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Frequencies and modes of rotating flexible shrouded bladed discs-shaft assemblies

Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
It is now increasingly necessary to predict accurately, at the design stage and without excessive computing costs, the dynamic behaviour of rotating parts of turbomachines, so that resonant conditions at operating speeds are avoided. In this study, global rotating mode shapes of flexible shrouded bladed disc-shaft assemblies are calculated. The rotating modes have been calculated by using a finite element cyclic symmetry approach. Rotational effects, such as centrifugal stiffening have been accounted for, and all the possible couplings between the flexible parts have been allowed. Gyroscopic effects have been neglected. The numerical results have been compared with the experimental. The calculations show the influence of shaft flexibility on the natural frequencies of shrouded bladed discs up to four nodal diameters for the two first frequencies series.
Słowa kluczowe
EN
Rocznik
Strony
215--231
Opis fizyczny
Bibliogr. 15 poz., rys., tab.
Twórcy
  • Department of Dynamics of Machines, Institute of Fluid Flow Machinery, Polish Academy of Sciences, J. Fiszera 14, 80-952 Gdansk, Poland
  • Department of Dynamics of Machines, Institute of Fluid Flow Machinery, Polish Academy of Sciences, J. Fiszera 14, 80-952 Gdansk, Poland
  • Polish Naval Academy, Śmidowicza 71, 81-919 Gdynia, Poland
autor
  • Department of Dynamics of Machines, Institute of Fluid Flow Machinery, Polish Academy of Sciences, J. Fiszera 14, 80-952 Gdansk, Poland
  • Department of Dynamics of Machines, Institute of Fluid Machinery, Polish Academy of Sciences, J. Fiszera 14, 80-952 Gdańsk, Poland, jsokolow@imp.gda.pl
Bibliografia
  • [1] Berger H and Kulig T S 1981 Simulation Models for Calculating the Torsional Vibrationsof Large Turbine-generator Units after Electrical System Faults, Simens Forsch.-u.Entwickl.-Ber., Springer-Verlag10(4) 237
  • [2] Bogacz R, Irretier H and Szolc T 1992 Trans. ASME, J. Vibration and Acoustics114149
  • [3] Chivens D R and Nelson H D 1975 J. Engng. for Industry 97881
  • [4] Rao J S 1991 Rotor Dynamics, 2nd Edition, John Wiley & Sons
  • [5] Dopkin J A and Shoup T E 1974 Trans. ASME 961328
  • [6] Dubigeon S and Michon J C 1986 J. Sound and Vibration106(1) 53
  • [7] Huang S C and Ho K B 1996 Trans. ASME118100
  • [8] Shahab A A S and Thomas J 1987 J. Sound and Vibration114(3) 435
  • [9] Filippow A P and Kosinow J P 1973 Maszinowedenije323 (in Russian)
  • [10] Rao J S 1991 Turbomachine Blade Vibration, Wiley Eastern Limited, New Delhi
  • [11] Rządkowski R 1998 Fluid Flow Machinery 22, Part Two, Wroclaw, Ossolineum
  • [12] Loewy R G and Khader N 1984 Am. Inst. of Aeronautic and Astronautics J.221319
  • [13] Khader N and Loewy R G 1990 J. Sound and Vibration139(3) 469
  • [14] Khader N and Masoud S 1991 J. Sound and Vibration149(3) 471
  • [15] Jacquet-Richardet G, Ferraris G and Rieutord P 1996 J. Sound and Vibration191(5) 901
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT3-0010-0021
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