Acoustic Identification of Turbocharger Impeller Mistuning—A New Tool for Low Emission Engine Development
Source abstract
Abstract
At present, exhaust gas turbochargers not only form the basis for the economical operation of petrol, diesel or gas engines of all power categories, but also have an irreplaceable role on reducing their emissions. In order to reduce emissions from internal combustion engines, various systems are being developed, all of which have a turbocharger as an important component. Demands on turbocharger system durability and reliability keep growing, which requires the application of increasingly advanced computational and experimental methods at the development beginning of these systems. The design of turbochargers starts with a mathematical description of their rotationally cyclic impellers. However, mistuning, i.e., a slight individual blade property deviation from the intended design parameters, leads to a disturbance of the rotational cyclic symmetry. This article deals with the effects of manufacturing-related deviations on the structural dynamic behaviour of real turbine rotors. As opposed to methods exploiting expensive scanning vibrometers for experimental modal analysis or time-consuming accurate measurement of the geometry of individual blades using 3D optical scanners. A suitable microphone and a finite element rotor wheel model are the basis of this new method. After comparing the described acoustic approach with the laser vibrometer procedure, the results seemed to be practically identical. In comparison with the laser technique the unquestionable added value of this new method is the fact that it brings a significant reduction in the financial requirements for laboratory equipment. Another important benefit is that the measuring process of bladed wheel mistuning is significantly less time-consuming.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Bladed Disk Vibration Dynamics · Technical Engine Diagnostics and Monitoring · Advanced Measurement and Detection Methods
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Institute of Automotive Engineering, Brno University of Technology, Technická 2896/2, 616 69 Brno, Czech Republic
Department of Cars and Carriage Facilities, State University of Infrastructure and Technologies, Kyrylivska str., 9, 04071 Kyiv, Ukraine
Department of Wagons, Ukrainian State University of Railway Transport, Feuerbach sq., 7, 61050 Kharkiv, Ukraine
Funding
Brno University of Technology
References (30)
Show source-provided references
1. Analysis of the Worst Mistuning Patterns in Bladed Disk Assemblies10.1115/1.1622710 ↗
2. Über die Schwingungen von Dampfturbinen-Laufrädern
3. The protection of steam turbine disk wheels from axial vibration
4. The influence of dynamical imperfections on the vibration of rotating disks10.1243/PIME_PROC_1957_171_056_02 ↗
5. Effect of mistuning on the vibration of turbomachine blades induced by wakes10.1243/JMES_JOUR_1966_008_004_02 ↗
6. The effect of detuning upon the forced vibration of bladed disks10.1016/0022-460X(69)90264-8 ↗
7. Maximum amplification of blade response due to mistuning: Localization and mode shape aspects of the worst disks10.1115/1.1506958 ↗
8. Chan, Y. (2009). Variability of Blade Vibration in Mistuned Bladed Discs. [Ph.D. Thesis, Imperial College London].
9. Petrov, E. (2010, January 14–18). Reduction of forced response levels for bladed discs by mistuning: Overview of the phenomenon. Proceedings of the ASME TurboExpo, Glasgow, UK.10.1115/GT2010-23299 ↗
10. Beirow, B., Kühhorn, A., Giersch, T., and Nipkau, J. (2014, January 16–20). Optimization-aided forced response analysis of a mistuned compressor blisk. Proceedings of the ASME TurboExpo, Düsseldorf, Germany.10.1115/GT2014-25915 ↗
11. Localization phenomena in mistuned assemblies with cyclic symmetry Part 1: Free vibrations10.1115/1.3269547 ↗
12. Localization phenomena in mistuned assemblies with cyclic symmetry Part 2: Free vibrations10.1115/1.3269548 ↗
13. Experimental investigation of mode localization and forced response amplitude magnification for a mistuned bladed disk10.1115/1.1377872 ↗
14. Forced response of turbine engine bladed disks and sensitivity to harmonic mistuning10.1115/1.1498269 ↗
15. Asymptotic description of maximum mistuning amplification of bladed disk forced response
16. Figaschewsky, F., and Kühhorn, A. (2015, January 15–19). Analysis of mistuned blade vibrations based on normally distributed blade individual natural frequencies. Proceedings of the ASME TurboExpo, Montreal, QC, Canada.10.1115/GT2015-43121 ↗
17. Irwanto, B. (2006). Schaufelschwingungsanalyse am Elastischen Beschaufelten Rotor: Numerische und Experimentelle Untersuchungen. [Ph.D. Thesis, Technische Universität Dresden].
18. Drozdowski, R. (2011). Berechnung der Schwingbeanspruchungen in Radialturbinenrädern unter Berücksichtigung realer Bauteilgeometrien. [Ph.D. Thesis, Technische Universität Dresden].
19. Hemberger, D., Filsinger, D., and Bauer, H.J. (2013, January 3–7). Mistuning modelling and its validation for small turbine wheels. Proceedings of the ASME TurboEspo, San Antonio, TX, USA.10.1115/GT2013-94019 ↗
20. Hemberger, D., Filsinger, D., and Bauer, H.J. (2014, January 16–20). Identification of mistuning for casted turbine wheels of small size. Proceedings of the ASME TurboEspo, Düsseldorf, Germany.10.1115/GT2014-25099 ↗
21. Beirow, B. (2009). Grundlegende Untersuchungen zum Schwingungsverhalten von Verdichterlaufrädern in Intergralbauweise, Shaker Verlag.
22. Model Update and Validation of a Mistuned High Pressure Compressor10.1017/aer.2018.149 ↗
23. Hattori, H. (2014, January 16–20). Study on mistuning identification of vehicle turbocharger turbine BLISK. Proceedings of the ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Düsseldorf, Germany.10.1115/GT2014-27217 ↗
24. Tip-Timing measurements and numerical analysis of last-stage steam turbine mistuned bladed disc during run-down10.1007/s42417-019-00185-2 ↗
25. Fan, C., Wu, Y., Russhard, P., and Wang, A. (2020). An Improved Blade Tip-timing Method for Vibration Measurement of Rotating Blades during Transient Operating Conditions. J. Vib. Eng. Technol.10.1007/s42417-019-00195-0 ↗
26. Numerical simulation of the aerodynamic tonal noise generation in a backward-curved blades centrifugal fan
27. Cravero, C., and Marsano, D. (2018, January 11–15). Numerical prediction of tonal noise in centrifugal blowers. Proceedings of the Turbo Expo 2018: Turbomachinery Technical Conference & Exposition, Oslo, Norway. ASME Paper GT2018-75243.
28. Application of a Bandpass Filter for the Active Vibration Control of High-Speed Rotors10.20855/ijav.2019.24.31515 ↗
29. Píštěk, V., Kučera, P., Fomin, O., and Lovska, A. (2020). Effective Mistuning Identification Method of Integrated Bladed Discs of Marine Engine Turbochargers. J. Mar. Sci. Eng., 8.10.3390/jmse8050379 ↗
30. Weber, R. (2019). Ein Beitrag zur schwingungssicheren Auslegung von radialen Turbomaschinen mit Fokus auf Mistuning und Dämpfung. [Ph.D. Thesis, Mensch & Buch Verlag: BTU Cottbus-Senftenberg].