• 제목/요약/키워드: Bearing Design

검색결과 2,033건 처리시간 0.029초

초소형 가스 터빈용 스러스트 베어링 내의 유동특성 해석 (ANALYSIS OF FLUID CHARACTERISTICS OF THRUST BEARING ON MILLIMETER-SCALE MICRO GAS TURBINE)

  • 서준혁;백제현
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2010년 춘계학술대회논문집
    • /
    • pp.258-262
    • /
    • 2010
  • Since MEMS based micro actuators or generating devices showed high efficiency per volume, plenty of research are ongoing. Among them, MEMS based millimeter-scale micro gas turbine is one of the most powerful item for replacing chemical batteries. However, due to MEMS manufacturing technique, it is very difficult that makes wide turbine bearing area. It causes low DN number, so sufficient bearing force is hard to achieve. Thus, the most important issue on micro gas turbine is to design the proper bearing which can keep rotor stable during operation. In order to that, micro-scale gas-lubricated bearing is generally used. In this paper, basic feasibility study of thrust bearing of 10mm diameter turbine is described. Thrust bearing is hydrostatic gas-lubricated type. Numerical simulation is performed with ANSYS CFX 11.0 which is commercial numerical tool. Relationship between bearing inlet pressure and mass flow rate and bearing force is figured while changing bearing gap and number of capillaries. The simulation results will be used for further design of micro gas turbine.

  • PDF

선박 추진축 선미 베어링 압력 분포 해석 (Pressure Distribution Analysis for After Bush Bearing of Ship Propulsion Shaft)

  • 신상훈;최익흥
    • 대한조선학회논문집
    • /
    • 제41권3호
    • /
    • pp.35-40
    • /
    • 2004
  • Since the scale of vessels is growing up recently, some troubles between the shaft and after bush bearing are frequently reported. Generally, mean pressure on bush bearing is used as a design criterion. However, in some case of the long bearing such as after bush bearing of the propulsion shaft, it might be liable to be locally under high pressure. As for the main engine bearings and the intermediate shaft bearing, it is reasonable to take the mean pressure as a design criterion. But, in case of after bush bearing, it is not sufficient because of the possibility of high pressure caused by local contact. In this study, Hertzian contact condition was applied to evaluation of the local pressure for after bush bearing. To reduce the local maximum pressure, the height of the after bush bearing was controlled. It was found that local maximum pressure could be reduced effectively by taking a partial slope on the white metal of the aft bush bearing.

A Study on Indicial Response Characteristics of a Gas-Lubricated Spiral-Grooved proceeding Bearing

  • Yabe, H.;Kaneshiro, T.;Hirayama, T.
    • 한국윤활학회:학술대회논문집
    • /
    • 한국윤활학회 2002년도 proceedings of the second asia international conference on tribology
    • /
    • pp.101-102
    • /
    • 2002
  • Indicial response characteristics of a rotor supported by a gas-lubricated, spiral-grooved proceeding bearing are studied theoretically to develop a fundamental investigation for the bearing design with considering NRRO characteristics. The trajectory of rotor movement is calculated by applying the non-linear orbit scheme against a prescribed impulse load, then two characteristic quantities are introduced to evaluate the indicial response performance of the bearing, i.e., 'maximum deviation of rotor center' and 'integrated rotor center deviation'. The effects of some design parameters of spiral grooves to these representative quantities are studied so that 'robust' design against impulse load is discussed.

  • PDF

레이디얼 볼베어링의 내륜 끼워맞춤에 관한 유한요소해석 (Finite Element Analysis on the Shaft Fitting to Inner Raceway of Radial Ball Bearing)

  • 고병두;이하성
    • Design & Manufacturing
    • /
    • 제6권1호
    • /
    • pp.45-51
    • /
    • 2012
  • The main goal of this paper is to establish an interference tolerance for determining optimal amount of clearance in the shaft-bearing system supported by radial ball bearings. The 2-D frictional contact model was employed for the FE analysis between the shaft and the inner raceway. Several examples were simulated using different material properties for the solid shaft. Efforts were focused on the deformation applied in the radial direction to select suitable bearings. The analysis results showed that the initial axial preload applied on the bearings plays a significant role to reduce bearing fatigue life. The proposed design parameters obtained by numerical simulations can approximately predict a rate of bearing life reduction as a function of shaft diameter ratio. This analysis can also be used to calculate the optimal initial radial clearance in order to obtain a shaft-bearing system design for high accuracy and long life.

  • PDF

철도노반 침하저감을 위한 토목섬유 감쌈 쇄석말뚝 설계방안 고찰 (A Study on Design Method of Geogrid Encased Stone Colum for Settlement Reduction in Railroad)

  • 이대영
    • 한국지반신소재학회논문집
    • /
    • 제13권3호
    • /
    • pp.31-38
    • /
    • 2014
  • 지오그리드 감쌈 쇄석말뚝 공법은 지오그리드의 인장구속효과로 인해 연약지반에 시공된 쇄석말뚝의 지지력을 증가시켜주는 공법이다. 본 연구에서는 토목섬유 감쌈 쇄석말뚝(GESC)공법의 설계에 적용할 수 있는 토목섬유 인장저항력과 극한지지력을 산정할 수 있는 합리적인 설계법을 제안하였다. 제안된 설계방법의 적적성을 평가하기 위해 부산 경전선 연약지반 시험시공 결과로부터 산출된 GESC의 극한지지력과 설계법에의해 산정된 극한지지력을 비교 검증하였다. 연구결과 GESC 설계법에 의해 산정된 지지력이 현장시험의 지지력 보다 크게 나타나는 것으로 검토되었다.

