Predicting the influence of cracks on the dynamics of bladed disks is a very important challenge. Cracks change the structural response, which in turn changes the crack propagation characteristics. Hence, accurate and computationally effective means to model the dynamics of cracked bladed disks and blisks is particularly crucial in applications such as prognosis, guidance for repairs, characterization after repairs, design, and structural health monitoring. Most current models of bladed disks exploit cyclic symmetry to gain computational efficiency. However, the presence of cracks and mistuning destroys that symmetry and makes computational predictions much more expensive. In this work, we propose a new reduced order modeling methodology that can speed up computations by several orders of magnitude. There are two key components of the new methodology. First, the displacements and deformations of the crack surfaces are not modeled in absolute coordinates but relative coordinates, which allows for an effective model reduction based on (fixed-interface Craig–Bampton) component mode synthesis (CMS). The use of relative coordinates allows one to define one of the components in CMS as the pristine/uncracked structure (with mistuning). This approach is used in combination with a set of accurate approximations for the constraint modes used in CMS. Second, the effects of mistuning are captured by component mode mistuning, which allows the construction of extremely efficient reduced order models for the pristine/uncracked component with mistuning. The novel proposed method is applied to a finite element model of an industrial blisk. The combined presence of mistuning and cracks is shown to have important effects. Also, the proposed approach is shown to provide accurate predictions for the overall blisk while requiring computations using single-sector models only. The influence of various parameters on the accuracy of the reduced order models is investigated. Overall, the results show a very good agreement between full finite element analyses and the proposed reduced order modeling approach.

1.
Dimarogonas
,
A. D.
, 1970, “
Dynamic Response of Cracked Rotors
,” General Electric Co. Internal Report, Schenectady, NY.
2.
Dimarogonas
,
A. D.
, 1971, “
Dynamics of Cracked Shafts
,” General Electric Co. Internal Report, Schenectady, NY.
3.
Dimarogonas
,
A. D.
, 1976, “
Vibration Engineering
,” West Publishers, St. Paul.
4.
Pafelias
,
T.
, 1974, “
Dynamic Behavior of a Cracked Rotor
,” General Electric Co. Technical Report No. DF-74-LS-79.
5.
Shen
,
M. -H. H.
, and
Pierre
,
C.
, 1994, “
Free Vibrations of Beams With a Single-Edge Crack
,”
J. Sound Vib.
0022-460X,
170
(
2
), pp.
237
259
.
6.
Shen
,
M. -H. H.
, and
Chu
,
Y. C.
, 1992, “
Vibrations of Beams With a Fatigue Crack
,”
Comput. Struct.
0045-7949,
45
(
1
), pp.
79
93
.
7.
Shen
,
M. -H. H.
, and
Pierre
,
C.
, 1990, “
Natural Modes of Bernoulli-Euler Beams With Symmetric Cracks
,”
J. Sound Vib.
0022-460X,
138
(
1
), pp.
115
134
.
8.
Chondros
,
T.
,
Dimarogonas
,
A. D.
, and
Yao
,
J.
, 2001, “
Vibration of a Beam With a Breathing Crack
,”
J. Sound Vib.
0022-460X,
239
(
1
), pp.
57
67
.
9.
Chondros
,
T.
, and
Dimarogonas
,
A. D.
, 1998, “
Vibration of a Crack Cantilever Beam
,”
ASME J. Vibr. Acoust.
0739-3717,
120
(
3
), pp.
742
746
.
10.
Pugno
,
N.
,
Surace
,
C.
, and
Ruotolo
,
R.
, 2000, “
Evaluation of the Non-Linear Dynamic Response to Harmonic Excitation of a Beam With Several Breathing Cracks
,”
J. Sound Vib.
0022-460X,
235
(
5
), pp.
749
762
.
11.
Seo
,
Y. -H.
,
Lee
,
C. -W.
, and
Park
,
K. C.
, 2009, “
Crack Identification in a Rotating Shaft via the Reverse Directional Frequency Response Functions
,”
ASME J. Vibr. Acoust.
0739-3717,
131
(
1
), p.
011012
.
12.
Karthikeyan
,
M.
, and
Talukdar
,
S.
