• Title/Summary/Keyword: Cylinder Head

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Response of a prototype brain material subjected to rotational acceleration (회전가속에 대한 프로토타입 뇌재료의 반응)

  • Lee, E. S.
    • Journal of the korean Society of Automotive Engineers
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    • v.11 no.5
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    • pp.76-89
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    • 1989
  • With the objective of studying the response of brain tissue in a transient rotational acceleration of the head, as occurs in car crash, the problem of a cylindrical case containing a prototype brain material of silicone gel and subjected to a rotational acceleration around the axis of the cylinder is analysed. The prototype material is considered to be homogeneous and isotropic, and is modeled alternatively as a linear elastic or a linear viscoelastic solid. The computational model for the present problem consists of a 3-dimensional isoparametric finite element model, wherein large deformations and large strains are treated through the updated Lagrangian approach. A comparison of the results of the present 3-dimensional computations, with the attendant assumptions on material data, is made with the results of independent experimental study. The deformation profiles and the major characteristics of response of the brain material are in good agreement with the test results. Moreover, the study suggests the possibility that the use of more accurate material data may yield very useful results even appropriate for accurate quantification of deformations.

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The Characteristics of Backfire for 2 stroke Free-Piston Hydrogen Fueled Engine with Uni-flow Scavenging (Uni-flow 소기방식 2행정 프리피스톤 수소기관의 스트로크변화에 따른 역화 특성)

  • Cho, Kwan-Yeon;Cho, Hyung-Wook;Lee, Jong-Tae
    • Transactions of the Korean hydrogen and new energy society
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    • v.20 no.5
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    • pp.371-377
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    • 2009
  • Backfire characteristics for hydrogen fueled free piston engine with uni-flow scavenging is investigated with different stroke, exhaust vlave openning timing and fuel-air equivalence ratio by using RICEM (Rapid Intake Compression Expansion Machine) for combustion research of free piston engine. As results, it is found that backfire can be occurred due to slow combustion of unhomogeneous mixture in the piston crevice volume or/and in the cylinder near piston head. And the more stroke of free piston H2 engine with uni-flow scavenging is short the more opening timing of exhaust valve have to be advanced to control backfire.

Numerical and Theoretical Study on the Fluid Flow in the Cooling System of a Marine Diesel Engine (선박용 디젤엔진의 냉각수 유동에 대한 수치해석적 및 이론적 연구)

  • Suh, Yong-Kweon;Heo, Seong-Gyu;Chung, Sung-Sik
    • Journal of Advanced Marine Engineering and Technology
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    • v.32 no.1
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    • pp.119-130
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    • 2008
  • Diesel engine is one of the most expensive and important components in a ship. Many researchers are interested in increasing the performance of diesel engines. Design of an optimum cooling system should also contribute to the enhancement of the performance as well as the efficiency of engines. In this study, we investigated the flow pattern within the cooling system of a marine diesel engine by using numerical simulation prior to the study of the heat-transfer problem. The engine cooling system is composed of five cooling units each unit containing a water-jacket and a cylinder head. Based on the calculated data, we also conducted theoretical analysis that can predict the flow-rate delivery in each of the five units.

A Study on the Effects of the Design Parameters and Sealing Mechanism of the Exhaust Gas in Engine Exhaust System (엔진 배기계의 배기가스 누설 메카니즘과 설계인자들의 영향에 관한 연구)

  • Choi, B.L.
    • Journal of Power System Engineering
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    • v.14 no.4
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    • pp.37-42
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    • 2010
  • This paper deals with the sealing mechanism of the gasket component and the effects of design parameters for the exhaust manifold. The finite element model includes hot-end exhaust system and a simplified gasket model supplied by ABAQUS software. The mechanical behaviors of bead and body of a gasket are measured after several times of cyclic loads by gasket supplier. From the finite element analysis due to the cyclic thermal loads, the flange of exhaust manifold shows thermal expansion and contraction in longitudinal direction as well as convex and concave deformations with respect to the engine cylinder head. And, the contact pressures of the gasket beads suddenly changes by normal deformation of inlet flanges. Therefore, the magnitudes of contact pressures could be used to determine the sealing characteristics of the exhaust gas in the exhaust system. The distributions of contact pressures in gasket bead lines shows a good agreement with the engine test results.

Vibration Experiments of the Cylindrical Structure for Verifying the Reliability of Power Flow Finite Element Method (파워흐름해석법의 신뢰성 검증을 위한 원통형 구조물의 진동실험)

  • 이호원;홍석윤;박영호;길현권;김창열;전재진;류정수
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.05a
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    • pp.290-297
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    • 2002
  • Vibration experiments have been performed to observe the analytic characteristics of power How finite element method(PFFEM) for the reinforced cylindrical structure. For this, the vibration experimental results are compared with the numerical solutions obtained by PFFEM in medium-to-high frequency ranges. Input Power into the experimental structure is measured using the impedance head adhered to the exciter, and that input power is used for the vibration analysis. Using the developed PFFEM program(PFADS), the reinforced cylindrical structure modeled by beam and plate elements is analyzed, and very reliable results for PFFEM are obtained by the comparisons of the experimental results.

