Vibration Measurement of Rotating Blades Using a Root Embedded PZT Sensor

Finite element and experimental studies are carried out to test the suitability of a piezoelectric (PZT) sensor in measuring vibrations of blades modeled as beams. The rotating system contains twelve blades mounted to the shaft through a rotor. The PZT sensor is secured in the root between the rotor and blade. First, finite element results are obtained using the finite element package ANSYS. A modal analysis is performed on the system to identify modes and mode shapes. Transient, harmonic and steady-state responses are then computed to test the ability of the PZT sensor in generating signals for blade vibrations. For the experimental part, the blade vibration signals are produced using the PZT sensor and a strain-gage, and the outputs are compared with each other. From both the finite element and experimental results, it is concluded that the root-embedded PZT sensor can be effectively used for blade vibration measurements in a wide range of cases.

[1]  J. S. Rao,et al.  Determination of Blade Stresses Under Constant Speed and Transient Conditions With Nonlinear Damping , 1996 .

[2]  B. O. Al-Bedoor Reduced-Order Nonlinear Dynamic Model of Coupled Shaft-Torsional and Blade-Bending Vibrations in Rotors , 2001 .

[3]  Daniel J. Inman,et al.  Coupled bending-bending-torsion vibration of a rotating pre-twisted beam with aerofoil cross-section and flexible root by finite element method , 2004 .

[4]  Y. N. Al-Nassar,et al.  On the vibration of a rotating blade on a torsionally flexible shaft , 2003 .

[5]  E. F. Crawley,et al.  Analytical and Experimental Investigation of the Coupled Bladed Disk/Shaft Whirl of a Cantilevered Turbofan , 1986 .

[6]  B. O. Al-Bedoor,et al.  Dynamic model of coupled shaft torsional and blade bending deformations in rotors , 1999 .

[7]  R. Loewy Structural dynamics studies of rotating bladed-disk assemblies coupled with flexible shaft motions , 1983 .

[8]  Earl H. Dowell,et al.  Experimental and Theoretical Study for Nonlinear Aeroelastic Behavior of a Flexible Rotor Blade , 1992 .

[9]  R. A. Cookson,et al.  A Fiber-Optic Laser-Doppler Probe for Vibration Analysis of Rotating Machines , 1979 .

[10]  K. Mathioudakis,et al.  Casing Vibration and Gas Turbine Operating Conditions , 1989 .

[11]  A. V. Srinivasan,et al.  Vibrations of Bladed-Disk Assemblies—A Selected Survey (Survey Paper) , 1984 .

[12]  Osami Matsushita,et al.  An Equivalent Reduced Modelling Method and its Application to Shaft—Blade Coupled Torsional Vibration Analysis of a Turbine—Generator Set , 1991 .

[13]  Ranjan Ganguli,et al.  Helicopter rotor blade frequency evolution with damage growth and signal processing , 2005 .

[14]  P Castellini,et al.  Vibration measurements on blades of a naval propeller rotating in water with tracking laser vibrometer , 1998 .

[15]  A. J. Scalzo,et al.  Analysis and Solution of a Non-Synchronous Vibration Problem in the Last Row Turbine Blade of a Large Industrial Combustion Turbine , 1986 .

[16]  Olivier A. Bauchau,et al.  Finite Element Approach to Rotor Blade Modeling , 1987 .

[17]  R. S. Abhari,et al.  Optimum Strain Gage Application to Bladed Assemblies , 2002 .

[18]  A. Muszynska,et al.  Periodic and Continuous Vibration Monitoring for Preventive/Predictive Maintenance of Rotating Machinery , 1987 .

[19]  R. S. Abhari,et al.  Optimum Strain Gauge Application to Bladed Assemblies , 2002 .

[20]  Singiresu S Rao,et al.  Recent Advances in Sensing and Control of Flexible Structures Via Piezoelectric Materials Technology , 1999 .

[21]  B. O. Al-Bedoor TRANSIENT TORSIONAL AND LATERAL VIBRATIONS OF UNBALANCED ROTORS WITH ROTOR-TO-STATOR RUBBING , 2000 .