• Title/Summary/Keyword: 왕복엔진

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Distributed and Dispersed Power Resources : Paradigm Shift of Energy Technology (에너지 기술의 패러다임 전환 : 분산형 전원)

  • 김형택;신영균;천원기
    • Journal of Energy Engineering
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    • v.10 no.1
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    • pp.1-9
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    • 2001
  • 전력 사업 구조 개편과 전력계통 신뢰도에 대한 우려 증대, 풍부하고 저렴한 천연가스, 새로운 대기 오염 규제, 부정전전원의 가치 증대로 인하여 분산형 발전의 수요가 증가하고 있다. 본고에서는 미국의 사례를 중심으로 분사형 전원의 현황을 개략적으로 살펴보고 핵심기술인 왕복동엔진, 가스터빈, 마이크로터빈, 연료전지, 태양광발전 기술들의 특징, 장점, 경제성 등을 서술하고 이 기술들의 활용범위 및 분산형 시스템으로서의 적합성에 대하여 논하며 관련 연구개발, 기존 전력망과의 연계, 문제점과 전망에 대해서 살펴보고자 한다.

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Prgress in MEMS Engine Development for MAV Applications (KAIST의 MAV용 MEMS 엔진 개발 현황)

  • Lee, Dae-Hoon;Park, Dae-Eun;Yoon, Eui-Sik;Kwon, Se-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.6
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    • pp.1-6
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    • 2002
  • Micro engine that includes Micro scale combustor is fabricated. Design target was focused on the observation of combustion driven actuation in MEMS scale. Combustor design parameters are somewhat less than the size recommended by feasibility test. The engine structure is fabricated by isotropic etching of the photosensitive glass wafers. Electrode is formed by electroplating of the Nickel. Photosensitive glass can be etched isotropically with almost vertical angle. Bonding and assembly of structured photosensitive glass wafer from the engine. Combustor size was determined to be 1mn scale. Piston in cylinder moves by fuel injection and reaction. In firing test, adequate engine operation including ignition, flame propagation and piston motion was observed. Present study warrants further application research on MEMS scale internal combustion power units.

Establishment of Multi-Stage Turbocharger Layout for HALE UAV Engine and Its Performance Assessment (고고도 장기체공 무인기 엔진용 다단 터보차저 구성 및 성능해석)

  • Kang, Young Seok;Lim, Byung Jun;Kim, Jong Kuk
    • The KSFM Journal of Fluid Machinery
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    • v.18 no.6
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    • pp.31-36
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    • 2015
  • A multi-stage turbocharger system has been constructed for HALE UAV internal combustion engine. To boost rarefied intake air up to sea level condition, the turbocharger system should consist of 3 stages including heat exchanger located after compressor outlet to drop compressed air temperature. One dimensional system analysis has been conducted by matching required power between compressor and turbine and adequate turbochargers have been searched for from commercially available models targeting for automobiles. By applying commercial automobile turbochargers to the multi-stage turbocharger system, it is expected that considerable amount of research resources will be saved.

Dynamic Analysis Design of Balance Shaft for Reducing Engine Inertia Force and Pitching Moment (엔진 관성력과 피칭모멘트 저감을 위한 밸런스샤프트의 동역학 설계)

  • Kim, Byeong Jun;Boo, Kwang Suk;Kim, Heung Seob
    • Journal of the Korea Convergence Society
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    • v.13 no.4
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    • pp.307-313
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    • 2022
  • The importance of engine vibration reduction is increasing as the vehicle interior noise becomes more serious due to higher output and lighten weight trends. Recently, the balance shaft attachment has been proposed as a representative method for the engine vibration reduction. The balance shaft is a device that cancels the vibrations generated in the reciprocating motion of the piston and the conrod by using an arbitrary eccentric mass, and can improve fuel efficiency and ride comfort at the same time. This paper proposes the unbalance amount and shape of the balance shaft to induce and offset the inertia force generated by the engine structure. The proposed two-shaped balance shaft was implemented as an ADAMS multi-body dynamics model, and the reduction of the inertial force in the actual behavior was confirmed through dynamic simulation.

