BLADE-TIP TIMING MEASUREMENT OF SYNCHRONOUS VIBRATIONS OF ROTATING BLADED ASSEMBLIES

Blade-tip timing (BTT) is a promising method for the detection, measurement and analysis of blade vibrations in rotating bladed assemblies. However, the intricacies of the method when applied to real rotating structures undergoing synchronous (Engine Ordered) vibrations are not yet fully understood. In this paper, a mathematical model is developed to simulate data from typical BTT tests of rotating assemblies. The simulator is then used in order to provide a qualitative analysis of several phenomena that can be associated with the synchronous vibrations of rotating assemblies, including mistuning, coupling, excitation at multiple Engine Orders and simultaneous synchronous and asynchronous responses. It is concluded that none of these phenomena on its own will render the identification of the frequency and amplitude of blade vibrations impossible. However, there is no single BTT data analysis method that is able to deal with all of these phenomena.

[1]  J. R. Wright Flutter test analysis in the time domain using a recursive system representation , 1974 .

[2]  A. Srinivasan,et al.  Influence of Mistuning on Rotor-Blade Vibrations , 1975 .

[3]  Giancarlo Genta A fast modal technique for the computation of the Campbell diagram of multi-degree-of-freedom rotors , 1992 .

[4]  Mehmet Imregun,et al.  An improved single-parameter tip-timing method for turbomachinery blade vibration measurements using optical laser probes , 1996 .

[5]  Izhak Bucher,et al.  MULTIDIMENSIONAL DECOMPOSITION OF TIME-VARYING VIBRATION RESPONSE SIGNALS IN ROTATING MACHINERY , 1997 .

[6]  A. V. Srinivasan Flutter and Resonant Vibration Characteristics of Engine Blades: An IGTI Scholar Paper , 1997 .

[7]  Steve Heath,et al.  A New Technique for Identifying Synchronous Resonances Using Tip-Timing , 1999 .

[8]  Abdulnaser I. Sayma,et al.  AN INTEGRATED NONLINEAR APPROACH FOR TURBOMACHINERY FORCED RESPONSE PREDICTION. PART I: FORMULATION , 2000 .

[9]  Abdulnaser I. Sayma,et al.  AN INTEGRATED NONLINEAR APPROACH FOR TURBOMACHINERY FORCED RESPONSE PREDICTION. PART II: CASE STUDIES , 2000 .

[10]  Peter J. Fleming,et al.  System identification strategies applied to aircraft gas turbine engines , 2000 .

[11]  M. Zielinski,et al.  Noncontact vibration measurements on compressor rotor blades , 2000 .

[12]  Jianzhong Li,et al.  Numerical analysis of dynamic behavior of stream turbine blade group , 2000 .

[13]  Grigorios Dimitriadis,et al.  A comparison of blade tip timing data analysis methods , 2001 .