Oil-free turbochargers (TCs) will increase the power and efficiency of internal combustion engines, both sparking ignition and compression ignition, without engine oil lubricant feeding or scheduled maintenance. Using gas foil bearings (GFBs) in passenger vehicle TCs enables compact, lightweight, oil-free systems, along with accurate shaft motion. This paper presents extensive test measurements on GFBs for oil-free TCs, including static load-deflection measurements of test GFBs, rotordynamic performance measurements of a compressed air driven oil-free TC unit supported on test GFBs, and bench test measurements of the oil-free TC driven by a passenger vehicle diesel engine. Two configurations of GFBs, one original and the other modified with three shims, are subjected to a series of experimental tests. For the shimmed GFB, three metal shims are inserted under the bump-strip layers, in contact with the bearing housing. The installation of shims creates mechanical preloads that enhance a hydrodynamic wedge in the assembly radial clearance to generate more film pressure. Simple static load-deflection tests estimate the assembly radial clearance of the shimmed GFB, which is smaller than that of the original GFB. Model predictions agree well with test data. The discrepancy between the model predictions and test data is attributed to fabrication inaccuracy in the top foil and bump strip layers. Test GFBs are installed into a TC test rig driven by compressed air for rotordynamic performance measurements. The test TC rotor, 335 g in weight and 117 mm long, is coated with a commercially available, wear-resistant solid lubricant, Amorphous M, to prevent severe wear during start-up and shutdown in the absence of an air film. A pair of optical proximity probes positioned orthogonally at the compressor end record lateral rotor motions. Rotordynamic test results show that the shimmed GFB significantly diminishes the large amplitude of subsynchronous rotor motions arising in the unmodified GFB. Predicted synchronous rotor amplitudes and rigid body mode natural frequencies agree reasonably well with recorded test data. Finally, the oil-free TC is installed into a passenger vehicle diesel engine test bench. The TC rotor speed is controlled by the vehicle engine. Speed-up tests show dominant synchronous motion (1X) of the rotor. Whirl frequencies of the relatively small subsynchronous motions are associated with the rigid body natural mode of the TC rotor-GFB system as well as (forced) excitation from the four-cylinder diesel engine. The bench test measurements demonstrate a significant reduction in the amplitude of subsynchronous motions for the shimmed GFB, thus verifying the preliminary test results in the TC test rig driven by compressed air.

References

1.
Holt
,
C.
, San
Andres
,
L.
,
Sahay
,
S.
,
Tang
,
P.
,
La Rue
,
G.
, and
Gjika
,
K.
, 2005, “
Test Response and Nonlinear Analysis of a Turbocharger Supported on Floating Ring Bearings
,”
ASME J. Vibr. Acoust.
,
127
, pp.
107
115
.
2.
San Andres
,
L.
,
Rivadeneira
,
J. C.
,
Gjika
,
K.
,
Groves
,
C.
, and
LaRue
,
G.
, 2007, “
Rotordynamics of Small Turbochargers Supported on Floating Ring Bearings – Highlights in Bearing Analysis and Experimental Validation
,”
ASME J. Tribol.
,
129
, pp.
391
397
.
3.
Gjika
,
K.
, San
Andres
,
L.
, and
Larue
,
G. D.
, 2010, “
Nonlinear Dynamic Behavior of Turbocharger Rotor-Bearing Systems With Hydrodynamic Oil Film and Squeeze Film Damper in Series: Prediction and Experiment
,”
ASME J. Comput. Nonlinear Dyn.
,
5
,
041006
.
4.
Howard
,
S.
, 1999, “
Rotordynamics and Design Methods of an Oil-Free Turbocharger
,”
STLE Tribol. Trans.
,
49
, pp.
174
179
.
5.
Heshmat
,
C. A.
,
Heshmat
,
H.
,
Valco
,
M. J.
,
Radil
,
K. C.
, and
DellaCorte
,
C.
, 2005, “
Foil Bearings Make Oil-Free Turbocharger Possible
,”
Proceedings of the ASME World Tribology Congress
,
Washington, USA
, WTC Paper No. 2005-63724.
6.
Lee
,
Y. B.
,
Park
,
D. J.
, and
Kim
,
C. H.
, 2008, “
Stability and Efficiency of Oil-Free Turbocharger With Foil Bearings for SUV
,”
Proceedings of SAE International Congress
,
Shanghai, China
, Paper No. 08SFI-0086.
