The use of gas bearings has increased over the past several decades to include microturbines, air cycle machines, and hermetically sealed compressors and turbines. Gas bearings have many advantages over traditional bearings, such as rolling element or oil lubricated fluid film bearings, including longer life, ability to use the process fluid, no contamination of the process with lubricants, accommodating high shaft speeds, and operation over a wide range of temperatures. Unlike fluid film bearings that utilize oil, gas lubricated bearings generate very little damping from the gas itself. Therefore, successful bearing designs such as foil bearings utilize damping features on the bearing to improve the damping generated. Similar to oil bearings, gas bearing designers strive to develop gas bearings with good rotordynamic stability. Gas bearings are challenging to design, requiring a fully coupled thermo-elastic, hydrodynamic analysis including complex nonlinear mechanisms such as Coulomb friction. There is a surprisingly low amount of rotordynamic force coefficient measurement in the literature despite the need to verify the model predictions and the stability of the bearing. This paper describes the development and testing of a 60,000 rpm gas bearing test rig and presents measured stiffness and damping coefficients for a 57 mm foil type bearing. The design of the rig overcomes many challenges in making this measurement by developing a patented, high-frequency, high-amplitude shaker system, resulting in excitation over most of the subsynchronous range.

1.
DellaCorte
,
C.
,
Valco
,
M. J.
,
Radil
,
K. C.
, and
Heshmat
,
H.
, 2000, “
Performance and Durability of High Temperature Foil Air Bearings for Oil-Free Turbomachinery
,” Report No. NASA/TM-2000-209187.
2.
Barnett
,
M. A.
, and
Silver
,
A.
, 1970, “
Application of Air Bearings to High-Speed Turbomachinery
,” SAE Paper No. 700720.
3.
Lubell
,
D.
,
DellaCorte
,
C.
, and
Stanford
,
M.
, 2006, “
Test Evolution and Oil-Free Engine Experience of a High Temperature Foil Air Bearing Coating
,” ASME Paper No. GT2006-90572.
4.
Lubell
,
D.
,
DellaCorte
,
C.
, and
Standford
,
M.
, 2008, “
Identification and Correction of Rotor Instability in an Oil-Free Gas Turbine
,” ASME Paper No. GT2008-50305.
5.
Bosley
,
R. W.
, 1995, “
Compliant Foil Hydrodynamic Fluid Film Radial Bearing
,” U.S. Patent No. 5,427,455.
6.
Agrawal
,
G. L.
, “
Foil Air/Gas Bearing Technology—An Overview
,” ASME Paper No. 97-GT-347.
7.
Alford
,
J. S.
, 1965, “
Protecting Turbomachinery From Self-Excited Rotor Whirl
,”
ASME J. Eng. Power
0022-0825,
87
, pp.
333
334
.
8.
Vance
,
J. M.
, and
Laudadio
,
F. J.
, 1982, “
Experiment Measurement of Alford’s Force in Axial Flow Turbomachinery
,”
Rotordynamic Instability Problems in High-Performance Turbomachinery-1982, NASA Conference
,
2250
, pp.
260
273
.
9.
Heshmat
,
H.
,
Walton
,
J. F.
,
Della Corte
,
C.
, and
Valco
,
M.
, 2000, “
Oil-Free Turbocharger Paves Way to Gas Turbine Engine Applications
,” ASME Paper No. GT2000-620.
10.
Howard
,
S.
,
DellaCorte
,
C.
,
Valco
,
M.
,
Prahl
,
J.
, and
Heshmat
,
H.
, 2001, “
Dynamic Stiffness and Damping Characteristics of a High-Temperature Air Foil Journal Bearing
,”
International Joint Tribology Conference
, Oct. 21–24.
11.
Ertas
,
B.
,
Camatti
,
M.
, and
Mariotti
,
G.
, 2009, “
A General Purpose Test Facility for Evaluating Gas Bearings
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
131
, p.
022502
.
12.
Conlon
,
M. J.
,
Dadouche
,
A.
,
Dmochowski
,
W.
,
Payette
,
R.
,
B’edard
,
J. P.
, and
Liko
,
B.
, 2009, “
Experimental Evaluation of Foil Bearing Performance: Steady-State and Dynamic Results
,” ASME Paper No. GT2009-60186.
13.
Valco
,
M. J.
, and
DellaCorte
,
C.
, 2003, “
Emerging Oil-Free Turbomachinery Technology for Military Propulsion and Power Applications
,”
Proceedings of the ARMY Sciences Conference
, Ft. Lauderdale, FL.
You do not currently have access to this content.