• 제목/요약/키워드: Fuel Quantity

검색결과 300건 처리시간 0.021초

승용차 연료탱크의 유량변화에 따른 진동 소음 특성 (Characteristics of Vibration and Noise due to Various Fuel Quantity in Vehicle Fuel Tank)

  • 안성덕;김찬묵;강태원;사종성;권요섭;임동민
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2007년도 추계학술대회논문집
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    • pp.626-629
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    • 2007
  • Vibration originated from the fuel pump is transmitted to the fuel pump module and fuel tank. Fuel tank transmits it to chassis of vehicle. Also, noise perturbed through fuel and fuel tank is radiated out. Dynamic characteristics of fuel tank are composed of tank structure and containing fuel quantity. Therefore, this study is focused at fuel tank with various quantity. As a result, characteristics of vibration for various fuel quantity in a tank are identified as the more mass of fuel is, the less the 1st resonance frequency decrease. Also, between acoustic camera and mode shape of modal analysis are used for searching the positions of radiated noise and are found to be in accordance with each other.

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정전용량형 연료센서를 이용한 항공기 연료량측정시스템 구현 (Implementation of Fuel Quantity Measurement System for Aircraft Using Capacitive Fuel Sensor)

  • 양준모;양성욱;이상철;이용식
    • 항공우주시스템공학회지
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    • 제12권6호
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    • pp.17-22
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    • 2018
  • 항공기 항속시간에 영향을 미치는 요소인 연료량은 정확한 측정이 필요하다. 본 논문에서는 정전용량형 연료센서, DAQ 보드, Labview 소프트웨어로 구현된 연료량측정시스템을 다루었다. 연료량에 따라 변화하는 파라미터를 확인하기 위해 Pspice를 이용하여 구현된 시스템의 주회로가 시뮬레이션 되었다. 시뮬레이션을 통해 연료량에 따라 변화하는 파라미터인 Vrms를 찾아내었다. 연료 센서의 출력인 Vrms는 구현된 연료량측정시스템의 DAQ 보드를 통해 Labview 소프트웨어로 전송되고, 이 소프트웨어를 사용하여 연료량이 계산된다. 그 결과, 필터가 적용되지 않은 연료량측정시스템보다 정확도가 향상되었다.

최신 전투기 사례를 통한 T-50 FFP 시스템 최적 설계 연구 (A Study on Optimal design of T-50 Aircraft FFP system through a case of F-16 Aircraft)

  • 남용석;김태환;정년수
    • 항공우주시스템공학회지
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    • 제4권1호
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    • pp.10-14
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    • 2010
  • The Fuel system of T-50 Advanced Trainer is equipped with two boost pump and fuel flow proportioner for feeding fuel to turbo jet engine. when an unexpected failure occurs, they can feed the fuel to turbo jet engine which fuel quantity required. fuel quantity control method is applied for minimizing the center of gravity change. and fuel quantity control method is controlled by FQMS(Fuel Quantity Measuring System) and FFP(Fuel Flow Proportioner). This paper presents life cycle extension plans of FFP hydraulic motor by design improvements of connecting and arrangement of pipe comparing with KF-16.

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A Study of Unit Commitment Considering Environmental Effects by Fuel Substitution

  • Lee, Buhm;Kim, Yong-Ha;Park, Nam-Sup
    • Journal of information and communication convergence engineering
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    • 제1권2호
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    • pp.93-97
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    • 2003
  • This paper proposes a new generation scheduling algorithm which can consider total quantity of contamination and energy limits based on Lagrangian Relaxation. First, we formulate a Lagrangian function which consider quantity of contamination including substitution of fuel, and quantity of fuel. Second, we developed Multi-state S.U.D.P. which can treat multiple fuels. Third, we propose an effective generation scheduling algorithm including Multi-state S.U.D.P.. As a results, unit commitment and generating power can be obtained to meet the environmental and fuel constraints with fuel substitution. By applying it to the test system, effectiveness of the method is verified.

