This paper presents the dynamic behavior of a 225 kW class (300 HP), 60,000 rpm, permanent magnet synchronous (PMS) motor–generator system supported on gas foil bearings (GFBs). The rotor of a 225 kW PMS motor is supported by two identical gas foil journal bearings (GFJBs) and one pair of gas foil thrust bearings (GFTBs). The total weight and axial length of the coupled rotors are 272 N and 1042 mm, respectively. During the speed-up test to 60,000 rpm, unexpected large subsynchronous rotor motions appear at around 120–130 Hz above 35,040 rpm. After disassembling the motor, an inspection of the top foils of the GFJBs reveals significant rotor rubbing. Thus, the GFJBs are redesigned to have a smaller load capacity by reducing their axial length to 45 mm. In addition, three 50 μm thick shims are installed in the GFJBs at 120 deg intervals for reducing the swirl speed of air and producing bearing preloads. The modification delays the onset speed of subsynchronous motions to 43,200 rpm and decreases the amplitude of the subsynchronous motions from 20 to 15 μm. These results indicate that the modification improves the stability margin of the high-speed rotor system with increasing stiffness and damping. In addition, the logarithmic decrement trends are in good agreement with the test results.

References

1.
Heshmat
,
H.
,
Walowit
,
J. A.
, and
Pinkus
,
O.
,
1983
, “
Analysis of Gas Lubricated Compliant Thrust Bearings
,”
ASME J. Tribol.
,
105
(
4
), pp.
638
646
.10.1115/1.3254696
2.
Agrawal
,
G. L.
,
1997
, “
Foil Air/Gas Bearing Technology—An Overview
,”
ASME
Paper No. 97-GT-347.10.1115/97-GT-347
3.
Dellacorte
,
C.
, and
Valco
,
M. J.
,
2000
, “
Load Capacity Estimation of Foil Air Journal Bearings for Oil-Free Turbomachinery Applications
,”
STLE Tribol. Trans.
,
43
(
4
), pp.
795
801
.10.1080/10402000008982410
4.
DellaCorte
,
C.
,
Radil
,
K.
,
Bruckner
,
R.
, and
Howard
,
S.
,
2007
, “
Design, Fabrication and Performance of Open Source Generation I and II Compliant Hydrodynamic Gas Foil Bearings
,” NASA Glenn Research Center, Cleveland, OH, Report No. NASA/TM-2007-214691.
5.
Heshmat
,
H.
,
1994
, “
Advancements in the Performance of Aerodynamic Foil Journal Bearings: High Speed and Load Capacity
,”
ASME J. Tribol.
,
116
(
2
), pp.
287
294
.10.1115/1.2927211
6.
Kim
,
T. H.
, and
San Andrés
,
L.
,
2007
, “
Analysis of Advanced Gas Foil Bearings With Piecewise Linear Elastic Supports
,”
Tribol. Int.
,
40
(
8
), pp.
1239
1245
.10.1016/j.triboint.2007.01.022
7.
Kim
,
T. H.
, and
San Andrés
,
L.
,
2009
, “
Effects of a Mechanical Preload on the Dynamic Force Response of Gas Foil Bearings: Measurements and Model Predictions
,”
STLE Tribol. Trans.
,
52
(
4
), pp.
569
580
.10.1080/10402000902825721
8.
Heshmat
,
H.
, and
Walton
,
J. F.
,
2007
, “
On the Coupling of Foil Bearing Supported Rotors: Part 1—Analysis
,”
ASME
Paper No. GT2007-27821.10.1115/GT2007-27821
9.
Heshmat
,
H.
, and
Walton
,
J. F.
,
2007
, “
On the Coupling of Foil Bearing Supported Rotors: Part 2—Experiment
,”
ASME
Paper No. GT2007-27825.10.1115/GT2007-27825
10.
Lee
,
Y. B.
,
Jo
,
S. B.
,
Kim
,
T. Y.
,
Kim
,
C. H.
, and
Kim
,
T. H.
,
2010
, “
Rotordynamic Performance Measurement of an Oil-Free Turbocompressor Supported on Gas Foil Bearings
,”
IFToMM 8th International Conference on Rotor Dynamics
,
Seoul, South Korea
, Sept. 12–15, pp.
372
378
.
11.
Axis, 2010, Rapp User Manual
, Axis Communications AB, Lund, Sweden, http://www.nongnu.org/rapp/doc/rapp/, last accessed Nov. 14, 2011.
You do not currently have access to this content.