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    Measurement of Temperature and Load Versus Bearing Displacement in a Thrust Foil Bearing: Differences Between Light Load and High Load Operation

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 003::page 31004-1
    Author:
    San Andrés, Luis
    ,
    Duran-Castillo, Azael
    ,
    Jauregui, Juan
    ,
    de Santiago, Oscar
    ,
    Lubell, Daniel
    DOI: 10.1115/1.4063545
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a test rig for evaluation of gas thrust foil bearings (GTFBs) and details measurements of load capacity conducted with a commercial GTFB comprising a single 360 deg, 0.127 mm thick top foil divided into six continuous arc segments with a formed taper of 0.102 mm. Coated with Teflon®, the top foil rests on a stack of shims above six underspring structures, each comprising three strips of bump foils, 0.102 mm thick. Measurements include the applied static load and break-away torque, rotor speed, bearing axial displacements at three locations 120 deg apart, the flow of a cooling stream, and temperatures in and out of the bearing. Static load tests produce the underspring deformation and a dry-sliding friction coefficient f ∼ 0.12. The underspring is rather flexible though quickly hardening for specific load (P*) > 25 kN/m2 to reach an ultimate deformation of ∼0.320 mm. Measurements at 30 krpm (OD surface speed = 111 m/s) and increasing static loads produce bearing displacements that parallel the displacements without shaft rotation. Most importantly, the difference between displacements approaches ∼0.060 mm for P* > 45 kN/m2. The test bearing operated safely to P* = 90 kN/m2 and failed at P* = 120 kN/m2. When heavily loaded, the GTFB is significantly stiffer than when lightly loaded. Designed for easiness of installation and operation, the test bearing demonstrated a stable and repeatable performance with likely a uniform gap or film thickness even for the largest loads applied.
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      Measurement of Temperature and Load Versus Bearing Displacement in a Thrust Foil Bearing: Differences Between Light Load and High Load Operation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4302865
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    contributor authorSan Andrés, Luis
    contributor authorDuran-Castillo, Azael
    contributor authorJauregui, Juan
    contributor authorde Santiago, Oscar
    contributor authorLubell, Daniel
    date accessioned2024-12-24T18:51:05Z
    date available2024-12-24T18:51:05Z
    date copyright11/3/2023 12:00:00 AM
    date issued2023
    identifier issn0742-4795
    identifier othergtp_146_03_031004.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302865
    description abstractThis paper presents a test rig for evaluation of gas thrust foil bearings (GTFBs) and details measurements of load capacity conducted with a commercial GTFB comprising a single 360 deg, 0.127 mm thick top foil divided into six continuous arc segments with a formed taper of 0.102 mm. Coated with Teflon®, the top foil rests on a stack of shims above six underspring structures, each comprising three strips of bump foils, 0.102 mm thick. Measurements include the applied static load and break-away torque, rotor speed, bearing axial displacements at three locations 120 deg apart, the flow of a cooling stream, and temperatures in and out of the bearing. Static load tests produce the underspring deformation and a dry-sliding friction coefficient f ∼ 0.12. The underspring is rather flexible though quickly hardening for specific load (P*) > 25 kN/m2 to reach an ultimate deformation of ∼0.320 mm. Measurements at 30 krpm (OD surface speed = 111 m/s) and increasing static loads produce bearing displacements that parallel the displacements without shaft rotation. Most importantly, the difference between displacements approaches ∼0.060 mm for P* > 45 kN/m2. The test bearing operated safely to P* = 90 kN/m2 and failed at P* = 120 kN/m2. When heavily loaded, the GTFB is significantly stiffer than when lightly loaded. Designed for easiness of installation and operation, the test bearing demonstrated a stable and repeatable performance with likely a uniform gap or film thickness even for the largest loads applied.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMeasurement of Temperature and Load Versus Bearing Displacement in a Thrust Foil Bearing: Differences Between Light Load and High Load Operation
    typeJournal Paper
    journal volume146
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4063545
    journal fristpage31004-1
    journal lastpage31004-11
    page11
    treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 003
    contenttypeFulltext
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