• 제목/요약/키워드: self ignition

검색결과 86건 처리시간 0.027초

Aluminum-Copper(II) Oxide Composite의 정전기에 의한 반응 특성 연구 (Reaction Characteristics Study of Aluminum-Copper(II) Oxide Composites Initiated by the Electrostatic Discharge)

  • 김민준;김성호;김자영;임예슬
    • 한국군사과학기술학회지
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    • 제21권5호
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    • pp.591-598
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    • 2018
  • The reaction characteristics of aluminum-copper(II) oxide composites initiated by the electrostatic discharge were studied as changing the aluminum particle size. Three different sizes of aluminum particles with nano-size copper(II)-oxide particle were used in the study. These composites were manufactured by two methods i.e. a shock-gel method and a self-assembly method. The larger aluminum particle size was, the less sensitive and less violent these composites were based on the electrostatic test. On the analysis of high speed camera about ignition appearances and burning time, the burning speed was faster when aluminum particle size was smaller.

극초음속 스크램제트 엔진의 연소특성 (Combustion Characteristics of Hypersonic SCRamjet Engine)

  • 원수희;정은주;정인석;최정열
    • 한국추진공학회지
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    • 제8권1호
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    • pp.61-69
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    • 2004
  • 본 연구는 극초음속 모델 스크램제트 엔진 연소기의 화염지지와 연료-공기 혼합과정의 특성을 살펴보기 위하여 수치해석을 이용하여 수행되었다. 연료분사 방법으로 수소연료가 초음속 유동장에 수직분사되는 경우와 공동내부에 분사되는 두 가지 경우를 채택하였으며 각각 UQ(University of Queensland, Australia)와 ANU(Australian National University, Australia)의 충격파 풍동을 이용하여 실험이 수행되었다. 수치해석을 통하여 수직분사 상류의 박리영역과 공동주변에서 연소현상이 관찰되었다. 수직분사의 박리영역과 공동내부분사의 공동은 재순환 영역을 발생시키며, 이 재순환 영역은 연료-공기의 혼합을 촉진시킨다. 또한 자발점화가 박리영역-자유류, 공동-자유류 경계면에서 발생함을 알 수 있었다.

가속노화시험을 이용한 단기추진제의 저장수명예측에 관한 연구 (A Study on the Shelf-life Prediction of the Single Base Propellants Using Accelerated Aging Test)

  • 이종찬;윤근식;김용화;조기홍
    • 품질경영학회지
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    • 제35권2호
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    • pp.45-52
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    • 2007
  • The danger of self-ignition of single base propellants will increase with time. Therefore, a good prediction of the safe storage time is very important. In order to determine the remaining shelf-life of the propellants, the content of stabilizer is determined. The propellants stored under normal storage conditions about 10 to 18 years were investigated and accelerated aging test was carried out by storing propellant sample at higher temperature. Finally, we analyzed the results by various methods in order to show the best way to predict the realistic shelf-life. The safe storage life of the propellants will be 24 years, at least 15 years. In case of applying Arrhenius's law, using the reaction rate constant at 28$^{\circ}C$ to 30$^{\circ}C$ to predict the shelf-life by accelerated aging test is reasonable for a good prediction.

단가추진제의 저장수명 예측에 관한 연구 (A study on the shelflife prediction of single base propellants)

  • 이종찬;윤근식;김용화;조기홍
    • 한국품질경영학회:학술대회논문집
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    • 한국품질경영학회 2006년도 추계 학술대회
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    • pp.321-326
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    • 2006
  • The danger of self-ignition of single base propellants will increase with time. Therefore, a good prediction of the safe storage time is very important In order to determine the remaining shelf1ife of the propellants, the content of stabilizer is determined. The propellants stored under normal storage conditions about 10 to 18 years were investigated and accelerated aging test was carried out by storing propellant sample at higher temperature. Finally, we analyzed the results by various methods in order to show the best way to predict the realistic shelflife. The safe storage life of the propellants will be 24 years, at least 15 years. In case of applying Arrhenius's law, using the reaction rate constant at $28^{\circ}C$ to $30^{\circ}C$ to predict the shelflife by accelerated aging test is reasonable for a good prediction.

