• 제목/요약/키워드: High Temperature & High Pressure Combustion

검색결과 406건 처리시간 0.031초

미세폭발을 가진 혼화 이성분 연료 액적의 증발 현상 (Microexplosive Vaporization of Miscible Binary Fuel Droplets)

  • 호잿가세미;백승욱;카심살월칸
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2005년도 제31회 KOSCO SYMPOSIUM 논문집
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    • pp.120-131
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    • 2005
  • The evaporation characteristics of single and multicomponent droplets hanging at the tip of a quartz fiber are studied experimentally at the different environmental conditions under normal gravity. Heptane and Hexadecane are selected as two fuels with different evaporation rates and boiling temperatures. At the first step, the evaporation of single component droplet of both fuels has been examined separately. At the next step the evaporation of several blends of these two fuels, as a binary component droplet, has been studied. The temperature and pressure range is selected between 400 and 700 $^{\circ}C$, and 0.1 and 2.5 MPa, respectively. High temperature environment has been provided by a falling electrical furnace. The initial diameter of droplet was in range of 1.1 and 1.3 mm. The evaporation process was recorded by a high speed CCD camera. The results of binary droplet evaporation show the three staged evaporation. In the the first stage the more volatile component evaporates. The droplet temperature rises after an almost non evaporating period and in the third stage a quasi linear evaporation takes place. The evaporation of the binary droplet at low pressure is accompanied with bubble formation and droplet fragmentation and leads to incomplete microexplosion. The component concentration affects the evaporation behavior of the first two stages. The bubble formation and droplet distortion does not appear at high environment pressure. Nomenclature

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음파를 이용한 연소 안정성 개선에 관한 연구 (A Study of Improving Combustion Stability with Sonic Wave Radiation)

  • 민선기
    • 한국산학기술학회논문지
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    • 제21권8호
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    • pp.401-406
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    • 2020
  • 자동차에서 배출되는 배기가스 중 질소산화물은 요사이 문제가 되는 미세먼지의 주요 요인 중 하나이다. 질소산화물(NOx)은 고온 조건에서 연소가 진행될 때 발생하므로 연소시 온도를 낮추는 방법으로 발생을 억제하고 있다. 자동차에서는 일반적으로 배기가스 재순환(EGR)을 사용하여 연소 온도를 낮추는 방법으로 감소시킨다. 그러나 EGR 비율이 높아질수록 NOx의 양은 저감되나 연소 안정성의 하락으로 인한 불완전연소 가능성의 증가로 일산화탄소와 미연탄화수소의 양이 증가하여 오히려 오염물질이 증가하는 문제를 발생시킬 수 있다. 여기에서는 연료 입자에 음파를 조사하여 연료 입자의 운동성을 향상시켜 연소가 원활히 진행되게 하여 연소의 안정성을 향상시키는 방안에 대하여 해석적 및 실험적 방법으로 연구하였다. 해석적 방법으로는 유동해석 소프트웨어를 사용하여 연료 입자에 다양한 주파수의 음파를 조사하여 연료 입자의 움직임 변화에 대한 연구를 진행하였다. 해석 결과, 작은 연료 입자의 조건에서는 고주파의 음파에 의해 영향을 많이 받고, 연료 입자가 큰 조건에서는 저주파의 음파에 의해 영향을 많이 받아 운동성이 증가함을 알 수 있었다. 실험적 방법으로는 연소실을 구성하여 정해진 당량비 조건에서 연소시키며 다양한 주파수의 음파를 조사하며 연소실내 압력을 측정하는 연구를 진행하였다. 측정된 압력으로부터 열방출량을 계산하면 연소의 진행 상황에 대한 정보를 얻을 수 있는데, 실험 결과 초기 연소시 상대적 저주파 조사 조건에서 열방출량이 증가한 것을 확인할 수 있었다.

농도성충화가 DME HCCI 엔진의 운전 영역 확장에 미치는 영향에 관한 수치해석 연구 (Effect of the Fuel Stratification on the Operating Range for a DME HCCI Engine based on Numerical Analysis)

  • 권오석;정동원;백영순;임옥택
    • 한국수소및신에너지학회논문집
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    • 제20권3호
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    • pp.256-263
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    • 2009
  • The operating range of HCCI engine is narrow due to excessive rate of pressure rise on high load. The fuel stratification is proposed to solve the problem. The purpose of this study is to gain a better understanding of the effects of fuel stratification on reducing the pressure-rise rate at high load in HCCI combustion and to investigate that the operating range is expanded for fuel stratification in the preceding condition of initial temperature and equivalence ratios. The engine is fueled with Di-Methyl Ether (DME) which has unique 2-stage heat release. The computations were conducted using SENKIN application of the CHEMKINll kinetics rate code. Calculation result shows that proper fuel stratification prolongs combustion duration and reduce pressure rise rate.

