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2015 | OriginalPaper | Buchkapitel

The Rise and Fall of the Rotor Blade Strain Gauge

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Abstract

In any gas turbine the understanding of the way in which the rotor blades vibrate is essential for both the development and production phases. For many years the standard method of obtaining such data has been with the use of strain gauges in conjunction with radio telemetry units or slip rings. With the complexity of the machine increasing and as the operating environment becomes more and more hostile for such systems, new methods are being investigated that will ultimately lead to a non-intrusive technology being developed. Here we review the progress and pioneers of strain gauge measurement dating back to the 1930s and look at a number of technologies that have tried to displace them from their positions as the mainstay of rotor blade vibration measurement.

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Literatur
1.
Zurück zum Zitat Russhard P (2010) Development of a blade tip timing based engine health monitoring system—thesis, Faculty of Engineering and Physical Sciences, School of Mechanical Aerospace and Civil Engineering, Manchester University, Sept 2010 Russhard P (2010) Development of a blade tip timing based engine health monitoring system—thesis, Faculty of Engineering and Physical Sciences, School of Mechanical Aerospace and Civil Engineering, Manchester University, Sept 2010
2.
Zurück zum Zitat Niska H (2012) Strain Gage Pioneers and Propulsion Engine History Joint EVI-GTI and PIWG conference, Oct 2012 Niska H (2012) Strain Gage Pioneers and Propulsion Engine History Joint EVI-GTI and PIWG conference, Oct 2012
3.
Zurück zum Zitat Kadambi JR, Quinn RD, Adams ML (1989) Turbomachinery blade vibration and dynamic stress measurements utilizing nonintrusive techniques. J Turbomach 111(4):468–474CrossRef Kadambi JR, Quinn RD, Adams ML (1989) Turbomachinery blade vibration and dynamic stress measurements utilizing nonintrusive techniques. J Turbomach 111(4):468–474CrossRef
4.
Zurück zum Zitat Heath S (1996) A study of tip-timing techniques for the determination of bladed disk vibration characteristics, Imperial College of Science and Technology, University of London, PhD Thesis, 1996 Heath S (1996) A study of tip-timing techniques for the determination of bladed disk vibration characteristics, Imperial College of Science and Technology, University of London, PhD Thesis, 1996
5.
Zurück zum Zitat Kearns CM Jr (1936) Stress measuring means—US patent application Kearns CM Jr (1936) Stress measuring means—US patent application
6.
Zurück zum Zitat Jackson PS (1953) Foil strain gauge England—patent application Jackson PS (1953) Foil strain gauge England—patent application
7.
Zurück zum Zitat ThomasJC (1962) A new technique for investigating blade vibrations. Bristol Siddeley J ThomasJC (1962) A new technique for investigating blade vibrations. Bristol Siddeley J
8.
Zurück zum Zitat Chi RM et al (1984) Conceptual design of a non-interference stress measurement system for gas turbine engines. Arnold Engineering Development Centre 1984 Chi RM et al (1984) Conceptual design of a non-interference stress measurement system for gas turbine engines. Arnold Engineering Development Centre 1984
9.
Zurück zum Zitat Chi RM et al (1988) Demonstration of testing of a non-interference technique for measuring rotor blade stress, AIAA/ASME/SAE/ASEE 24th joint propulsion conference 1988 Chi RM et al (1988) Demonstration of testing of a non-interference technique for measuring rotor blade stress, AIAA/ASME/SAE/ASEE 24th joint propulsion conference 1988
10.
Zurück zum Zitat Russhard P (2012) Analysis of rotating stall in a contra-rotating system using blade tip timing, IIS conference June 2012 Russhard P (2012) Analysis of rotating stall in a contra-rotating system using blade tip timing, IIS conference June 2012
Metadaten
Titel
The Rise and Fall of the Rotor Blade Strain Gauge
verfasst von
Peter Russhard
Copyright-Jahr
2015
DOI
https://doi.org/10.1007/978-3-319-09918-7_2

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