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Analiza drgań łopatek wentylatora metodą bezdotykową
Języki publikacji
Abstrakty
Composite fan blades are more and more common both in aviation and ground applications. This work aims to characterize the vibration parameters of plastic blades installed in a wind tunnel fan by a non-contact method, namely blade tip timing (BTT). Blade dynamics was predicted with finite element modelling (FEM) and confirmed experimentally by tip timing measurements and analysis of data. BTT results were acquired and compared in two different configurations. A good agreement between predicted and measured frequency values was obtained for the fundamental mode. Significant differences were observed for the second and third modes due to material anisotropy and contact effects which could not be modelled because necessary material data were unavailable.
Czasopismo
Rocznik
Tom
Strony
341--357
Opis fizyczny
Bibliogr. 29 poz., rys.
Twórcy
autor
- Politecnico di Torino (Politechnika Turyńska)
autor
- Air Force Institute of Technology (Instytut Techniczny Wojsk Lotniczych)
autor
- Politecnico di Torino (Politechnika Turyńska)
Bibliografia
- 1. Amoo L.M.: On the design and structural analysis of jet engine fan blade structures. Prog Aerosp Sci. 2013;60:1-11. DOI:10.1016/j.paerosci.2012.08.002.
- 2. Barbero E.J.: Introduction to Composite Materials Design, Second Edition CRC Press 2010.
- 3. Eberlinc M, Dular M, Širok B, Lapanja B.: Influence of blade deformation on integral characteristic of axial flow fan. Stroj Vestnik/Journal Mech Eng. 54(3), 2008.
- 4. Ewins D.J.: Modal testing: Theory, practice and application. Research studies press Ltd., second ed., 2000.
- 5. Heath S., Imregun M.: An improved single-parameter tip-timing method for turbomachinery blade vibration measurements using optical laser probes, International Journal of Mechanical Sciences, Vol. 38, No. 10, 1996.
- 6. Heinemann T, Becker S.: Axial fan blade vibration assessment under inlet cross-flow conditions using laser scanning vibrometry. Appl Sci. 7(8), 2017, DOI: 10.3390/app7080862.
- 7. IEEE Standard for Digitizing Waveform Recorders, IEEE Std 1057TM-2007. IEEE 2007.
- 8. Kaźmierczak K., Przysowa R.: Standard sine fitting algorithms applied to blade tip timing data. Journal of Konbin, Vol. 30, No. 2, 2014, DOI: 10.2478/jok-2014-0012.
- 9. Kharyton V.: Faults Detection in Blades of an Aviation Engine in Operation, PhD thesis, Ecole Centrale de Lyon, 2009.
- 10. Kmak F.: Modernization and activation of the NASA Ames 11- by 11-Foot Transonic Wind Tunnel. In: 21st Aerodynamic Measurement Technology and Ground Testing Conference. Vol 53. Reston, Virginia: American Institute of Aeronautics and Astronautics; 2000:1689-1699. DOI:10.2514/6.2000-2680.
- 11. Maynard K., Trethewey M.: Blade and shaft crack detection using torsional vibration measurements Part 3: Field application demonstrations. Noise Vib Worldw. 2001;32(11):16-23. DOI: 10.1260/0957456011499145.
- 12. Mileshin V.: A Review of New Experimental Technologies for the Development of Advanced Fans with High Bypass Ratio. Int J Turbomachinery, Propuls Power. 2018;3(3):21. DOI: 10.3390/ijtpp3030021.
- 13. Muiyser J., Els DN, van der Spuy SJ, Zapke A.: Investigation of Large-Scale Cooling System Fan Blade Vibration. In: Proceedings of the ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. Volume 1A: Aircraft Engine; Fans and Blowers. Düsseldorf, Germany. June 16–20, 2014. V01AT10A008. ASME 2014:1-13. DOI: 10.1115/GT2014-25498.
- 14. Muiyser J.: Investigation of Large-Scale Cooling System Fan vibration. PhD Thesis. Stellenbosch University 2016.
- 15. Pickering T. M.: Methods for Validation of a Turbomachinery Rotor Blade Tip Timing System Methods, Masters Thesis. Virginia Tech, Blacksburg, Virginia, USA 2014.
- 16. Pierluigi P.: Characterization of fan blade vibration with a non-contact method. Rel. Daniele Botto. Politecnico di Torino, Master of Science in Mechanical Engineering, 2019, https://webthesis.biblio.polito.it/13365/17. Przysowa R., Russhard P.: Non-Contact Measurement of Blade Vibration in an Axial Compressor. Sensors. 2020;20(1):68. DOI:10.3390/s20010068.
- 18. Przysowa R.: The analysis of synchronous blade vibration using linear sine fitting, Journal of Konbin, Vol. 30, No. 2, 2014, DOI: 10.2478/jok-2014-0011.
- 19. Przysowa R.: Health monitoring of industrial fan blades in desulphurization system. In 6th EVI-GTI International Gas Turbine Instrumentation Conference. Baden 2013.
- 20. Russhard P.: MultiTool Blade Tip Timing Acquisition, Analysis and Data Simulation Software; EM0102–Analysis Manual; Technical Report; EMTD Ltd.: Nottingham, UK, 2016.
- 21. Russhard P.: The Rise and Fall of the Rotor Blade Strain Gauge. In: Sinha JK, ed. Vibration Engineering and Technology of Machinery. Vol 23. Mechanisms and Machine Science. Cham: Springer International Publishing; 2015:27-38, DOI: 10.1007/978-3-319-09918-7.
- 22. Savitzky A., Golay M.J.E.: Smoothing and Differentiation of Data by Simplified Least Squares Procedures. Analytical Chemistry 1964. 36 (8):1627-39, DOI: 10.1021/ac60214a047.
- 23. Stepanov A., Fateev V., Mileshin V.: Study of Rotor Blades Vibration Behavior of Counter Rotating Fan Models. In: Volume 7B: Structures and Dynamics. American Society of Mechanical Engineers; 2014:1-10, DOI: 10.1115/GT2014-26310.
- 24. Szczepanik R.: Early Detection of Fatigue Cracks in Turbine Aero-Engine Rotor Blades During Flight, Journal of KONES. Powertrain and Transport, Vol. 20, No. 1, 2015.
- 25. Szczepanik R.: Experimental Investigations of Aircraft Engine Rotor Blade Dynamics, Air Force Institute of Technology, Warszawa 2013.
- 26. Witoś M., Olzak B.: Theoretical foundations of tip timing measurements. In: Bouckaert J.F., Tip timing and tip clearance problem in turbomachines, VKI Lecture Series 2007-03, von Karman Institute for Fluid Dynamics, Sint-Genesius-Rode, Belgium 2007.
- 27. Witoś M.: High Sensitive Methods for Health Monitoring of Compressor Blades and Fatigue Detection. Sci World J. 2013;1-31, DOI: 10.1155/2013/218460.
- 28. Woike M.R., Roeder J.W., Hughes C.E., Bencic T.J.: Testing of a microwave blade tip clearance sensor at the NASA Glenn Research Center. 47th AIAA Aerosp Sci Meet Incl New Horizons Forum Aerosp Expo. 2009:1-14, DOI: 10.2514/6.2009-1452.
- 29. Wollmann T., Dannemann M., Langkamp A. et al.: Combined experimentalnumerical approach for the 3D vibration analysis of rotating composite compressor blades: An introduction. ECCM 2018 - 18th Eur Conf Compos Mater. June 2018.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-26e807ea-80b3-4301-83fb-40e92fe740ea