7.
Lee
,
Y. B.
,
Park
,
D. J.
,
Kim
,
T. H.
, and
Sim
,
K.
, 2011, “
Development and Performance Measurement of Oil-Free Turbocharger Supported on Gas Foil Bearings
,”
ASME J. Eng. Gas Turbines Power
, (in press).
8.
Lee
,
Y. B.
,
Park
,
D. J.
, and
Kim
,
C. H.
, 2009, “
Design and Preliminary Test of the Oil-Free Turbocharger for SUV
,”
Proceedings of the ASME World Tribology Congress
,
Kyoto, Japan
, WTC Paper No. 2009-90788.
9.
DellaCorte
,
C.
,
Zaldana
,
A.
, and
Radil
,
K.
, 2003, “
A System Approach to the Solid Lubrication of Foil Air Bearing for Oil-Free Turbomachinery
,”
ASME J. Tribol.
,
126
(
1
), pp.
200
207
.
10.
Lee
,
Y. B.
,
Park
,
D. J.
,
Jo
,
J. H.
, and
Kim
,
C. H.
, 2007, “
High Temperature Lubricants for Air Foil Bearings: Friction and Wear Characteristics of Corona Series From 25 to 1,000 °C
,”
Proceedings of STLE Annual Meeting
,
Philadelphia, USA
.
11.
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.
12.
DellaCorte
,
C.
,
Valco
,
M. J.
,
Radil
,
K. C.
, and
Heshmat
,
H.
, 1999, “
Performance and Durability of High Temperature Foil Air Bearings for Oil-Free Turbomachinery
,” Report No. NASA/TM-1999-209187.
13.
Kim
,
T. H.
, and San
Andres
,
L.
, 2009, “
Effect of Side End Pressurization on the Dynamic Performance of Gas Foil Bearings-A Model Anchored to Test Data
,”
ASME J. Eng. Gas Turbines Power
,
131
,
012501
.
14.
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
,”
Tribol. Trans.
,
52
, pp.
569
580
.
15.
Rubio
,
D.
, and
San Andrés
,
L.
, 2006, “
Bump-Type Foil Bearing Structural Stiffness: Experiments and Predictions
,”
ASME J. Eng. Gas Turbines Power
,
128
(
3
), pp.
653
660
.
16.
Walton
,
J. F.
,
Heshmat
,
H.
, and
Tomaszewski
,
M. J.
, 2008, “
Testing of a Small Turbocharger / Turbojet Sized Simulator Rotor Supported on Foil Bearings
,”
ASME J. Eng. Gas Turbines Power
,
130
,
035001
.
17.
Kim
,
T. H.
,
Breedlove
,
A. W.
, and
San Andrés
,
L.
, 2009, “
Characterization of Foil Bearing Structure at Increasing Shaft Temperatures: Static Load and Dynamic Force Performance
,”
ASME J. Tribol
,
131
(
4
),
041703
.
18.
Kim
,
T. H.
, 2007, “
Analysis of Side End Pressurized Bump Type Gas Foil Bearings: A Model Anchored to Test Data
,” Ph.D. dissertation, Texas A&M University, College Station, TX.
19.
DellaCorte
,
C.
, and
Valco
,
M. J.
, 2000, “
Load Capacity Estimation of Foil Air Journal Bearings for Oil-Free Turbomachinery Applications
,” Report No. NASA/TM-2000-209782.
20.
Iordanoff
,
I.
, 1999, “
Analysis of an Aerodynamic Compliant Foil Thrust Bearing: Method for a Rapid Design
,”
ASME J. Tribol
,
121
, pp.
816
822
.
21.
Childs
,
D.
, 1993,
Turbomachinery Rotordynamics –Phenomena, Modeling, & Analysis
,
John Wiley & Sons
,
New York
, pp. 458-460.
22.
San Andrés
,
L.
, and
Kim
,
T. H.
, 2008, “
Forced Nonlinear Response of Gas Foil Bearing Supported Rotors
,”
Tribol. Int.
,
41
(
8
), pp.
704
715
.
23.
Nakada
,
T.
,
Tonosaki
,
H.
, and
Yamashita
,
H.
, 1996, “
Excitation Mechanism for Engine Vibration of Half-Order Components
,”
JSAE Review
,
17
, pp.
387
393
.
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