Quantification of Blade Vibration Amplitude in Turbomachinery
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Published:2024-03-04
Issue:1
Volume:9
Page:10
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ISSN:2504-186X
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Container-title:International Journal of Turbomachinery, Propulsion and Power
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language:en
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Short-container-title:IJTPP
Author:
Schneider Alexandra P.1, Paoletti Benoit1, Ottavy Xavier1ORCID, Brandstetter Christoph1ORCID
Affiliation:
1. Univ Lyon, Ecole Centrale de Lyon, CNRS, Univ. Claude Bernard Lyon 1, INSA Lyon, LMFA, UMR 5509, 69134 Ecully, France
Abstract
Experimental monitoring of blade vibration in turbomachinery is typically based on blade-mounted strain gauges. Their signals are used to derive vibration amplitudes which are compared to modal scope limits, including a safety factor. According to industrial guidelines, this factor is chosen conservatively to ensure safe operation of the machine. Within the experimental campaign with the open-test-case composite fan ECL5/CATANA, which is representative for modern lightweight Ultra High Bypass Ratio (UHBR) architectures, measurements close to the stability limit have been conducted. Investigation of phenomena like non-synchronous vibrations (NSV) and rotating stall require a close approach to the stability limit and hence demand for accurate (real-time) quantification of vibration amplitudes to ensure secure operation without exhaustive safety margins. Historically, short-time Fourier transforms of vibration sensors are used, but the complex nature of the mentioned coupled phenomena has an influence on amplitude accuracy, depending on evaluation parameters, as presented in a previous study using fast-response wall-pressure transducers. The present study investigates the sensitivity of blade vibration data to evaluation parameters for different spectral analysis methods and provides guidelines for fast and robust surveillance of critical vibration modes.
Reference22 articles.
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