• Title/Summary/Keyword: Engine speed

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The Effects of Intake Pulsating Flow on Volumetric Efficiency in a Diesel Engine (디젤기관의 흡기 맥동류가 체적효율에 미치는 영향)

  • Kang, H.Y.;Koh, D.K.;Ahn, S.K.
    • Journal of Power System Engineering
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    • v.9 no.2
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    • pp.19-25
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    • 2005
  • Empirical experiments have been undertaken to investigate the effects of Intake Pulsating Flow on volumetric efficiency in a diesel engine. Waves occurs in the manifolds of engine owing to the periodic nature of the induction and exhaust processes caused by piston motion. During induction process, as waves travel both directions, they are reflected and interacted each other and pressure waves are transmitted through it. Hence, the flow become more complex and unsteady flow. These pressure waves act upon intake pulsating flow and affects on volumetric efficiency. In this paper the effects of change in length of induction pipes and wide range of engine speed on volumetric efficiency was examined and evaluated. It was found that volumetric efficiency was affected by intake pulsating flow with engine speed and the pipe length. The results obtained were considered by adopting a theory of wave action.

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A Numerical Study on Combustion Characteristics of Single Cylinder Engine Fueled with DME (DME를 사용한 단기통 엔진의 연소특성에 관한 수치해석적 연구)

  • Kim, Hyun-Chul;Kang, Woo;Na, Byung-Chul;Kim, Myung-Hwan
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.4
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    • pp.39-48
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    • 2006
  • In this research, in order to study the spray, combustion, and emission characteristics of the common rail DME engine, the target engine was disassembled, and 3D CAD file was constructed using a 3D measurement machine and a rapid prototyping machine. Using the obtained 3D geometry, fine moving meshes are generated, and three dimensional non-steady turbulence flow field and combustion phenomenon including spray were numerically analyzed. As a result, IMEP of DME and diesel in medium and high speed revolution showed similar performance. As the DME fuel start to burn in spray area, the vaporized fuel rapidly spreads squish area in low speed revolution. In the case of DME engine, CO and NOx are relatively consistent with experiment results. It was found that the break-up, evaporation, collision model of DME fuel need to be properly adjusted through matching the characteristics of fuel and injector for further improvement.

The Study on the Control Performance of a Screw Type Super-charger for Automotive Use (자동차용 스크류형 과급기의 제어성능에 관한 연구)

  • 배재일;배신철
    • Transactions of the Korean Society of Automotive Engineers
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    • v.11 no.6
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    • pp.21-29
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    • 2003
  • Boosting of engine power by using Turbo- or Super-charger is a solution to comply with $CO_2$-regulation in Europe. Turbo-charger is now playing a major role in the field of charging system thank to its technical advantages such as no demand of operation power from engine. A mechanically driven Super-charger, however, is now popular due to quick speed response to change of the driving mode-high engine torque even at low engine speed. Since Super-charger needs operation power from engine, it is difficult to improve its relatively higher fuel consumption than that of Turbo-charger. This negative point is still an obstacle to the wide use of Super-charger. This study aims to develop power control concept to achieve the minimization of operation power when it is not necessary to charge at idling or part load driving condition. A screw type Super-charger was modified in design partially and adapted an internal bypass valve and a bypass tube to control charging pressure at part load. The various control concepts show a possibility to reduce operation power of Super-charger and result in improvement of fuel consumption.

An Experimental Study on Correlation of Compression Ignition Condition at Cold Start with Hydrogen HCCI Engine (냉시동시 압축착화 조건의 상관관계에 관한 수소 HCCI 기관의 실험적 연구)

  • Lee, Kwangju;Lee, Jonggoo;Ahn, Byunghoh;Lee, Jongtai
    • Transactions of the Korean hydrogen and new energy society
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    • v.23 no.6
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    • pp.628-633
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    • 2012
  • It was found that the pure hydrogen-air pre-mixture was self-ignited at a high compression ratio without any assisting method in room temperature, thus refuting the preconception that compression ignition of hydrogen engine was impossible. Therefore, in order to analyze the correlation of compression ignition condition at cold start with hydrogen HCCI engine clearly, the possibility of compression igniting compression ratio is investigated with the change of equivalence ratio and engine speed, experimentally. As the results, it is confirmed that the possibility of compression-igniting compression ratio at cold start was decreased by increasing equivalence ratio due to decreasing auto-ignition temperature. In addition, it is grasped that the possibility of compression-igniting compression ratio at cold start is decreased around 14.9% by increasing engine speed at same supply energy.

Vibration characteristics and reduction of Diesel Power Plant(DPP) (육상용 중속 디젤엔진 발전기세트의 진동 특성 및 저감)

  • Kim, Won-Hyun;Jung, Kun-Hwa;Lee, Soo-Mok;Ryoo, Young-Seok
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2006.06a
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    • pp.39-40
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    • 2006
  • Diesel power plant(DPP) with the medium speed diesel engine is operated under the very severe condition in aspect of load and operating time as compared with the marine diesel generator set. So, minimized vibration level have to be insured for the more stable operation of engine and generator. The vibration of generator set mainly comes from the resonance between the rigid modes by resilient mount or distortion modes by structural stiffness and the excitation forces of engine. Then, avoidance of resonance with structural modification is generally well known. In this paper, the first order vibration in non-resonance range and local vibration modes were investigated by impact test, response/ODS(operational deflection shape) measurement and 3D finite element analysis for the additional reduction of vibration. The proposed countermeasures were actually applied and their final effects were verified through the in-situ measurement.

