• 제목/요약/키워드: Full engine model

검색결과 87건 처리시간 0.026초

배기매니폴드의 열응력 해석을 위한 배기계 모델 구성에 관한 연구 (A Study on the Exhaust System Model for Thermal Stress Analysis of Exhaust Manifold)

  • 최복록;이경우;장훈
    • 한국자동차공학회논문집
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    • 제18권6호
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    • pp.7-13
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    • 2010
  • In this study, we investigated the efficient FE modelling techniques for thermal stress analysis of the exhaust manifold subject to thermo-mechanical cyclic loadings. At first, full engine model was considered to identify the critical locations and their results were compared to failure site shown by the engine bench test. And the equivalent system model was proposed based on the mechanical behavior of the full engine model. The weak areas of both FE models show a good agreement with the experimental crack location. As a result, a simplified modelling methodology was verified to estimate the thermo-mechanical behaviors of the exhaust manifold under thermal shock test condition.

ENGINE CONTROL USING COMBUSTION MODEL

  • Ohyama, Y.
    • International Journal of Automotive Technology
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    • 제2권2호
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    • pp.53-62
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    • 2001
  • The combination of physical models of an advanced engine control system was proposed to obtain sophisticated combustion control in ultra-lean combustion, including homogeneous compression-ignition and activated radical combustion with a light load and in stoichiometric mixture combustion with a full load. Physical models of intake, combustion and engine thermodynamics were incorporated, in which the effects of residual gas from prior cycles on intake air mass and combustion were taken into consideration. The combined control of compression ignition at a light load and sparit ignition at full load for a high compession ratio engine was investigated using simulations. The control strategies of the variable valve timing and the intake pressure were clarified to keep auto-ignition at a light load and prevent knock at a full load.

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연비향상을 위한 하이브리드 엔진 시스템 모델 개발과 최적화에 관한 연구 (Development and Optimization of the Hybrid Engine System Model to Improve the Fuel Economy)

  • 이동은;황인구;전대일;박심수
    • 한국자동차공학회논문집
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    • 제16권6호
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    • pp.65-73
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    • 2008
  • The purpose of this study is development of universal engine model for integrated Hybrid Electric Vehicle (HEV) simulator and a optimization of engine model. The engine model of this study is based on the MATLAB Simulink for universal and include engine fuel economy technologies for HEV. Various engine fuel economy technologies for HEV is estimated by commercial engine 1-D simulation program - WAVE. And, the 1-D simulation model of base version is compared with engine experiment result. The analyzed engine technologies with 1-D simulation are Dual-CVVT, Atkinson-Cycle and Cylinder-Deactivation System. There are improvement of fuel economy and power performance with Dual-CVVT model at part load and full load, pumping loss reduction with Cylinder-Deactivation System at idle and regeneration. Each estimated technologies are analyzed by 1-D simulation on all operation region for base data to converse simulink. The simulink based engine model maintains a signal with ECU for determination of engine operation point.

승용차의 진동해석모델 개발 (Development of the Vibration Analysis Model of Passenger Car)

  • 권순기
    • 한국소음진동공학회논문집
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    • 제21권4호
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    • pp.291-298
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    • 2011
  • According to the developments of automobile industry, the technology to enhance noise, vibration and harshness(NVH) performance has been studying in a point of view of ride comfort and quietness. Especially the use of computer aided engineering(CAE) simulation tools such as finite element(FE) analysis allows engineers to efficiently evaluate NVH performance. This paper presents the method to bulid FE models for full vehicle including engine, transmission. suspension and steering system, also to evaluate vibration performance of full vehicle. The full vehicle model, which is discussed, is correlated with the result of the frequency response measurement in the case of the car shake performance for high speed driving.

75톤급 로켓엔진용 터보펌프의 실회전수 상사매질 시험 (Model-Fluid Full-Speed Test of a Turbopump for a 75 Ton Class Rocket Engine)

  • 홍순삼;김대진;김진한
    • 항공우주시스템공학회지
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    • 제7권4호
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    • pp.49-54
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    • 2013
  • A turbopump for a 75 ton class liquid rocket engine was tested at full speed for 20 seconds using model fluid. Liquid nitrogen is used for the oxidizer pump, water for the fuel pump, and hot gas for the turbine. The non-cavitating head of pump from the turbopump assembly test showed a good agreement with that from the pump component test. The relative difference of turbine efficiency between the turbopump assembly test and the turbine component test was 0.3% only. Suction performance from the turbopump assembly test was higher than that of pump component test, which resulted from the thermodynamic effect of cavitation.

