Measurement of Temperature and Load Versus Bearing Displacement in a Thrust Foil Bearing: Differences Between Light Load and High Load OperationSource: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 003::page 31004-1Author:San Andrés, Luis
,
Duran-Castillo, Azael
,
Jauregui, Juan
,
de Santiago, Oscar
,
Lubell, Daniel
DOI: 10.1115/1.4063545Publisher: 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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| contributor author | San Andrés, Luis | |
| contributor author | Duran-Castillo, Azael | |
| contributor author | Jauregui, Juan | |
| contributor author | de Santiago, Oscar | |
| contributor author | Lubell, Daniel | |
| date accessioned | 2024-12-24T18:51:05Z | |
| date available | 2024-12-24T18:51:05Z | |
| date copyright | 11/3/2023 12:00:00 AM | |
| date issued | 2023 | |
| identifier issn | 0742-4795 | |
| identifier other | gtp_146_03_031004.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4302865 | |
| description 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. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Measurement of Temperature and Load Versus Bearing Displacement in a Thrust Foil Bearing: Differences Between Light Load and High Load Operation | |
| type | Journal Paper | |
| journal volume | 146 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4063545 | |
| journal fristpage | 31004-1 | |
| journal lastpage | 31004-11 | |
| page | 11 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 003 | |
| contenttype | Fulltext |