• 제목/요약/키워드: Piston engine

검색결과 465건 처리시간 0.023초

소형 회전식 압축기의 동수압적 윤활해석 (Hydrodynamic Lubrication Analysis of a Small Rotary Compressor)

  • 송기선;장시열;한동철
    • Tribology and Lubricants
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    • 제4권1호
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    • pp.74-80
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    • 1988
  • For an analytic investigation on the dynamic behaviour of the eccentric piston and roller in the cylinder of small rotary vane compressors the hydrodynamic lubrication theory is opplied, analogous to the dynamic analysis of a engine bearing. An adequate modification of the equation of journal motion permits stable convergencies of the numeric calculation of the journal orbits. The increase of the outer diameter of the roller and the eccentricity of the piston gives a relative large decrease of the minimum gap between the roller and cylinder.

피스톤 헤드 온도에 오일 제트가 미치는 영향에 대한 연구 (Study of Oil Jet Effect on the Temperature of Piston Head)

  • 민선기
    • 한국산학기술학회논문지
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    • 제19권11호
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    • pp.536-540
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    • 2018
  • 엔진의 성능이 향상될수록 엔진 내부에서 연소되는 연료의 양이 증가하고 그에 따라 엔진의 온도는 증가하게 된다. 특히 피스톤 헤드의 경우 냉각이 어려우므로 피스톤 헤드의 온도가 높아지게 된다. 그러나 피스톤 헤드의 온도가 너무 높게 되면 피스톤 헤드 표면에서 이상 연소가 발생하기 쉬워 토크 저하 및 엔진 파손과 같은 결과를 가져온다. 피스톤 헤드의 온도를 낮게 하기 위하여 오일을 피스톤 헤드 하단부로 분사하는 오일 제트가 사용되는데, 본 연구에서는 오일 제트에 의한 피스톤 헤드 냉각 효과를 확인하기 위하여 템플러그를 사용하여 엔진 작동시 피스톤 헤드의 온도를 측정하였다. 템플러그는 일종의 센서로 피스톤 헤드의 온도에 따라 템플러그의 경도가 변화하여 변화된 경도를 이용하여 피스톤 헤드의 온도를 측정한다. 템플러그를 사용하여 피스톤 헤드의 최고 온도를 오일 제트가 없는 상태와 설치된 상태에서 측정하였다. 오일 제트가 설치됨에 따라 피스톤 헤드의 온도는 변화되었다. 최고 온도 부위가 중앙부위에서 전후부위로 변경되었다. 또한 피스톤 헤드 내에서 온도 편차가 감소하여 좀 더 균일한 피스톤 헤드 온도 분포를 얻을 수 있었다.

오일유막의 연료 흡수 및 방출에 관한 연구 (Modeling of Absorption/Desorption of Fuel in Oil film on the Cylinder Liner in SI Engines)

  • 유상석;민경덕
    • 한국자동차공학회논문집
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    • 제7권9호
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    • pp.165-171
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    • 1999
  • An oil layer fuel absorption /desorption modeling was developed. Multi-component fuel model has showed more reasonable condition than single component model. Henry's constant which is related to solubility is the most important variable in the oil layer absorption/desorption mechanism. The oil segments close to the top of the cylinder liner have more significant contribution to the fuel absorption and desorption process than other oil segments. At the warmed-up condition, the effect of the engine speed on the precent fuel absorbed/desorbed is minimal. But at low il film temperature, percent of fuel abosrbed/desorbed is decreased with increasing the engine speed because of low value of molecular diffusion coefficient of fuel. The amount of fuel trapped in the piston crevice is from 2 to 2.3 times larger than that of fuel in the oil fim. However, fuel form oil film slowly desorbs into the combustion chamber compared with fuel from the piston crevices when the engines is cold.

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디젤엔진 피스톤용 SCM440의 레이저 표면경화부의 잔류응력 (Residual Stress Distribution of Laser Hardened SCM440 for Diesel Engine Piston)

  • 이동석;유웅재;김재도
    • 열처리공학회지
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    • 제8권3호
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    • pp.182-186
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    • 1995
  • SCM440, which is widely used as the diesel engine piston of vessel, has been hardened by a $CO_2$ laser with the wavelength of $10.6{\mu}m$. Laser hardening experiment has been carried out for the condition of a laser power 1kW, the travel speed between 0.4 and 1.5m/min, and a rectangular-Gaussian beam. Residual stress has been measured by using middle point technique of half value width of X-ray diffraction method. It was found that the compressive residual stress with the range between 400 and 600MHz has distributed in the laser hardening zones and the tensile residual stress between 100 and 200MHz has distributed in the boundary of hardening zones.

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피스톤 냉각용 오일제트 비정상 유동 해석 (Unsteady Flow Analysis of Oil Jet for Cooling the Piston)

  • 권지혁;이연원;김재환
    • 한국자동차공학회논문집
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    • 제16권2호
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    • pp.1-7
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    • 2008
  • In order to enhance the performance of an automotive engine, many researchers have been carried out. An oil jet cooling a piston is one of important parts for engine performance. Therefore, the efficient cooling system of an oil jet is needed. In this paper, unsteady flow analysis of the oil jet which consists of a check valve and a nozzle has been accomplished. And the reaction between mass flow rate and ball movement was also investigated.