IDI 디젤기관의 개선된 단일영역 열발생량 계산 (Advanced One-zone Heat Release Analysis for IDI Diesel Engine)

  • 김규보;전충환;장영준;이석영
    • Journal of Advanced Marine Engineering and Technology
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    • 제28권7호
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    • pp.1101-1110
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    • 2004
  • An one-zone heat release analysis was applied to a 4 cylinder indirect injection diesel engine. The objective of the study is to calculate heat release accurately considering the effect of specific heat ratio. heat transfer and crevice model and to find out combustion characteristics of an indirect diesel engine considering the effect of the pressures in main and swirl chambers. Especially specific heat ratio indicating combustion characteristics is adapted. instead of that indicating matter properties, which has been used in former studies Moreover by adaption of blowby model, cylinder gas mass became accurately calculated. Therefore, with ideal gas equation, calculating cylinder gas temperature, it was found to affect heat transfer loss and heat release. Determining heat transfer constants $C_1$. $C_2$ as 0.6 respectively. the integrated gross heat release values were predicted well for the measured value at various engine speed, full load operating conditions. The curve of heat release rate was similar to SI engine rather than DI engine. That is originated from that swirl chamber reduce an instant combustion which occurs in DI engine due to ignition delay on early stage of combustion.

MODELING OF DIRECT INJECTION DIESEL ENGINE EMISSIONS FOR A QUASI-DIMENSIONAL MULTI-ZONE SPRAY MODEL

  • Jung, D.;Assanis, D.N.
    • International Journal of Automotive Technology
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    • 제5권3호
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    • pp.165-172
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    • 2004
  • Phenomenological models for direct injection diesel engine emissions including NO, soot, and HC were implemented into a full engine cycle simulation and validated with experimental data obtained from representative heavy-duty DI diesel engines. The cycle simulation developed earlier by Jung and Assanis (2001) features a quasi-dimensional, multi-zone, spray combustion model to account for transient spray evolution, fuel-air mixing, ignition and combustion. In this study, additional models for HC emissions were newly implemented and the models for NO, soot, and HC emissions were validated against experimental data. It is shown that the models can predict the emissions with reasonable accuracy. However, additional effort may be required to enhance the fidelity of models across a wide range of operating conditions and engine types.

한국형발사체 7톤급 엔진의 개발 시험 현황 (Development Status of the 7-Tonf-class Engine for KSLV-II)

  • 이광진;김성룡;김성혁;김승한;김채형;서대반;우성필;유병일;소윤석;이승재;이정호;임지혁;전준수;조남경;황창환;한영민;김진한
    • 한국추진공학회지
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    • 제22권1호
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    • pp.89-97
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    • 2018
  • 한국형발사체 3단에 사용하기 위한 7톤급 엔진의 개발 시험 결과를 제시하였다. 2기의 engineering model 엔진을 가지고 수행된 연소시험은 시험조건에 따라 지상 시험과 고공 시험으로 구분된다. 엔진의 작동성 검증을 위해 수행된 short duration과 long duration 시험은 성공적으로 완료되었다. 내구성 검증을 위해 수행된 full duration 시험에서는 일부 개선 사항들이 발견되었다. 종합적으로, 엔진 개발에 힘을 더할 수 있는 고무적인 데이터들이 7톤급 엔진 시험으로부터 획득되었다. 이 결과를 바탕으로 새 엔진들이 제작되고, 제작된 엔진은 연소시험을 통해 지속적으로 검증될 예정이다.

액체로켓엔진용 터보펌프의 고온 성능시험 (Hot Test of a Turbopump for a Liquid Rocket Engine)

  • 홍순삼;김대진;김진선;김진한
    • 대한기계학회논문집B
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    • 제33권12호
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    • pp.933-938
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    • 2009
  • Hot test of a full-scale turbopump for a 30-ton-thrust liquid rocket engine was carried out. The turbopump is composed of an oxidizer pump, a fuel pump, and a turbine on a single shaft. Model fluid was used in the test, that is, hot air for the turbine and water for the pumps. The turbopump was operated stably at full speed for 120 seconds. In terms of performance characteristics of pumps and turbine, the results from the turbopump assembly test are compared with those from the turbopump component tests which were performed at about half of the design rotational speed.

선체 마운트 지지점에서의 리셉턴스를 고려한 선박용 디젤 엔진의 고체전달음 해석 (Structure-borne Noise Analysis of Marine Diesel Engine Considering Receptance of Hull Structure at Mounting Point)

  • 장성길;정의봉;홍진숙;배수룡
    • 한국소음진동공학회논문집
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    • 제21권2호
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    • pp.120-128
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    • 2011
  • This paper presents an efficient method to analyze noise and vibration of marine diesel engines mounted on flexible hull structure. The analysis model should in general include the hull structure, leading to lots of computational efforts. To minimize the computational efforts, in this paper, the transfer synthesis utilizing the receptance at the mounting points is proposed. The procedure is then verified by comparing the results with those from the full model calculation. The effects of flexible hull structure on the acoustic power from engine block are finally investigated. It is found that the effect of the hull is significant when the receptance of hull structure is similar to or greater than that of mount or engine block.