• Title/Summary/Keyword: Combustion Response

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Development of Oxygen Sensor for the Oxygen Concentration Measuring of Air-fuel Ratio Measuring System (공연비 측정시스템의 산소농도 측정을 위한 센서 개발)

  • Lee, Jin-Hui;Choi, Ko-Yeol;Jang, Hyang-Dong;Kim, Yang-Soo;Cho, Dong-Hoe;Park, Myon-Yong;Chung, Koo-Chun;Cho, Jin-Weon
    • Analytical Science and Technology
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    • v.12 no.6
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    • pp.472-477
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    • 1999
  • It was developed the oxygen sensor of air-fuel ratio measuring system that was controlled the needed air amounts in optimum combustion according to the analysis of oxygen concentration of exhaust gas. The oxygen sensor was prepared by using gold as cathode, which the detection range for the oxygen concentration was from 0.0% to 30.0%. Response time was observed 15 to 20 sec. rapidly and selectively. It was appeared a good result in reproducibility and stability.

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Effect of Changing the Intake Air Temperature in a Marine Diesel Engine on the Characteristics of Exhaust Gas Emission (선박 디젤기관의 배기배출물 특성이 흡기 온도변화에 미치는 영향)

  • Cho, Sang-Gon
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.25 no.6
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    • pp.788-794
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    • 2019
  • Recently, global climate change caused by greenhouse gases has emerged as a significant air-environmental problem. Technical innovation in response to this phenomenon is ongoing, with an emphasis on the environmental impacts of unusually high temperatures and unexpected heavy rainfall. In this study, we investigated the effects of temperature change on air pollution for a concomitant rapid temperature increase. The test conditions include loading from 0 % to 100 % at 1400 rpm, 1600 rpm, and 1800 rpm for a change in the intake air temperature of a marine diesel engine from 20 ℃ to 50 ℃. The experimental results revealed that CO and HC decreased slightly, whereas the brake specific fuel consumption, NOx, and PM increased slightly when the intake air temperature changed. In addition, it was determined that the combustion temperature did not change significantly.

A Study on Flash Points and Fire Points of Acids Using Closed Cup and Open-cup Apparatus (밀폐식과 개방식 장치를 이용한 Acid류의 인화점과 연소점에 관한 연구)

  • Ha, Dong-Myeong;Han, Jong-Geun;Lee, Sung-Jin
    • Fire Science and Engineering
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    • v.20 no.3 s.63
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    • pp.29-34
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    • 2006
  • The flash and fire point are the most important combustible properties used to determine the potential for the fire and explosion hazards of flammable material. The flash point is defined as the lowest temperature at which a flammable liquid gives off sufficient vapor to form an ignitable mixture with air near its surface or within a vessel. The fire point is the temperature of the flammable liquid at which there will be flaming combustion, sustained 5 seconds in response to the pilot flame. In this study, the flash points and fire points were measured to present raw data of the flammable risk assessment for acids, using Pensky-Martens Closed Cup(C.C.) apparatus (ASTM-D93) and Tag Open-cup (O.C.) apparatus(ASTM D 1310-86). The measured fire points were compared with the estimated values based on 1.11 times stoichiometric concentration. The values calculated by the proposed equation were in good agreement with measured values.

Statistical Energy Analysis of Low-Altitude Earth Observation Satellite (저궤도 지구관측 위성의 통계적 에너지 해석)

  • Woo, Sung-Hyun;Kim, Hong-Bae;Im, Jong-Min;Kim, Kyung-Won
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2006.05a
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    • pp.197-202
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    • 2006
  • The low-altitude earth observation satellite is generally equipped with high performance camera as a main payload which is vulnerable to vibration environment. During the launch process of a satellite, the combustion and jet noise of launch vehicle produce severe acoustic environment and the acoustic loads induced may damage the critical equipments of the satellite including the camera. Therefore to predict and simulate the effect of the acoustic environment which the satellite has to sustain at the lift-off event is very important process to support the load-resistive design and test-qualification of components. Statistical Energy Analysis(SEA) has been widely used to estimate the vibro-acoustic responses of the structures and gives statistical but reliable results in the higher frequency region with less modeling efforts and calculation time than the standard FEA. In this study, SEA technique has been applied to a 3-Dimensional model of a low-altitude earth observation satellite to predict the acceleration responses on the structural components induced by the high level acoustic field in the launch vehicle fairing. In addition, the expected response on each critical component panel was calculated by the classical method in consideration of the mass loading and imposed sound pressure level, and then compared with SEA results.

