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

Author:

Tocci Tommaso1ORCID,Capponi Lorenzo1ORCID,Rossi Gianluca1ORCID,Marsili Roberto1ORCID,Marrazzo Marco2

Affiliation:

1. Department of Engineering, University of Perugia, Via G. Duranti 93, 06125 Perugia, Italy

2. Baker Hughes, Via F. Matteucci 2, 50127 Florence, Italy

Abstract

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.

Publisher

MDPI AG

Subject

Electrical and Electronic Engineering,Biochemistry,Instrumentation,Atomic and Molecular Physics, and Optics,Analytical Chemistry

Reference35 articles.

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3. Noninterference technique for measurement of turbine engine compressor blade stress;McCarty;J. Aircr.,1982

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