디젤 저온연소 운전 영역에서 흡기압이 엔진 성능에 주는 영향 (Effect of Intake Pressure on Emissions and Performance in Low Temperature Combustion Operation of a Diesel Engine)

  • 이선엽;장재훈;이용규;오승묵;김용래;김득상
    • 한국자동차공학회논문집
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    • 제20권1호
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    • pp.88-94
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    • 2012
  • One of the effective ways to reduce both $NO_x$ and PM at the same time in a diesel CI engine is to operate the engine in low temperature combustion (LTC) regimes. In general, two strategies are used to realize the LTC operation-dilution controlled LTC and late injection LTC - and in this study, the former approach was used. In the dilution controlled regime, LTC is achieved by supplying a large amount of EGR to the cylinder. The significant EGR gas increases the heat capacity of in-cylinder charge mixture while decreasing oxygen concentration of the charge, activating low temperature oxidation reaction and lowering PM and $NO_x$ emissions. However, use of high EGR levels also deteriorates combustion efficiency and engine power output. Therefore, it is widely considered to use increased intake pressure as a way to resolve this issue. In this study, the effects of intake pressure variations on performance and emission characteristics of a single cylinder diesel engine operated in LTC regimes were examined. LTC operation was achieved in less than 8% $O_2$ concentration and thus a simultaneous reduction of both PM and $NO_x$ emission was confirmed. As intake pressure increased, combustion efficiency was improved so that THC and CO emissions were decreased. A shift of the peak Soot location was also observed to lower $O_2$ concentration while $NO_x$ levels were kept nearly zero. In addition, an elevation of intake pressure enhanced engine power output as well as indicated thermal efficiency in LTC regimes. All these results suggested that LTC operation range can be extended and emissions can be further reduced by adjusting intake pressure.

음향가진과 보염기형상이 확산화염의 특성에 미치는 영향 (Effect of Acoustical Excitation and Flame Stabilizer on a Diffusion Flame Characteristics)

  • 전충환;장영준
    • 한국연소학회지
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    • 제3권1호
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    • pp.1-10
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    • 1998
  • Lots of techniques are adopted for a flame stabilization and a high-load combustion. But the techniques being used were passive control method which have to change combustor shape like pilot flame, flame stabilizer, pressure profile, etc. Active control method which is not necessary to transform its shape is employed. Acoustical excitation is broadly used for its convenience in changing frequency and intensity. Both acoustical excitation and flame stabilizers were adopted to study their relationship. So, we investigated flammability limits. Flame visualization. And mean temperature in the condition of various frequencies, intensities, and flame stabilizers. As a consequence, flammability limit were advanced in acoustically excited flame at some frequencies. Coherent structure was extended to the downstream region through acoustical excitation and a size of vortice was curtailed. Also width of recirculation zone was magnified. In addition, Effects of acoustical excitation was stood out at 25mm flame stabilizer rather than another ones.

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미분탄 화염 영상 분석을 통한 취입랜스 최적 제어 기법 개발 (Development of injection lance position control method using fine Bituminous Coal combustion Image Analysis)

  • 김지언;이민철;백준영;정도영;안영진
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회A
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    • pp.806-810
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    • 2008
  • This paper introduces the automatic fine Bituminous Coal injection lance position control method using flame image process. The fine Coal injection lance is used to supply additional heat into the furnace in Mill plant. It injects fine coal into high pressured air flow and produces very heated and high pressured flame. For the such high temperature and pressure, the fine coal injection lance effects not only efficiency of burner but also furnace abrasion. To keep efficient combustion status and to avoid the abrasion, in this paper, the flame is monitored by computer image process. This paper proposes the flame image process method and lance position control according to calculated result for flame image process.

