• 제목/요약/키워드: High Pressure Combustion Performance

검색결과 209건 처리시간 0.023초

30톤급 액체로켓엔진 재생냉각 연소기 저압 연소시험 결과 (Low Pressure Test Results of Regenerative Cooling Combustion Chamber for 30tonf-Class Liquid Rocket Engine)

  • 한영민;김종규;이광진;임병직;안규복;김문기;서성현;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 춘계학술대회 논문집
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    • pp.71-75
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    • 2009
  • 30톤급 액체로켓엔진 재생냉각 연소기에서 넓은 영역에서의 연소기 작동성 및 연소성능 등을 확인하기 위한 저압 및 설계/탈설계점 연소시험 결과에 대해 기술하였다. 연소기의 연소압력은 60 bar, 추진제 유량은 약 89 kg/s 그리고 노즐 팽창비는 12이다. 연소특성속도에 대한 압력의 영향은 혼합비에 따라 크게 나타났다. 연소기의 비추력은 혼합비에 크게 영향을 받지 않았고 압력에 비례함을 알 수 있었다. 본 결과는 향후 대형 연소기에서 저압 연소시험의 가능성을 제시할 뿐만 아니라 대형 연소기의 고압 연소압력에서의 연소성능을 예측하는 기본 데이터로 활용될 수 있을 것이다.

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직접분사식 디젤기관의 연소실내 공기유동강화가 연소과정에 미치는 영향 (The Effect of Combustion Process by Intensifying the Air Flow in Combustion Chamber of D.I. Diesel Engine)

  • 방중철
    • 한국자동차공학회논문집
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    • 제15권5호
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    • pp.153-159
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    • 2007
  • The performance of a direct-injection type diesel engine often depends on the strength of air flow in the cylinder, shape of combustion chamber, the number of nozzle holes, etc. This is of course because the process of combustion in the cylinder was affected by the mixture formation process. In the present paper, high speed photography was employed to investigate the effectiveness of holes penetrated from the bottom of cavity wall to piston crown for some more useful utilization of air. The holes would function to improve mixing of fuel and air by the increase of air flow in the cylinder. The results obtained are summarized as follows, (1) Activated first of the combustion by shorten of ignition timing and rapid flame propagation (2) Raised the combustion peak pressure, more close to TDC the formation timing of peak pressure.

정적연소실내의 디젤분무증발과 연소특성에 관한 연구 (A Study on the Diesel Spray Evaporation and Combustion Characteristics in Constant Volume Chamber)

  • 김상호;김석준;이만복;김응서
    • 한국자동차공학회논문집
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    • 제2권6호
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    • pp.102-109
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    • 1994
  • As a fundamental study to apply high pressure injection system to direct injection diesel engine, fuel injection system and constant volume combustion chamber were made and the behaviors of evaporating spray with the variation of injection pressure and the ambient gas temperature were observed by using high speed camera, and the combusion characteristics with the variation of injection pressure and A/F ratio were analyzed. As injection pressure increases, spray tip penetration and spray angle increase and, as a results spray volume increases. This helps an uniform mixing of fuel and air. Spray liquid core length decreases as ambient gas temperature increases, while it decreases as injection pressure increases but the effect of ambient gas temperature is dorminant. As injection pressure increases, ignition delay is shortened and combustion rate being raised, maximum heat release rate increases. It become clear that High injection pressure has high level of potential to improve the performance of DI-diesel engine.

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액체로켓엔진 연소기용 단일 분사기 연소기와 축소형 연수고 수류/연소시험 결과 비교 (Comparison of Combustion Performance between Single Injector Combustor and Sub-scale Combustor)

