• 제목/요약/키워드: Fuel flow control

검색결과 385건 처리시간 0.027초

가솔린 직분식 인젝터의 분무 및 연소특성에 관한 연구 (A Study on the Spray and Combustion Characteristics of Gasoline Direct Injector)

  • 신민규;박종호;유철호;이내현;최규훈
    • 한국자동차공학회논문집
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    • 제5권5호
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    • pp.114-122
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    • 1997
  • Nowadays, gasoline direct injection engines are being commercialized by virtue of improvement in control technology of spray, flow, air fuel ratio. The stratified charge type has the advantage of improving lean limit. The homogeneous type has the advantage of reducing engine-out hydrocabon emissions in the first 30 seconds after a cold start, in addition, improving transient air fuel ratio control. The vaporization and mixing if injected fuel with air has to e completed in a short time and the fuel film in cylinder and on piston has to be minimized. So, the flow and injection should be well controlled. This paper surveyed the spray characteristics of gasoline direct injection by using laser equipment and the combustion characteristics of the single cylinder engine using homogeneousas-mixture type gasoline direct injection.

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가스터빈 제어 루프에 대한 신경망 튜닝 루프 보상형 2-자유도 PID 제어기의 응용 (Application a Loop Compensation type 2-DOF PID Controller tuned by Neural Network to Gas Turbine Control Loop)

  • 김동화
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 하계학술대회 논문집 B
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    • pp.781-786
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    • 1998
  • Since a gas turbine is still a significant contributor to peak time, it is very important to tune the gains of P. I. D to get a maximum power and stability within permissible limits. In the gas turbine, the main control loop must adjust the fuel flow to ensure the correct output power and frequency. but it is not easy, because the control loop is composed of many subsystems. In this paper we acquire a transfer function based on the operations data of Gun-san gas turbine and study to apply a loop compensation type 2-DOF PID controller tuning by neural-network to control loop of gas turbine to reduce phenomena caused by integral and derivative actions through simulation. We obtained satisfactory results to disturbances of subcontrol loop such as, fuel flow, air flow, turbine extraction temperature.

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비례적분 방식의 피드백 공연비 콘트롤 시스템 해석 (Analysis of PI air-fuel ratio feedback control system)

  • 이대영;박경석;노승탁;김응서;고상근
    • 오토저널
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    • 제13권5호
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    • pp.73-80
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    • 1991
  • Air/fuel ratio control system for gasoline engines has been analyzed to determine the control gain of the system. In this analysis the engine is modelled to be a simple time delaying element and the ramp-and-jump method is used to control air/fuel ratio. The result shows that it is necessary to measure the air flow rate accurately to enhance the control performance. And also it is shown that the control gain must be determined in some bounded region to meet the fast dynamic response and high catalyst conversion efficiency together.

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Numerical investigation of the critical heat flux in a 5 × 5 rod bundle with multi-grid

  • Liu, Wei;Shang, Zemin;Yang, Shihao;Yang, Lixin;Tian, Zihao;Liu, Yu;Chen, Xi;Peng, Qian
    • Nuclear Engineering and Technology
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    • 제54권5호
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    • pp.1914-1928
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    • 2022
  • To improve the heat transfer efficiency of the reactor fuel assembly, it is necessary to accurately calculate the two-phase flow boiling characteristics and the critical heat flux (CHF) in the fuel assembly. In this paper, a Eulerian two-fluid model combined with the extended wall boiling model was used to numerically simulate the 5 × 5 fuel rod bundle with spacer grids (four sets of mixing vane grids and four sets of simple support grids without mixing vanes). We calculated and analyzed 11 experimental conditions under different pressure, inlet temperature, and mass flux. After comparing the CHF and the location of departure from the nucleate boiling obtained by the numerical simulation with the experimental results, we confirmed the reliability of computational fluid dynamic analysis for the prediction of the CHF of the rod bundle and the boiling characteristics of the two-phase flow. Subsequently, we analyzed the influence of the spacer grid and mixing vanes on the void fraction, liquid temperature, and secondary flow distribution. The research in this article provides theoretical support for the design of fuel assemblies.

