NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A New Foil Air Bearing Test Rig for Use to 700 C and 70,000 rpmA new test rig has been developed for evaluating foil air bearings at high temperatures and speeds. These bearings are self acting hydrodynamic air bearings which have been successfully applied to a variety of turbomachinery operating up to 650 C. This unique test rig is capable of measuring bearing torque during start-up, shut-down and high speed operation. Load capacity and general performance characteristics, such as durability, can be measured at temperatures to 700 C and speeds to 70,000 rpm. This paper describes the new test rig and demonstrates its capabilities through the preliminary characterization of several bearings. The bearing performance data from this facility can be used to develop advanced turbomachinery incorporating high temperature oil-free air bearing technology.
Document ID
19970010249
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
DellaCorte, Chris
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Subject Category
Mechanical Engineering
Report/Patent Number
E-10493
NAS 1.15:107405
NASA-TM-107405
Meeting Information
Meeting: 1997 Tribology Conference
Location: London
Country: United Kingdom
Start Date: September 8, 1997
End Date: September 12, 1997
Sponsors: American Society of Mechanical Engineers, Society of Tribologists and Lubrication Engineers
Accession Number
97N15453
Funding Number(s)
PROJECT: RTOP 523-22-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available