Geometric Mistuning Identification of Integrally Bladed Rotors Using Modified Modal Domain Analysis

Author:

Bhartiya Yasharth1,Sinha Alok2

Affiliation:

1. ANSYS, Inc., Canonsburg, PA 15317 e-mail:

2. Department of Mechanical and Nuclear Engineering, The Pennsylvania State University, University Park, PA 16802 e-mail:

Abstract

Modified modal domain analysis (MMDA) is a novel method for the development of a reduced order model of a bladed rotor with geometric mistuning. This method utilizes proper orthogonal decomposition (POD) of coordinate measurement machine (CMM) data on blades' geometries, and sector analyses using ansys and solid modeling. In a recent paper, MMDA has been extended to use second order Taylor series approximations of perturbations in mass and stiffness matrices (δM and δK) instead of exact δM and δK. Taylor series expansions of deviations in mass and stiffness matrices due to geometric mistuning give a direct approach for generating the reduced order model from the components of POD features of spatial variations in blades' geometries. Reversing the process, algorithms for mistuning identification based on MMDA are presented in this paper to calculate the geometric mistuning parameters. Two types of algorithm, one based on modal analyses and the other on the forced responses, are presented. The validity of these methods are then verified through a mistuned academic rotor.

Publisher

ASME International

Subject

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

Reference12 articles.

1. Effect of Mistuning on the Vibration of Turbomachinery Blades Induced by Wakes;J. Mech. Eng. Sci.,1966

2. Identification of Mistuning Characteristics of Bladed Disks From Free Response Data—Part I;ASME J Gas Turbines Power,2001

3. Identification of Mistuning Characteristics of Bladed Disks From Free Response Data—Part II;ASME J Gas Turbines Power,2001

4. Lim, S. H., Pierre, C., and Castanier, M. P., 2004, “Mistuning Identification and Reduced-Order Model Updating for Bladed Disks on a Component Mode Mistuning Technique,” 9th National Turbine Engine High Cycle Fatigue Conference, Pinehurst, NC, March 16–19.

5. Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part 1: Theory;ASME J. Turbomach.,2004

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