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dc.contributor.authorSan Andrés, Luis
dc.contributor.authorDuran-Castillo, Azael
dc.contributor.authorJauregui, Juan
dc.contributor.authorde Santiago, Oscar
dc.contributor.authorLubell, Daniel
dc.date.accessioned2024-12-24T18:51:05Z
dc.date.available2024-12-24T18:51:05Z
dc.date.copyright11/3/2023 12:00:00 AM
dc.date.issued2023
dc.identifier.issn0742-4795
dc.identifier.othergtp_146_03_031004.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302865
dc.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.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleMeasurement of Temperature and Load Versus Bearing Displacement in a Thrust Foil Bearing: Differences Between Light Load and High Load Operation
dc.typeJournal Paper
dc.journal.volume146
dc.journal.issue3
dc.journal.titleJournal of Engineering for Gas Turbines and Power
dc.identifier.doi10.1115/1.4063545
dc.journal.fristpage31004-1
dc.journal.lastpage31004-11
dc.page11
dc.treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 003
dc.contenttypeFulltext


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