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기계화학적 방법에 의한 CuSbS2와 CuSbSe2 나노입자의 합성 (Synthesis of CuSbS2 and CuSbSe2 Nanocrystals by a Mechanochemical Method)

  • 박보인;이승용;이도권
    • Current Photovoltaic Research
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    • 제5권4호
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    • pp.140-144
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    • 2017
  • $CuSbS_2$ (CAS) and $CuSbSe_2$ (CASe) nanocrystals (NCs), which consist of earth-abundant elements, were synthesized by a mechanochemical method. Elemental precursors such as copper, antimony, sulfur, and selenium were used without adding any organic solvents or additives. The NCs were synthesized by milling for a few hours. The sudden phase changes occurred by self-ignition and propagation, as previously observed in other mechanochemical synthetic processes. The XRD, Raman, and TEM analysis were carried out to determine the crystallinity and secondary phase of the as-synthesized CAS and CASe NCs, confirming the phase-pure synthesis of CAS and CASe. Optical properties were investigated by UV-Vis spectroscopy and it was observed that the band gap energies were about 1.1 and 1.5 eV, respectively for CAS and CASe, suggesting the potential for the use as solar cell materials. The NC colloids dispersed in anhydrous ethanol were prepared and coated on Mo substrates by a facile doctor-blade method. The investigation on the solar cell properties of the as-synthesized materials is underway.

Numerical Simulation Study on Combustion Characteristics of Hypersonic Model SCRamjet Combustor

  • Won, Su-Hee;Eunju Jeong;Jeung, In-Seuck;Park, Jeong-Yeol
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.42-47
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    • 2004
  • Air-fuel mixing and flame-holding are two important factors that have to be considered in the design of an injection system. Different injection strategies have been proposed with particular concern for rapid air-fuel mixing and flame-holding. Two representative injection techniques can be applied in a supersonic combustor. One of the simplest approaches is a transverse(normal) injection. The cavity flame holder, an integrated fuel injection/flame-holding approach, has been proposed as a new concept for flame holding and air-fuel mixing in a supersonic combustor. This paper describes numerical efforts to characterize the flame-holding and air-fuel mixing process of a model scramjet engine combustor, where hydrogen is injected into a supersonic cross flow and a cavity. The combustion phenomena in a model scramjet engine, which has been experimentally studied at University of Queensland and Australian National University using a free-piston shock tunnel, were observed around the separation region of the transverse injector upstream and the inside cavity. The results show that this flow separation generates recirculation regions which increase air-fuel mixing. Self-ignition occurs in the separation-freestream and cavity-fteestream interfaces.

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탄화도별 발전연료의 자연발화 특성 평가 (Spontaneous Combustion of Various Fuels of Carbonization Rank)

  • 김재관;박석운;정재혁;신동익;홍준석;홍진표
    • 에너지공학
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    • 제26권3호
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    • pp.78-89
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    • 2017
  • 미분탄화력발전소에서 사용되는 각종 발전연료의 탄화도에 따른 발열개시온도(CPT;Cross Point Temperature), 발화온도(IT; Ignition temperature) 및 발화온도 승온속도(CPS;Cross Point Slope)는 전기로 내부에 설치된 백금망에 $74{\mu}m$이하 입도의 시료를 넣고 공기분위기, $25^{\circ}C$에서 $600^{\circ}C$까지의 승온조건에서 평가하였다. 발열개시온도 및 발화온도는 탄화도에 대한 의존성이 크지 않은 반면, 발화온도 승온속도는 탄화도에 크게 의존하는 것으로 나타났다. 탄화도가 낮은 우드펠렛의 발화온도 승온속도는 $20.995^{\circ}C/min$으로 기장 높은 자연발화성을 가지며, 아역청 KIDECO탄은 $15.370^{\circ}C/min$인 반면, 가장 높은 탄화도를 가지는 석유코크스는 $20.950^{\circ}C/min$로 나타냈다. 자연발화 경향성은 석탄 표면의 산화반응에 주요한 변수로서 작용하는 휘발분 함량 및 산소관능기의 농도 뿐만 아니라 촤의 비표면적, 정압몰비열이 높을수록 증가하는 것으로 확인되었다.