A Numerical Simulation of Unsteady Axisymmetric Turbulent Flow in a Reciprocating Engine Including Port/Valve Assembly (축대칭 왕복엔진의 비정상 난류유동에 대한 수치해석)

  • 조진행;유홍선;최영기
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.1
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    • pp.139-149
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    • 1994
  • A numerical simulation of unsteady axisymmetric turbulent flow was performed for a reciprocating engine including port/valve assembly. The governing equations based on a nonorthogonal coordinate formulation with Cartesian velocity components were used and discretised by the finite volume method with non-staggered variable arrangements. The modified $\kappa-\xi$. turbulence model which included the effect of compressibility was used. The results of twodimensional transient calculation for the axisymmetric configuration were compared with the experimental data. Although slightly low rms velocity was predicted compared to the experimental data, predicted velocity distributions at the valve exit and in-cylinder region showed good agreements with the experimental data. The flow at the valve exit was separated at the same valve lift position with the experimental data. Two vortices incylinder region were generated during the initial intake process. The clockwise main vortex became strong and moved upward to the top wall. The counter-clockwise second vortex became weak and stick to the upper left corner of the cylinder. After middle intake process, new vortex adjacent to upper cylinder wall appeared by the piston motion and therefore, the in-cylinder flow was formed into three vortices. The cylinder pressure just before bottom dead center of piston was higher than inlet pressure and then the reverse flow occured at the valve exit. The in-cylinder flow characteristics were strongly dependent on piston motion, but insensitive to valve motion.

Characteristics of Combustion by Varying Different Coolant-temperature in a Hydrogen Engine for HALE UAV (고고도 무인기용 수소연료엔진의 냉각수 온도변화에 따른 연소 특성)

  • Yi, Ui-Hyung;Jang, Hyeong-Jun;Park, Cheol-Woong;Kim, Yong-Rae;Choi, Young
    • Journal of the Korean Institute of Gas
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    • v.22 no.2
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    • pp.59-66
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    • 2018
  • Using hydrogen fuel is expected to be suitable as a reciprocating internal combustion engine with heightened interest in HALE(High Altitude Long Endurance) UAV(Unmanned Aerial Vehicle). Hydrogen is hightest energy density per mass so it can continue to charge for long periods of time and have positive part of the environmental effects. However, it is estimated that there is less research on hydrogen fuel engine currently applied, and many studies need to be done. Depending on the operation, there are factors that result in supercooling due to reduced radiation or reduce cooling performance due to low air density. Therefore, the experiment was to change the temperature of the cooling water and investigate the effect on engine combustions. The limitation of the stable operation range due to backfire is dominated by the excess air ratio rather than the effect of the cooling water temperature change. When the cooling water temperature increases, the volumetric efficiency decreases and the torque decreases. As the cooling water temperature decreases, the heat loss was increased and consequently the thermal efficiency was decreased.

Dynamic Performance of Natural Gas Injection Valve for Heavy-Duty Power Generation Engine - Part I (발전용 대형엔진용 천연가스 분사밸브 동특성 연구 (I))

  • Choi, Young;Kim, Yong-Rae;Lee, Seok-Whan;Kim, Chang-Gi
    • Journal of the Korean Institute of Gas
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    • v.19 no.6
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    • pp.15-21
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    • 2015
  • Natural gas fuel has known to be very promising in terms of abundancy and economic value. Therefore it is widely treated as research topics in a variety field of production, storage and utilization. Natural gas has become one of the major sources for the power generation by using internal combustion engines(ICE). Development of natural gas fuel injection device should be preceded to realize a reliable natural gas fuel supply system for a MW class power generation reciprocating ICE. In this research, an injection valve which consists of solenoid and body part with a moving plate was designed and its dynamic performance was experimented in the engine-like environment. As a result of the experiments, linearity of flow rate was obtained and overall around 2ms of response time was observed at the pressure difference of 1bar. In addition, more than 100Liter/min(@2Hz) of gas flow rate was witnessed, which is expected to be adequate for the fuel supply system of a MW class natural gas engine.

