• Title/Summary/Keyword: Piston Engine

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A Study on the Process Development of Mono Steel Forged Piston for Diesel Engine (디젤 엔진용 일체형 스틸 단조피스톤 공정 개발에 관한 연구)

  • Yeom, Sung-Ho;Nam, Kyoung-O;Hwang, Doo-Soon;Kwon, Hyuk-Sun;Hong, Sung-In
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.3
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    • pp.44-50
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    • 2006
  • The mono steel forged piston was improved a mechanical strength of an aluminum piston and reduced the weight of a articulated piston. The mono steel forged piston was composed of forged crown part and forged skirt part and was completed by friction welding process of two forged parts. Forging process analysis and friction welding analysis was done by finite element simulation using numerical package DEFORM. The preform shape and the initial billet dimension were decided by maximum stress of the die, amount of the flash and filling of die. The upset length of friction welding variable was decided by the shape of the flash that was created by friction welding analysis. Through this research, we developed a forging process of the mono steel forged piston, and decided the design variables of friction welding.

Durability Design of Composite Piston in Marine Diesel Engines (박용 디젤엔진용 분리형 피스톤의 내구설계)

  • Son, Jung-Ho;Ha, Man-Yeong;Ahn, Sung-Chan;Choi, Seong-Wook
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.34 no.5
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    • pp.651-657
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    • 2010
  • A composite piston with a crown made of steel and a skirt made of NCI is used in a marine diesel engine, which has a maximum firing pressure of over 180 bar and a high thermal load. In the fatigue design of the composite piston, the fatigue is influenced by factors such as the load type, surface roughness, and temperature; further, the distribution ratio of the firing force from the crown to the skirt is important for optimizing the design of the crown and skirt. In this study, the stress gradient method was used to consider the effect of the load type. The temperature field on the piston was predicted by cocktail-shaking cooling analysis, and influence of high temperature on fatigue strength was investigated. The load transfer ratio and contact pressure were optimized by design of the surface shape and accurate tolerance analysis. Finally, the cooling performance and durability design of the composite piston were verified by performing a long-term prototype test.

The Characteristics of High-speed Noncircular Machining Tool Feed Systme using Linear Motor (리니어 모터를 이용한 고속비진원 가공용 공구이송장치의 특성연구)

  • 서준호;민승환;김성식;이선규
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1995.10a
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    • pp.985-990
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    • 1995
  • Recently, the development of high speed and high precision NC-lathe for piston head machining is needed for the complexity and diversity of the piston head shape used in automobile reciprocating engine. THe piston head has many complex shapes in the aspect of fuel economy, such as ovality, profile, double ovality and recess. Among them, for the maching of the over shape of 0.1~1mm the cutting tool should move periodically symchronized with the rotation of piston workpiece. The cutting tool feeed system must have high positioning accuracy for the precise machining, high speed for the fast maching and high dynamic stiffness for the cutting force. The linear brushless DC motor is used for satisfying these coditions. The ballbush guide and supporting guide using turcite is used for the guidance of the feed drive system. Linear encoder, digital servo ampllifer and controller are used for driving the motor. THis paper presents the design and simulation of the new tool feed system for noncircular machining.

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An Analytical Study on the Lubrication Characteristics between the Piston Ring and Grooved Cylinder Liner (그루브가 있는 실린더 라이너와 피스톤 링 사이의 윤활 특성에 대한 해석적 연구)

  • 조명래;한동철
    • Tribology and Lubricants
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    • v.16 no.2
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    • pp.114-120
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    • 2000
  • This paper reports on the theoretical analysis on the lubrication characteristics between the piston ring and the grooved cylinder liner. The circular shape piston ring and two types grooves are consider, and the minimum oil film thickness during the full engine cycle are obtained by using iterative technique. The comparative results of minimum oil film thickness and viscous friction force between the smooth and grooved liner are presented. And various design parameter of piston ring and liner groove are tested. The groove in the liner generally reduces the minimum value of minimum oil film thickness, but the maximum viscous friction force is increased at the minimum film position.

Characteristics of in-cylinder flow near the spark-plug for different engine speeds (엔진속도 변화에 따른 연소실내 Spark Plug 주위의 유동특성 고찰)

  • Seong, Baek-Gyu;Jeon, Gwang-Min
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.20 no.7
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    • pp.2289-2297
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    • 1996
  • Flows in the combustion chamber near the spark plug are measured using LDv.A single cylinder DOHC S.I. engine of compression ratio 9.5:1 with a transparent quartz window piston is used. Combustion chamber shape is semi-wedge type. Measured data are analyzed using the ensemble averaged analysis and the cycle resolved analysis which uses FFT Filtering. Turbulent intensity and mean velocity are studied in the main flow direction and the normal to main flow direction as a function of engine speeds. The results shows that the turbulent intensity obtained by the ensemble averaged analysis is greater than that calculated by the cycle resolved analysis. Especially, the ensemble averaged analysis shows increase in turbulence at the end of compression stroke although the cycle resolved analysis shows increase only in the cycle-by-cycle variation with no noticeable increase in turbulence. The mean velocity in the main flow direction increase as engine speed increase. But the mean velocity normal to the main flow does not show such increase. Turbulent intensity in both direction increase in proportion to engine speeds. The magnitude of turbulent intensity is about 0.3 ~ 0.4 times the mean piston speeds at the end of the compression stroke.