피스톤 링그루브의 레이저 열처리 (Laser Hardening of Piston Ring Groove)

  • 송영기;서성재
    • 열처리공학회지
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    • 제10권3호
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    • pp.165-171
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    • 1997
  • Laser hardening for the piston ring groove of ductile cast iron was tried. Mechanical and microstructural investigation for the hardened area indicated that the laser heating technique could replace conventional induction hardening process completely and further showed that post grinding process would be eliminated by minimizing bulging of heat treated area. In laser hardening, the volume increase caused by martensitic phase transformation proved to be less than $10{\mu}m$, which insures no post machining on the hardened surface. As expected, the depth of hardening was inversely proportional to the beam scanning velocity and the highest surface hardness was obtained at the beam velocity of 0.75m/min. Heat treatment using phosphate coating demonstrated quite comparable result to the case of graphite suscepter.

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박용(舶用) 디이젤기관(機關)의 실린더 라이너 및 피스턴 링의 이상마모(異常摩耗)에 관(關)하여 (On the Abnormal Wear of Cylinder Liners and Piston Rings of the Marine Diesel Engine)

  • 정태준
    • 대한조선학회지
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    • 제8권1호
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    • pp.95-102
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    • 1971
  • Since the fuel oil of the bunker C grade, which is commonly burnt in the large marine diesel engine, causes the corrosive wear of cylinder liners and piston rings, a cylinder oil of high alkality is frequently used to prevent the wear. This practice, however, brings us an another problem to cause the abnormal wear. In this study the author made an investigation of the mechanism of the abnormal wear by the experiments surveying the influences of the alkality of a cylinder oil and the temperature of cylinder wall on the wear. The major results obtained from this study are as follows; A cylinder oil of low alkality is clearly effective for the preventation of the abnormal wear. Therefore, it is recommended that, prio to using a cylinder oil of high alkality, a cylinder oil of low alkality should be used until bringing an end to the initial wear. It is also observed that the abnormal wear depends largely on the temperature of the cylinder wall, that is, the higher the temperature goes up the severer the wear grows.

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Practical Calculation of Iron Loss for Cylindrical Linear Machine

  • Jeong, Sung-In
    • Journal of Electrical Engineering and Technology
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    • 제13권5호
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    • pp.1901-1907
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    • 2018
  • This paper is a study for accurate iron loss calculation of a cylindrical linear machine for free piston engine. This study presents that it is possible to accurately predict power loss in ferromagnetic laminations under magnetic flux by specially considering the dependence of hysteresis, classical, and excess loss components on the magnetic induction derivative. Significant iron loss in the armature core will not only compromise the machine efficiency, but may also result in excessive heating, which could lead to irreversible deterioration in the machine performance. Thus, correct prediction of power losses under a distorted flux waveform is therefore an important prerequisite to machine design, particularly when dealing with large apparatus where stringent efficiency standards are required. Finally, it will be discussed about the iron loss in various materials of cylindrical linear electric machine by geometric and electrical parameters. It will give elaborate information about the perfect design and design rules of cylindrical linear machine and in parallel tools for the calculation, simulation and design will be available.

Ground Test of Model SCRamjet Engine with Free-Piston Shock Tunnel

  • Kang, Sang-Hun;Lee, Yang-Ji;Yang, Soo-Seok;Smart, Michael;Suraweera, Milinda
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.452-455
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    • 2008
  • Model Scramjet engine is tested with T4 free-piston shock tunnel at University of Queensland, Australia. Basically, test condition is fixed as Mach 7.6 at 31 km altitude. With this condition, variation effects of fuel equivalence ratio, cavity, cowl setting and angle of attack were investigated. In the results, supersonic combustion was observed with low and middle fuel equivalence ratio. At high equivalence ratio, thermal choking was occurred due to the intensive reaction. Cavity and W-shape cowl showed early ignition and enhanced mixing respectively.

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유한요소법에 의한엔진 구조소음 해석 (An Engine Structure-Borne Noise Analysis by Finite Element Method)

  • 안상호;김주연;김규철
    • 한국자동차공학회논문집
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    • 제6권1호
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    • pp.122-133
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    • 1998
  • This paper presents the static analysis, the modal analysis and the forced vibration analysis on engine structures to find out the structure-borne noise sources by finite element method. The deformation of engine structures under the maximum combu- stion gas force was calculated through the static analysis, and the resonance possibilities were predicted by the modal analysis which ascertains mode shapes and the corresponding frequencies of engine global and its major noise sources in engine surfaces were investigated with the forced vibration analysis by means of finding the transfer mobilities on engine surfaces due to the piston impact and the velocity levels due to the combustion in consideration of oil film stiffness and damping coefficients. Finally, the direction of engine structure-borne noise reduction can be estabilished by the above-mentioned analysis procedure and the reduction effect of cost on proto-type engine build-up is expected.

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