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 in | Journal of sound and vibration Vol. 294; no. 3; pp. 486 - 502 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
London
Elsevier Ltd
01.06.2006
Elsevier |
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Online Access | Get full text |
ISSN | 0022-460X 1095-8568 |
DOI | 10.1016/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. |
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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 |
Author_xml | – sequence: 1 givenname: Bo-Wun surname: Huang fullname: Huang, Bo-Wun organization: Department of Mechanical Engineering, Cheng Shiu University, Kaohsiung, Taiwan, ROC – sequence: 2 givenname: Jao-Hwa surname: Kuang 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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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 |
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