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Abstrakty
As a failure of rotor blades in a gas turbine was reported, the rotating-mode shapes of flexible shrouded bladed disc assemblies were calculated using a finite element approach. Rotational effects, such as centrifugal stiffening were accounted for, and all couplings between the flexible parts were allowed. The spin softening effects were neglected. A dynamic analysis of the shrouded bladed disc demonstrated that it was designed with a sufficient safety region of resonance. In case of one blade getting loose, it is vibrating in resonance.
Słowa kluczowe
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Rocznik
Tom
Strony
83--95
Opis fizyczny
Bibliogr. 3 poz., 17 rys., 6 tab.
Twórcy
autor
autor
autor
autor
autor
- Institute of Fluid-Flow Machinery, Polish Academy of Sciences, Fiszera 14, 800-952 Gdansk, Poland, z3@imp.gda.pl
Bibliografia
- [1] Rao J S, Singh A K, Ramakrishnan C V and Gupta K 2000 Proc. 5th ASME Annual Engin. Sys. Design and Anal., Montreux, pp. 750-770
- [2] Rao J S 1991 Turbomachine Elade Vibration, Whey, New York
- [3] Rządkowski R 1998 Dynamics of Rotor Steam Turbine Rotor Blading. Part Two: Bladed Discs, Series Maszyny Przepływowe 22, Ossolineum, Wrocław
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPG5-0014-0007