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The Experimental Study on Exhaust Emission Characteristics with Oxygen Component Addition in Diesel Engine (디젤기관에서 산소성분 첨가에 의한 배기가스 배출특성의 실험적 연구)

  • Oh, Y.T.;Choi, S.H.;Jang, S.J.
    • Proceedings of the KSME Conference
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    • 2001.11b
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    • pp.800-805
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    • 2001
  • Recently, our world is faced with very serious and hard problems related to the air pollution due to the exhaust emissions of the diesel engine. So, lots of researchers have studied to reduce the exhaust emissions which influenced the environment strong. In this paper, the effect of oxygen component in fuel on the exhaust emissions has been investigated for diesel engine. And, we tried to analysis the quantities of the low and high hydrocarbon among the exhaust emissions in diesel engine. It have been investigated by the quantitative analysis of the hydrocarbon $C_1\simC_6$ using the gas chromatography. This study carried out by comparing the chromatogram with diesel fuel and diesel fuel blended DGM(diethylene glycol dimethyl ether) 5%. The results of this study show that the hydrocarbon $C_1\simC_6$ among the exhaust emissions of the mixed fuels are exhausted lower than those of the diesel fuel at the all load and speed. In particular, high boiling point hydrocarbons such as $C_5$ and $C_6$ were reduced remarkably in high speed and load region.

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The Effects of Engine's Misfiring Condition on the Dynamic Behaviour of Resilient Mounting Systems (엔진의 착화실패가 탄성지지계의 동적거동에 미치는 영향)

  • 장민오;손석훈;김의간;김의간
    • Journal of KSNVE
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    • v.6 no.4
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    • pp.503-511
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    • 1996
  • There is a tendency of using the resilient mounting system to control the structure born noise transimitted from a engine of which weight is comparatively light and of which speed is comparatively high. According to recent reports, the resilient mounting system is applied to control the vibration of a engine running up to 300 - 400 R.P.M.. Furthermore, the resilient system is also used to the ships such as marine exploring ships, fishing boats, and military vessels. It is not desirous to apply the results for the resilient mounting systems of automobile engines to the controls of the vibrations of marine engines. Marine engines are worked under the idle speed in port and are operated up to the maximum contineous revolution at sea(running up condition). And marine engines are usually worked in inevitable conditions such as a misfire and a cut-off cylinder operating condition. Concerning the above running conditions, a resilient mounting system should be designed in the case of marine engines. In this paper, we studied the effect of engine's misfire on the resilient mounting systems. And the influences of design parameters, such as dynamic characteristics and fitting angles of resilient rubber mountings, were also investigated respectively on the single and double resilient mounting systems.

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A Study on Implementation of a Real-Time Control Algorithm for Ship Main Engine Remote Control Systems (선박 주기관 원격제어시스템을 위한 실시간 제어알고리즘 구현에 관한 연구)

  • 김종화
    • Journal of Advanced Marine Engineering and Technology
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    • v.22 no.6
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    • pp.901-907
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    • 1998
  • This paper presents a real-time control technique for the development of a ship main engine remote control system, In general several tasks are executed by the event-driven method in real-time system. However when some tasks have time delay components it is difficult to achieve good real-time performance. To cope with this problem a number of timers in most conventional system have been used. In this paper we introduce a real-time control methodology of dealing effectively with tasks including time delay components using one hardware timer. And also a speed control method of main engine which includes critical revolution range a crash astern and a emergency ahead function a switching method of remote control position and a flickering method for the indication of multi-stage alarm are discussed. As long as functions and method are imple-mented as forms of tasks the development of main engine remote control systems can be easy for different types of engines.

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RDB-based Automatic Knowledge Acquisition and Forward Inference Mechanism for Self-Evolving Expert Systems

  • Kim, Jin-Sung
    • Journal of the Korean Institute of Intelligent Systems
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    • v.13 no.6
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    • pp.743-748
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    • 2003
  • In this research, we propose a mechanism to develop an inference engine and expert systems based on relational database (RDB) and SQL (structured query language). Generally, former researchers had tried to develop an expert systems based on text-oriented knowledge base and backward/forward (chaining) inference engine. In these researches, however, the speed of inference was remained as a tackling point in the development of agile expert systems. Especially, the forward inference needs more times than backward inference. In addition, the size of knowledge base, complicate knowledge expression method, expansibility of knowledge base, and hierarchies among rules are the critical limitations to develop an expert system. To overcome the limitations in speed of inference and expansibility of knowledge base, we proposed a relational database-oriented knowledge base and forward inference engine. Therefore, our proposed mechanism could manipulate the huge size of knowledge base efficiently. and inference with the large scaled knowledge base in a short time. To this purpose, we designed and developed an SQL-based forward inference engine using relational database. In the implementation process, we also developed a prototype expert system and presented a real-world validation data set collected from medical diagnosis field.

Technical Review and Analysis of Ramjet/Scramjet Technology II. Scramjet and Combined Cycle Engine (램제트/스크램제트의 기술동향과 기술분석 II. 스크램제트 및 복합엔진)

  • Sung Hong-Gye;Yoon Hyun-Gull
    • Journal of the Korean Society of Propulsion Engineers
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    • v.10 no.2
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    • pp.115-128
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    • 2006
  • A technical analysis of current scramjet and combined-cycle engine is presented. Substantial research has been pursued to characterize the operation mechanism of scramjet propulsion, especially in the areas of flame stabilization and system integration, dramatically over the years in support of both military and space access application. Major technology that had significant impact on the maturation of scramjet propulsion technology are dual combustion ramjet, dual mode ramjet, and combined cycle engine to cover a typical wide rage of flight, up to flight Mach number 10. Notable are the fundamental and practical techniques, for instance, scram propulsion itself, thermal relaxation and protection using endothermic fuel and/or CSiC composit materials, and design/manufacture of movable intake and nozzle, to realize high speed propulsion system in near future.