공기보조형 가솔린 연료분사기의 흡기포트내 연료분무 거동에 관한 연구 (A Study on the Spray Behavior of Air-Assist Type Gasoline Fuel Injector in Intake Port)

  • 노병준;강신재;김원태
    • 대한기계학회논문집B
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    • 제23권1호
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    • pp.92-103
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    • 1999
  • The fuel spray behavior in the intake port of an electronic control port irijection gasoline engine has a strong influence on engine performance, exhaust emission and fuel consumption. Thus, in this study, fuel spray behavior and flow characteristics of the air assist gasoline spray injected into a suction flow in a simulated rectangular intake port have boon investigated. Macro-behavior of spray characteristics was investigated by means of visualization and the measurements of SMD and velocity were made by PDPA. For analysis the flow field with droplets size, droplets are classified five droplets size groups. As a result, the normal distance of suction flow increasing, the relatively large droplets distribution and SMD increase because small droplets easily follow suction flow. Near impinging wail, after impinging against the wall, secondary atomized small droplets of D < $30{\mu}m$ bound from the wall. And the increasement of suction flow progress to the large droplets of D > $100{\mu}m$ distribution. Therefore, SMD are apparently increased near impinging wall, Z/d = 9.0.

한국형발사체 연료 동시충전을 위한 유량제어 방식에 대한 고찰 (Analysis on Flow Control Method for Simultaneous Fuel Filling of the Korea Space Launch Vehicle-II)

  • 여인석;이재준;안재철;강선일
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.5-13
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    • 2017
  • 한국형발사체 발사를 위하여 나로우주센터에 제 2발사대가 구축될 예정이며 연료공급설비 역시 새롭게 설치된다. 한국형발사체 발사대시스템의 연료공급설비는 나로호 발사대의 설계를 기본 바탕으로 하였다. 하지만 한국형발사체는 나로호 또는 시험발사체와는 달리 3단형 발사체이기 때문에 연료 이송펌프 1대로 1, 2, 3단의 발사체 연료 탱크로 연료를 공급해야한다. 유동해석을 통해 충전 시나리오를 선정하는 과정에서 펌프 토출압력의 급격한 상승 문제를 확인하였다. 이는 오리피스타입의 유량제어방식으로 각 단의 충전모드 전환에 따른 유량변화에 대해 리턴유량이 능동적으로 대응할 수 없기 때문에 발생하였다. 이 문제를 해결하기 위해 다양한 경우에 대해 유동해석을 통해 accumulator 설치와 각 단의 충전모드 전환 순서를 적절히 조정함으로써 안정적으로 공급할 수 있음을 확인하였다.

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한국형발사체 연료 동시충전을 위한 유량제어 방식에 대한 고찰 (Analysis on Flow Control Method for Simultaneous Fuel Filling of the Korea Space Launch Vehicle-II)

  • 여인석;이재준;안재철;강선일
    • 한국추진공학회지
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    • 제22권5호
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    • pp.132-140
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    • 2018
  • 한국형발사체 발사를 위하여 나로우주센터에 제 2발사대가 구축될 예정이며 연료공급설비 역시 새롭게 설치된다. 한국형발사체 발사대시스템의 연료공급설비는 나로호 발사대의 설계를 기본 바탕으로 하였다. 하지만 한국형발사체는 나로호 또는 시험발사체와는 달리 3단형 발사체이기 때문에 연료 이송펌프 1대로 1, 2, 3단의 발사체 연료 탱크로 연료를 공급해야한다. 유동해석을 통해 충전 시나리오를 선정하는 과정에서 펌프 토출압력의 급격한 상승 문제를 확인하였다. 이는 오리피스타입의 유량제어방식으로 각 단의 충전모드 전환에 따른 유량변화에 대해 리턴유량이 능동적으로 대응할 수 없기 때문에 발생하였다. 이 문제를 해결하기 위해 다양한 경우에 대해 유동해석을 통해 accumulator 설치와 각 단의 충전모드 전환 순서를 적절히 조정함으로써 안정적으로 공급할 수 있음을 확인하였다.

