Volume 5: Structures and Dynamics, Parts a and B 2008
DOI: 10.1115/gt2008-51169
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Condition Monitoring of Rotor Using Active Magnetic Actuator

Abstract: It has been widely recognized that the changes in the dynamic response of a rotor could be utilized for general fault detection and monitoring. Current methods rely on the monitoring of synchronous response of the machine during its transient or normal operation. Very little progress has been made in developing robust techniques to detect subtle changes in machine condition caused by rotor cracks. It has been demonstrated that the crack-induced changes in the rotor dynamic behavior produce unique vibration sig… Show more

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Cited by 21 publications
(23 citation statements)
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“…The approach is demonstrated on a test rig utilized at the Center for Rotating Machinery Dynamics and Control (RoMaDyC) at Cleveland State University [19,20]. The photo of rig and its schematic are presented in Fig.…”
Section: The Experimental Test Rigmentioning
confidence: 99%
“…The approach is demonstrated on a test rig utilized at the Center for Rotating Machinery Dynamics and Control (RoMaDyC) at Cleveland State University [19,20]. The photo of rig and its schematic are presented in Fig.…”
Section: The Experimental Test Rigmentioning
confidence: 99%
“…The alternative way is to analyze the corresponding Fourier spectrum [7,8], however in this approach one needs to examine longer time series. Note that the notch of 1mm does not posses all features of a real crack.…”
Section: Discussionmentioning
confidence: 99%
“…earlier by Sawicki et al [7] where the main issue was the identification of Fourier amplitudes related to rotational frequency and its multiple values as 1X, 2X, 3X, 4X with and without magnetic excitation. The preliminary experimental results were predicted by the modelling with FEM.…”
Section: T [S]mentioning
confidence: 99%
See 1 more Smart Citation
“…Lastly, 4 = it + 4 0 is the angle between the crack axis and the rotor response at the crack location and T is the transformation matrix from rotating to iner tial coordinates. Assuming weight dominance or Iq st I � IqI and taking into ac count that K 0 q st = W, one can obtain the parametrically excited cracked rotor model in fixed coordinates system as follows [3,4,6]:…”
Section: Introductionmentioning
confidence: 99%