Earthquake Vibrational Response of Turbo-Machines

1986 ◽  
pp. 311-323
Author(s):  
F. Ziegler ◽  
H. L. Hasslinger
Keyword(s):  
2008 ◽  
Vol 100 (17) ◽  
Author(s):  
Maria Sovago ◽  
R. Kramer Campen ◽  
George W. H. Wurpel ◽  
Michiel Müller ◽  
Huib J. Bakker ◽  
...  

ACS Nano ◽  
2021 ◽  
Author(s):  
Fadil Iyikanat ◽  
Andrea Konečná ◽  
F. Javier García de Abajo

2012 ◽  
Vol 331 (16) ◽  
pp. 3762-3773 ◽  
Author(s):  
Yong-Chen Pei ◽  
Qing-Chang Tan ◽  
Xin Yang ◽  
Chris Chatwin

Author(s):  
Pavel Goldman ◽  
Agnes Muszynska

Abstract This report presents experimental, analytical, and numerical results describing vibrational phenomena in a rotating machine with one loose pedestal. The loose-pedestal machine rotor vibrations represent unbalance-related excited vibrations of synchronous and fractional subsynchronous regimes. In this study the loose-pedestal machine is first simulated by a simple vibrating beam excited by a shaker mounted on it. The shaker simulates an unbalanced machine rotor. The beam occasionally enters in contact with the foundation. The excited vibrations are modified by impacting occurrences, and by periodic changes in system stiffness. A new model of the impact has been developed. The results of analytical and experimental studies stand in a good agreement. They illustrate the existence of the synchronous regime and several subsynchronous fractional regimes in various excitation frequency ranges. The analysis adequately predicts the occurrence of these regimes and determines the physical parameters affecting them. The analytical and experimental results are then compared with the responses of experimental rotor rig with one bearing pedestal looseness. They show the same qualitative pattern.


1990 ◽  
Vol 112 (4) ◽  
pp. 297-303 ◽  
Author(s):  
G. Moe ◽  
Z.-J. Wu

This paper reports an extensive program of forced and free vibration tests on a single circular cylinder moving mainly perpendicularly to a uniform current. For both free and forced vibration tests, two cases were investigated: one in which the cylinder was restrained in the in-line direction and the other in which it was supported on suitable springs. The cross-flow vibrational response and hydrodynamic forces on the cylinder were measured. Large variations of motion frequency in the “lock-in” range were found from the free vibration tests. This leads to two different definitions of reduced velocity, namely, a so-called nominal reduced velocity based on one reference frequency and the true reduced velocity based on the actual vibration frequency. When different results are compared, the true reduced velocity should be used. The forced vibration tests showed, as may be expected, that the transverse force in the “lock-in” range on the average will add energy to the cylinder at moderate motion amplitudes and subtract energy at large amplitudes. Some conditions resulting in a steady-state vibration of a flexibly mounted cylinder were analyzed. The actual force traces also show very large and apparently random deviations from the average force amplitude. The results from the forced and the free vibration tests are consistent with each other if the true reduced velocity and reduced amplitude are the same.


Nano Letters ◽  
2007 ◽  
Vol 7 (4) ◽  
pp. 1059-1063 ◽  
Author(s):  
Hristina Petrova ◽  
Chien-Hua Lin ◽  
Min Hu ◽  
Jingyi Chen ◽  
Andrew R. Siekkinen ◽  
...  

1974 ◽  
Vol 56 (6) ◽  
pp. 1782-1791 ◽  
Author(s):  
Henno Allik ◽  
Kenneth M. Webman ◽  
John T. Hunt

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