Maximum bladed disk forced response from distortion of a structural mode

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 4 B, Issue , 2002, Pages 965-980

  Kenyon, J A ^a   Griffin, J H ^b   Feiner, D M ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b CARNEGIE MELLON UNIVERSITY   (United States)

Author keywords

Blade vibration; Forced response; Maximum response; Mistuning; Robust

Indexed keywords

BLADE VIBRATION; FORCED RESPONSE; MISTUNED SYSTEM; STRUCTURAL MISTUNING; STRUCTURAL MODE;

CALCULATIONS; DYNAMIC RESPONSE; FAILURE ANALYSIS; FORCE MEASUREMENT; MACHINE VIBRATIONS;

TURBOMACHINE BLADES;

EID: 0036991784     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30426     Document Type: Conference Paper

References (23)

1. Srinivasan, A.V., 1997, "Flutter and Resonant Vibration Characteristics of Engine Blades," Journal of Engineering for Gas Turbines and Power, 119, 4, pp. 742-775.
2. Kenyon, J.A., and Griffin, J.H. 2001, "Harmonic Mistuning of Turbine Engine Bladed Disks and Implications on Sensitivity to Forced Response," ASME paper 2001-GT-0274, International Gas Turbine Institute Turbo Expo, New Orleans, Louisiana.
3. Kim, M., Moon, J., and Wickert, J.A., 2000, "Spatial Modulation of Repeated Vibration Modes in Rotationally Periodic Structures," Journal of Vibration and Acoustics, 122, pp. 62-68.
4. Ewins, D.J., 1969, "The Effects of Detuning Upon the Forced Vibrations of Bladed Disks," Journal of Sound and Vibration, 9, 1, pp. 65-79.
5. MacBain, J.C., and Whaley, P.W., 1984, "Maximum Resonant Response of Mistuned Bladed Disks," Journal of Vibration, Acoustics, Stress, and Reliability in Design, 106, pp. 218-223.
6. Whitehead, D.S., 1966, "Effect of Mistuning on the Vibration of Turbomachine Blades Induced by Wakes," Journal of Mechanical Engineering Science, 8, 1, pp. 15-21.
7. Whitehead, D.S., 1976, "Research Note: Effect of Mistuning on Forced Vibration of Blades with Mechanical Coupling," Journal of Mechanical Engineering Science, 18, 6, pp. 306-307.
8. Whitehead, D.S., 1998, "The Maximum Factor by Which Forced Vibration of Blades Can Increase Due to Mistuning," Journal of Engineering for Gas Turbines and Power, 120, 1, pp. 115-119.
9. Mignolet, M.P., Hu, W., and Jadic, I., 2000, "On the Forced Response of Harmonically and Partially Mistuned Bladed Disks. Part II: Partial Mistuning, and Applications" International Journal of Rotating Machinery, 6, 1, pp. 43-56.
10. Castanier, M.P., Ottarsson, G., and Pierre, C., 1997, "A Reduced Order Modeling Technique for Mistuned Bladed Disks," Journal of Vibration and Acoustics, 119, 3, pp. 439-447.
11. Kruse, M.J., and Pierre, C., 1996, "Forced Response of Mistuned Bladed Disks Using Reduce-Order Modeling," Proceedings of the 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Salt Lake City, Utah, 4, pp. 1938-1950.
12. Yang, M.-T., and Griffin, J.H., 1997, "A Reduced Order Approach for the Vibration of Mistuned Bladed Disk Assemblies," Journal of Engineering for Gas Turbines and Power, 119, 1, pp. 161-167.
13. Yang, M.-T., and Griffin, J.H., 1999, "A Reduced Order Model of Mistuning Using a Subset of Nominal System Modes," ASME Paper 99-GT-288, International Gas Turbine Institute Turbo Expo, Indianapolis, Indiana.
14. Bladh, R., Castanier, M.P., and Pierre, C., 2000a, "Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks, Part 1: Theoretical Models," ASME Paper 2000-GT-0360, International Gas Turbine Institute Turbo Expo, Munich, Germany.
15. Bladh, R., Castanier, M.P., and Pierre, C., 2000b, "Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks, Part II: Application," ASME Paper 2000-GT-0361, International Gas Turbine Institute Turbo Expo, Munich, Germany.
16. Rivas-Guerra, A.J., and Mignolet, M.P., 2001, "Local/Global Effects of Mistuning on the Forced Response of Bladed Disks," ASME Paper 2001-GT-0289, International Gas Turbine Institute Turbo Expo, New Orleans, Louisiana.
17. Petrov, E.P., and Ewins, D.J., 2001, "Analysis of the Worst Mistuning Patterns in Bladed Disc Assemblies," ASME Paper 2001-GT-0292, International Gas Turbine Institute Turbo Expo, New Orleans, Louisiana.
18. Petrov, E., Sanliturk, K., Ewins, D., and Elliot, R., 2000, "Quantitative Prediction of the Effects of Mistuning Arrangement on Resonant Response of a Practical Turbine Bladed Disks," Proceedings of the 5th National Turbine Engine High Cyclic Fatigue Conference, Chandler, Arizona.
19. Rivas-Guerra, A.J., and Mignolet, M.P., 2001, "Maximum Amplification of Blade Response Due to Mistuning: a Localization-Based Optimization," Proceedings of the 6th National Turbine Engine High Fatigue Conference, Jacksonville, Florida.
20. Sinha, A., 1997, "Computation of the Maximum Amplitude of a Mistuned Bladed Disk Assembly via Infinity Norm," Proceedings of the 1997 ASME International Mechanical Engineering Congress and Exposition, Dallas, Texas, AD-55, pp. 427-432.
21. Stange, W.A., and MacBain, J.C., 1983, "An Investigation of Dual Mode Phenomena in a Mistuned Bladed Disk," Journal of Vibration, Acoustics, Stress, and Reliability in Design, 105, pp. 402-407.
22. Kenyon, J.A., 2002, A Phenomenological Study of Robust Maximum Mistuned Bladed Disk Forced Response, Ph.D. Dissertation, Carnegie Mellon University.
23. Kruze, M.J., and Pierre, C., 1996, "Dynamic Response of an Industrial Turbomachinery Rotor," AIAA Paper 96-2820, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Lake Buena Vista, Florida.