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 a 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 the data collected during the mistuning ID, the overall procedure is integrated and efficient.

1.
Srinivasan
,
A. V.
, 1997, “
Flutter and Resonant Vibration Characteristics of Engine Blades
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
119
(
4
), pp.
742
775
.
2.
Slater
,
J. C.
,
Minkiewicz
,
G. R.
, and
Blair
,
A. J.
, 1999, “
Forced Response of Bladed Disk Assemblies—A Survey
,”
Shock Vib. Dig.
0583-1024,
31
(
1
), pp.
17
24
.
3.
Castanier
,
M. P.
, and
Pierre
,
C.
, 2006, “
Modeling and Analysis of Mistuned Bladed Disk Vibration: Status and Emerging Directions
,”
J. Propul. Power
0748-4658,
22
(
2
), pp.
384
396
.
4.
Thomson
,
D. E.
, and
Griffin
,
J. T.
, 1999, “
The National Turbine Engine High Cycle Fatigue Program
,”
The Global Gas Turbine Newsletter (GGTN)
,
39
(
1
), pp.
14
17
.
5.
Judge
,
J.
,
Pierre
,
C.
, and
Ceccio
,
S. L.
, 2001, “
Experimental Identification of Mistuning in Blisks
,”
Proceedings of the 6th National Turbine Engine High Cycle Fatigue Conference
,
Universal Technology Corporation
,
Dayton, OH
.
6.
Judge
,
J.
,
Pierre
,
C.
, and
Ceccio
,
S. L.
, 2001, “
Experimental Validation of Mistuning Identification Techniques and Vibration Predictions in Bladed Disks
,”
Proceedings of the International Forum on Aeroelasticity and Structural Dynamics
, Madrid, Spain.
7.
Mignolet
,
M.
,
Rivas-Guerra
,
A.
, and
Delor
,
J.
, 2001, “
Identification of Mistuning Characteristics of Bladed Disks From Free Response Data—Part I
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
123
(
2
), pp.
395
403
.
8.
Rivas-Guerra
,
A.
,
Mignolet
,
M.
, and
Delor
,
J.
, 2001, “
Identification of Mistuning Characteristics of Bladed Disks From Free Response Data—Part II
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
123
(
2
), pp.
404
411
.
9.
Pichot
,
F.
,
Thouverez
,
F.
,
Jezequel
,
L.
, and
Seinturier
,
E.
, 2001, “
Mistuning Parameters Identification of a Bladed Disk
,”
Key Eng. Mater.
1013-9826,
204–205
, pp.
123
132
, URL: http://www.scientific.nethttp://www.scientific.net.
10.
Judge
,
J.
,
Pierre
,
C.
, and
Mehmed
,
O.
, 2001, “
Experimental Investigation of Mode Localization and Forced Response Amplitude Magnification for a Mistuned Bladed Disk
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
123
(
4
), pp.
940
950
.
11.
Judge
,
J. A.
,
Pierre
,
C.
, and
Ceccio
,
S. L.
, 2002, “
Mistuning Identification in Bladed Disks
,”
Proceedings of the International Conference on Structural Dynamics Modelling
, Madeira, Portugal.
12.
Pierre
,
C.
,
Judge
,
J.
,
Ceccio
,
S. L.
, and
Castanier
,
M. P.
, 2002, “
Experimental Investigation of the Effects of Random and Intentional Mistuning on the Vibration of Bladed Disks
,”
Proceedings of the 7th National Turbine Engine High Cycle Fatigue Conference
,
Universal Technology Corporation
,
Dayton, OH
.
13.
Feiner
,
D. M.
, and
Griffin
,
J.
, 2003, “
A Completely Experimental Method of Mistuning Identification in Integrally Bladed Rotors
,”
Proceedings of the 8th National Turbine Engine High Cycle Fatigue Conference
,
Universal Technology Corporation
,
Dayton, OH
, pp.
1.1
1.13
.
14.
Kim
,
N. E.
, and
Griffin
,
J.
, 2003, “
System Identification in Higher Modal Density Regions of Bladed Disks
,”
Proceedings of the 8th National Turbine Engine High Cycle Fatigue Conference
,
Universal Technology Corporation
,
Dayton, OH
, pp.
