Variation in the stability of a rotating blade disk with a local crack defect

The effect of a near root local blade crack on the stability of a grouped blade disk is investigated in this paper. A bladed disk comprised of periodically shrouded blades is used to simulate the coupled periodic structure. The blade crack is modeled using the local flexibility with coupling terms....

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Published inJournal of sound and vibration Vol. 294; no. 3; pp. 486 - 502
Main Authors Huang, Bo-Wun, Kuang, Jao-Hwa
Format Journal Article
LanguageEnglish
Published London Elsevier Ltd 01.06.2006
Elsevier
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ISSN0022-460X
1095-8568
DOI10.1016/j.jsv.2005.11.028

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Abstract The effect of a near root local blade crack on the stability of a grouped blade disk is investigated in this paper. A bladed disk comprised of periodically shrouded blades is used to simulate the coupled periodic structure. The blade crack is modeled using the local flexibility with coupling terms. The mode localization phenomenon introduced by the blade crack on the longitudinal and bending vibrations in the rotating blades has also been considered. Using the Galerkin's method, the imperturbation equations of a bladed disk in which one of the blades is cracked, subject to fluctuations in the rotation speed, can be derived. Employing the multiple scales method, the boundaries of the instability zones in the mistuned turbo blade system are approximated. Numerical results indicate that an additional unstable zone is introduced near the localization frequency and the regions of unstable zones are varied with the crack size and fluctuations in disk speed.
AbstractList The effect of a near root local blade crack on the stability of a grouped blade disk is investigated in this paper. A bladed disk comprised of periodically shrouded blades is used to simulate the coupled periodic structure. The blade crack is modeled using the local flexibility with coupling terms. The mode localization phenomenon introduced by the blade crack on the longitudinal and bending vibrations in the rotating blades has also been considered. Using the Galerkin's method, the imperturbation equations of a bladed disk in which one of the blades is cracked, subject to fluctuations in the rotation speed, can be derived. Employing the multiple scales method, the boundaries of the instability zones in the mistuned turbo blade system are approximated. Numerical results indicate that an additional unstable zone is introduced near the localization frequency and the regions of unstable zones are varied with the crack size and fluctuations in disk speed. A cross section area of the blade a depth of crack b width of the blade c.c. complex conjugate of the preceding term E Young's modulus of material of blade F(t) the varying rotating speed s the number of blade I moment of inertia ks the stiffness L length of cantilever beam N total number of blades {p}s{q}s displacement vectors of the radial and transverse directions of sth blade determined coefficient for radial and transverse direction for the sth blade, i=1,2,...,5 Rc position of coupled spring RhRo inner and outer diameter of disk r arbitrary position on the blade dimensionless cracked position on the blade t thickness of the blade us(r,t) deflection in radial direction of the sth blade vs(r,t) deflection in transverse direction of the sth blade dimensionless stiffness perturbation frequency epsilon perturbation parameter lambdai coefficient rho density of blade sigmai coefficient comparison functions Omega rotation speed Omega0 the steady-state rotating speed excitating frequency on the system the lowest natural frequency of the tuned system natural frequency of the mistuned system
The effect of a near root local blade crack on the stability of a grouped blade disk is investigated in this paper. A bladed disk comprised of periodically shrouded blades is used to simulate the coupled periodic structure. The blade crack is modeled using the local flexibility with coupling terms. The mode localization phenomenon introduced by the blade crack on the longitudinal and bending vibrations in the rotating blades has also been considered. Using the Galerkin's method, the imperturbation equations of a bladed disk in which one of the blades is cracked, subject to fluctuations in the rotation speed, can be derived. Employing the multiple scales method, the boundaries of the instability zones in the mistuned turbo blade system are approximated. Numerical results indicate that an additional unstable zone is introduced near the localization frequency and the regions of unstable zones are varied with the crack size and fluctuations in disk speed.
Author Kuang, Jao-Hwa
Huang, Bo-Wun
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  surname: Huang
  fullname: Huang, Bo-Wun
  organization: Department of Mechanical Engineering, Cheng Shiu University, Kaohsiung, Taiwan, ROC
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  givenname: Jao-Hwa
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  fullname: Kuang, Jao-Hwa
  email: kuang@mail.nsysu.edu.tw
  organization: Department of Mechanical and Electromechanical Engineering, National Sun Yat-Sen University, Kaohsiung, Taiwan, ROC
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Issue 3
Keywords Longitudinal crack
Localized mode
Blade shroud
Rotation speed
Modeling
Varying speed
Cantilever beam
Periodic structure
Longitudinal vibration
Multiscale method
Rotating disk
Crack length
Turbine blade
Defect
Galerkin method
Bending vibration
Rotating beam(mechanics)
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Snippet The effect of a near root local blade crack on the stability of a grouped blade disk is investigated in this paper. A bladed disk comprised of periodically...
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SubjectTerms Exact sciences and technology
Fracture mechanics (crack, fatigue, damage...)
Fundamental areas of phenomenology (including applications)
Physics
Solid mechanics
Structural and continuum mechanics
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
Title Variation in the stability of a rotating blade disk with a local crack defect
URI https://dx.doi.org/10.1016/j.jsv.2005.11.028
https://www.proquest.com/docview/29782025
Volume 294
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