• 제목/요약/키워드: Fuel Film Dynamics

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Calculation of Fuel Spray Impingement and Fuel Film Formation in an HSDI Diesel Engine

  • Kyoungdoug Min;Kim, Manshik
    • Journal of Mechanical Science and Technology
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    • 제16권3호
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    • pp.376-385
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    • 2002
  • Spray impingement and fuel film formation models with cavitation have been developed and incorporated into the computational fluid dynamics code, STAR-CD. The spray/wall interaction process was modeled by considering the effects of surface temperature conditions and fuel film formation. The behavior of fuel droplets after impingement was divided into rebound, spread and splash using the Weber number and parameter K(equation omitted). The spray impingement model accounts for mass conservation, energy conservation, and heat transfer to the impinging droplets. The fuel film formation model was developed by integrating the continuity, momentum, and energy equations along the direction of fuel film thickness. Zero dimensional cavitation model was adopted in order to consider the cavitation phenomena and to give reasonable initial conditions for spray injection. Numerical simulations of spray tip penetration, spray impingement patterns, and the mass of film-state fuel matched well with the experimental data. The spray impingement and fuel film formation models have been applied to study spray/wall impingement in high-speed direct injection diesel engines.

직접분사식 디젤엔진에서의 분무충돌과 연료액막형성 해석 (Simulation of Spray Impingement and Fuel Film Formation in a Direct Injection Diesel Engine)

  • 김만식;민경덕;강보선
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.919-924
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    • 2000
  • Spray impingement model and fuel film formation model were developed and incorporated into the computational fluid dynamics code, STAR-CD. The spray/wall interaction process were modelled by considering the change of behaviour with surface temperature condition and fuel film formation. We divided behaviour of fuel droplets after impingement into stick, rebound and splash using Weber number and parameter K. Spray impingement model accounts for mass conservation, energy conservation and heat transfer to the impinging droplets. A fuel film formation model was developed by Integrating the continuity, the Navier-Stokes and the energy equations along the direction of fuel film thickness. The validation of the model was conducted using diesel spray experimental data and gasoline spray impingement experiment. In all cases, the prediction compared reasonably well with experimental results. Spray impingement model and fuel film formation model have been applied to a direct injection diesel engine combustion chamber.

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제어기 설계를 위한 비선형 동적 엔진 모델링 (A Nonlinear Dynamic Engine Modeling for Controller Design)

  • 윤팔주;선우명호
    • 한국자동차공학회논문집
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    • 제7권7호
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    • pp.167-180
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    • 1999
  • A control-oriented nonlinear dynamic engine model is developed to represent a spark ignited engine over a wide range of operating conditions. The model includes intake manifold dynamics,. fuel film dynamics, and engine rotational dynamics with transport delays inherent in the four stroke engine cycles. The model is mathematically compact enough to run in real time, and can be used as an embedded model within a control algorithm or an observer. The model is validated with engine-dynamometer experimental data, and can be used in design and development of a powertrain controller.

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고속직분식 디젤엔진에서의 분무충돌과 연료액막형성 모델링 (Modeling of Spray Impingement and Fuel Film Formation in HSDI Diesel Engines)

  • 김만식;민경덕;강보선
    • 대한기계학회논문집B
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    • 제25권2호
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    • pp.187-194
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    • 2001
  • Spray impingement and fuel film formation models were developed and incorporated into the computational fluid dynamics code. STAR-CD. The spray/wall interaction process was modeled by considering the change of behaviour with surface temperature conditions and the fuel film formation. We divided the behaviour of fuel droplets after impingement into rebound, spread and splash using the Weber number and the parameter K. The Spray impingement model accounts for mass conservation, energy conservation and heat transfer to the impinging droplets. The fuel film formation model was developed by integrating the continuity, Navier-Stokes and energy equations along the direction of fuel film thickness. Validation of the models was conducted using previous diesel spray experimental data and the present experimental results for the gasoline spray impingement. In all the cases, the prediction compared reasonably well with the experimental results. The spray impingement and fuel film formation models have been applied to the spray/wall impingement in high speed direct injection diesel engines.