1.68
1.82
.
15.
Feiner
,
D.
, and
Griffin
,
J.
, 2004, “
Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part I: Theory
,”
ASME J. Turbomach.
0889-504X,
126
(
1
), pp.
150
158
.
16.
Feiner
,
D.
, and
Griffin
,
J.
, 2004, “
Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part II: Application
,”
ASME J. Turbomach.
0889-504X,
126
(
1
), pp.
159
165
.
17.
Lim
,
S. -H.
,
Castanier
,
M. P.
, and
Pierre
,
C.
, 2004, “
Mistuning Identification and Reduced-Order Model Updating for Bladed Disks Based on a Component Mode Mistuning Technique
,”
Proceedings of the 9th National Turbine Engine High Cycle Fatigue Conference
,
Universal Technology Corporation
,
Dayton, OH
.
18.
Lim
,
S. -H.
,
Pierre
,
C.
, and
Castanier
,
M. P.
, 2006, “
Predicting Blade Stress Levels Directly From Reduced-Order Vibration Models of Mistuned Bladed Disks
,”
ASME J. Turbomach.
0889-504X,
128
(
1
), pp.
206
210
, URL: http://dx.doi.org/10.1115/1.2098754http://dx.doi.org/10.1115/1.2098754.
19.
Lim
,
S.
,
Bladh
,
R.
,
Castanier
,
M. P.
, and
Pierre
,
C.
, 2007, “
Compact, Generalized Component Mode Mistuning Representation for Modeling Bladed Disk Vibration
,”
AIAA J.
0001-1452,
45
(
9
), pp.
2285
2298
.
20.
Li
,
J.
,
Pierre
,
C.
, and
Ceccio
,
S. L.
, 2005, “
Validation of a New Technique for Mistuning Identification and Model Updating Based on Experimental Results for an Advanced Bladed Disk Prototype
,”
Evaluation, Control and Prevention of High Cycle Fatigue in Gas Turbine Engines for Land, Sea and Air Vehicles (Meeting Proceedings RTO-MP-AVT-121)
,
NATO Research and Technology Organisation
,
Neuilly-sur-Seine, France
, pp.
36.1
36.16
.
21.
Pichot
,
F.
,
Laxalde
,
D.
,
Sinou
,
J. J.
,
Thouverez
,
F.
, and
Lombard
,
J. P.
, 2006, “
Mistuning Identification for Industrial Blisks Based on the Best Achievable Eigenvector
,”
Comput. Struct.
0045-7949,
84
(
29–30
), pp.
2033
2049
.
22.
Laxalde
,
D.
,
Thouverez
,
F.
,
Sinou
,
J. -J.
,
Lombard
,
J. -P.
, and
Baumhauer
,
S.
, 2007, “
Mistuning Identification and Model Updating of an Industrial Blisk
,”
Int. J. Rotating Mach.
1023-621X,
2007
(
17289
), pp.
1
10
, URL: http://dx.doi.org/10.1155/2007/17289http://dx.doi.org/10.1155/2007/17289.
23.
Li
,
J.
, 2007, “
Experimental Investigation of Mistuned Bladed Disks System Vibration
,” Ph.D. thesis, University of Michigan, Ann Arbor, MI.
24.
Madden
,
A. C.
,
Castanier
,
M. P.
, and
Epureanu
,
B. I.
, 2008, “
Reduced-Order Model Construction Procedure for Robust Mistuning Identification of Blisks
,”
AIAA J.
0001-1452,
46
(
11
), pp.
2890
2898
.
25.
Judge
,
J. A.
, 2002, “
Experimental Investigations of the Effects of Mistuning on Bladed Disk Dynamics
,” Ph.D. thesis, University of Michigan, Ann Arbor, MI.
26.
Penny
,
J. E. T.
,
Friswell
,
M. I.
, and
Garvey
,
S. D.
, 1994, “
Automatic Choice of Measurement Locations for Dynamic Testing
,”
AIAA J.
0001-1452,
32
(
2
), pp.
407
414
.
27.
Kammer
,
D. C.
, 1991, “
Sensor Placement for On-Orbit Modal Identification and Correlation of Large Space Structures
,”
J. Guid. Control Dyn.
0731-5090,
14
(
2
), pp.
251
259
.
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