Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk

Author:

Seeger Benjamin1,Kohlmann Lukas2,Schoenenborn Harald2,Schwarz Stefan2,Krack Malte3

Affiliation:

1. TTI GmbH/NoVibTech , Stuttgart 70569, Germany

2. MTU Aero Engines AG , Munich 80995, Germany

3. Institute of Aircraft Propulsion Systems, University of Stuttgart , Stuttgart 70569, Germany

Abstract

Abstract We develop a novel method for the identification of mistuned blisks. The method relies on forced response measurements in a certain target frequency band. Modal stiffness deviations and an overall structural damping coefficient are obtained using a least-squares fit, fully consistent with a component-mode-based reduced-order model. To achieve a high frequency resolution in a very short test, we carry out rapid frequency sweeps and use a noise-robust, wavelet-based estimation of the steady-state response. The forcing is eliminated from the equations governing the mistuning parameters, and it is identified separately to reconstruct the forced response if requested. We first validate the method numerically and then apply it experimentally to a compressor blisk with an alternating (B-A) mistuning pattern. While most previous works on mistuning identification are limited to the lowest 1-2 mode families, we assess the method for the seventh (1C) and eighth (3T) mode family. Measured and reconstructed frequency responses are in good to very good agreement. We conclude that the developed method is useful to obtain high-quality estimates of mistuning parameters, which can then be used for vibration prediction.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference35 articles.

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3. Uncertainties of an Automated Optical 3D Geometry Measurement, Modeling, and Analysis Process for Mistuned Integrally Bladed Rotor Reverse Engineering;ASME J. Eng. Gas Turbines Power,2013

4. Geometric Mistuning Identification of Integrally Bladed Rotors Using Modified Modal Domain Analysis;ASME J. Eng. Gas Turbines Power,2014

5. Experimental and Numerical Analysis of Geometrical Induced Mistuning,2015

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