, 2008, “
Development of a Novel Algorithm for a Crack Detection, Localization, and Sizing in a Beam Based on Forced Response Measurements
,”
ASME J. Vibr. Acoust.
0739-3717,
130
(
2
), p.
021002
.
13.
Abraham
,
O. N. L.
, and
Brandon
,
J. A.
, 1995, “
The Modeling of the Opening and Closure of a Crack
,”
ASME J. Vibr. Acoust.
0739-3717,
117
, (3A), pp.
370
377
.
14.
Lee
,
C. -W.
,
Yun
,
J. -S.
, and
Jun
,
O. S.
, 1992, “
Modeling of a Simple Rotor With a Switching Crack and Its Experimental Verification
,”
ASME J. Vibr. Acoust.
0739-3717,
114
(
2
), pp.
217
225
.
15.
Yang
,
M. -T.
, and
Griffin
,
J. H.
, 1997, “
A Reduced Order approach for the vibration of mistuned bladed disks assemblies
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
119
(
1
), pp.
161
167
.
16.
Moyroud
,
F.
,
Fransson
,
T.
, and
Jacquet-Richardet
,
G.
, 2002, “
A Comparison of Two Finite Element Reduction Techniques for Mistuned Bladed Disks
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
124
(
4
), pp.
942
952
.
17.
Bladh
,
R.
,
Castanier
,
M. P.
,
Pierre
,
C.
, and
Kruse
,
M. J.
, 2002, “
Dynamic Response Prediction for a Mistuned Industrial Turbo Machinery Rotor Using Reduced-Order Modeling
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
124
(
2
), pp.
311
324
.
18.
Tran
,
D. M.
, 2001, “
Component Mode Synthesis Methods Using Partial Interface Modes: Application to Structures With Cyclic Symmetry
,”
Comput. Struct.
0045-7949,
79
(
2
), pp.
209
222
.
19.
Bladh
,
R.
,
Castanier
,
M. P.
, and
Pierre
,
C.
, 2001, “
Component-Mode Based Reduced Order Modeling Techniques for Mistuned Bladed Disks Part I: Theoretical Models
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
123
(
1
), pp.
89
99
.
20.
Yang
,
M. -T.
, and
Griffin
,
J. H.
, 2001, “
A Reduced Order Model of Mistuning Using a Subset of Nominal System Modes
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
123
(
4
), pp.
893
900
.
21.
Feiner
,
D. M.
, and
Griffin
,
J. H.
, 2002, “
A Fundamental Model of Mistuning for a Single Family of Modes
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
124
(
4
), pp.
597
605
.
22.
Petrov
,
E. P.
,
Sanliturk
,
K. Y.
, and
Ewins
,
D. J.
, 2002, “
A New Method for Dynamic Analysis of Mistuned Bladed Disks Based on the Exact Relationship Between Tuned and Mistuned Systems
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
124
(
3
), pp.
586
597
.
23.
Saito
,
A.
,
Castanier
,
M. P.
, and
Pierre
,
C.
, 2009, “
Effects of a Cracked Blade on Mistuned Turbine Engine Rotor Vibration
,”
ASME J. Vibr. Acoust.
0739-3717,
131
(
6
), p.
061006
.
24.
Saito
,
A.
,
Castanier
,
M. P.
, and
Pierre
,
C.
, 2009, “
Efficient Nonlinear Vibration Analysis of the Forced Response of Rotating Cracked Blades
,”
ASME J. Comput. Nonlinear Dyn.
1555-1423,
4
(
1
), p.
011005
25.
Kharyton
,
V.
,
Laine
,
J. -P.
,
Thouverez
,
F.
, and
Kucher
,
O.
, 2009, “
Cracked Blade Detection From Blade Disk Forced Response
,”
ASME TurboExpo 2009, Power for Land, Sea and Air
, Vol.
124
, pp.
586
597
.
26.
Bampton
,
C. R.
, 1968, “
Coupling of Substructures for Dynamics Analysis
,”
AIAA J.
0001-1452,
6
(
7
), pp.
1313
1319
.
27.
Lim
,
S.
,
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
.
You do not currently have access to this content.