  • 김승한;한영민;서성현;문일윤;이광진
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.451-454
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    • 2006
  • This paper describes the results of cold flow test and hot firing tests of an uni-element coaxial swirl injector and hot firing tests of a subscale combustor, as to the development effort of coaxial swirl injector for high performance liquid rocket engine combustor. A major design parameter for coaxial swirl injector is the recess number of a bi-swirl injector. The results of hot firing tests of the uni-element injector combustor and the sub-scale combustor are analyzed to investigate the effect of the recess number influencing on the combustion performance and pressure fluctuation. The test results of a cold flow test of the unielement combustor shows that it was shown that the change in recess number has significant effect on mixing characteristics and efficiency, while the effect of recess number on atomization characteristic is not The results of a series of firing tests using unielement and subscale combustor show that the recess length significantly affects the hydraulic characteristics, the combustion efficiency, and the dynamics of the liquid oxygen/kerosene bi-swirl injector. As a point of combustion performance, combustion efficiencies are 90% for unielement combustor and 95% for subscale combustor. The difference in the characteristic velocities between the unielement combustor and the subscale combustor may be caused by the difference in thermal loss to the combustor wall and the relative lengths of the combustion chamber. For a mixed type coaxial swirl combustor, the pressure drop across the injector increases as recess number becomes larger. The low frequency pressure fluctuation observed in unielement combustor can be related to the propellant mixing characteristics of the coaxial bi-swirl injector. The effect of the recess number on the pressure fluctuation inside the combustion chamber is more significant in un i-element combustor than the subscale combustor, of which the phenomena are also observed in time domain and frequency domain.

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비정상연소의 특성과 연소진동 평가 (Evaluation on Characteristics of Unsteady Combustion and Combustion Oscillation)

  • 양영준
    • 한국기계가공학회지
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    • 제10권5호
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    • pp.125-130
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    • 2011
  • The characteristics of unsteady combustion were experimentally investigated using confined premixed flames stabilized by a rearward-facing step. The unsteady combustion used in this experiment plays an important role in controlling self-excited combustion oscillations and it has usually desirable performance such as high load combustion and low pollutant emission. It is known that combustion oscillation is occurred if Rayleigh's criterion is satisfied. The pressure fluctuation and OH-emission fluctuation were measured using pressure transducer and OH optical fiber respectively and then cross-corelation and phase difference were calculated to apply Rayleigh's criterion.

연소실 직접분사식 성층급기 가솔린기관 개발에 관한 연구 - 연료분사압력과 부하변동에 따른 연소특성 해석 - (A Study on Stratified Charge GDI Engine Development - Combustion Analysis according to the Variations of Injection Pressure and Load -)

  • 이상만;정영식;채재우
    • 대한기계학회논문집B
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    • 제22권9호
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    • pp.1317-1324
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    • 1998
  • In general, DI gasoline engine has the advantages of higher power output, higher thermal efficiency, higher EGR tolerance and lower emissions due to the operation characteristics of increased volumetric efficiency, compression ratio and ultra-lean combustion scheme. In order to apply the concept of stratified charge into direct injection gasoline engine, some kinds of methodologies have been adapted in various papers. In this study, a reflector was adapted around the injector nozzle to apply the concept of stratified charge combustion which leads the air-fuel mixture to be rich near spark plug. Therefore, the mixture near the spark plug is locally rich to ignite while the lean mixture is wholly introduced into the combustion chamber. The characteristics of combustion is analyzed with the variations of fuel injection pressure and load in a stratified -charge direct injection single cylinder gasoline engine. The obtained results are summarized as follows ; 1. The MBT spark timing approached to TDC with the increase of load on account of the increase of evaporation energy, but has little relation with fuel injection pressure. 2. The stratification effects are apparent with the increase of injection pressure. It is considered by the development of secondary diffusive combustion and the increase of heat release of same region, but proceed rapidly than diesel engine. Especially, in the case of high pressure injection (l70bar) and high load (3.0kgf m), the diffusive combustion parts are developed excessively and results in the decrease of peak pressure than in the case of middle load. 3. The index of engine stability, COVimep value, is drastically decreased with the increase of load. 4. To get better performance of DI gasoline engine development, staged optimizaion must be needed such as injection pressure, reflector, intake swirl, injection timing, chamber shape, ignition system and so on. In this study, the I50bar injection pressure is appeared as the optimum.

