한 시료용기가 커질수록 자연발화온도는 낮아지고 발화유도시간은 길어지는 것으로 나타났다.

정용연소장치에 의한 어유의 착화지연에 관한 연구 (A Study on the Ignition Delay of Fish Oil Using a Constant Volume Combustion Bomb)

  • 서정주;왕우경;안수길
    • 한국자동차공학회논문집
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    • 제1권1호
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    • pp.50-58
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    • 1993
  • The ignition delay of diesel oil and fish oil blended with diesel oils was investigated at various pressure and temperature conditions in a constant volume combustion bomb. The evaporation and combustion duration of diesel oil and fish oil blended with diesel oils were respectively different in high and low temperature. The dependence of ignition delay on the temperature was different in high and low temperature ranges which were divided at the 773K. The dependence of ignition delay on the pressure was almost linear, regardless of the test fuels at the constant temperature(863K). The ignition delay became longer as the blending rate of fish oil increased at the constant temperature and pressure, but it was especially short with 20% fish oil blended with diesel oils.

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고온 고압 환경에서 레이저를 이용한 알루미늄 입자 생성과 점화 (Aluminum ignition in laser-generated aluminum particles in high temperature and high pressure environment)

  • 이경철;타이라 쯔바사;구군모;이재영;박정수;여재익
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2012년도 제45회 KOSCO SYMPOSIUM 초록집
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    • pp.101-103
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    • 2012
  • Characteristic of aluminum ignition under high temperature and high pressure is studied using lasers. The laser ablation method is used to generate aluminum particles exposed to a high pressure by using a nanosecond pulsed laser where the range of ablation pressure varies between 0.35 and 2.2 GPa. A $CO_2$ laser is used to supply radiative heat to the aluminum target surface for providing high temperature ranging between 5000~9300 Kelvin. The ignition is confirmed using spectroscopy analysis of AlO vibronic band 484 nm wavelength. Also the radiative temperature is measured in various high pressure range for tracing the ignition temperature in high pressure conditions.

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A Study on the Flash Point and Spontaneous Ignition Determination of Diethylene Glycol

  • 김정훈;최재욱
    • 한국태양에너지학회 논문집
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    • 제36권2호
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    • pp.73-78
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    • 2016
  • This study investigates the main factors of fire prevention, such as spontaneous ignition and flash point, while using Diehylene Glycol (DEG) as the antifreeze for automobile and industrial machines. Our results show the flash point of $142^{\circ}C$ and the minimum ignition temperature of $388^{\circ}C$ in the range of $130{\mu}{\ell}{\sim}150{\mu}{\ell}$. By increasing temperature to ignite in 1 second, an instantaneous ignition temperature of the sample is $569^{\circ}C$ in the sample amount of $140{\mu}{\ell}$.

마이크로터빈의 새로운 점화 기법과 점화 인식 로직 개발 (New Ignition Method and Ignition Recognition Logic for a Microturbine)

  • 김기래;최영규;노민식
    • 제어로봇시스템학회논문지
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    • 제13권2호
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    • pp.179-186
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    • 2007
  • This paper presents new ignition method and ignition recognition logic for a microturbine. New ignition method is designed by constant speed control of a microturbine with pre-determined time during a ignition period. It make more accurate air-fuel ratio as well as give enough time to ignition system to have full performance under cold temperature. And ignition recognition logic is designed by observing output current change of inverter by generating output torque of a microturbine in the instant of ignition. For filtering a output torque current of inverter with high frequency, we applied a moving average method. So far, ignition recognition is usually implemented by measuring of exhausted gas temperature(EGT) of microturbine. The proposed logic can give more accurate judgement of ignition as well as keep a good working of starting system under out of order a temperature measuring system and biased initial value of EGT sensor. Finally, the two proposed logics are proved by field operating a microturbine under various conditions.

고체추진기관에서 점화현상의 성능해석 연구

  • 김유;류계열
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 1995년도 제5회 학술강연회논문집
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    • pp.139-144
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    • 1995
  • The main purpose of igniter is sure ignition of main propellant at desired ignition delay times. Since ignition mechanism of solid rocket propellant involves so many complicated physical and chemical phenomena, it is almost impossible to predict ignition behavior with pure analytical means. In this study, one dimensional and unsteady ignition transient phenomena in solid rocket was analyzed by finite volume method. In analysis, assumption was made that ignition occurs when propellant surface temperature reaches to it's auto-ignition temperature.

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도장 폐기물의 자연발화에 관한 연구 (A Study on Spontaneous Ignition of Painting Waste)

  • 최재욱;목연수;옥곤;사공성호
    • 한국안전학회지
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    • 제14권2호
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    • pp.90-96
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    • 1999
  • The characteristics of spontaneous ignition of painting waste was investigated at constant ambient temperature in oven. As the results of experiments, the spontaneous ignition temperature decreased as the sample vessel became large, and the spontaneous ignition temperature of the sample in small, intermediate and large vessels was $165.5^{\circ}C$, $144.5^{\circ}C$ and $134.5^{\circ}C$ respectively. The apparent activation energy calculated by the Frank-Kamentskii's thermal ignition theory was 34.73 kcal/mol.

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산소농도 변화에 따른 입상활성탄의 자연발화에 관한 연구 (A Study on the Autoignition of Granulated Activated Carbon with Change of Oxygen Concentration)

  • 목연수;최재욱;류동현;최일곤;김상렬
    • 한국안전학회지
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    • 제10권2호
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    • pp.84-91
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    • 1995
  • The characteristics of critical spontaneous ignition of granulated activated carbon were investigated In atmospheres of differing oxygen concentration. At the same concentration the larger vessels yielded the lower critical spontaneous ignition temperature. At the same vessel, as the concentration of oxygen was reduced, Ignition occurred later and at higher ambient temperature, and critical spontaneous ignition temperature increased. The apparent activation energy calculated from the Frank-Kamenetskii's ignition theory appeared to be the slight different value respectively and the mean apparent activation energy was 19850㎈/㏖.

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MBS 공중합물의 자연발화 특성에 관한 연구 (A Study on Autoignition Characteristics of Methylmethacrylate-butadiene-styrene Copolymer)

  • 목연수;최재욱
    • 한국안전학회지
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    • 제16권3호
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    • pp.83-88
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    • 2001
  • This study was preformed by measuring the minimum ignition temperature of MBS according to the change of sample vessel size and the minimum ignition temperature of MBS dust cloud The minimum ignition temperature of MBS product decreased as the vessel size was large, and it was obtained in the range from $120.5^{\circ}C$ to $94.5^{\circ}C$ and the apparent activation energy was obtained with 32.94Kcal/mol. The minimum ignition temperature of MBS dust cloud was measured by using Godbert-Greenwald furnace and it was obtained at $407^{\circ}C$ with the sample of 0.4g in the air and the ignition of dust cloud was not occurred below 13% oxygen concentration.

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