• 제목/요약/키워드: Thermodynamic engine model

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동축와류형 분사기의 케로신/액체산소 초임계 혼합특성 수치적 연구 (Numerical Study for Kerosene/LOx Supercritical Mixing Characteristics of Swirl Injector)

  • 허준영;김국진;성홍계;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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    • pp.103-108
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    • 2011
  • 초임계환경에서 작동하는 케로신/액체산소 동축와류형 분사기의 혼합특성을 수치적으로 연구하였다. 케로신 물성치를 계산하기 위하여 써로게이트 모델이 적용되었다. 난류모델은 LES를 기반으로 하였고, 초임계영역의 상태량을 계산하기위해 SRK 상태방정식, 점성계수와 열전도도에 대하여 Chung이 제안한 고압상태 혼합물에 대한 방정식, 확산계수에 대하여 Fuller 이론에 Takahashi가 제안한 고압상태의 특징을 고려한 식을 적용하였다. 연소실 압력변화에 따른 분사기와 연소실에서의 열역학적 물성치와 혼합특성을 관찰하였다. 또한 분사기의 압력섭동 스펙트럼밀도를 분석하였다.

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Quantitative Vapor Phase Exciplex Fluorescence Measurements at High Ambient Temperature and Pressure

  • Kim, Tongwoo;Jaal B. Ghandhi
    • Journal of Mechanical Science and Technology
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    • 제17권1호
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    • pp.157-167
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    • 2003
  • The exciplex fluorescence technique with the TMPD (tetamethyl-Ρ-phenylene-diamine) / naphthalene dopant system was applied in a combustion-type constant-volume spray chamber. A detailed set of calibration experiments has been performed in order to quantify the TMPD fluorescence signal. It has been demonstrated that the TMPD fluorescence intensity was directly proportional to concentration, was independent of the chamber pressure, and was not sensitive to quenching by either water vapor or carbon dioxide. Using a dual heated-jet experiment, the temperature dependence of TMPD fluorescence up to 1000 K was measured. The temperature field in the spray images was determined using a simple mixing model, and an iterative solution method was used to determine the concentration and temperature field including the additional effects of the laser sheet extinction. The integrated fuel vapor concentration compared favorably with the measured amount of injected fuel when all of the liquid fuel had evaporated.

단기통 4사이클 스파아크 점화기관 동력사이클의 시뮬레이션 (Simulation of a power cycle for a single-cylinder 4-stroke cycle spark ignition engine)

  • 조양수;유병철
    • 오토저널
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    • 제5권4호
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    • pp.47-61
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    • 1983
  • In this paper the simulation of a thermodynamic power cycle for a 4-stroke, single-cylinder, spark-ignition engine was studied. In this simulation the cylinder volume was restricted to two zones, a burnt and an unburnt zone, and the convective heat transfer from cylinder contents to surroundings was considered. The chemical species in burnt gas considered was 12 species including H$_{2}$O, H$_{2}$, OH, H, N$_{2}$, NO, N, CO$_{2}$, CO, $O_{2}$, O and Ar. Using this model, computer program for compression, ignition and expansion processes was composed and pressure, temperature and composition of cylinder gas at each crank angle were computed. The composition of CO$_{2}$, CO, $O_{2}$ in the burnt gas when exhaust valve opens, the maximum temperature, the maximum flame speed and the combustion duration were also computed as a function of equivalence ratio. The relation between burnt mass fraction and burnt volume fraction was also computed.

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다기관 4사이클 스파크 점화기관의 가스 교환과정에 관한 예측 (Prediction on gas exchange process of a multi-cylinder 4-stroke cycle spark ignition engine)