고압 축소형 연소기의 연소 성능 시험 (Combustion Performance Tests of High Pressure Subscale Liquid Rocket Combustors)

  • 김종규;이광진;서성현;임병직;안규복;한영민;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.128-134
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    • 2007
  • 본 논문은 고압 축소형 액체로켓엔진 연소기의 연소 성능과 특성에 관한 것이다. 4개의 고압 축소형 연소기 모델에 대하여 연소시험을 수행하였다. 고압 축소형 연소기는 크게 분사기 헤드부, 재생냉각 방식의 연소실부, 그리고 강제 물냉각 노즐부로 구성되어 있고, 1개의 모델은 연소실을 냉각한 연료가 헤드부로 유입되는 재생냉각 방식의 연소기이다. 연소압력은 70 bar이며 재생냉각 방식의 연소기 모델은 연소시험 중 고주파 연소불안정이 발생하여 하드웨어가 손상되었다. 각각의 고압 축소형 연소기의 연소시험 결과, 성능 비교 및 정압, 동압 특성에 대해 기술하였다.

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횡단압력파 발생을 위한 단일 펄스건의 압력파 성능시험 (Performance Test of a Single Pulse Gun for Transverse Pressure Wave Generation)

  • 이종권;송우석;구자예
    • 한국항공우주학회지
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    • 제47권8호
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    • pp.599-606
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    • 2019
  • 펄스건 장치는 연소실 내, 다중 분사기 배열에 따른 연소 유동장으로의 횡단 압력파 전파/감쇠 메커니즘 규명을 목적으로 제작되었다. 제작된 펄스건은 성능시험을 통해 목표 연소압에서의 운용 가능 여부와 압력파 강도 제어 여부를 확인하였다. 기체질소를 사용하여 고압관에 가압을 하였으며 다이아프램에는 $100{\mu}m$ 두께의 OHP 필름을 사용하였다. 압력파의 속도와 강도를 확인하기 위해 압력 트랜스듀서를 이용하여 동압과 정압을 측정하였다. 제작된 펄스건은 공급압력에 따라 압력파의 강도 조절이 가능하며 횡방향성을 가지는 압력파를 생성할 수 있음을 성능시험을 통해 확인하였다.

전자제어식 직접분사 디젤 엔진 연소실내의 분무연소 특성에 관한 연구 (A study on the spray combustion characteristics in a cylinder of a D.I.diesel engine with the electronically controlled injector)

  • 정재우;김성중;이기형;선우명호
    • 한국자동차공학회논문집
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    • 제8권2호
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    • pp.50-56
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    • 2000
  • It is well known that the combustion phenomenon of diesel engine is an unsteady turbulent diffusion combustion. Therefore, the combustion performance of diesel engine is related to a complex phenomenon which involves the various factors of combustion, such as a injection pressure, injection timing, injection rate, and operation conditions of engine. In this study, the spray and the flame development processes in a single cylinder D.I. diesel visualization engine which uses the electronically controlled injection system were visualized to interpret the complicated combustion phenomenon by using high speed CCD camera. In addition, the cylinder pressure and heat release rate were also obtained in order to analyze the diesel combustion characteristics under several engine conditions.

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배열회수형 순산소연소 발전시스템의 성능해석: CO2 포집의 영향 (Performance Analysis of an Oxy-fuel Combustion Power Generation System Based on Waste Heat Recovery: Influence of CO2 Capture)

  • 탁상현;박성구;김동섭;손정락;이영덕
    • 대한기계학회논문집B
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    • 제33권12호
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    • pp.968-976
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    • 2009
  • As the global warming becomes a serious environmental problem, studies of reducing $CO_2$ emission in power generation area are in progress all over the world. One of the carbon capture and storage(CCS) technologies is known as oxy-fuel combustion power generation system. In the oxy-fuel combustion system, the exhaust gas is mainly composed of $CO_2$ and $H_2O$. Thus, high-purity $CO_2$ can be obtained after a proper $H_2O$ removal process. In this paper, an oxy-fuel combustion cycle that recovers the waste heat of a high-temperature fuel cell is analyzed thermodynamically. Variations of characteristics of $CO_2$ and $H_2O$ mixture which is extracted from the condenser and power consumption required to obtain highly-pure $CO_2$ gas were examined according to the variation of the condensing pressure. The influence of the number of compression stages on the power consumption of the $CO_2$ capture process was analyzed, and the overall system performance was also investigated.