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Journal ArticleDOI

Testing and Calibration Procedures for Mistuning Identification and Traveling Wave Excitation of Blisks

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TLDR
In this article, an integrated testing and calibration procedure is presented for performing mistuning identification (ID) and traveling wave excitation (TWE) of one-piece bladed disks (blisks).
Abstract
In this work, an integrated testing and calibration procedure is presented for performing mistuning identification (ID) and traveling wave excitation (TWE) of one-piece bladed disks (blisks). The procedure yields accurate results while also being highly efficient and is comprised of three basic phases. First, selected modes from a tuned blisk finite element model are used to determine a minimal set of measurement degrees of freedom (and locations) that will work well for mistuning ID. Second, a testing procedure is presented that allows the mistuning to be identified from relatively few vibration response measurements. A numerical validation is used to investigate the convergence of the mistuning ID results to a prescribed mistuning pattern using the proposed approach and alternative testing strategies. Third, a method is derived to iteratively calibrate the excitation applied to each blade so that differences among the blade excitation magnitudes can be minimized for single blade excitation, and also the excitation phases can be accurately set to achieve the desired traveling wave excitation. The calibration algorithm uses the principle of reciprocity and involves solving a least squares problem to reduce the effects of measurement noise and uncertainty. Because the TWE calibration procedure re-uses data collected during the mistuning ID, the overall procedure is integrated and efficient.Copyright © 2009 by ASME

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Citations
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Journal ArticleDOI

Reduced-Order Model Construction Procedure for Robust Mistuning Identification of Blisks

TL;DR: In this article, a procedure is introduced for constructing a reduced-order model referred to as the inverse ROM (IROM) that is well suited for solving the mistuning identication inverse problem.
Journal ArticleDOI

A Test Rig for Non-Contact Travelling Wave Excitation of a Bladed Disk With Underplatform Dampers

TL;DR: In this article, a static test rig called "Octopus" is presented for the validation of numerical models aimed at calculating the nonlinear dynamic response of a bladed disk with under-platform dampers (UPDs).
Journal ArticleDOI

Nodal energy weighted transformation: A mistuning projection and its application to FLADE™ turbines

TL;DR: In this paper, a nodal energy weighted transformation (NewT) was proposed to construct a reduced-order model of a blisk and a dual flow path system, such as a FLADE turbine.
Journal ArticleDOI

Detection of Cracks in Mistuned Bladed Disks Using Reduced-Order Models and Vibration Data

TL;DR: In this article, a hybrid-interface method based on component mode synthesis is employed to develop reduced order models (ROMs) of the tuned system with a cracked blade, and the resulting (reducedorder) nonlinear equations of motion are solved by applying an alternating frequency/time-domain method.
Journal ArticleDOI

A component damping identification method for mistuned blisks

TL;DR: In this article, a new method is introduced which identifies the component damping of a structure, and the method is applied to mistuned blisks in regions of low and high modal density.
References
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Journal ArticleDOI

Sensor placement for on-orbit modal identification and correlation of large space structures

TL;DR: In this paper, a method for the selection of a set of sensor locations from a larger candidate set for the purpose of on-orbit identification and correlation of large space structures is presented.
Proceedings ArticleDOI

Sensor Placement for On-Orbit Modal Identification and Correlation of Large Space Structures

TL;DR: In this paper, a method for the selection of a set of sensor locations from a larger candidate set for the purpose of on-orbit identification and correlation of large space structures is presented.
Journal ArticleDOI

Modeling and Analysis of Mistuned Bladed Disk Vibration: Status and Emerging Directions

TL;DR: The literature on reduced-order modeling, simulation, and analysis of the vibration of bladed disks found in gas-turbine engines is reviewed in this paper, where an emphasis is placed on key developments in the last decade that have enabled better prediction and understanding of the forced response of mistuned bladed disk, especially with respect to assessing and mitigating the harmful impact of mistuning on blade vibration, stress increases, and attendant high cycle fatigue.
Journal ArticleDOI

Flutter and Resonant Vibration Characteristics of Engine Blades

TL;DR: In this article, the authors present an in-depth study of blade vibration problems that seriously impact development of advanced gas turbine configurations, and they conclude that structural integrity of power plants is the dominant factor that influences the quality, reliability, and marketability of the product.
Journal ArticleDOI

Compact, Generalized Component Mode Mistuning Representation for Modeling Bladed Disk Vibration

TL;DR: In this article, a component-based modeling framework is developed by partitioning the system into a tuned bladed disk component and virtual blade mistuning components, defined by the differences between the mistuned and tuned blade mass and stiffness matrices.
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