• Title/Summary/Keyword: Leaf type foil bearing

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A study on hydrostatic characteristics of air-lubricated journal bearing using multi-leaf type foils (다엽형상의 포일을 사용한 공기 저널 베어링의 정특성에 관한 연구)

  • 김태호;이용복;김창호;이남수;장건희
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 2000.11a
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    • pp.177-185
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    • 2000
  • The characteristics of multi-leaf feil bearing are investigated. The Foil bearing is preloaded and has several leaf foils modeled by curved beams. An analysis of the air foil bearing was performed, considering effects of foil deflection and compressible lubrication equation simultaneously. A parametric study shows that the number of foils significantly affect the static characteristics of air foil bearings and describes what the minimum film thickness means. The results include pressure profile, load capacity, dimensionless torque and minimum film thickness in the foil bearing.

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Internal Flow Characteristic Analysis and Deformation of Foil Considering Slip between Foils (Foil사이의 미끄러짐을 고려한 Foil Bearing변형 및 내부유동특성해석)

  • Lee, S.H.;Won, C.S.;Hur, N.;Jeon, S.B.
    • 유체기계공업학회:학술대회논문집
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    • 2001.11a
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    • pp.482-487
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    • 2001
  • Leaf type foil bearings have been used successfully in many aerospace applications such as air cycle machines, turbocompressors and turboexpander. These applications are characterized by light loads, constant speeds and low to moderate temperatures. But, as system on start-up or shutdown, sliding contact between the shaft and foil surfaces cause wear. So, in present study, to understand pressure-flow characteristics and deformation of foil bearing, flow/structure interaction analysis was used. and using this method, 2D and 3D calculation was peformed for shape of foil bearing to know circumferential direction flow and leakage flow characteristics of axial direction.

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An Analysis of Characteristics of Air-Lubricated Foil Journal Bearings (공기윤활 포일 베어링의 특성해석)

  • 김종수;이준형;최상규
    • Tribology and Lubricants
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    • v.17 no.2
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    • pp.97-108
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    • 2001
  • This paper describes the development of performance analysis technique for a leaf-type gas lubricated fail bearing. Stiffness coefficient and frictional damping due to the slip between all contacts of leaves are evaluated for various leaf structures. The fluid film thickness and pressure distribution are computed but it is not considered the elastic deformation by film pressure. The analysis results include the effects that the curvature radius and the length of leaf and the friction coefficient have on the static and dynamic characteristics of the foil bearings.

Development of Air Foil Bearing for High Speed Generator (고속 발전기용 Air Foil Bearing 개발)

  • 염병용;박희용;백기영;이영섭;김명섭
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.11a
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    • pp.349-353
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    • 2001
  • An air foil bearing is developed for the high speed generator. The bearing is type of multi-leaf and is stable on 60,000RPM. The vibration level is 12um(p-p) and the highest temperature level is below 100$^{\circ}C$. The dynamic parameter of air foil bearing is acquired by experimental method using exciter. The air foil bearing is also good condition at test of real generator and load condition. The condition of foil is very good after 3,000cycle start-stop test. Therefore the air foil bearing is ideal for high speed, light weight and modem turbo-machinery.

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A test on passing through bending critical speed of Flexible Rotor supported by AFB (AFB으로 지지된 탄성회전체의 위험속도 통과시험)

  • 이영섭;염병용;김진형;김명섭
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.11a
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    • pp.354-359
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    • 2001
  • A flexible rotor was smoothly passed through its bending critical speed, which is supported by AFB. Then, maximum magnitude of the rotor vibration at the middle point was 25${\mu}$m. The test rig was largely consisted of air turbine, multi-leaf type air foil bearing and flexible rotor and its bending critical speed was 32,600 rpm. And the balancing system and method for field balancing of the flexible rotor were developd successfully.

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