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Vibroacoustical diagnosis of the crack-like damages of aircraft engine blades at the steady-state and non-steady-state modes

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Konferencja
Symposium “Vibrations In Physical Systems” (24 ; 11-15.05.2010 ; Będlewo koło Poznania ; Polska)
Języki publikacji
EN
Abstrakty
EN
The work is devoted to condition monitoring and vibroacoustical diagnosis of the crack-like damages of the gas-turbine engines (GTE) blades at the steady-state and non-steady-state modes of GTE. The developed diagnostic model of GTE is presented and the influence of damage on the measured vibro- and acoustical signals at the steady-state and non-steady-state modes of GTE is determined. The application of the following signal processing methods: Polyspectral (Higher-Order Spectral) analysis, Wavelet-transformation and dimensionless characteristics of the vibroacoustical signals is proved. The efficiency of signal processing methods is demonstrated by the results of numerical simulations of the turbine stage at the steady-state and non-steady-state modes of vibration excitation. The fault features are detected and investigated.
Rocznik
Tom
Strony
69--74
Opis fizyczny
Bibliogr. 4 poz.
Twórcy
autor
  • National Technical University of Ukraine "Kiev Polytechnic Institute" 37 Peremogy Pr., Kyiv, Ukraine, 03056
autor
  • National Technical University of Ukraine "Kiev Polytechnic Institute" 37 Peremogy Pr., Kyiv, Ukraine, 03056
Bibliografia
  • 1. N. Bouraou, P. Marchuk, A. Tyapchenko Condition Monitoring Diagnosis Method of Aircraft Engine Rotating Details, In Proceedings of the 15th World Conference on Non-Destructive Testing (2000).
  • 2. C. Cempel Diagnostically Oriented Measures of Viroacoustical Process, J. of Sound and Vibration, 73(4) (1980) 547-561.
  • 3. N. Bouraou, Yu. Sopilka, A. Protasov The features Detection of the small rigidity faults of rotary machine element, In Review of Progress in QNDE: Abstracts book (2003).
  • 4. N. Bouraou, Yu. Sopilka, A. Protasov, O. Zazhitskiy Decision Making of Aircraft Engine Blades on Bispectral Analysis of the Vibroacoustical Signal, In Review of Progress in QNDE: Conference Proceedings, 24A(2005) 760-766.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-ff2077cc-615b-4231-8b17-c9c9fd746103
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