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The evaluation of the crack-like damage parameter of blades at the vibroacoustical diagnosis of the gas-turbine engines

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Konferencja
Jubilee Symposium Vibrations In Physical Systems (25 ; 15-19.05.2012 ; Będlewo koło Poznania ; Polska)
Języki publikacji
EN
Abstrakty
EN
This work is devoted to vibroacoustical condition monitoring of the gas-turbine engines (GTE) blades and diagnosis of the crack-like damages at the steady-state and non-steady-state modes of GTE. For detection of the mentioned damages we proposed the application and further development of the low-frequency vibroacoustical diagnostic methods which use vibrating and acoustical noise as diagnostic information. The following amplitude dimensionless characteristics are used as fault features: probability factor, peak factor and factor of background. The evaluation of the crack-like damage of the blades is carried out at the steady-state and nonsteady-state modes by using the generalized likelihood method. The statistical quality of the received estimations is investigated.
Rocznik
Tom
Strony
83--88
Opis fizyczny
Bibliogr. 3 poz., wykr.
Twórcy
autor
  • National Technical University of Ukraine "Kiev Polytechnic Institute", 37 Peremogy Pr., Kyiv, Ukraine, 03056
  • National Aviation University, 1 Kosmonavta Komarova Pr., Kyiv, Ukraine, 03058
Bibliografia
  • 1. N. Bouraou, Iu. Sopilka, Vibroacoustical diagnosis of the crack-like damages of aircraft engine blades at the steady-state and non-steady-state modes, Vibrations in Physical Systems, 24 (2010) 69-74.
  • 2. C. Cempel Diagnostically Oriented Measures of Vibroacoustical Process, J. of Sound and Vibration, 73(4) (1980) 547-561.
  • 3. B. Levin, Theoretical principles of radio-electronics, Sovetskoe radio, Moscow 1975.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-b0cc2453-ed76-49ac-8404-e0029c7c3651
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