• Title/Summary/Keyword: heat engine

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Performance Simulation of Motorcycle Engine Exhaust Heat Recovery System using Thermoelectric Element (열전소자를 이용한 모터사이클용 엔진 배기 폐열 회수 시스템 성능 해석)

  • Lee, Moo-Yeon;Kim, Kihyun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.19 no.2
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    • pp.695-701
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    • 2018
  • Research into exhaust heat recovery has been actively carried out to improve the thermal efficiency of internal combustion engines. In this study, the performance of thermoelectric generation from exhaust heat recovery for motorcycle engines was analyzed by 1-D thermo-fluid simulation. GT-SUITE, which was developed by Gamma Tech., was used for the simulation of the internal combustion engine and thermoelectric generation system. The basic performance of the engine was analyzed in the range of engine speed of 1000~7000 rpm and engine load of 0~100%. The ratio of exhaust heat energy to fuel chemical energy was found to be about 40~60%. A combined simulation of the engine model and thermoelectric generation model was carried out to analyze the voltage, current and power generated by the thermoelectric material. The generation characteristics of the thermoelectric material was dominantly affected by the exhaust gas temperature. The maximum generated power of the current thermoelectric generation system was found to be about 2.2% of the total exhaust heat energy. The design optimization of the thermoelectric generation system will be carried out to maximize its power generation and economic feasibility.

Integrated Building Energy Supply System : An Overview of Technical Trends for Gas Engine Driven Combined Heat and Power System (가스엔진 구동 건물에너지 통합 공급시스템 개발을 위한 기술동향 사례연구)

  • Park, Beungyong;Jeong, Yongdae;Shin, Hyunchul;Cho, Jinkyun
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.29 no.11
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    • pp.612-620
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    • 2017
  • Power consumption in Southeast Asia is steadily increasing due to industrialization and the effects of hot and humid climates. However, there are not enough energy generation facilities and infrastructures to meet the growing demand because it is difficult to secure the construction and operation costs of the transmission and distribution systems. This study aims to develop a gas engine driven heat pump system that supplies heating, cooling and electric power to buildings. This system, besides its normal function to produce heat, has the capacity to generate electricity on a household level. This paper investigates similar cases overseas before developing the system. Through the investigation of commercialized similar systems, the level of technology and market trend of development system were identified. Features and specifications of commercial and industrial systems will be used for system development.

Conjugate Heat Transfer Analysis of High Pressure Turbine with Secondary Flow Path and Thermal Barrier Coating (2차유로 및 열차폐 코팅을 고려한 고압터빈의 열유동 복합해석)

  • Kang, Young-Seok;Rhee, Dong Ho;Cha, Bong Jun
    • The KSFM Journal of Fluid Machinery
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    • v.18 no.6
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    • pp.37-44
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    • 2015
  • Conjugate heat analysis on a high pressure turbine stage including secondary flow paths has been carried out. The secondary flow paths were designed to be located in front of the nozzle and between the nozzle and rotor domains. Thermal boundary conditions such as empirical based temperature or heat transfer coefficient were specified at nozzle and rotor solid domains. To create heat transfer interface between the nozzle solid domain and the rotor fluid domain, frozen rotor with automatic pitch control was used assuming that there is little temperature variation along the circumferential direction at the nozzle solid and rotor fluid domain interface. The simulation results showed that secondary flow injected from the secondary flow path not only prevents main flow from penetrating into the secondary flow path, but also effectively cools down the nozzle and rotor surfaces. Also thermal barrier coating with different thickness was numerically implemented on the nozzle surface. The thermal barrier coating further reduces temperature gradient over the entire nozzle surface as well as the overall temperature level.

Effects of Novel Fin Shape of High Temperature Heat Exchanger on 1 kW Class Stirling Engine (1kW급 스털링엔진 고온 열교환기의 Fin 형상 개선 효과 분석)

  • Ahn, Joon;Kim, Seok Yeon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.8
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    • pp.545-552
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    • 2017
  • In this research, numerical analysis was carried out on novel and existing fins, adjusted in terms of factors such as length, spacing, and angle, of a high-temperature heat exchanger for a 1 kW class Stirling engine, designed as a prime mover for a domestic cogeneration system. The performance improvement as a result of shape optimization was confirmed with numerical analysis by including the air preheater, which was not considered during optimization. However, a negative heat flux was observed in the cylinder head portion. This phenomenon was clarified by analyzing the exhaust gas and wall surface temperature of the combustion chamber. Furthermore, assuming an ideal cycle, the effects of heat transfer enhancement on the thermodynamic cycle and system performance were predicted.

Heat Exchangers for Gas Turbine Cycles and Thermal Management (롤스로이스 기술개발 동향)

  • Stieger, Rory
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.465-465
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    • 2011
  • Rolls-Royce is a global company producing advanced power systems for use on land, at sea and in the air. In order to develop competitive products and services, Rolls-Royce invests in technology, infrastructure and capability with much of the research carried out in a global network of University Technology Centres, such as the UTC in Thermal management at Pusan National University. Heat exchangers and thermal management play a critical role in today's gas turbine engines, maintaining the fuel and oil temperatures within the correct operational range. Future products are likely to place an increased duty on the thermal management system and thus require advances in heat exchanger design, installation and manufacturing. Heat exchangers further have the potential to play a vital role in Advanced Cycle Gas Turbine products. The Intercooled and recuperated WR21 marine gas turbine engine recently entered service with the Royal Navy and is delivering very attractive fuel burn in service. The development of an advanced cycle aero-engine is a significantly greater challenge, requiring better understanding of compact and light weight heat exchanger surfaces, novel installations and ducting systems and may required novel manufacturing techniques to achieve the volume, weight and cost necessary to realise a viable advanced cycle gas turbine aero-engine.