A Study on the Fuel Behaivor with Cavity Diameter in a Gasoline Direct Injection Engine (직분식 가솔린 엔진에서 피스톤 캐비티 반경에 따른 연료 거동 분석)

  • Kim, Tae-An;Kang, Jeong-Jung;Kim, Duck-Jool
    • Proceedings of the KSME Conference
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    • 2003.11a
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    • pp.472-477
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    • 2003
  • This study was performed to investigate the behavior of vapor phase of fuel mixtures with different piston cavity diameters in a optically accessible engine. The images of vapor phases were measured in the motoring engine using exciplex fluorescence method. The conventional engine was modified as GDI engine with swirl flow. Fuel was injected into atmospheric nitrogen to prevent quenching phenomenon by oxygen. Injection pressure is 5.1MPa. Two dimensional spray fluorescence image of vapor phases was acquired to analyze spray behavior and fuel distribution inside of cylinder. Three injection timings were set at BTDC $180^{\circ}$, $60^{\circ}$and $60^{\circ}$. With a fuel injection timing of BTDC $60^{\circ}$, fuel-rich mixture was concentrated in near the cavity center. With a fuel injection timing of BTDC $60^{\circ}$, fuel-rich mixture level in the center region was highest in the S-type during the late compression stroke. With a fuel injection timing of BTDC $180^{\circ}$, fuel was not affected in a piston cavity and generally distributed as homogeneous mixture.

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Thermal-flow analysis of a simple LTD (Low-Temperature-Differential) heat engine

  • Kim, Yeongmin;Kim, Won Sik;Jung, Haejun;Chen, Kuan;Chun, Wongee
    • Journal of Energy Engineering
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    • v.26 no.1
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    • pp.9-22
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    • 2017
  • A combined thermal and flow analysis was carried out to study the behavior and performance of a small, commercial LTD (Low-Temperature-Differential) heat engine. Laminar-flow solutions for annulus and channel flows were employed to estimate the viscous drags on the piston and the displacer and the pressure difference across the displacer. Temperature correction factors were introduced to account for the departure from the ideal heat transfer processes. The analysis results indicate that the work required to overcome the viscous drags on engine moving parts and to move the displacer is much smaller than the moving-boundary work produced by the power piston for temperature differentials in the neighborhood of $20^{\circ}C$ and engine speeds below 10 RPS. A comparison with experimental data reveals large degradations from the ideal heat transfer processes. Thus, heat-transfer devices inside the displacer cylinder are recommended.

An analytic solution for the stirling engines with saw-toothed piston motions in adiabatic cylinders (단열실린더내에서 톱날파형 피스톤운동을 하는 스터링기관에 대한 해석적인 해)

  • 유호선
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.12 no.5
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    • pp.1197-1205
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    • 1988
  • An analytical method to predict qualitative performance characteristics of the Stirling Engines in the preliminary design stages is investigated. Both the expansion and the compression cylinder are treated as adiabatic and piston motions are approximated as saw-toothed waves. Basic equations which were originally proposed by Finkelstein consist of mass conservation and energy balances for each adiabatic cylinder. The approximation on piston motions and physical conditions make it possible to divide an engine cycle into four fundamental processes. In each process, first, pressure can be expressed as a function of the crank angle by solving a nonlinear first order ordinary differential equation and other thermodynamic variables are determined in turn. Application of the cyclic steady condition to the whole processes can complete a cycle. Also, further analysis results in analytic expressions for cyclic work and heat transfer in terms of the engine parameters and thermodynamic variables at boundary points. The results are expected useful as a quick reference for the engine performances. Finally, the present method can be applied to the other adiabatic analyses on the Stirling Engines with piece wise linear piston motions, if mass variations are predictable.

Rig Tester Development for the Performance Validation of a Piston Oil Cooling Gallery (피스톤 오일 냉각 유로의 성능 검증을 위한 리그 시험기 개발)

  • Chun, Sang-Myung;Lee, Jeong-Keun;Joo, Dae-Heon;Ryu, Kwan-Ho;Ha, Dae-Hong
    • Tribology and Lubricants
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    • v.25 no.6
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    • pp.387-398
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    • 2009
  • The operation condition of recently designed pistons for high power and high speed diesel engine become more severe due to the increment of combustion pressure and temperature. So, in order to overcome high temperature, the application of the mono-metal cast aluminum alloy piston featuring an enclosed cast-in open cooling gallery has increased. In this research, it is developed a PCJ (piston cooling jet) rig tester, described the test procedure and validated the performance of sample piston cooling gallery design. Then the test rig will be used for developing the design technology of piston cooling gallery. The test rig is composed with oil reservoir and pumping system, oil jet system, piston fixing and moving system, collecting oil measuring system, and data measuring and recording system. It will be measured collecting efficiencies under conditions of a few piston positions, oil jet pressures and oil viscosities for a piston cooling gallery. Furthermore, the PCJ rig tester will be used for the optimum design of the oil cooling gallery which being applied to increase the cooling efficiency of pistons in diesel engines satisfying the EURO V emission regulation and the more.