• Title/Summary/Keyword: 플레넘챔버

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An Experimental Study on the Flow characteristics in the Plenum Chamber (플레넘 챔버 내의 유동 특성에 관한 실험적 연구)

  • 정재우;이기형;이창식
    • Transactions of the Korean Society of Automotive Engineers
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    • v.7 no.7
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    • pp.24-31
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    • 1999
  • The MPI engine becomes increasingly popular because it meets two requirements of stringent pollutant emission and the lower fuel consumption. Even though supplies the same amount of fuel to each cylinder , it is hard to precisely control the air-duel ration due to the different amount of air flowing into each cylinder. The uniformity of air-fuel ration in each cylinder is considerably affected by the plenum chamber configuration . This study is focused on experimentally analyzing the flow characteristics within the plenum chamber In the present experiment , steady and valve dynamic state flow tests are performed and the flow field inside the plenum chamber is visualized and measured by utilizing a laser sheet visualization technique and a PTV method. These measured results indicate that the flow structure in the plenum chamber is highly influenced by the plenum chamber configurations, suction flow rates, crank speeds and so on.

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An Experimental Study on the Effects of Intake Manifold Shapes on the Torque Characteristics in a 3-Cylinder LPG Engine (흡기다기관 형상변화가 3기통 LPG엔진의 토크 특성에 끼치는 영향에 관한 실험적 연구)

  • 이지근;이한풍;강신재;노병준
    • Transactions of the Korean Society of Automotive Engineers
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    • v.5 no.6
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    • pp.175-182
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    • 1997
  • The purpose of this study is to investigate the effects of intake manifold shapes to improve the engine performance in a 3-cylinder LPG engine with a closed loop fuel supply system. To know the flow resistance of intake manifolds with shape, the intake negative pressure of each runner in intake manifolds were measured by using the digital pressure meter at each driving condition. And, the engine torque and power have been measured with an engine dynamometer while adjusting the optimal fuel consumption ratio with a solenoid driver. As 속 results form this experiment, the torque characteris- tics were more improved with the plenum chamber(B type intake manifold) than with the banana type(A type intake manifold). The torque characteristics were improved at mid-engine speed(rpm) range as the inner diameter of the intake manifold became smaller. And also the optimum volume among the examined plenum chamber volume was 0.74 times(590cc) the displacement of the test engine.

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Development of Automated Program for Noise Prediction in Shipboard Compartments (선내 격실 소음 추정 자동화 프로그램 개발)

  • Oh, Young-Keun;Park, Keun-Hyo;Ryu, Seong-Sun;Kang, Tae-Wook;Lee, Dong-Hyun
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2011.10a
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    • pp.519-524
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    • 2011
  • The aim of this study is to develop an automated program for noise prediction in shipboard compartments, for this purpose of calculating noise levels accurately and quickly. The program calculates sound power level at HVAC components based on the empirical method suggested by NEBB and utilizing the manufacturer's test data. The program developed uses the GUI functions to help in efficient modeling and calculation. To verify the reliability of developed program, the predicted data was compared with the measured data in shipboard compartments. As a result, the average difference between predicted and measured data is ${\pm}3dB$.

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스마트 무인기 흡기구 설계 및 성능해석

  • Jung, Yong-Wun;Jun, Yong-Min;Yang, Soo-Seok
    • Aerospace Engineering and Technology
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    • v.3 no.2
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    • pp.197-207
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    • 2004
  • The developing Smart UAV in KARI supposes high speed flight as like a conventional plane, as well as vertical takeoff and landing as like a helicopter. Therefore, the air intake system should be designed to provide the sufficient air flow to the engine and the maximum possible total pressure recovery at the engine intake screen over a wide range of flight conditions. For this purpose, we designed the intake system using a pitor type intake model and plenum chamber. In this paper, we designed the intake model and analyzed the performance of designed intake system using the general-purpose commercial CFD code, CFD-ACE+. The analysis results of the total pressure variation and the velocity distribution were illustrated in this paper. The pressure recovery and distortion coefficient at a plane coincident with the compressor inlet were calculated and streamline variation through the intake system was investigated at the worst flight condition as well as the standard flight condition.

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