The paper presents results from film thickness measurements in a bearing chamber test rig. The measurements were performed at different operating conditions and with two offtake designs. A discussion of the measurement technique using in situ calibrated capacitive sensors shows good accuracy and repeatability. The film thickness results are first compared to measurements with the same chamber in a vented configuration. The analysis of the measurements at various operating conditions shows a strong influence of the shaft speed, the chamber pressure, and the offtake design. In contrast to that, flow rate and scavenge ratio have only minor influence. Furthermore, the momentum flux of the core air flow is proposed as a suitable parameter with which the influence of shaft speed and pressure can be correlated to the film thickness distribution.
Skip Nav Destination
Article navigation
November 2013
Research-Article
Capacitive Film Thickness Measurements in a Ventless Aero-Engine Bearing Chamber—Influence of Operating Conditions and Offtake Design
Hans-Jörg Bauer
Hans-Jörg Bauer
Institut für Thermische Strömungsmaschinen,
Karlsruhe Institute of Technology (KIT)
,Karlsruhe 76131
, Germany
Search for other works by this author on:
Wolfram Kurz
e-mail: wolfram.kurz@kit.edu
Hans-Jörg Bauer
Institut für Thermische Strömungsmaschinen,
Karlsruhe Institute of Technology (KIT)
,Karlsruhe 76131
, Germany
Contributed by the Structures and Dynamics Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received June 28, 2013; final manuscript received July 17, 2013; published online September 17, 2013. Editor: David Wisler.
J. Eng. Gas Turbines Power. Nov 2013, 135(11): 112504 (7 pages)
Published Online: September 17, 2013
Article history
Received:
June 28, 2013
Revision Received:
July 17, 2013
Citation
Kurz, W., Dullenkopf, K., and Bauer, H. (September 17, 2013). "Capacitive Film Thickness Measurements in a Ventless Aero-Engine Bearing Chamber—Influence of Operating Conditions and Offtake Design." ASME. J. Eng. Gas Turbines Power. November 2013; 135(11): 112504. https://doi.org/10.1115/1.4025067
Download citation file:
Get Email Alerts
Cited By
Swirl Ratio Prediction Model in Rotor-Stator Cavity With Superposed Outward Radial Throughflow Based on Region Partition
J. Eng. Gas Turbines Power (August 2022)
Intercooled Recuperative Aero Engine System Optimization
J. Eng. Gas Turbines Power (August 2022)
Experimental Study of Various Low-Friction Coatings for High-Temperature Gas Foil Bearings Under Cold-Start Conditions
J. Eng. Gas Turbines Power (August 2022)
Performance Optimization of the High-Pressure Compressor in Series Two-Stage Turbocharging System Based on Low-Speed Performance Requirements of Diesel Engine
J. Eng. Gas Turbines Power (August 2022)
Related Articles
Performance of Balancing Wedge Action in Textured Hydrodynamic Pad Bearings
J. Tribol (January,2017)
Tribological Study of a Slider Bearing in the Supersonic Regime
J. Tribol (October,2016)
Related Proceedings Papers
Related Chapters
A Simple Carburetor
Case Studies in Fluid Mechanics with Sensitivities to Governing Variables
Case Studies
Nonlinear Regression Modeling for Engineering Applications: Modeling, Model Validation, and Enabling Design of Experiments
Evaluating Functional Coupling in Aeration Basin Air Distribution Systems
Advances in Multidisciplinary Engineering