자동차용 연료펌프의 진동 저감에 대한 연구 (A Study on the Vibration Reduction of an Automobile Fuel Pump)

  • 김병진;원홍인;이성원;박상준;정진태
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2013년도 춘계학술대회 논문집
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    • pp.772-777
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    • 2013
  • This article presents the reduction of vibration generated by an automobile fuel pump. In order to analysis the vibration of the fuel pump, a simplified dynamic model is established, which is composed of a rigid rotor and a equivalent springs. The equivalent stiffnesses of the upper and lower assemblies are evaluated by the comparison of modal testing results and the finite element analysis. the stiffness for the oil film of the journal bearing is extracted by using Reynold's equation. In addition, the time responses for the vibration of the fuel pump are computed by using a commercial multi-body dynamics software, RecurDyn. Based on these results, some design suggestions are proposed to reduce the vibration of an automobile fuel pump.

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자동차용 연료펌프의 진동 저감에 대한 연구 (A Study on the Vibration Reduction of an Automobile Fuel Pump)

  • 김병진;원홍인;이성원;박상준;정진태
    • 한국소음진동공학회논문집
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    • 제23권6호
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    • pp.520-526
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    • 2013
  • This article presents the reduction of vibration generated by an automobile fuel pump. In order to analyze the vibration of the fuel pump, a simplified dynamic model is established, which is composed of a rigid rotor and a equivalent springs. The equivalent stiffnesses of the upper and lower assemblies are evaluated by the comparison of modal testing results and the finite element analysis. The stiffness for the oil film of the journal bearing is extracted by using Reynold's equation. In addition, the time responses for the vibration of the fuel pump are computed by using a commercial multi-body dynamics software, RecurDyn. Based on these results, some design suggestions are proposed to reduce the vibration of an automobile fuel pump.

TRIGGERING AND ENERGETICS OF A SINGLE DROP VAPOR EXPLOSION: THE ROLE OF ENTRAPPED NON-CONDENSABLE GASES

  • Hansson, Roberta Concilio
    • Nuclear Engineering and Technology
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    • 제41권9호
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    • pp.1215-1222
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    • 2009
  • The present work pertains to a research program to study Molten Fuel-Coolant Interactions (MFCI), which may occur in a nuclear power plant during a hypothetical severe accident. Dynamics of the hot liquid (melt) droplet and the volatile liquid (coolant) were investigated in the MISTEE (Micro-Interactions in Steam Explosion Experiments) facility by performing well-controlled, externally triggered, single-droplet experiments, using a high-speed visualization system with synchronized digital cinematography and continuous X-ray radiography. The current study is concerned with the MISTEE-NCG test campaign, in which a considerable amount of non-condensable gases (NCG) are present in the film that enfolds the molten droplet. The SHARP images for the MISTEE-NCG tests were analyzed and special attention was given to the morphology (aspect ratio) and dynamics of the air/ vapor bubble, as well as the melt drop preconditioning. Energetics of the vapor explosion (conversion ratio) were also evaluated. The MISTEE-NCG tests showed two main aspects when compared to the MISTEE test series (without entrapped air). First, analysis showed that the melt preconditioning still strongly depends on the coolant subcooling. Second, in respect to the energetics, the tests consistently showed a reduced conversion ratio compared to that of the MISTEE test series.