디젤엔진 연료분사펌프 캐비테이션 손상 방지를 위한 실험적 연구 (Experimental Study for the Prevention of Cavitation Damage in the Diesel Fuel Injection Pumps)

  • 김동훈;박태형;허정윤;류승협;강상립
    • 한국마린엔지니어링학회:학술대회논문집
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    • 한국마린엔지니어링학회 2011년도 후기공동학술대회 논문집
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    • pp.61-61
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    • 2011
  • Cavitation phenomena during the injection process of the conventional fuel injection pump for a medium-speed diesel engine can cause surface damage with material removal or round-off on the plunger and barrel port and may shorten their expected life time. An experiment of flow visualization was carried out to investigate the main cause of these cavitation damages and find the prevention method. Experimental results of flow visualization show that these damages are mainly affected by fountain-like cavitation and jet-type cavitation generated before and after the end of fuel delivery process and therefore the prevention method was designed to control these cavitation flows. From the visualization and endurance test, it was proved that this method can effectively prevent cavitation damages by controlling cavitation flows.

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기체연료엔진의 제어시스템 설계를 위한 엔진 모델링 및 검증 (Engine Modeling and Validation for Control System Design of a Gaseous-fuel Engine)

  • 심한섭;선우명호
    • 한국자동차공학회논문집
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    • 제11권1호
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    • pp.7-17
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    • 2003
  • Highly accurate control of an air-fuel ratio is very important to reduce exhaust gas emissions of gaseous-fuel engines. In order to achieve this purpose, a precise engine model is required to estimate engine performance from the engine design process which is applied to the design of an engine controller. Engine dynamics are considered to develop a dynamic engine model of a gaseous-fuel engine. An effective air mass ratio is proposed to study variations of the engine dynamics according to the water vapor and the gaseous-fuel in the mixture. The dynamic engine model is validated with the LPG engine under steady and transient operating conditions. The experimental results in the LPG gaseous-fuel engine show that the estimation of the air flow and the air-fuel ratio based upon the effective air mass ratio is more accurate than that of a normal engine model.

전자제어 디젤엔진의 연료압력 레귤레이터 고장에 따른 진단 및 성능 연구 (Study on Performance of an Fuel Pressure Regulator under Failure Condition in an Electric Control Diesel Engine)

  • 김태중;조홍현
    • 한국산학기술학회논문지
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    • 제16권3호
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    • pp.1677-1683
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    • 2015
  • 배출가스 규제강화에 대응하기 위해 전자제어 디젤엔진의 적용으로 연료 분사량과 연료 분사시기를 정밀하게 제어하여 연료소비율과 출력 향상 및 소음과 진동이 감소되었다. 전자제어 디젤엔진 시스템의 성능을 유지하기 위해서는 연료압력을 정밀하게 제어하는 중요한 부품이 연료압력 레귤레이터이며 제어불량이 발생할 경우 연료압력이 정밀하게 제어되지 않아 시동불량, 시동지연, 가속불량, 엔진부조 등 이상 현상이 초래된다. 본 실험에서는 연료압력 레귤레이터의 고장에 따른 성능변화를 고찰하기 위하여 연료압력 레귤레이터 제어율에 변화를 주어 연료압력, 회수된 연료유량과 엔진회전수에 미치는 영향을 실험적으로 고찰하였다. 실험결과, 연료압력 레귤레이터의 제어율이 기준에서 4-6% 정도 낮아지면 엔진회전수, 회수되는 연료유량의 변화가 크게 나타났으며 이 때 이상현상이 발생함을 확인하였다. 또한 이를 통하여 연료압력 레귤레이터의 고장 유무을 판단할 수 있다.