  • 이병해;이재철;송준호
    • 오토저널
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    • 제13권2호
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    • pp.67-87
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    • 1991
  • The computer program which predicts the gas exchange process of multi-cylinder 4-Stroke cycle spark-ignition engine, can be great assistance for the design and development of new engine. In this study, the computer program was developed to predict the gas exchange process of multi-cylinder four stroke cycle spark ignition engine including intake and exhaust systems. When gas exchange process is to be calculated, the evaluation of the variation of the thermo-dynamic properties with time and position in the intake and exhaust systems is required. For the purpose, the application of the generalized method of characteristics to the gas exchange process is known as one of the method. The simulation model developed was investigated to the analysis of the branch system of multi-cylinder. The models used were the 2-zone expansion model and single zone model for in cylinder calculation and the generalized method of characteristic including area change, friction, heat transfer and entropy gradients for pipe flow calculation. The empirical constants reduced to least number as possible were determined through the comparison with the experimented indicator diagram of one particular operation condition and these constants were applied to other operating condition. The predicted pressures in cylinder were compared with the experimental results over the wide range of equivalence ratio and ignition timing. The predicted values have shown good agreement with the experimental results. The thermodynamic properties in the intake and exhaust system were predicted over the wide range of equivalence ratio and ignition timing. The obtained results can be summarized as follows. 1. Pressures in the exhaust manifold have a little influence on the equivalence ratio, a great influence on the ignition timing. 2. Pressures in the inlet manifold are nearly unchanged by the equivalence ratio and the ignition timing. 3. In this study, the behaviors of the exhaust temperature, gas in the exhaust manifold were ascertained.

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DC 모터방식 EGR 밸브를 적용한 승용디젤엔진의 앞먹임 공기량 제어에 관한 연구 (Feedforward EGR Control of a Passenger Car Diesel Engine Equipped with a DC Motor Type EGR Valve)

  • 오병걸;이민광;박영섭;이강윤;선우명호;남기훈;조성환
    • 한국자동차공학회논문집
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    • 제19권5호
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    • pp.14-21
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    • 2011
  • In diesel engines, accurate EGR control is important due to its effect on nitrogen oxide and particulate matter emissions. Conventional EGR control system comprises a PI feedback controller for tracking target air mass flow and a feedforward controller for fast response. Physically, the EGR flow is affected by EGR valve lift and thermodynamic properties of the EGR path, such as pressures and temperatures. However, the conventional feedforward control output is indirectly derived from engine operating conditions, such as engine rotational speed and fuel injection quantity. Accordingly, the conventional feedforward control action counteracts the feedback controller in certain operating conditions. In order to improve this disadvantage, in this study, we proposed feedforward EGR control algorithm based on a physical model of the EGR system. The proposed EGR control strategy was validated with a 3.0 liter common rail direct injection diesel engine equipped with a DC motor type EGR valve.

고압상태에서의 연료액적의 증발특성 해석 (Analysis of Fuel Droplet Vaporization at High-Pressure Environment)

  • 이재철;김용모
    • 한국분무공학회지
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    • 제1권1호
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    • pp.35-43
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    • 1996
  • A vaporization model for single component fuel droplet has been developed for applying to sub- and supercritical conditions. This model can account for transient liquid heat ins and circulation effect inside the droplet, forced and natural convection, Stefan flow effect, real gas effect and ambient gas solubility into the liquid droplet in high-pressure conditions. Thermodynamic and transport properties are calculated as functions of temperature and pressure in both phases. Numerical calculations are carried out for several validation cases with the detailed experimental data. Numerical results confirm that this supercritical vaporization model is applicable to the high-pressure conditions encountered in the combustion processes of diesel engine.

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이중연소 램제트 엔진의 예비 성능해석 (Preliminary Performance Analysis of a Dual Combustion Ramjet Engine)

  • 변종렬;안중기;윤현걸;임진식
    • 한국추진공학회지
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    • 제15권5호
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    • pp.72-81
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    • 2011
  • 이중연소 램제트 엔진의 작동특성 및 주요 설계인자를 파악하기 위하여 공기역학 및 열역학적 이론을 기반으로 한 기본적인 성능해석 모델을 수립하였다. 이중연소 램제트 엔진의 예비 성능해석을 수행하였고, 그 결과는 흡입구, 가스발생기, 초음속 연소기 사이의 상세한 관계를 설명하고 있다. 본 연구에서 제시된 방법은 가스발생기와 초음속 연소기의 기하학적 형상을 정량적으로 결정하고, 엔진 각 구성품의 성능에 대한 영향을 평가하기 위한 도구를 제공한다. 또한 예비 성능해석을 통해 이중연소 램제트 엔진의 기본 형상 설계 결과를 도출하였다.