부상특성 향상을 위한 극소 공기윤활막을 지닌 헤드 슬라이더의 형상 최적 설계 (Optimum Design of Head Slider with Ultra-Thin Air-Lubricated Spacing for Enhanced Flying Characteristics)

  • 강태식;최동훈;정태건;박노열;이성창
    • 대한기계학회논문집A
    • /
    • 제25권4호
    • /
    • pp.725-733
    • /
    • 2001
  • Flying attitudes of the slider, which are flying height, pitch and roll, are affected by the air flow velocity, the skew angle, and the manufacturing tolerances. Traditional designs of the air bearing surface have considered only the flying performances for the variations in the air flow velocity and the skew angle, which are determined by the radial position. In this study, we present the new shape design of the air bearing surface by considering the track seek performance and the air bearing stiffness as well as the traditional design requirements. The optimization technique is used to improve the dynamic characteristics and operating performance of the newly proposed air bearing surface shape design further. The optimized configuration is obtained automatically and the optimally designed sliders show the enhanced flying and dynamic characteristics.

공작기계용 고속 볼베어링의 최적 끼워맞춤에 관한 연구 (A Study on the Optimum Shrink-fit for High Speed Ball Bearing of Machine Tool)

  • 김웅;이춘만;황영국
    • 한국정밀공학회지
    • /
    • 제27권9호
    • /
    • pp.94-102
    • /
    • 2010
  • The spindle is the main component in machine tools. To develop high speed machine tools, a lot of studies have been carried out for high speed spindle. Bearing is very important part in spindle. The bearing clearance is influenced by shrink fit and thermal expansion during operation. The designer must take into account the reduction of shrink fits. The aims of this study are to grasp the shrink fits and behavior of a bearing which is a deeply connected with fatigue life of bearing and performance of spindle through FEM(Finite Element Method). This paper proposed optimum value of shrink fit considering deformation of spindle and stress of fitting area using design of experiments. Thus, the proposed formula can be used to obtain bearing internal clearance.

초고속 원심분리 회전축계의 최적설계 (An Optimum Design of a Rotor-Bearing Spindle System for a Ultra Centrifuge)

  • 김종립;윤기찬;박종권
    • 한국정밀공학회지
    • /
    • 제15권6호
    • /
    • pp.145-152
    • /
    • 1998
  • This paper presents an optimum design of a rotor-bearing spindle system for a ultra centrifuge (80,000 RPM) supported by ball bearings with nonlinear stiffness characteristics. To obtain the nonlinear bearing stiffnesses, a ball bearing is modeled in five degrees of freedom and is analyzed quasi-statically. The dynamic behaviors of the nonlinear rotor-bearing system are analyzed by using a transfer-matrix method iteratively. For optimization. we use the cost function that simultaneously minimizes the weight of a rotor and maximizes the separation margins to yield the critical speeds as far from the operating speed as possible. Augmented Lagrange Multiplier (ALM) method is employed for the nonlinear optimization problem. The result shows that the rotor-bearing spindle system is optimized to obtain 9.5% weight reduction and 21% separation margin.

  • PDF

교량용 탄성받침의 설계압축응력에 대한 고찰 (The Design Criteria of Elastomeric Bearing for Highway Bridges)

  • 전규식
    • 한국지진공학회:학술대회논문집
    • /
    • 한국지진공학회 1998년도 추계 학술발표회 논문집 Proceedings of EESK Conference-Spring 1998
    • /
    • pp.136-143
    • /
    • 1998
  • Elastomeric bearing is used as one of the most useful way for isolation structures, because the horizontal stiffness is much lower than the vertical stiffness. The quality of Elastomeric bearing depends on the vulcanization procedure to manufacture, which produces the elasticity of the rubber from the compound of rubber and sulphur. The durability of Elastomeric bearing is affected by the deterioration due to ozone and ultra-violet attack. but the durability during the design life of bridges can be assured by the sufficient size of the bearing in spite of the deterioration in surface. In the design criteria of Elastomeric bearing, the stability of the bearings is evaluated by shear strain due to compression, lateral displacement, and rotation. The question how soft rubber can sustain heavy structure is now able to be solved by Ultimate capacity test of Laminated elastomeric Bearings, which results 1,200kg/$\textrm{cm}^2$ of the max. compressive stress and this shows what a sufficient safety factor Elastomeric bearing has!

  • PDF

접촉해석을 이용한 볼 베어링의 Shoulder Height 설계 (Design of Shoulder Height for Ball Bearing using Contact Analysis)

  • 김태완;윤기찬;조용주
    • Tribology and Lubricants
    • /
    • 제24권5호
    • /
    • pp.228-233
    • /
    • 2008
  • In this study, the methodology for determination of shoulder height in the internal shape design of ball bearing using 3D contact analysis is proposed. The static analysis of a ball bearing was performed to calculate the distribution of applied contact load and angles among the rolling elements. From each rolling element loads and the contact geometry between ball and inner/outer raceway, 3D contact analyses using influence function are conducted. These methodology is applied to HDD ball bearing. A critical axial load and a critical shoulder height which are not affected by edge are calculated. The proposed methodology may be applied to other rolling element bearing for the purpose of reducing the material cost and improving the efficiency of the bearing design process.