Bubbly, Slug, and Annular Two-Phase Flow in Tight-Lattice Subchannels

  • Prasser, Horst-Michael;Bolesch, Christian;Cramer, Kerstin;Ito, Daisuke;Papadopoulos, Petros;Saxena, Abhishek;Zboray, Robert
    • Nuclear Engineering and Technology
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    • 제48권4호
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    • pp.847-858
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    • 2016
  • An overview is given on the work of the Laboratory of Nuclear Energy Systems at ETH, Zurich (ETHZ) and of the Laboratory of Thermal Hydraulics at Paul Scherrer Institute (PSI), Switzerland on tight-lattice bundles. Two-phase flow in subchannels of a tight triangular lattice was studied experimentally and by computational fluid dynamics simulations. Two adiabatic facilities were used: (1) a vertical channel modeling a pair of neighboring sub-channels; and (2) an arrangement of four subchannels with one subchannel in the center. The first geometry was equipped with two electrical film sensors placed on opposing rod surfaces forming the subchannel gap. They recorded 2D liquid film thickness distributions on a domain of $16{\times}64$ measuring points each, with a time resolution of 10 kHz. In the bubbly and slug flow regime, information on the bubble size, shape, and velocity and the residual liquid film thickness underneath the bubbles were obtained. The second channel was investigated using cold neutron tomography, which allowed the measurement of average liquid film profiles showing the effect of spacer grids with vanes. The results were reproduced by large eddy simulation + volume of fluid. In the outlook, a novel nonadiabatic subchannel experiment is introduced that can be driven to steady-state dryout. A refrigerant is heated by a heavy water circuit, which allows the application of cold neutron tomography.

액체추진제 로켓 엔진 연소장치 개발에 있어서의 전산유체역학 응용 (Application of Computational Fluid Dynamics to Development of Combustion Devices for Liquid-Propellant Rocket Engines)

  • 조미옥;김성구;한상훈;최환석
    • 항공우주기술
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    • 제13권2호
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    • pp.150-159
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    • 2014
  • 본 연구에서는 액체산소/케로신 추진 로켓 엔진 연소장치의 국내 개발에 있어서의 전산유체역학 응용 사례를 간략히 소개하였다. 추진제 공급부에 대한 다차원 유동 해석을 통해 유동 균일성을 확인하고 및 압력 손실을 예측할 수 있으며, 개념 설계 단계에서 추진제 매니폴드 형상 설계안을 비교/선택할 수 있다. 다분야 연소/냉각 성능 통합 해석을 통해 로켓 엔진 연소기의 연료 막냉각 및 열차폐 코팅 조건 등 연소/냉각 성능 관련 설계 문제 해결에 필요한 주요 정보를 도출할 수 있다. 향후 분사면 근처에서의 추진제 혼합 및 연소특성을 파악할 수 있는 해석 모델/기법을 개발할 필요가 있다.

해군 함정 격실 유류화재 대응을 위한 수성막포 분사 최적화에 대한 CFD 해석 연구 (CFD Analysis Study on Aqueous Film Foaming Foam Injection Optimization to Respond to Oil Fires in Naval Ship Compartment)

  • 전길송;김휘성;심재웅;유용호;박진욱
    • 공업화학
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    • 제35권3호
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    • pp.239-247
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    • 2024
  • 해군 함정에서 화재가 발생하면 잠재적인 인적, 물적 손실을 완화하기 위해 신속한 진압과 통제가 필수적이다. 해군 함정의 특성상 유류화재 발생 가능성이 크며 이에 유류화재 대응에 탁월한 수성막포(AFFF)를 사용하는 것이 화재 진압에 매우 중요하다. 또한 함정의 격실 내에서 화재가 발생하는 상황 역시 고려해야 한다. 이러한 상황에서 수성막포의 궤적과 적용 범위를 이해하는 것이 중요하므로 격실 환경에 맞는 소화 시스템 설계가 반드시 필요하다. 본 연구에서는 수성막포에 대한 전산유체역학 (CFD) 방법론을 검증하기 위한 해석으로 분사 높이 및 각도에 대한 적용 가능성을 조사하였다. 이러한 내용을 바탕으로 하여 함정 격실에 적용가능한 CFD 해석 결과를 얻었다. 이 결과는 해군 함정 격실 내 유류 화재에 신속하게 대응할 수 있는 소화 시스템 개발의 기반이 될 것이다.