The governing equations of motion for a rotating flexible blade-rigid disk-flexible shaft system are derived. The bladed disk is attached at one end of an asymmetric shaft with uniformly distributed mass, mass moment of inertia, and stiffness. The shaft is held by two isotropic supports; one at the far end from the bladed disk, modeled by two translational and two rotational springs, and an intermediate support, modeled by two translational springs only. The effect of shaft asymmetry on the dynamics behavior of the rotating bladed disk shaft system is examined over a wide range of rotational speed, and for different combinations of springs’ stiffness, which determines the type of shaft supports. The cantilever, and the simply supported shaft with an over hang can be looked upon as special cases of the described above shaft configuration, since the former is obtained by assigning large stiffness for both translational and rotational springs at the end support, and zero spring stiffness at the intermediate one, whereas the latter is obtained by assigning large stiffness for the translational springs at both supports and zero stiffness for the rotational springs. Stability boundaries are calculated, and presented in terms of shaft asymmetry and rotor speed for given bearing stiffness.
Skip Nav Destination
ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1997
Orlando, Florida, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7871-2
PROCEEDINGS PAPER
Stability Analysis for Unsymmetrical Shaft With Flexible Bladed-Disk
Samer Masoud,
Samer Masoud
University of Science and Technology, Irbid, Jordan
Search for other works by this author on:
Naim Khader
Naim Khader
University of Science and Technology, Irbid, Jordan
Search for other works by this author on:
Samer Masoud
University of Science and Technology, Irbid, Jordan
Naim Khader
University of Science and Technology, Irbid, Jordan
Paper No:
97-GT-201, V004T14A038; 27 pages
Published Online:
December 24, 2014
Citation
Masoud, S, & Khader, N. "Stability Analysis for Unsymmetrical Shaft With Flexible Bladed-Disk." Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award. Orlando, Florida, USA. June 2–5, 1997. V004T14A038. ASME. https://doi.org/10.1115/97-GT-201
Download citation file:
172
Views
Related Proceedings Papers
Related Articles
Coupling of a State-Space Inflow to Nonlinear Blade Equations and Extraction of Generalized Aerodynamic Force Mode Shapes
Appl. Mech. Rev (November,1993)
An Improved Transfer Matrix-Direct Integration Method for Rotor Dynamics
J. Vib., Acoust., Stress, and Reliab (April,1986)
Instability and Chaos of a Flexible Rotor Ball Bearing System: An Investigation on the Influence of Rotating Imbalance and Bearing Clearance
J. Eng. Gas Turbines Power (August,2011)
Related Chapters
Average Shaft Centerline Plots
Fundamentals of Rotating Machinery Diagnostics
Summary and Conclusions
Bearing Dynamic Coefficients in Rotordynamics: Computation Methods and Practical Applications
Research on an Electric Loading System without Inertia Disk for Actuators
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3