바이오디젤-CNG 혼소엔진에서 파일럿 분사량이 연소 및 배기 특성에 미치는 영향 (Effects of Pilot Injection Quantity on the Combustion and Emissions Characteristics in a Diesel Engine using Biodiesel-CNG Dual Fuel)

  • 유경현
    • 한국분무공학회지
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    • 제21권2호
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    • pp.95-103
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    • 2016
  • The effect of pilot injection quantity on the combustion and emissions characteristics of a compression ignition engine with a biodiesel-compressed natural gas (CNG) dual fuel combustion (DFC) system is studied in this work. Biodiesel is used as a pilot injection fuel to ignite the main fuel, CNG of DFC. The pilot injection quantity is controlled to investigate the characteristics of combustion and exhaust emissions in a single cylinder diesel engine. The injection pressure and injection timing of pilot fuel are maintained at approximately 120 MPa and BTDC 17 crank angle, respectively. Results show that the indicated mean effective pressure (IMEP) of biodiesel-CNG DFC mode is similar to that of diesel-CNG DFC mode at all load conditions. Combustion stability of biodiesel-CNG DFC mode decreased with increase of engine load, but no notable trend of cycle-to-cycle variations with increase of pilot injection quantity is discovered. The combustion of biodiesel-CNG begins at a retarded crank angle compared to that of diesel-CNG at low load, but it is advanced at high loads. Smoke and NOx of biodiesel-CNG are simultaneously increased with the increase of pilot fuel quantity. Compared to the diesel-CNG DFC, however, smoke and NOx emissions are slightly reduced over all operating conditions. Biodiesel-CNG DFC yields higher $CO_2$ emissions compared to diesel-CNG DFC over all engine conditions. CO and HC emissions for biodiesel-CNG DFC is decreased with the increase of pilot injection quantity.

승용디젤엔진의 과도구간 입자상물질 저감 및 운전성능 향상을 위한 연료분사량 및 커먼레일압력 제어전략 (A Control Strategy of Fuel Injection Quantity and Common-rail Pressure to Reduce Particulate Matter Emissions in a Transient State of Diesel Engines)

  • 홍승우;정동혁;선우명호
    • 한국자동차공학회논문집
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    • 제23권6호
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    • pp.623-632
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    • 2015
  • This study proposes a control strategy of the common rail pressure with a fuel injection limitation algorithm to reduce particulate matter (PM) emissions under transient states. The proposed control strategy consists of two parts: injection quantity limitation and rail pressure adaptation. The injection limitation algorithm determines the maximum allowable fuel injection quantity to avoid rich combustion under transient states. The fuel injection quantity is limited by predicting the burned gas rate after combustion; however, the reduced injection quantity leads to deterioration of engine torque. The common rail pressure adaptation strategy is designed to compensate for the reduced engine torque. An increase of the rail pressure under transient states contributes to enhancement of the engine torque as well as reduction of PM emissions by promoting atomization of the injected fuel. The proposed control strategy is validated through engine experiments. The rail pressure adaptation reduced the PM emission by 5-10% and enhanced the engine torque up to 2.5%.

항공기 보조연료탱크 연료량측정시스템 개발 (Development of Fuel Quantity Measurement System for Aircraft Supplementary Fuel Tank)

  • 양준모;김봉균;한성현;이상철
    • 한국항공우주학회지
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    • 제48권11호
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    • pp.927-933
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    • 2020
  • 본 논문에서는 항공기 자세 변화를 고려한 항공기 보조연료탱크 연료량측정시스템을 제시하였다. 개발된 연료량측정시스템은 연료센서, 데이터 처리장치, 계기 및 센서 데이터로부터 연료량을 추정하는 소프트웨어로 구성되었다. 지상에서의 롤 및 피치 자세 변화를 모사하기 위해 모사시험 장치가 개발되었다. 모사시험장치를 이용하여 다양한 연료량, 롤 및 피치 각도의 센서 데이터를 자동으로 측정하여 트레이닝 데이터 세트를 획득하였다. 연료량을 추정하는 연료량 측정 소프트웨어를 트레이닝 데이터 세트와 함께 삼선형보간법을 사용하여 개발하였다. 개발된 연료량측정시스템은 참값을 알고 있는 테스트 데이터 세트의 연료 추정 오차를 측정하여 검증하였다. 테스트를 통해 개발된 연료량측정시스템의 오차가 TSO-C55 문서의 기준을 충족하는 것을 확인하였다.

