Skip to main content
main-content

Tipp

Weitere Kapitel dieses Buchs durch Wischen aufrufen

2021 | OriginalPaper | Buchkapitel

Gas Turbine Engine Fan Blade Flutter Detection Using Casing Vibration Signals by Application of Recurrence Plots and Recurrence Quantification Analysis

verfasst von: A. N. Viswanatha Rao, V. P. S. Naidu, Soumendu Jana

Erschienen in: Proceedings of the 6th National Symposium on Rotor Dynamics

Verlag: Springer Singapore

share
TEILEN

Abstract

Gas turbine aero engines are a specific class of turbomachinery wherein compression system and turbine are realized as spinning discs on an interconnecting shaft. Fan-bladed disc undergoes an unsteady aeroelastic phenomenon known as flutter during various operational regimes, which might lead to structural failure of blades. Study of this mode of flutter induced structural response by measuring casing vibration is of interest in health monitoring of aero engines. In this paper, authors present a novel application of detecting the rotating blade flutter based on the feature space constructed using statistical parameters, recurrence plots (RP) and recurrence quantification analysis (RQA) of engine casing vibration data. Feature vectors thus obtained are visualised in several 3D vector space plots to cluster the data points which separate flutter mode from the normal mode of operation. Results obtained through the proposed method have been compared with engine flutter test results obtained through dedicated rotating blade strain gauge instrumentation.

Sie möchten Zugang zu diesem Inhalt erhalten? Dann informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 69.000 Bücher
  • über 500 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Testen Sie jetzt 15 Tage kostenlos.

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 50.000 Bücher
  • über 380 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




Testen Sie jetzt 15 Tage kostenlos.

Literatur
1.
Zurück zum Zitat Technology Focus Gas Turbine Research Bulletin of Defence Research and Development Organisation DRDO, Ministry of Defence, India, vol 17, no 5 October 2009. ISSN 0971-4413 Technology Focus Gas Turbine Research Bulletin of Defence Research and Development Organisation DRDO, Ministry of Defence, India, vol 17, no 5 October 2009. ISSN 0971-4413
2.
Zurück zum Zitat Srinivasan AV (1997) Flutter and resonant vibration characteristics of engine blades. In: AnIGTI scholar paper, 97-GT-533, Presented at the international gas turbine &aero engine congress & exhibition, Orlando, FL 2–5 June 1997 Srinivasan AV (1997) Flutter and resonant vibration characteristics of engine blades. In: AnIGTI scholar paper, 97-GT-533, Presented at the international gas turbine &aero engine congress & exhibition, Orlando, FL 2–5 June 1997
3.
Zurück zum Zitat Purushotaman K, Jeyaraman SK, Pratap A, Deshkulakarni KP (2017) Aeroelastic flutter investigation and stability enhancement of a transonic axial compressor rotor using casing treatment. In: Paper No. GTINDIA 2017–4767, pp V001 T0 1A015, https://​doi.​org/​10.​1115/​gtindia2017-4767 presented during ASME 2017 gas turbine india conference, Bangalore, India, 7–8 Dec 2017. ISBN 978-0-7918-5850-9 Purushotaman K, Jeyaraman SK, Pratap A, Deshkulakarni KP (2017) Aeroelastic flutter investigation and stability enhancement of a transonic axial compressor rotor using casing treatment. In: Paper No. GTINDIA 2017–4767, pp V001 T0 1A015, https://​doi.​org/​10.​1115/​gtindia2017-4767 presented during ASME 2017 gas turbine india conference, Bangalore, India, 7–8 Dec 2017. ISBN 978-0-7918-5850-9
4.
Zurück zum Zitat Viswanatha Rao AN et al. Challenges in engine health monitoring instrumentation during developmental testing of gas turbine engines. In: Paper no 153, proceedings of the 2nd national aero propulsion conference, NAPC-2018 7–19 Dec 2018, IIT Kharagpur, West Bengal (proceedings yet to be released) Viswanatha Rao AN et al. Challenges in engine health monitoring instrumentation during developmental testing of gas turbine engines. In: Paper no 153, proceedings of the 2nd national aero propulsion conference, NAPC-2018 7–19 Dec 2018, IIT Kharagpur, West Bengal (proceedings yet to be released)
5.
Zurück zum Zitat Riazet S et al (2017) Vibration feature extraction and analysis for fault diagnosis of rotating machinery—A literature survey. Asia Pac J Multi Research 5(1):103–110 Riazet S et al (2017) Vibration feature extraction and analysis for fault diagnosis of rotating machinery—A literature survey. Asia Pac J Multi Research 5(1):103–110
7.
Zurück zum Zitat Gill JD, Capece VR, Fost RB (2004) Experimental methods applied in a study of stall flutter in an axial flow fan. Shock Vib 11(2004):597–613. ISSN 1070-9622/04/2004 (IOS Press) Gill JD, Capece VR, Fost RB (2004) Experimental methods applied in a study of stall flutter in an axial flow fan. Shock Vib 11(2004):597–613. ISSN 1070-9622/04/2004 (IOS Press)
8.
Zurück zum Zitat recommended practices for measurement of gas path pressures and temperatures for performance assessment of aircraft turbine engines and components, AGARD AR-245, 1990 recommended practices for measurement of gas path pressures and temperatures for performance assessment of aircraft turbine engines and components, AGARD AR-245, 1990
9.
Zurück zum Zitat Holanda R. Analysis of strain gage reliability in F-100Jet engine testing at NASA Lewis Research Centre, 1983 NASA Technical Memorandum 83325 Holanda R. Analysis of strain gage reliability in F-100Jet engine testing at NASA Lewis Research Centre, 1983 NASA Technical Memorandum 83325
10.
12.
Zurück zum Zitat Marwan N, Carmen Romano M, Thiel M, Kurths J (2007) Recurrence plots for the analysis of complex systems. Elsevier Phys Rep 438(2007):237–329. Nonlinear Dynamics Group, Institute of Physics, University of Potsdam, Potsdam 14415, Germany Marwan N, Carmen Romano M, Thiel M, Kurths J (2007) Recurrence plots for the analysis of complex systems. Elsevier Phys Rep 438(2007):237–329. Nonlinear Dynamics Group, Institute of Physics, University of Potsdam, Potsdam 14415, Germany
13.
Zurück zum Zitat Marwan N, Saparin P, Kurths J (2005) Generalisation of recurrence plot analysis for spatial data international symposium on nonlinear theory and its applications (NOLTA2005) Bruges, Belgium, 18–21 Oct 2005 Marwan N, Saparin P, Kurths J (2005) Generalisation of recurrence plot analysis for spatial data international symposium on nonlinear theory and its applications (NOLTA2005) Bruges, Belgium, 18–21 Oct 2005
Metadaten
Titel
Gas Turbine Engine Fan Blade Flutter Detection Using Casing Vibration Signals by Application of Recurrence Plots and Recurrence Quantification Analysis
verfasst von
A. N. Viswanatha Rao
V. P. S. Naidu
Soumendu Jana
Copyright-Jahr
2021
Verlag
Springer Singapore
DOI
https://doi.org/10.1007/978-981-15-5701-9_31

Premium Partner

    Marktübersichten

    Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.