Analytical investigation of the SAFE diagram for bladed wheels, numerical and experimental validation

Abstract Compressor and turbine bladed wheels interact with the fluid distributed by the stator vanes. They are subject to vibration and fatigue loading, especially when resonance conditions are excited. Avoiding resonance is fundamental when designing bladed wheels. The Campbell diagram approach is too conservative since bladed wheels show many close frequency natural modes, thus it is almost impossible to avoid frequency matching. Singh׳s Advanced Frequency Evaluation (SAFE) diagram, or interference diagram, also introduces shape matching in addition to the frequency, for resonance prediction, therefore many frequency matching cases can be identified as non-critical and thus tolerated. The present paper explains and demonstrates the SAFE diagram by introducing an analytical expression to identify bladed wheel resonance conditions. The mode shape matching with a harmonic component is investigated by means of specific examples. Symmetry properties of the matching distribution of harmonic indices and mode shapes are also introduced and demonstrated. Finally, a bladed wheel analysis is used for validation, both in FE simulations and experiments.

[1]  R. Bishop,et al.  The Mechanics of Vibration , 2011 .

[2]  Murari P. Singh,et al.  Fatigue Damage Of Steam Turbine Blade Caused By Frequency Shift Due To Solid Buildup - A Case Study. , 1994 .

[3]  R. Abhari,et al.  Experimental Study on Impeller Blade Vibration During Resonance—Part I: Blade Vibration Due to Inlet Flow Distortion , 2009 .

[4]  E. Christensen Structural Dynamic Analysis of Cyclic Symmetric Structures , 2005 .

[5]  P BlochHeinz,et al.  STEAM TURBINES DESIGN, APPLICATIONS, AND RE-RATING , 2009 .

[6]  Teresa Maria Berruti,et al.  A Test Rig for Noncontact Traveling Wave Excitation of a Bladed Disk With Underplatform Dampers , 2011 .

[7]  David A. Evensen Vibration Analysis of Multi-Symmetric Structures , 1975 .

[8]  C. Hah,et al.  Inlet Flow Distortion and Unsteady Blade Response in a Transonic Axial-Compressor Rotor , 1999 .

[9]  William E. Sullivan,et al.  Resonance Identification For Impellers. , 2003 .

[10]  Indranil Chattoraj,et al.  An investigation of the failure of low pressure steam turbine blades , 1998 .

[11]  A. Demeulenaere,et al.  Unsteady Blade and Disk Resonant Stress Analysis Due to Supersonic Inlet Guide Vane Wakes , 2008 .

[12]  J. S. Rao,et al.  Turbomachine blade damping , 2003 .

[13]  P. S. Heyns,et al.  Online condition monitoring of axial-flow turbomachinery blades using rotor-axial Eulerian laser Doppler vibrometry , 2009 .

[14]  R Coats,et al.  BLADE FAILURES IN THE H.P. TURBINES OF R.M.S. QUEEN ELIZABETH 2 AND THEIR RECTIFICATION , 1970 .

[15]  Lee,et al.  [American Institute of Aeronautics and Astronautics 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Austin, Texas ()] 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Aeroelastic Studies on a Folding Wing Configuration , 2005 .

[16]  M. P. Singh,et al.  Reliability evaluation of shrouded blading using the SAFE Interference Diagram , 1989 .

[17]  F. Kushner,et al.  Rotating Component Modal Analysis And Resonance Avoidance Recommendations. , 2004 .

[18]  Pavel Polach Evaluation of the Suitability of the Bladed Disk Design Regarding the Danger of the Resonant Vibration Excitation , 2011 .

[19]  T. G. Sofrin,et al.  Axial Flow Compressor Noise Studies , 1962 .

[20]  X. Sheng,et al.  Model identification and order response prediction for bladed wheels , 2009 .

[21]  John Vargo,et al.  Safe Diagram - A Design And Reliability Tool For Turbine Blading. , 1988 .

[22]  Matthew P. Castanier,et al.  Modeling and Analysis of Mistuned Bladed Disk Vibration: Status and Emerging Directions , 2006 .

[23]  Yves Bidaut,et al.  Identification of Eigenmodes and Determination of the Dynamical Behaviour of Open Impellers , 2012 .