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Test Results of the Mechanical Face Seal for a Turbopump

  • Kwak, Hyun-D.;Jeon, Seong-Min;Kim, Jin-Han
    • KSTLE International Journal
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    • 제8권1호
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    • pp.11-15
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    • 2007
  • The mechanical face seal has been tested in Korea Aerospace Research Institute (KARl) for turbopump applications. In the turbopump under current development, the mechanical face seal is installed between fuel pump and turbine to prevent a mixture of fuel and combustion gas. Generally the mechanical face seal in turbopump is exposed to severe environment because of great rotational speed, high temperature of combustion gas and high level of pressure difference. Thus a series of tests were performed to guarantee the reliability of mechanical face seal by means of simulating the practical operating conditions. The tests were conducted up to 20,000 rpm with pressure difference of 800 kPa and temperature of 620 K In addition several carbon materials for mechanical face seal were conducted to the tests to compare the life time. During the tests, the performance against leakage was monitored and the carbon wear was also measured to estimate the life of a mechanical face seal The results show that the leakage flow rates of mechanical face seal is ignorable compared to an overall flow rate of fuel pump. The carbon material which has the finest wear resistance was found during the tests. Lastly no critical failure of mechanical face seal was found during the tests and the reliability of mechanical face seal for turbopump was successfully proved.

Measurement of Heat Flux in Rocket Combustors Using Plug-Type Heat Flux Gauges

  • Kim, Min Seok;Yu, I Sang;Kim, Wan Chan;Shin, Dong Hae;Ko, Young Sung
    • International Journal of Aeronautical and Space Sciences
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    • 제18권4호
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    • pp.788-796
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    • 2017
  • This paper proposes a new measurement method to improve the shortcomings of an existing integral method for measuring heat flux in plug-type heat flux gauges in the high-temperature and high-pressure environments of liquid-rocket combustors. Using the existing integral measurement method, the calculation of the surface area for the heat flux in the gauge exhibits error in relation to the actual surface area. To solve this problem, transient profiles obtained from ANSYS Fluent were used to calculate unsteady heat flux as it adjusted to the measured temperature. First, a heat flux gauge was designed and manufactured specifically for use in the high-temperature and high-pressure conditions that are similar to those of liquid rocket combustors. A calibration test was performed to prove the reliability of the manufactured gauge. Then, a combustion experiment was conducted, in which the gauge was used to measure unsteady heat flux in a liquid rocket combustor that used kerosene and liquid oxygen as propellants. Reasonable heat flux values were obtained using the gauge. Therefore, the proposed measurement method is considered to offer significant improvement over the existing integral method.

HCCI 엔진에서 엔진성능 및 배출에 미치는 EGR의 영향 (A Study on the Effects of EGR on Engine Performance and Emissions of a HCCI(Homogeneous Charge Compression Ignition) Engine)

  • 한성빈;장용훈
    • 대한기계학회논문집B
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    • 제27권11호
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    • pp.1630-1636
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    • 2003
  • Automobile companies and research institutions in leading automobile-manufacturing nations have recently been very active with research regarding the HCCI engine for use in future vehicles. Because HCCI engines take advantage of high compression ratio and heat release rate, they exhibit high efficiency found in compression ignition engines. HCCI engines also utilize a lean air/fuel ratio resulting in low emissions of NO$_{x}$ and PM (particulate matter). The objective of this research is to determine the effects of EGR rate on the combustion processes of HCCI. for this purpose, a 4-cylinder, compression ignition engine was converted into a HCCI engine, and a heating device was installed to raise the temperature of the intake air and also to make it more consistent. In addition, a pressure sensor was inserted into each of the cylinders to investigate the differences in characteristics among the cylinders. The experimental study of the effects of EGR rate on various gas emissions, engine performance, etc. should prove to be a valuable source of information for the development of the HCCI engine.e.

초고온 동압을 받는 제트 베인의 구조 안전성 평가에 대한 연구 (A study on structural safety evaluation of jet vane under very high temperature and dynamic pressure)

  • 박성한;이상연;박종규;김원훈;문순일
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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    • pp.99-105
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    • 2005
  • 초고온($2700^{\circ}C$) 연소가스에 직접 노출된 상태에서 가스유동에 의한 동압을 받는 추력편향장치용 제트 베인의 열구조 안전성을 평가하기 위하여 내열합금의 초고온 인장시험 및 3차원 비선형 수치해석을 수행하였다. 고온 구조거동을 분석하여 제트 베인의 구조안전성을 평가하였으며 구조해석결과를 지상연소시험결과와 비교하였다. 구조 및 열 하중의 대부분은 제트 베인 축에 집중되었으며, 축은 $1400^{\circ}C$ 이하에서 구조적으로 안전한 것으로 밝혀졌다. 지상연소시험결과와 구조해석결과의 비교를 통하여 베인 하중과 축의 변위를 기준으로 구조안전계수를 평가하는 것이 등가응력에 의한 평가 기준보다 더 유용한 기준으로 판단되었다.

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