4.6 Article

State-Space Model for Arrival Time Simulations and Methodology for Offline Blade Tip-Timing Software Characterization

期刊

SENSORS
卷 23, 期 5, 页码 -

出版社

MDPI
DOI: 10.3390/s23052600

关键词

tip-timing; diagnostics; blade vibration; turbomachinery; state-space; arrival time; aeromechanics

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Blade tip-timing is a widely used technique in turbine and compressor stages to measure blade vibrations. This study proposes a mathematical model to generate synthetic tip-timing signals for specific test conditions, which are then used to thoroughly characterize post-processing software for tip-timing analysis. This work is the first step in quantifying the uncertainty introduced by tip-timing analysis software into user measurements and can provide essential information for sensitivity studies on data analysis parameters during testing.
Blade tip-timing is an extensively used technique for measuring blade vibrations in turbine and compressor stages; it is one of the preferred techniques used for characterizing their dynamic behaviors using non-contact probes. Typically, arrival time signals are acquired and processed by a dedicated measurement system. Performing a sensitivity analysis on the data processing parameters is essential for the proper design of tip-timing test campaigns. This study proposes a mathematical model for generating synthetic tip-timing signals, descriptive of specific test conditions. The generated signals were used as the controlled input for a thorough characterization of post-processing software for tip-timing analysis. This work represents the first step in quantifying the uncertainty introduced by tip-timing analysis software into user measurements. The proposed methodology can also offer essential information for further sensitivity studies on parameters that influence the accuracy of data analysis during testing.

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