Study on Forced Vibration Behavior of WIG Vehicle Main Wing Structure Excited by Propulsion System (프로펠러 엔진에 의해 가진되는 소형 위그선 주날개의 진동 거동 해석에 관한 연구)

  • Kong, Chang-Duk;Yoon, Jae-Huy;Park, Hyun-Bum
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.7-12
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    • 2007
  • Previously study on structural design of the main wing of the twenty-seat class WIG (Wing in Ground Effect) craft. In the final design, three spars construction was selected for safety in the critical flight load, and the Carbon-Epoxy material was selected for lightness and structural stability. In this study, the forced vibration analysis was performed on the composite main wing structure of the twenty-seat class WIG craft with two-stroke pusher type reciprocating engine. The vibration analysis based on the finite element method was performed using a commercial FEM code, MSC/NASTRAN. Excitations for the frequency response analysis were assumed as the Y-mode (lateral mode), the Z-mode (vertical mode) and the $M_{xyz}$-mode (twisted mode) which are typical main vibration modes of engine. And excitations for the transient response analysis were assumed as the X-mode (longitudinal mode) with the oscillating propeller thrust which occurs in operation.

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The SIMDIST (Simulated Distillation) Analysis of Distributing Engine Oil (국내 유통 엔진오일 고온모사증류시험 분석)

  • Lim, Young-Kwan;Kim, Jiyeon;Kim, Jong-Ryeol;Ha, Jong-Han
    • Applied Chemistry for Engineering
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    • v.28 no.6
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    • pp.632-637
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    • 2017
  • The vehicle lubricant occupies upto 35% in a total lubricant market and engine oil occupies upto 77% in the vehicle lubricant market in Korea. A suitable quality management of the circulating engine oil is necessary for driver and engine protection. But, KS and synthetic engine oil products (involved over 30% synthetic oil) are exempt to any quality management under Petroleum and Alternative Fuel Business Act. It is also known that synthetic oils such as PAO (poly alpha olefin) have excellent properties and performance like anti-wear, varnish control and oxidation stability than those of mineral oils. For this reason, PAO has been used for an engine oil, rotary screw and reciprocating compressor in addition to heavy duty and other extreme service applications. In this study, our research group analyzed the chromatogram pattern for the mineral oil, PAO and mineral oil involved a typical ratio of PAO using SIMDIST (simulated distillation). In the SIMDIST chromatogram, the mineral oil showed a broad peak, while PAO showed a sharp typical peak. Also the oil with a large viscosity grade exhibited a long retention time due to the heavy molecular weight and high boiling point. In particular, the blended mineral oil with 20% PAO sample showed a distinctly different pattern compared to that of using the conventional mineral oil. For monitoring PAO contents in distributing engine oils, we analyzed the SIMDIST for 27 kinds of engine oils which were popularly sold in Korea. The analytic results indicate that all kinds of engine oils showed that PAO contents were below 20% in engine oil products. Moreover, the PAO titled product was found to have a small amount of PAO. Thus, we conclude that the related laws for the proper quality management of synthetic oils are needed to be established.

Numerical calculations of flow and heat transfer in an axisymmetric reciprocating engine at it's suction and compression stage (축대칭 왕복 엔진의 흡입 및 압축과정에서 유동 및 열전달의 수치해석)

  • 강신형;이창훈
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.11 no.3
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    • pp.395-408
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    • 1987
  • Turbulent flows in an axisymmetric reciprocating engine are numerically simulated at it's suction and compression stage. Amounts of heat transfer through the wall of the cylinder are also estimated. k-.epsilon. turbulence model is adopted and the law of the wall is applied at grid-points near the wall. More than 40 * 40 grids are reguried to reasonably predict flows and the 3-level finite difference scheme for the time derivative term appears to be effective rather than the 2-level scheme. Calculated mean velocity distributions shows good agreements with an available experimental data. The program reasonably simulates flow patterns and pressures throughout the suction and the compression stages of the reciprocating engine. Predicted intensities of turbulence are still deviated from measured data. Further researches for turbulence modeling are expected.