Probabilistic Response of a Bladed Disk With Uncertain Geometry

Author:

Carassale Luigi1,Cavicchi Andrea2,Bruzzone Silvia2,Marrè Brunenghi Michela2

Affiliation:

1. Department of Mechanical, Energy, Management and Transportation Engineering, University of Genova, Genova 16145, Italy

2. Ansaldo Energia, Genova 16152, Italy

Abstract

AbstractGeometric uncertainties in the blade manufacturing process have important consequences in terms of dynamical properties of bladed disks. In this paper, we address the problem of modeling a full bladed disk composed by blades having uncertain geometry. The geometric imperfection of the blades is represented and analyzed according to a procedure previously presented by the authors, based on the principal component analysis (PCA) and the mesh morphing. The dynamical model of the full disk is constructed following the component mode synthesis (CMS) approach. The blade geometry is represented using a probabilistic model constructed from an experimental dataset. The effect of the geometric uncertainties is assessed using a linear uncertainty propagation approach, leading to a procedure that is fast enough to be embedded into a Monte Carlo simulation (MCS) loop.

Publisher

ASME International

Subject

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

Reference22 articles.

1. Representation and Analysis of Geometric Uncertainties in Rotor Blades,2018

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3. Coupling of Substructures for Dynamic Analyses;AIAA J.,1968

4. Interface Reduction in Craig–Bampton Component Mode Synthesis by Orthogonal Polynomial Series;ASME J. Eng. Gas Turbines Power,2017

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