Results 21 to 30 of about 73,894 (273)

Stator Design Method in Rotor–Stator Interference Flow Fields in Order to Suppress the Vibration of Bladed Disks

open access: yesApplied Sciences, 2022
Based on the computation and analysis of three-dimensional unsteady flow induced by rotor/stator interactions, the characteristics of flow excitation towards bladed disks were studied, including frequency components and circumferential wave components ...
Haoran Ma, Zhou Zhou, Lin Li
doaj   +1 more source

Analysis of the Mode Shapes of Kaplan Runners

open access: yesApplied Sciences, 2022
To prevent lifetime shortening and premature failure in turbine runners, it is of paramount importance to analyse and understand its dynamic response and determine the factors that affect it.
Greco Moraga   +4 more
doaj   +1 more source

Study on the friction damping characteristics of bladed disk (Comparison of microslip model and macroslip model)

open access: yesNihon Kikai Gakkai ronbunshu, 2022
The vibration characteristics of a bladed disk with the continuous ring type structure have been studied extensively, and the vibration response analyses considering the friction damping between adjacent shrouds have been performed in the recent blade ...
Yasutomo KANEKO   +3 more
doaj   +1 more source

Blade Manufacturing Tolerances Definition for a Mistuned Industrial Bladed Disk [PDF]

open access: yesJournal of Engineering for Gas Turbines and Power, 2004
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
openaire   +2 more sources

Study on the friction damping characteristics of bladed disk (Effect of the friction model on the transient response passing through resonance)

open access: yesNihon Kikai Gakkai ronbunshu, 2022
The vibration characteristics of a bladed disk with the continuous ring type structure have been studied extensively, and the vibration response analyses considering the friction damping between adjacent shrouds have been performed in the blade design ...
Yasutomo KANEKO   +2 more
doaj   +1 more source

Modelling friction contacts in structural dynamics and its application to turbine bladed disks [PDF]

open access: yes, 2011
Non
ZUCCA, Stefano   +6 more
core   +1 more source

Validation of a Modal Work Approach for Forced Response Analysis of Bladed Disks

open access: yesApplied Sciences, 2021
The paper describes a numerical method based on a modal work approach to evaluate the forced response of bladed disks and its validation against numerical results obtained by a commercial FEM code.
Lorenzo Pinelli   +4 more
doaj   +1 more source

Dynamic Analysis of a Bladed Disk With Friction and Fretting-Wear in Blade Attachments [PDF]

open access: yesVolume 6: Structures and Dynamics, Parts A and B, 2009
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
openaire   +1 more source

Vibration Characteristics of Rotating Mistuned Bladed Disks considering the Coriolis Force, Spin Softening, and Stress Stiffening Effects

open access: yesShock and Vibration, 2019
Bladed disks of engine rotors usually operate at harsh conditions of high rotating speeds, which may lead to nonnegligible rotordynamic effects, including Coriolis force, spin softening, and stress stiffening effects.
Shuai Wang   +3 more
doaj   +1 more source

A Modal Interpretation for Aeroelastic Stability Enhancement of Mistuned Bladed Disks

open access: yesAerospace, 2022
Understanding the mechanism of the aeroelastic stability improvement induced by mistuning is essential for the design of bladed disks in aero-engines. In this paper, a quantitative interpretation is given. It starts by projecting the mistuned aeroelastic
Xin Liu, Yu Fan, Lin Li, Xiaoping Yu
doaj   +1 more source

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