The present work describes the detailed design and operational capabilities of a general purpose test facility developed to evaluate the dynamics and performance of gas lubricated journal bearings. The component level test facility was developed to serve as an initial tollgate test platform for certifying gas lubricated journal bearings into aircraft engine applications. A rotating test rig was engineered to test 70–120 mm diameter bearings at 40,000–80,000 rpm and 1200°F. The test rig described in this paper possesses design elements that enable the simultaneous application of dynamic and static load profiles of up to 1000 lb while monitoring and measuring the bearing torque. This capability allows for the characterization of several critical metrics such as bearing lift off speed characteristics, load capacity, and frequency dependent rotordynamic force coefficients. This paper discusses the functionality of the test facility and presents sample test measurements from several experiments.

1.
Spring
,
S. D.
,
Kaminske
,
M.
,
Leone
,
S.
,
Drexel
,
M. V.
,
Ertas
,
B. H.
,
Ames
,
E. C.
,
Agarwal
,
G.
,
Burr
,
D.
, and
Brophy
,
M.
, 2006, “
Application of Compliant Foil Air Bearings for Oil Free Operation of Advanced Turboshaft Engines
,”
Proceedings of the American Helicopter Society 62nd Annual Forum
, Phoenix, AZ, May 8–11, Vol.
III
, pp.
2070
2075
.
2.
Hagg
,
A. C.
, and
Sankey
,
G. O.
, 1974, “
The Containment of Disk Burst Fragments by Cylindrical Shells
,”
ASME J. Eng. Power
0022-0825,
96
, pp.
114
123
.
3.
Ertas
,
B. H.
, and
Vance
,
J. M.
, 2004, “
The Effect of Static and Dynamic Misalignment on Ball Bearing Radial Stiffness
,”
J. Propul. Power
0748-4658,
20
(
4
), pp.
634
647
.
4.
Ertas
,
B. H.
,
Al-Khateeb
,
E. M.
, and
Vance
,
J. M.
, 2002, “
Rotordynamic Bearing Dampers for Cryogenic Rocket Engine Turbopumps
,”
J. Propul. Power
0748-4658,
20
(
4
), pp.
674
682
.
5.
Heshmat
,
H.
, 1994, “
Advancements in the Performance of Aerodynamic Foil Journal Bearings; High Speed and Load Capability
,”
ASME J. Tribol.
0742-4787,
116
, pp.
287
295
.
6.
Dellacorte
,
C.
, 1997, “
A New Foil Air Bearing Test Rig for Use to 700°C and 70,000 rpm
,”
NASA
Technical Report No. TM-107405.
7.
Howard
,
S. A.
,
Dellacorte
,
C.
,
Valco
,
M. J.
,
Prahl
,
J. M.
, and
Hesmat
,
H.
, 2001, “
Steady-State Stiffness of Foil Air Journal Bearings at Elevated Temperatures
,”
Tribol. Trans.
1040-2004,
44
(
3
), pp.
489
493
.
8.
Howard
,
S. A.
,
Dellacorte
,
C.
,
Valco
,
M. J.
,
Prahl
,
J. M.
, and
Hesmat
,
H.
, 2001, “
Dynamic Stiffness and Damping Characteristics of a High Temperature Air Foil Journal Bearing
,”
Tribol. Trans.
,
44
(
4
), pp.
657
663
. 0742-4787
9.
San Andres
,
L.
, 2006, “
Hybrid Flexure Pivot-Tilting Pad Gas Bearings: Analysis and Experimental Validation
,”
ASME J. Tribol.
0742-4787,
128
, pp.
551
558
.
10.
Lee
,
Y. B.
,
Park
,
D. J.
, and
Kim
,
H.
, 2006, “
Numerical Analysis for Bump Foil Journal Bearing Considering Top Foil Effect and Experimental Investigation
,”
Proceedings of the IFToMM-Conference on Rotor Dynamics
, Vienna, Austria, Sept. 25–28, Paper No. 229.
11.
Rouvas
,
C.
, and
Childs
,
D.
, 1993, “
A Parameter Identification Methods for the Rotordynamic Coefficients of a High Reynolds Number Hydrostatic Bearing
,”
ASME J. Vibr. Acoust.
0739-3717,
115
, pp.
264
270
.
12.
Childs
,
D. W.
, and
Hale
,
K.
, 1994, “
A Test Apparatus and Facility to Identify the Rotordynamic Coefficients of High Speed Hydrostatic Bearings
,”
ASME J. Tribol.
0742-4787,
116
, pp.
337
334
.
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