• 한국자동차공학회논문집
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• 제19권5호
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• pp.51-57
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• 2011

Parametric studies based on analysis of lubrication system of a four cylinder gasoline engine are illustrated system in this paper. In development process of engine lubrication system, parts of failure cases are related with oil pull over and oil churning phenomenon. The crankcase & head system pressure by oil churning phenomenon are gradual increased. It cause oil pull over phenomenon at engine breather line and oil over-consumption. In order to improve oil reduction and oil pull over phenomenon are also considered in the developing state. For this study, the characteristics of engine lubrication system are measured at various tilting angle and drain hole sizes. In addition, the oil flow & oil quantity are tested by blow by meter and catch jar. Results are presented to stabilize the oil supply system at sever driving condition. The data from present study are available for the engine lubrication system.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2001년도 제33회 춘계학술대회 개최
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• pp.224-230
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• 2001

A numerical analysis for the gas lubricated flexure-pivot tilting pad journal bearing has been accomplished. The film pressure are obtained by Newton-Raphson method and the dynamic coefficients are evaluated by the pad assembly method. The effects of the pivot position of the pad on the static and dynamic characteristics are presented for three pads journal bearing with LBP. The optimum pivot positions for the static performance is different from that of the dynamic performance.

• 한국가스학회지
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• 제25권4호
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• pp.27-35
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• 2021

최근 "전력 예비율" 급감에 대한 해결책으로 양방향 송배전이 가능한 마이크로 그리드로 전환되고 있다. 마이크로 그리드는 소규모 분산전원과 부하로 구성되는데, 분산전원의 대표적인 기술로 가정·건물에 적용하는 소형 열병합 발전시스템이 있다. 본 연구에서 가스 소비량 232.6kW(20만 kcal/h) 이내의 소형 가스엔진 발전시스템의 안전기준을 도출하고 발전 시스템, 냉각시스템, 윤활 시스템, 배기 시스템으로 구분하여 안전기준(안)을 개발하였다. 발전시스템의 경우 필터를 설치하고 가스 누출 및 엔진 회전수나 출력에 이상이 발생할 경우 이를 감지하여 시스템이 정지하도록 하였고, 냉각시스템은 냉각수 부족이나 과열이 발생할 경우 시스템이 정지하도록 규정하였다. 윤활 시스템은 윤활유의 압력과 온도를 모니터링 하고 이상이 발생할 경우 시스템을 정지하도록 하고, 배기 시스템은 국내·외 기준과 부합하여 배기가스 배출 농도 규제 값을 지정하였다. 본 연구 결과를 통해 가스엔진 발전시스템의 안전성을 향상시키고 제품 확산·보급에 이바지할 수 있다고 판단한다.

• 대한기계학회논문집A
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• 제24권9호
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• pp.2159-2166
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• 2000

Recently, high performance machining center requires special type of sealing mechanism that prevent a leakage of oil jet or oil mist lubrication system. Sealing of oil-air mixture plays important r oles to have an enhanced lubrication for performance machining center. Current work emphasizes on investigations of the air jet effect on the protective collar type labyrinth seal. To improve sealing capabilities of conventional labyrinth seals, air jet is injected against the leakage flow. In this study, an adapted model is introduced to improve sealing capability of conventional non-contact type seals. It has a combined geometry of a protective collar type and an air jet type. Both of a numerical analysis by CFD (Computational Fluid Dynamics) and experimental measurements are carried out to verify sealing improvement. The sealing effects of the leakage clearance and the air jet magnitude aic studied in various parameters. Gas or liquid has been used as a working fluid for most of nori-contact types seals including the labyrinth seal. However, it is more reasonable to regard two-phase flows because oil mist or oil jet are used for high performance spindle's lubrication. In this study, working fluid is regarded as two phases that are mixed flow of oil and air phase. Both of turbulence and compressible flow model are also introduced in a CFD analysis to represent an isentropic process. Estimation of non-leaking property is determined by amount of pressure drop in the leakage path. Results of pressure drop in the experiment match reasonably to those of the simulation by introducing a flow coefficient. Effect of the sealing improvement is explained as decreasing of leakage clearance by air jetting. Thus, sealing effect is improved by amount of air jetting even though clearance becomes larger

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제31회 추계학술대회논문집
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• pp.424-426
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• 2008