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Combustion Characteristics and Performance Prediction of PE-GOX Hybrid Rocket Motor Part II : Internal Ballistic Performance (PE-GOX 하이브리드 모터의 연소특성 및 성능 예측 기법 Part II : 내탄도 성능)

  • Yoon, Chang-Jin;Song, Na-Young;Yoo, Woo-Jun;Jeon, Chang-Soo;Kim, Jin-Kon;Moon, Hee-Jang;Sung, Hong-Gye
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.2
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    • pp.79-85
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    • 2007
  • An internal ballistic model to predict the performance of a Polyethylene-GOX (PE-GOX) hybrid motor was proposed and evaluated. A theoretical treatment of the model was followed by detail discussion of each of the factors affecting the overall performance. The present model consists of the governing equations by considering the unsteady burn-back rate of the fuel grain and on-off response characteristics of a oxygen-supply valve. The numerical results using the 4th order Runge-Kutta scheme with temporal physicochemical properties showed good agreements with test results and the global effects of the performance parameters, such as the burning area of the fuel grain, O/F ratio, and etc., on the performance of the motor were analyzed.

Effect of Genistein on the Benzo(k)fluoranthene Regulated CYP1B1 Gene Expression (Genistein이 Benzo(k)fluoranthene에 의한 CYP1B1 유전자조절 작용에 미치는 영향)

  • Seo, Mi-Jung;Sheen, Yhun-Yhong
    • Environmental Mutagens and Carcinogens
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    • v.24 no.4
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    • pp.163-170
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    • 2004
  • CYP1B1 enzyme metabolize PAHs and estradiol. CYP1B1 metabolize estradiol to 4-hydroxyestradiol that is considered as carcinogenic metabolite. Luciferase activity was induced about 20 folds over that control by 1 nM TCDD (2,3,7,8-tetrchlorodibenzo-p-dioxin) and these inductions were dose-dependent. Recent industrialized society, human hasbeen widely been exposed to widespread environmental contaminants such as PAHs (polycyclic aromatic hydrocarbon) that are originated from the incomplete combustion of hydrocarbons. PAHs are known to be ligands of the AhR (aryl hydrocarbon receptor). Induction of cytochrome P4501B1(CYP1B1) in cell culture is widely used as a biomarket for PAHs. Therefore we have studied the effect of PAHs in the human breast cancer cells MCF-7 to evaluate bioactivity of PAHs. Cytochrome P4501B1(CYP1B1) is known to be inducible by xenobiotic compounda such as policyclic aromatic hydrocarbon (PAH) and dioxins such as 2,3,7,8-tetrachloro-dibenzo-p-dioxin(TCDD). And these induction of CYP1B1 is also regulated by many categories of chemicals. In order to investigate the effects of several chemicals on CYP1B1 gene expression in luciferase gene, and then transfected into these cells. After treatment of chemicals, the luciferase activity was measured. We examined effects of PAHs on the CYP1B1-lucifrease reporter gene and CYP1B1 mRNA level. Benzo(k)fluoranthene showed strong response to CYP1B1 promoter activity stimulation, and also CYP1B1 mRNAs increase in MCF-7 cells in a concentration-dependent manner. flvonoids such as genistein decreased B(k)F induced luciferase activity at low concentration. it exhibited stimulatory effect at high concentration.

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Reexamination of the combustion instability of solid propellant with radiative heat transfer (복사 열전달을 고려한 고체 추진제의 연소 불안정 현상에 관한 재해석)

  • 이창진;변영환;이재우
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1997.11a
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    • pp.10-11
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    • 1997
  • 고체 추진제를 사용하는 추진 시스템을 개발하는데 가장 커다란 문제로 인식되고 있는 것은 추진제의 연소 특성을 이해하는 일이다. 그 중에서도 연소실의 압력 진동과 추진제 벽면으로 흡수되는 복사 열전달에 의한 연소율(burning rate)의 변화로 인하여 발생하는 연소 불안정에 대한 이해는 아직도 완전히 규명되지 않고 있다. 고체 추진제의 연소 불안정에 대한 이론적 해석은 준-정상 1차원 해석(Quasi-Steady Homogeneous One-Dimension) 방법에 의하여 단순화된 지배방정식을 해석하는 것이 일반적으로 잘 알려져 있는 방법이다. 이 가정은 고체 추진제가 연수되는 영역을 두께가 매우 얇은 영역의 표면반응영역(surface reaction layer)과 화학반응이 없는 응축상태영역(condensed phase zone) 그리고 기체상태의 연료와 화염이 존재하는 기체상태영역(gas phase zone) 등의 3영역으로 구분하며, 기체상태영역에서 발생하는 교란에 대한 응축상태영역의 반응시간 크기(response time scale)가 매우 크기 때문에 응축상태영역의 반응은 준 정상적으로 일어난다고 가정하는 것이다.그러나, 연소실의 온도가 $3000^{\circ}K$ 정도의 높은 온도이어서 복사 열전달에 의한 고체 추진제의 가열이 중요한 열전달 방법으로 작용하게 되므로 이를 무시한 이론적 해석은 물리적인 중요성이 약하여질 수밖에 없다. 본 연구에서는 기체영역으로부터 전달되는 복사 열전달은 투명(transparent)한 표면반응영역을 통과하여 응축상태영역에서 모두 흡수되며 추진제 표면에서의 복사열방출(emission)을 고려하였다. 또한 연소불안정 현상을 해석하기 위하여 표면반응영역에서의 경계조건은 선형교란량으로 대치하는 Zn(Zeldovich-Novozhilov) 방법을 사용하였다. 이 방법은 기체상태영역에 대한 구체적인 해석없이도 연소불안정 현상을 해석할 수 있는 장점이 잇다. 즉 응축상태영역에서의 연소율과 표면온도는 각각 기체영역으로부터 전달되는 온도구배와 연소압력, 그리고 복사 열전달의 함수관계이므로 선형교란에 의한 추진제표면에서의 교란경계조건을 얻을 수 잇으며, 응축영역의 교란지배방정식과 함께 사용하여 압력교란과 복사 열전달의 교란에 대한 연소율의 교란 증감 여부를 판단하여 연소 불안정 현상을 해석할 수 있다.