디젤 및 DME 연료의 거시적 분무특성 비교 (Comparisons of Diesel and DME Fuel in Macroscopic Spray Characteristics)

  • 박준규;전문수;박성욱
    • 한국분무공학회지
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    • 제17권4호
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    • pp.205-209
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    • 2012
  • This study focused on comparing macroscopic characteristics of DME and diesel fuel experimentally. DME fuel is one of the most promising alternative fuels because of its superiority in atomization characteristic and clearness in terms of exhaust gas compared with existing fossil fuels. In addition, DME fuel has high cetane number so it could be applied to compression ignition engine. However because DME fuel exists in gas phase at room temperature and atmospheric pressure, and it corrodes rubber parts of fuel line, DME fuel is hard to apply to commercial vehicles. To establish knowledge about DME fuel and furthermore, to develop commercial DME vehicles such as passenger cars, many research have been proceeded steadily. The present study, by comparing spray characteristics of DME fuel to those of diesel fuel, improved atomization characteristics in DME were revealed. Injection quantity measurement and spray visualization experiment were progressed and it was revealed that DME fuel shows small injection quantity than that of diesel fuel and axial development of spray in terms of spray tip penetration decreases when DME fuel was injected.

인젝터 구동 전류 패턴 변화가 솔레노이드 타입 커먼레일 인젝터 분사율 특성에 미치는 영향에 대한 컴퓨터시뮬레이션 (A Computer Simulation of Injection Rate Characteristics of Solenoid Type Common Rail Injector According to Injector Driving Current Patterns)

  • 이충훈
    • 한국분무공학회지
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    • 제24권3호
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    • pp.114-121
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    • 2019
  • The effect of injector driving current pattern on fuel injection rate of solenoid diesel common rail injector was studied by computer simulation. The time resolved fuel injection rate and injected quantity per stroke of a common rail injector driven with the five current patterns were computer simulated. The fuel injection rate and injected quantity per stroke according to the rail pressure and fuel injection period were also computer simulated. When the common rail injector was driven with the five driving current patterns of peak & hold, there was no difference in the fuel injection rate in the peak section regardless of all the current patterns of the five cases. On the other hand, the magnitude of the hold current value influenced the injection rate and injected quantity per stroke. That is, in the current pattern of three cases where the hold current value is equal to or more than a constant value of the peak current value, the fuel injection rates for the given common rail rail pressure and injection period are same one another. On the other hand, the current pattern of the two cases, in which the hold current value is smaller than a certain value, there is a large fluctuation in the fuel injection rate.

디젤 연료 온도에 따른 분무 발달 특성 (Characteristics of the Spray Development with Diesel Fuel Temperatures)

  • 이진우
    • 한국산학기술학회논문지
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    • 제17권3호
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    • pp.270-275
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    • 2016
  • 본 연구에서는 디젤 연료 온도에 따른 실제 분사되는 연료량, 분사율 그리고 거시적 분무 발달 과정에 대한 특성을 파악하고자 하였다. 시험 결과 동일한 분사 시작 신호 및 분사 기간 신호를 입력하였음에도 불구하고, 연료 온도가 낮아짐에 따라 실제 연료 분사량이 감소하는 경향을 보였다. 분사율 측정 결과를 통해 연료 온도가 낮은 조건에서 실제 분사 시작 시점이 지연되며, 실제 분사가 유지되는 기간이 짧아지는 것을 확인하였으며, 이를 통해 실제 분사되는 연료량 저감에 대한 근거를 찾을 수 있었다. 거시적 분무 이미지 촬영 결과를 연료 온도 별 분무 도달 거리로 표현하여 비교 하였으며, 낮은 연료 온도 조건에서 분무 미립화 성능 악화로 인해 분무 도달 거리가 길어지는 것을 확인하였다. 저온 조건에서의 연소 개선을 위해 향후 시도할 선행 평가로서 피스톤 타켓팅 평가를 수행하였으며, 이른 시기에 분사되는 파일럿 연료가 크레비스 영역으로 유입되는 것을 확인하였으며, 이를 통해 파일럿 분사 방식 적용 시 연료량 분배 및 분사 시기 선정이 매우 중요한 인자가 됨을 파악하였다.