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On the flame propagation in a spark-ignited gasoline engine (전기점화식 내연기관에 있어서 화염전파에 관한 연구)

  • 이종원;이형인
    • Journal of the korean Society of Automotive Engineers
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    • v.4 no.2
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    • pp.69-78
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    • 1982
  • The purpose of this study is to investigate the flame propagation phenomenon in the combustion chamber of spark-ignition gasoline engine for the idling condition. by means of four ion probes located through the cylinder head, the time intervals for the flame to arrive at the respective probes are read on th visicorder char. As results, the flame is considered to initiate after some ignition delay and to propagate through the central space of combustion chamber with rather constant speed on the order of 25m/sec, and thereafter to be slowed down approaching the wall. Additionally, the retardation of flame in the wall boundary layer could be inferred. The maximum pressure is developed when the flame nearly touches the wall diagonal to the spark plug. And some features of flame propagation are elucidate.

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A Study on the Kernel Formation & Development for Lean Burn and EGR Engine (희박연소 및 EGR 엔진에서 초기 화염액 생성 및 성장에 관한 연구)

  • 송정훈;선우명호
    • Transactions of the Korean Society of Automotive Engineers
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    • v.7 no.8
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    • pp.24-33
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    • 1999
  • This paper investigate the effects of the variations of engine operation condition in the flame kernel formation and developmnet . A model for calculating the initial kernel development in spark ignition engines is formualted. It considered input of electrical energy, combustion energy release and heat transfer to the spark plyg, cylinder head, and unburned mixture. The model also takes into accounts strain rate of initial kernel and residual gas fraction. The breakdown process and the subsequent electrical power input initially control the kernel growth while intermediate growth is mainly dominated by diffusion or conduction. Then, the flame propagates by the chemical energy and turbulent flame expansion. Flame kernel development also influenced by engine operating conditions, for example, EGR rate, air-fuel ration and intake manifold pressure.

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A Study on Unsteady Thermal Loading of Hydrogen Engine with Dual Injection (이중분사식 수소기관의 비정상 열부하 해석에 관한 연구)

  • Wei, Shin-Whan;Kim, Yun-Young;Kim, Hong-Jun;Lee, Jong-Tai
    • Transactions of the Korean hydrogen and new energy society
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    • v.12 no.2
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    • pp.147-155
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    • 2001
  • To measure of thermal loading in the combustion chamber of hydrogen engine with dual injection, instantaneous wall-surface temperature and unsteady heat flux of the cylinder head are measured and analyzed. The maximum wall surface temperature is shown in direct injection region which has large heat supplied. Partial and spatial temperatures have slight deviation in transient region of injection, though injection method change suddenly. All of thermal characteristics such as instantaneous temperature, temperature swing and heat flux of hydrogen engine with dual injection are remarkably higher than those of gasoline engine. It means necessity of additional countermeasure of thermal loading.

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An Analysis on Charateristics of Separate Oiling to Reduce Oil Consumption for a 2 Stroke Free-Piston H2 Engine (오일 소모 저감을 위한 역단류 2행정 프리피스톤 수소기관의 분리 윤활 특성 해석)

  • Byun, Cahng-Hee;Baek, Dae-Ha;Lee, Jong-Tae
    • Transactions of the Korean hydrogen and new energy society
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    • v.22 no.6
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    • pp.794-799
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    • 2011
  • In order to reduce the oil consumption for a 2 stroke free piston hydrogen fueled engine, the behaviors of residual lubricant oil of the cylinder wall surface were visualized and oil mass emitted into exhaust port was measured by using research engine with cross-head and eccentric crankshaft. As the results, it was shown that characteristics of residual lubricant oil such as oil thickness and distribution were remarkably different from a conventional 4 stroke engine. It was also analyzed that these tendencies relied on the configuration and installed position of the exhaust port, piston pin boss and so on.

Cooling Design and Flight Test for Airplane Reciprocating Engine (항공기 왕복엔진 냉각설계 및 인증시험)

  • Lee, Kangyi;Park, Jonghyuk;Park, Sunghwan
    • Journal of Aerospace System Engineering
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    • v.6 no.2
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    • pp.35-41
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    • 2012
  • A reciprocating engine installed on a normal category airplane shall be effectively cooled by air flown through the engine compartment. A airplane powerplant designer has to design cooling air inlets, baffles, seals, and outlets to maintain cylinder head temperatures and oil temperature under the limits, and show compliance with appropriate airworthiness standard. In this study, cooling designs of the installed engine and compliance requirements applicable to the cooling designs were reviewed, and engine cooling flight test results were evaluated for design changes. Engine cooling certification test will be conducted in a next step.