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    Effect of Centrifugal Force of Gas Film on the Load Capacity of Thrust Gas Bearing

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 001::page 11006-1
    Author:
    Kim, Daejong
    DOI: 10.1115/1.4063319
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A modified Reynolds equation including centrifugal force of gas film was derived, and it was used to study the effect of gas film centrifugal force and associated streamline on the load capacity of both rigid and foil thrust bearings operating in hydrodynamic and hybrid modes. The thrust bearings have six pads with an outer diameter of 82 mm and an inner diameter of 47 mm with typical aper-flat geometry. The setup for the simulations is a single-acting air thrust bearing operating at various ambient pressures and isothermal temperature. Air was chosen for the gas film for the investigations, but the modified Reynolds equation can handle any general gas films through nondimensional parameter governing the centrifugal force. The simulations were performed with varying ambient pressure from 1 to 9 bar. The simulation results at different ambient pressures and temperatures are presented in forms of pressure profiles, streamlines, and bearing's load capacity. The bearings' load capacity becomes worse when the centrifugal force is considered at very low temperature, and the reduction of the load capacity grows more noticeable with the increase of the ambient pressure and the decrease of the ambient temperature. However, at higher temperature where centrifugal force is not large enough to create large leakage, the centrifugal force helps to redistribute the streamline to favorable way to increase the load capacity.
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      Effect of Centrifugal Force of Gas Film on the Load Capacity of Thrust Gas Bearing

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4295157
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorKim, Daejong
    date accessioned2024-04-24T22:24:19Z
    date available2024-04-24T22:24:19Z
    date copyright10/17/2023 12:00:00 AM
    date issued2023
    identifier issn0742-4795
    identifier othergtp_146_01_011006.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295157
    description abstractA modified Reynolds equation including centrifugal force of gas film was derived, and it was used to study the effect of gas film centrifugal force and associated streamline on the load capacity of both rigid and foil thrust bearings operating in hydrodynamic and hybrid modes. The thrust bearings have six pads with an outer diameter of 82 mm and an inner diameter of 47 mm with typical aper-flat geometry. The setup for the simulations is a single-acting air thrust bearing operating at various ambient pressures and isothermal temperature. Air was chosen for the gas film for the investigations, but the modified Reynolds equation can handle any general gas films through nondimensional parameter governing the centrifugal force. The simulations were performed with varying ambient pressure from 1 to 9 bar. The simulation results at different ambient pressures and temperatures are presented in forms of pressure profiles, streamlines, and bearing's load capacity. The bearings' load capacity becomes worse when the centrifugal force is considered at very low temperature, and the reduction of the load capacity grows more noticeable with the increase of the ambient pressure and the decrease of the ambient temperature. However, at higher temperature where centrifugal force is not large enough to create large leakage, the centrifugal force helps to redistribute the streamline to favorable way to increase the load capacity.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Centrifugal Force of Gas Film on the Load Capacity of Thrust Gas Bearing
    typeJournal Paper
    journal volume146
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4063319
    journal fristpage11006-1
    journal lastpage11006-13
    page13
    treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 001
    contenttypeFulltext
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