이중연소 램제트 엔진의 예비 성능해석 (Preliminary Performance Analysis of a Dual Combustion Ramjet Engine)

  • 변종렬;안중기;윤현걸;임진식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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    • pp.318-325
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    • 2011
  • 이중연소 램제트 엔진의 작동특성 및 주요 설계인자를 파악하기 위하여 공기역학 및 열역학적 이론을 기반으로 한 기본적인 성능해석 모델을 수립하였다. 이중연소 램제트 엔진의 예비 성능해석을 수행하였고, 그 결과는 흡입구, 가스발생기, 초음속 연소기 사이의 상세한 관계를 설명하고 있다. 본 연구에서 제시된 방법은 가스발생기와 초음속 연소기의 기하학적 형상을 정량적으로 결정하고, 엔진 각 구성품의 성능에 대한 영향을 평가하기 위한 도구를 제공한다. 또한 예비 성능해석을 통해 이중 연소 램제트 엔진의 기본 형상 설계 결과를 도출하였다.

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초임계 상태에서의 LOx 스월 인젝터에 대한 동적 수치 모델링 (Dynamic Numerical Modeling for LOx Swirl Injector at Supercritical Conditions)

  • 김국진;허준영;김종찬;성홍계
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 제33회 추계학술대회논문집
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    • pp.42-46
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    • 2009
  • 고압 조건에서 작동하는 고성능 액체 로켓 엔진에 대한 이해를 위해 초임계 조건의 스월 인젝터에서 액체 산소의 동적 특성이 수치적으로 연구되었다. 난류 수치 모델은 large eddy simulation을 기반으로 하였으며 보존 방정식과 SRK 상태 방정식, Chung의 기법을 포함하고 있다. 또한 수렴 속도의 증가를 위해 예조건화 기법이 적용되었다. 수치 해석 결과는 이상 기체 상태 방정식을 적용한 결과와 비교 되었으며 인젝터 내부와 연소실에서 액상이 존재하는 영역에서의 상태량과 동적 특성의 차이가 관찰되었다.

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DEVELOPMENT OF A SIMPLIFIED MODEL FOR ANALYZING THE PERFORMANCE OF KALIMER-600 COUPLED WITH A SUPERCRITICAL CARBON DIOXIDE BRAYTON ENERGY CONVERSION CYCLE

  • Seong, Seung-Hwan;Lee, Tae-Ho;Kim, Seong-O
    • Nuclear Engineering and Technology
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    • 제41권6호
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    • pp.785-796
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    • 2009
  • A KALIMER-600 concept which is a type of sodium-cooled fast reactor, has been developed at KAERI. It uses sodium as a primary coolant and is a pool-type reactor to enhance safety. Also, a supercritical carbon dioxide ($CO_2$) Brayton cycle is considered as an alternative to an energy conversion system to eliminate the sodium water reaction and to improve efficiency. In this study, a simplified model for analyzing the thermodynamic performance of the KALIMER-600 coupled with a supercritical $CO_2$ Brayton cycle was developed. To develop the analysis model, a commercial modular modeling system (MMS) was adopted as a base engine, which was developed by nHance Technology in USA. It has a convenient graphical user interface and many component modules to model the plant. A new user library for thermodynamic properties of sodium and supercritical $CO_2$ was developed and attached to the MMS. In addition, some component modules in the MMS were modified to be appropriate for analysis of the KALIMER-600 coupled with the supercritical $CO_2$ cycle. Then, a simplified performance analysis code was developed by modeling the KALIMER-600 plant with the modified MMS. After evaluating the developed code with each component data and a steady state of the plant, a simple power reduction and recovery event was evaluated. The results showed an achievable capability for a performance analysis code. The developed code will be used to develop the operational strategy and some control logics for the operation of the KALIMER-600 with a supercritical $CO_2$ Brayton cycle after further studies of analyzing various operational events.