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Measurements of Drag Torque, Lift-Off Journal Speed, and Temperature in a Metal Mesh Foil Bearing

Authors
Andres, Luis-SanChirathadam, Thomas AbrahamRyu, KeunKim, Tae Ho
Issue Date
Nov-2010
Publisher
ASME
Keywords
Frictional loss; Maintenance intervals; Torque; Reduced systems; Helicopter rotors; Turbomachinery; Rotordynamic; Static loads; Drag torque; Extreme temperatures; Hydrodynamic gas; Load capacity; Gas turbines; Solid lubricants; Continuous operation; Gas l
Citation
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, v.132, no.11, pp 1 - 7
Pages
7
Indexed
SCI
SCIE
SCOPUS
Journal Title
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME
Volume
132
Number
11
Start Page
1
End Page
7
URI
https://scholarworks.bwise.kr/erica/handle/2021.sw.erica/39426
DOI
10.1115/1.4000863
ISSN
0742-4795
1528-8919
Abstract
Metal mesh foil bearings (MMFBs) are a promising low cost gas bearing technology for high performance oil-free microturbomachinery. Elimination of complex oil lubrication and sealing system by deploying MMFBs in rotorcraft gas turbine engines offers distinctive advantages such as reduced system weight, enhanced reliability at high rotational speeds and extreme temperatures, and extended maintenance intervals compared with mineral oil lubricated bearings. MMFBs for oil-free rotorcraft engines must demonstrate adequate load capacity, reliable rotordynamic performance, and low frictional losses in a high temperature environment. The paper presents the measurements of MMFB breakaway torque, rotor lift-off and touchdown. speeds, and temperature at increasing static load conditions. The tests, which were conducted in a test rig driven by an automotive turbocharger turbine, demonstrate the airborne operation (hydrodynamic gas film) of the floating test MMFB with little frictional loses at increasing loads. The measured drag torque peaks when the rotor starts and stops, and drops significantly once the bearing lifts off The estimated rotor speed for lift-off increases linearly with the applied static load. During continuous operation, the MMFB temperature measured at the back surface of the top foil increases both with rotor speed and static load. Nonetheless, the temperature rise is mild, demonstrating reliable performance. Application of a sacrificial layer of solid lubricant on the top foil surface reduces the rotor break-away torque. The measurements give confidence on this simple bearing technology for ready application into oil-free turbomachinery. [DOI: 10.1115/1.4000863]
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ERICA 공학대학 (DEPARTMENT OF MECHANICAL ENGINEERING)
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