Oil-free turbochargers (TCs) require gas bearings in compact units of enhanced rotordynamic stability, mechanical efficiency, and improved reliability with reduced maintenance costs compared with oil-lubricated bearings. Implementation of gas bearings into automotive TCs requires careful thermal management with accurate measurements verifying model predictions. Gas foil bearings (GFBs) are customarily used in oil-free microturbomachinery because of their distinct advantages including tolerance to shaft misalignment and centrifugal/thermal growth, and large damping and load capacity compared with rigid surface gas bearings. Flexure pivot tilting pad bearings (FPTPBs) are widely used in high-performance turbomachinery since they offer little or no cross-coupled stiffnesses with enhanced rotordynamic stability. The paper details the rotordynamic performance and temperature characteristics of two prototype oil-free TCs; one supported on foil journal and thrust bearings and the other one is supported on FPTP journal bearings and foil thrust bearings of identical sizes (outer diameter (OD) and inner diameter (ID)) with the same aerodynamic components. The tests of the oil-free TCs, each consisting of a hollow rotor (∼0.4 kg and ∼23 mm in OD at the bearing locations), are performed for various imbalances in noise, vibration, and harshness (NVH; i.e., cold air driven rotordynamics rig) and gas stand test facilities up to 130 krpm. No forced cooling air flow streams are supplied to the test bearings and rotor. The measurements demonstrate the stable performance of the rotor–gas bearing systems in an ambient NVH test cell with cold forced air into the turbine inlet. Post-test inspection of the test FPTPGBs after the hot gas stand tests evidences seizure of the hottest bearing, thereby revealing a notable reduction in bearing clearance as the rotor temperature increases. The compliant FPTPGBs offer a sound solution for stable rotor support only at an ambient temperature condition while demonstrating less tolerance for shaft growth, centrifugal, and thermal, beyond its clearance. The current measurements give confidence in the present GFB technology for ready application into automotive TCs for passenger car and commercial vehicle applications with increased reliability.
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April 2016
Research-Article
Bump-Type Foil Bearings and Flexure Pivot Tilting Pad Bearings for Oil-Free Automotive Turbochargers: Highlights in Rotordynamic Performance
Keun Ryu,
Keun Ryu
Assistant Professor
Department of Mechanical Engineering,
Hanyang University,
Ansan, Gyeonggi-do 15588, South Korea
e-mail: kryu@hanyang.ac.kr
Department of Mechanical Engineering,
Hanyang University,
Ansan, Gyeonggi-do 15588, South Korea
e-mail: kryu@hanyang.ac.kr
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Zachary Ashton
Zachary Ashton
Global Engineering Core Science,
BorgWarner Turbo Systems,
Arden, NC 28704
e-mail: zashton@borgwarner.com
BorgWarner Turbo Systems,
Arden, NC 28704
e-mail: zashton@borgwarner.com
Search for other works by this author on:
Keun Ryu
Assistant Professor
Department of Mechanical Engineering,
Hanyang University,
Ansan, Gyeonggi-do 15588, South Korea
e-mail: kryu@hanyang.ac.kr
Department of Mechanical Engineering,
Hanyang University,
Ansan, Gyeonggi-do 15588, South Korea
e-mail: kryu@hanyang.ac.kr
Zachary Ashton
Global Engineering Core Science,
BorgWarner Turbo Systems,
Arden, NC 28704
e-mail: zashton@borgwarner.com
BorgWarner Turbo Systems,
Arden, NC 28704
e-mail: zashton@borgwarner.com
Contributed by the Structures and Dynamics Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received July 13, 2015; final manuscript received August 16, 2015; published online October 13, 2015. Editor: David Wisler.
J. Eng. Gas Turbines Power. Apr 2016, 138(4): 042501 (10 pages)
Published Online: October 13, 2015
Article history
Received:
July 13, 2015
Revised:
August 16, 2015
Citation
Ryu, K., and Ashton, Z. (October 13, 2015). "Bump-Type Foil Bearings and Flexure Pivot Tilting Pad Bearings for Oil-Free Automotive Turbochargers: Highlights in Rotordynamic Performance." ASME. J. Eng. Gas Turbines Power. April 2016; 138(4): 042501. https://doi.org/10.1115/1.4031440
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