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$\mu\textrm{p}$-based Electronic Control System for Automobiles Part1. Electronic Engine Control System (자동차의 마이크로프로셋서를 이용한 전자식 제어시스템에 대한 연구 제1편 : 전자식 엔진 제어시스템)

  • Chae, Suk;Kim, Young-Lip;Liu, Joon;Kim, Kwang-Rak;Bien, Zeungnam
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.17 no.5
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    • pp.15-21
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    • 1980
  • An engine control system in which the conventional mechanical ignition system is studied. The contact point of the breaker is replaced by the contactless magnetic pick up sensor from which the information of the speed and the position of the crankshaft is extracted , and further an electronic High Energy Ignitim System Is designed, implemented and tested . The High Energy Igniticwl System increases the secondary spark voltage of the ignition coil from the conventional 10000~15000 volts to the 30000~40000 volts resulting in improving the combustion efficiency. Also, instead of the conventional advimce mechanism forigniliontiming control, a microprocessorbased timinng mechanisn is installed to determine the ignition timing data in response to the engine rpm and the intake manifold vacuum.

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Study for the Development of a Main Oxidizer Shut-off Valve for Liquid Rocket Engines (발사체 연소기용 산화제 개폐밸브의 핵심요소 기술 개발)

  • Kim, Dohyung;Hong, Moongeun;Park, Jaesung;Lee, Soo Yong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.6
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    • pp.113-119
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    • 2013
  • A main oxidizer shut-off valve (MOV) controls the supply of cryogenic liquid oxygen to the combustion chamber of liquid rocket engines by on/off operations. The main subjects to be introduced are not only the valve transient response during valve on/off procedures but also the characteristics of pneumatic and seat/poppet parts as core technologies in the development of the MOV, which is expected to be adopted for the Korea Space Launch Vehicle II. It is shown that the analytical prediction of the transient valve travel is in good agreement with experimental results. Friction and elastic forces on the valve moving part are quantitatively evaluated by structural analysis.

Procedure of Seismic Performance Evaluation of LNG Receiving Terminal Facilities (천연가스 생산기지 시설물의 내진성능평가 절차)

  • Lee, Tae-Hyung;Lee, Eunsuk;Park, Taekyu;Hong, Seong Kyeong;Kim, Joonho
    • Journal of the Korean Society of Safety
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    • v.29 no.4
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    • pp.110-115
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    • 2014
  • It is crucial for important facilities to withstand strong earthquakes because their damage may cause undesirable socio-economic effect. A liquefied natural gas (LNG) receiving terminal is one of the lifeline facilities whose seismic safety needs to be guaranteed. Even though all operating LNG receiving terminals in Korea were seismically designed, old design codes do not guarantee to comply with the current seismic design codes. In addition, if the constructional materials have been deteriorated, the seismic capacity of facilities may be also deteriorated. Therefore, it is necessary that the seismic performance of LNG receiving terminals is evaluated and the facilities that lack of seismic capacity have to be rehabilitated. In this paper, a procedure of seismic performance evaluation of such facilities is developed such that the procedure consists of three phases, namely pre-analysis, analysis, and evaluation phases. In the pre-analysis phase, design documents are reviewed and walk-on inspection is performed to determine the current state of the material properties. In the analysis phase, a structural analysis under a given earthquake or a seismic effect is performed to determine the seismic response of the structure. In the evaluation phase, seismic performance of the structure is evaluated based on limit states. Two of the important facilities, i.e. the submerged combustion vaporizer (SMV) and pipe racks of one of the Korean LNG receiving terminals are selected and evaluated according to the developed procedure. Both of the facilities are safe under the design level earthquake.