Results 21 to 30 of about 221,137 (269)
Modelling of the bladed disk vibration with damping elements in blade shroud
The requirement for wide operation range of steam turbine can cause, that the blades work close to resonant frequency. For decreasing of blade’s vibration there are placed damping elements in the blade shroud.
Kellner J., Zeman V.
doaj +2 more sources
Localization of energy in a perfectly symmetric bladed disk assembly due to nonlinearities
Although a bladed disk is typically designed to have identical blades, manufacturing tolerances, wear,and other causes may cause random deviations among the blades. The blade-to-bladediscrepancies, denoted as mistuning, lead to vibratory responses mostly
Maxime Peeters (10571657) +4 more
core +7 more sources
Although bladed disks are nominally designed to be cyclically symmetric (tuned system), the vibration characteristics of all blades on a disk are slightly different due to the manufacturing tolerance, deviations in the material properties, and wear ...
Yasutomo KANEKO +3 more
doaj +1 more source
Mode Localization of a Cracked Blade-Disks [PDF]
In this paper, the effect of blade crack on the mode localization of a rotating blade-disk is studied. Pretwisted taper beams are used to simulate blades of a blade-disk. The crack on the blade can be regarded as a local disorder of this periodically coupled blades system.
J. H. Kuang, B. W. Huang
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Blade Manufacturing Tolerances Definition for a Mistuned Industrial Bladed Disk [PDF]
This paper deals with the characterization of the blade manufacturing geometric tolerances in order to get a given level of amplification in the forced response of a mistuned bladed-disk. The theory is based on the use of a nonparametric probabilistic model of blade random uncertainties. The dispersion parameters controlling the nonparametric model are
Capiez-Lernout, Evangéline +4 more
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Vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique [PDF]
The arrangement optimization algorithm of blades can reduce the vibration localization of mistuned bladed disk in a compressor of aero-engine, however, it will destroy the dynamic balance of bladed disk. A new arrangement optimization method of isolation
Hongyuan Zhang, Hongyun Sun, Huiqun Yuan
core +1 more source
Tabu genetic cat swarm optimization algorithm is proposed for optimization arrangement on mistuned blades. Furthermore, it is improved to be an innovative parallel algorithm based on Compute Unified Device Architecture (CUDA), whose performance is ...
Yi Cai +4 more
doaj +1 more source
Research on vibration localization of mistuned bladed disk system [PDF]
In order to assess the vibration localization influences of different parameters of structural of the mistuned bladed disk system, the pre-stressed component mode synthesis method was adopted, and reduced-order models (ROMs) of the aero-engine compressor
Tianyu Zhao +3 more
core +2 more sources
Dynamic Analysis of a Bladed Disk With Friction and Fretting-Wear in Blade Attachments [PDF]
Assembled bladed disks have many contact interfaces (blade-disk joint, blade shrouds, friction dampers...). Because of relative displacements at these interfaces, fretting-wear occurs, which affects negatively the lifetime of the structure. Methods exist to predict fretting-wear in quasi-static analysis.
Salles, Loïc +4 more
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Detuning Optimization of Nonlinear Mistuned Bladed-Disks
Abstract One major industrial challenge is to consider the detuning as a technological means to reduce the dynamical amplifications induced by mistuning. Due to technological evolutions, the nonlinear geometrical effects induced by the large displacements cannot longer be neglected.
Capiez-Lernout, Evangéline +1 more
openaire +2 more sources

