2020
DOI: 10.1016/j.ijmecsci.2019.105363
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Simulation and experiment on lateral vibration transmission control of a shafting system with active stern support

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Cited by 26 publications
(16 citation statements)
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“…To derive the lateral, longitudinal, and torsional vibration equations of a multi-segment Timoshenko beam, the relationships between the coefficients of two adjacent segments, which are given in Appendix A, are first obtained with the compatibility and equilibrium conditions at the point x i (i = 1, 2, ., n + 1). 25,26 (a) Lateral vibration of a single beam The coefficients of the first segment C 11 , C 21 , C 31 , and C 41 can be expressed by the following matrix equation:…”
Section: Modelling Of the Shaft Bracketmentioning
confidence: 99%
“…To derive the lateral, longitudinal, and torsional vibration equations of a multi-segment Timoshenko beam, the relationships between the coefficients of two adjacent segments, which are given in Appendix A, are first obtained with the compatibility and equilibrium conditions at the point x i (i = 1, 2, ., n + 1). 25,26 (a) Lateral vibration of a single beam The coefficients of the first segment C 11 , C 21 , C 31 , and C 41 can be expressed by the following matrix equation:…”
Section: Modelling Of the Shaft Bracketmentioning
confidence: 99%
“…The propulsion-shaft system is an important part of a ship’s power system, and the stern bearing is an essential equipment of this system [ 1 ]. The stern bearing is used to support the stern shaft and propeller to ensure the regular operation of the propulsion-shaft system.…”
Section: Introductionmentioning
confidence: 99%
“…Vibration control methods and facilities have been proposed to suppress the noise generated by the fluctuating propeller forces, for example, the resonance changer (Goodwin, 1960), the auxiliary magnetic thrust bearing (Lewis et al, 1989a(Lewis et al, , 1989b, the active stern support (Xie et al, 2019(Xie et al, , 2020, and the dynamic antiresonant vibration isolator (Liu et al, 2018). Baz et al (1990) used an active vibration control system to attenuate the thrust-induced vibration, and the amplitude is reduced by approximately 11 dB.…”
Section: Introductionmentioning
confidence: 99%