초소형 가스터빈에 사용되는 소형 고속 구름베어링의 연료윤활 특성을 실험적으로 조사하였다. 윤활유로는 항공용 가스터빈에서 사용되는 MIL-PRF-7808 터빈오일과 항공용 가스터빈의 추진연료로 사용되는 JP-8 연료를 사용하여 운용특성을 비교하였고, 시험용 베어링으로는 내경 17 mm의 깊은 홈(deep groove) ball bearing과 내경 20 mm의 원통형(cylindrical) roller bearing을 사용하였다. 베어링의 연료윤활에 따른 특성을 비교하기 위하여 오일 및 연료를 공급하며 고속베어링 시험을 수행할 수 있는 시험 장치를 개발하여 하중, 냉각공기 온도, 윤활유량 및 회전속도를 변화시키면서 시험을 수행하였다. 30,000 rpm에서 70,000 rpm까지 회전속도를 변화시키면서 시험한 결과 깊은 홈 볼베어링은 축하중과 회전속도가 증가하는 경우 베어링 케이지에 마모가 발생하였으며 마모상태는 오일윤활보다 연료윤활시 마모가 더 많이 발생하였고 본 베어링의 속도한계인 59,000 rpm까지는 연료 윤활로 운용이 가능하다는 것을 확인할 수 있었다. 연료윤활의 경우가 오일윤활의 경우보다 베어링 온도가 더 낮은 것을 알 수 있었는데 이는 베어링의 냉각특성이 연료윤활인 경우가 오일윤활의 경우보다 더 좋기 때문이라 판단된다. 본 실험을 통하여 소형 항공용 가스터빈의 주축 베어링 윤활방식으로 연료윤활 방식이 적용 가능함을 확인할 수 있었다.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2000년도 제31회 춘계학술대회
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• pp.201-210
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• 2000

The noncontacting groove end face seal is one of various approaches to sealing gases with a single seal. Gas pumped into groove maintains operating gap and lubricates between primary ring and mating ring. So it removes heat and decreases face wear. In this paper, K-type and T-type grooved seals have been analyzed numerically using the finite element method. It explains the effects of groove shapes in gas seals along rotating speeds with a temperature gradient, face distortion, stress and so on. The calculated FEM results show the operating gap and rotating speed are strongly related to the leakages of a gas seal and that T-type groove seal shows a good thermal performance compared to K-type groove seal.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2002년도 proceedings of the second asia international conference on tribology
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• pp.103-104
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• 2002

The influence of the slip flow on the MEMS/MST based gas-lubricated proceeding bearing is investigated. Based on the modified Reynolds equation, the numerical analysis of the finite difference method was developed by applying the first order slip flow approximation. The numerical prediction of bearing performance provides the significant results concerning the slip flow effect in micro scale gas-lubricated proceeding bearing. The result indicates that the load-carrying capacity as well as the rotordynamic coefficients were significantly reduced due to the slip flow. Through this work, it is concluded that the slip flow effect could not be ignored in the micro gas-lubricated proceeding bearing.

• 한국전산유체공학회지
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• 제14권1호
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• pp.86-95
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• 2009

A kinetic theory analysis is used to study the ultra-thin gas flow field in gas bearings. The Boltzmann equation simplified by a collision model is solved by means of a finite difference approximation with the discrete ordinate method. Calculations are made for flows inside micro-channels of backward-facing step, forward-facing step, and slider bearings. The results are compared well with those from the DSMC method. The present method does not suffer from statistical noise which is common in particle based methods and requires less computational effort.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2001년도 제34회 추계학술대회 개최
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• pp.273-281
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• 2001

Feasibility study of gas-lubricated bearing in micro gas turbine was performed. Based on Reynolds equation, finite difference method with coupled boundary was developed to analyze bearing characteristics, such as load-carrying capacity, mass flow rates and stiffness. By the bearing force and mass flow rates analysis with the variation of supply pressure, bearing clearance and capillary radius, acceptable range of design parameters were suggested in terms of load capacity and stiffness of bearings. Additionally, coupled boundary effect on pressure distribution was investigated and it is stated that coupling could reduce all excitation force due to narrow pressure distribution.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2000년도 제32회 추계학술대회 정기총회
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• pp.243-249
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• 2000

In case of the limitation of Deep RIE fabrication for Micro Gas Turbine, bearing aspect ratio is limited in very small value. The characteristics such as pressure distribution load capacity and non-linearity of a short bearing of L/D=0.083 and a conventional bearing of L/D=1.0 with coupled boundary effects are investigated far Micro Gas Tlubine bearings. The coupled efffect was analyzed by mass conservation at coupled end area. The results, increasing load capacity and non-linearity due to the coupled effect of thrust and journal bearing, are obtained and the selection of journal bearing type is discussed.