연속적 폭굉속도 측정 시스템을 이용한 테르밋 반응 혼합물의 연소전파속도 측정에 관한 연구 (Determination of Combustion Propagation Velocity of Thermite Reaction Mixture Using Continuous VOD Measurement System)

  • 김민성;강형민;정상선;정윤영;박훈;조상호
    • 화약ㆍ발파
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    • 제33권3호
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    • pp.21-28
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    • 2015
  • 본 연구의 목적은 연속적 폭굉속도(VOD) 측정시스템을 이용하여 상용 테르밋 반응 혼합제의 연속적인 연소전파거동을 측정하기 위한 방법을 제안하기 위함이다. 두 종류의 상용 VOD 센서(VOD PROBEROD-OS, VOD PROBEROD-HS)와 자체개발한 VOD 센서(VOD PROBEROD-ES)를 기존 연속적 VOD 측정시스템에 적용하여 테르밋 반응과정에서 발생하는 연소전파속도(VOC)를 측정한 결과, 자체 개발한 VOD PROBEROD-ES 센서만 정상적인 연속적 연소전파거동을 보여주었다. 결과적으로, 철재튜브 내 장전된 테르밋 반응 혼합제는 기폭점으로부터 100mm 이내에서 약 200m/s의 연소전파속도를 보였으며, 100mm와 300mm 구간에서 급작스럽게 증가하여 음속의 2배에 가까운 VOC를 나타내었다. 그 이후 서서히 증가하여 최종적으로 800m/s까지 증가하는 경향을 보였다. 이러한 결과는 테르밋 반응 혼합제를 이용하여 정상적인 VOC나 위력을 기대하기 위해서는 철재튜브 등으로 완전히 구속된 상태에 길이 300mm 이상 장전하여야 함을 의미한다.

초음파분무 연소법에 의한 나노결정 ZnO 초미분체 제조 (Preparation of Nanocrystalline ZnO Ultrafine Powder Using Ultrasonic Spraying Combustion Method)

  • 김광수;황두선;구숙경;이강;전치중;이은구;김선재
    • 한국재료학회지
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    • 제12권10호
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    • pp.784-790
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    • 2002
  • For mass product of nanocrystalline ZnO ultrafine powders, self-sustaining combustion process(SCP) and ultrasonic spray combustion method(USCM) were applied at the same time. Ultrasonic spray gun was attached on top of the vertical type furnace. The droplet was sprayed into reaction zone of the furnace to form SCP which produces spherical shape with soft agglomerate crystalline ZnO particles. To characterize formed particles, fuel and oxidizing agent for SCP were used glycine and zinc nitrate or zinc hydroxide. Respectively, with changing combustion temperature and mixture ratio of oxidizing agent and fuel, the best ultrasonic spray conditions were obtained. To observe ultrasonic spray effect, two types of powder synthesis processes were compared. One was directly sprayed into furnace from the precursor solution (Type A), the other directly was heated on the hot plate without using spray gun (Type B). Powder obtained by type A was porous sponge shape with heavy agglomeration, but powder obtained using type B was finer primary particle size, spherical shape with weak agglomeration and bigger value of specific surface area. 9/ This can be due to much lower reaction temperature of type B at ignition time than type A. Synthesized nanocrystalline ZnO powders at the best ultrasonic spray conditions have primary particle size in range 20~30nm and specific surface area is about 20m$^2$/g.

액체수소 사고피해 완화기술에 대한 연구 (A Study on Mitigating Accidents for Liquid Hydrogen)

  • 조영도;김진준
    • 한국가스학회지
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    • 제16권6호
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    • pp.29-33
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    • 2012
  • 이 연구에서는 최근의 액체수소안전관련 연구현황을 간략히 살펴보고자 한다. 액체수소 저장용기가 파손되어 액체수소가 누출될 수 있다. 누출된 액체수소는 풀을 형성하고 증발하여 수소증기 운을 형성한 뒤 증기운 폭발이 일어날 수 있다. 액체수소를 저장하고 있는 용기가 외부로부터 유입되는 열에 의하여 증발하는 가스를 처리하지 못할 경우에는 BLEVE가 발생할 수 있다. 압축된 수소가스가 있는 시설에서는 수소누출에 의한 제트화제가 발생하고 지연점화에 의하여 개방공간에서 플래시 화재 및 폭발이 발생할 수 있다. 이러한 여러 가지 사건에 대하여 최근의 기술개발과 향후연구개발 방향에 대하여 간략히 살펴보았다.