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A Study on the Effects of EGR on Engine Performance and Emissions of a HCCI(Homogeneous Charge Compression Ignition) Engine (HCCI 엔진에서 엔진성능 및 배출에 미치는 EGR의 영향)

  • Han, Sung-Bin;Chang, Yong-Hoon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.27 no.11
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    • pp.1630-1636
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    • 2003
  • Automobile companies and research institutions in leading automobile-manufacturing nations have recently been very active with research regarding the HCCI engine for use in future vehicles. Because HCCI engines take advantage of high compression ratio and heat release rate, they exhibit high efficiency found in compression ignition engines. HCCI engines also utilize a lean air/fuel ratio resulting in low emissions of NO$_{x}$ and PM (particulate matter). The objective of this research is to determine the effects of EGR rate on the combustion processes of HCCI. for this purpose, a 4-cylinder, compression ignition engine was converted into a HCCI engine, and a heating device was installed to raise the temperature of the intake air and also to make it more consistent. In addition, a pressure sensor was inserted into each of the cylinders to investigate the differences in characteristics among the cylinders. The experimental study of the effects of EGR rate on various gas emissions, engine performance, etc. should prove to be a valuable source of information for the development of the HCCI engine.e.

A cycle simulation of the S.I. engine and it's verification test (S.I. 엔진의 사이클 시뮬레이션 및 이의 확인 실험)

  • 목희수;김승수
    • Journal of the korean Society of Automotive Engineers
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    • v.10 no.6
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    • pp.72-84
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    • 1988
  • Engine performance is one of the main objectives specified at the beginning of a new engine design project. The cycle simulation for SI engine is based on the zero-dimensional gas exchange model and a heat release expression by Viebe. This program also requires minimum input data and takes only a short time to run. Heat transfer from cylinder transfer formula. The flow coefficient (effective area) is calculated from valve lift using the standard flow coefficient curve and engine friction is calculated from the Millington and Hartles' engine friction formula. The chemical species considered in burned gas are 6 species CO, CO, H$_{2}$, H$_{2}$O, $O_{2}$, N$_{2}$ and the cylinder pressure, homogeneous cylinder temperature, gas composition and burned fraction are calculated at each crank angle through the cycle. To check the validity and accuracy, experimental study was done with 3 engines for measuring cylinder pressure, indicated mean effective pressure, brake mean effective pressure and air flow rate, etc. Despite its simple assumptions, cycle simulation showes excellent breathing and performance correlation when compared with data of tested engines, and have been proved useful in engine design.

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A Study on the Measurement of Temperature and Soot for Diffusion Flame in a Visualized D.I Diesel Engine Using the Two-color Method (이색법을 이용한 직분식 디젤 가시화 엔진내의 확산화염 온도 및 매연 측정에 관한 연구)

  • Han, Yong-Taek;Lee, Ki-Hyung
    • Transactions of the Korean Society of Automotive Engineers
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    • v.15 no.1
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    • pp.177-185
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    • 2007
  • The temperature and soot of the visualized diesel engine's turbulent flow of flame was qualitatively measured. In combustion chamber, in order to judge the affect that the swirl has on the in-cylinder's current, was used two different heads with different values. Using the high speed camera, and the results were analyzed using the heat release rate produced by the pressure sensor. In order to measure the temperature and soot of the turbulent flames like that of the diesel flames two color methods were used temperature and the soot of the flames according to the conditions through analyzing the two wavelengths of the flames. It was possible to measure the highest temperature of the non-swirl head visualized engine which is approximately 2400K, and that swirl head engine managed up to 2100K. With respect to the visualized diesel engine soot, we got the grasp of the KL factor which bears the qualitative information of soot. This study is dedicated to suggesting the possibility of measuring not only the temperature but also soot of the diffusion flame of the diesel engine turbulent flames through such method.

Analysis of Temprature and Thermal Stress Distribution of a DI Diesel Engine Cylinder Head(PART I) (직접분사식 디젤엔진 실린더헤드의 온도 및 열응력 분포해석(PART I))

  • 이진호;이교승;장경준
    • Transactions of the Korean Society of Automotive Engineers
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    • v.4 no.5
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    • pp.187-196
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    • 1996
  • In this study, 3-dimensional finite element model of a diesel engine cylinder head was made to accomplish heat transfer analysis and also thermal stress and deformation analysis. Heat release analysis and Nusselt-Reynolds correlations were applied to determine the convective boundary conditions which are required for heat transfer analysis to calculate temperature distribution. Thermal stress distribution was also investigated from heat transfer analysis results. Steady state temperature and heat flux were measured by using K-type thermocouples and then compared with numerical results to give a guarantee for the propriety of numerical analyses.

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Maximum power design conditions of heat engine with heat transfer processes (열전달을 고려한 열기관의 최대출력 설계조건)

  • 김수연;정평석
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.13 no.4
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    • pp.734-738
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    • 1989
  • As a basic study of optimum design conditions of the heat engines, Curzon-Ahlborn cycle has been analyzed by considering the capacity of heat exchanger as a design parameter. The result shows that the maximum power output is just unity. In addition, the optimum ratio is slightly decreased from the unity as the irreversibility of the cycle is increased.