This paper focuses on extending an earlier investigation on the systematic and rational consideration of uncertainty in reduced order models of rotordynamics systems. The current effort concentrates on the consistent introduction of uncertainty in mass properties on the modal mass and gyroscopic matrices and on the unbalance force vector. The uncertainty in mass is separated into uncertainty that maintains the rotor symmetry and the one which disrupts it. Both types of uncertainties lead to variations in the system modal matrices but only the latter induces an unbalance. Accordingly, the approach permits the selection of separate levels on the uncertainty on the system properties (e.g., natural frequencies) and on the unbalance. It was first found that the unbalanced response is increased by considering the uncertainty in the rotor modal mass matrices. It was next noted that the approach presented not only permits the analysis of uncertain rotors but it also provides a computational framework for the assessment of various balancing strategies. To demonstrate this unique feature, a numerical experiment was conducted in which a population of rotors were balanced at low speed and their responses were predicted at their first critical speed. These response predictions were carried with the uncertainty in the system modal mass matrices but with or without the balancing weights effects on these matrices. It was found that the balancing at low speed may, in fact, lead to an increase in both the mean and 95th percentile of the response at critical speed.

References

1.
Sankar
,
T. S.
,
Ramu
,
S. A.
, and
Ganesan
,
R.
,
1993
, “
Stochastic Finite Element Analysis for High Speed Rotors
,”
ASME J. Vibr. Acoust.
,
115
(
1
), pp.
59
64
.10.1115/1.2930315
2.
Murthy
,
R.
,
Mignolet
,
M. P.
, and
El-Shafei
,
A.
,
2010
, “
Nonparametric Stochastic Modeling of Structural Uncertainty in Rotordynamic Systems—Part I: Formulation
,”
ASME J. Eng. Gas Turbines Power
,
132
(9), p. 092501. 10.1115/1.3204645
3.
Murthy
,
R.
,
Mignolet
,
M. P.
, and
El-Shafei
,
A.
,
2010
, “
Nonparametric Stochastic Modeling of Structural Uncertainty in Rotordynamic Systems—Part II: Applications
,”
ASME J. Eng. Gas Turbines Power
,
132
(9), p. 092502.10.1115/1.3204650
4.
Sarrouy
,
E.
,
Dessombz
,
O.
, and
Sinou
,
J.-J.
,
2012
, “
Stochastic Analysis of the Eigenvalue Problem for Mechanical Systems Using Polynomial Chaos Expansion—Application to a Finite Element Rotor
,”
ASME J. Vibr. Acoust.
,
134
(5), p. 051009.10.1115/1.4005842
5.
Didier
,
J.
,
Faverjon
,
B.
, and
Sinou
,
J.-J.
,
2012
, “
Analysing the Dynamic Response of a Rotor System Under Uncertain Parameters by Polynomial Chaos
,”
J. Vib. Control
,
18
(5), pp.
712
732
.10.1177/1077546311404269
6.
Koroishi
,
E. H.
,
Cavalini
,
A. A.
,
Lima
,
A. M. G.
, and
Steffen
, V
.
,
2012
, “
Stochastic Modeling of Flexible Rotors
,”
1st International Symposium on Uncertainty Quantification and Stochastic Modeling (Uncertainties 2012)
, Maresias, Sao Paulo, Brazil, February 26-March 2.
7.
Soize
,
C.
,
2000
, “
A Nonparametric Model of Random Uncertainties on Reduced Matrix Model in Structural Dynamics
,”
Probab. Eng. Mech.
,
15
(
3
), pp.
277
294
.10.1016/S0266-8920(99)00028-4
8.
Soize
,
C.
,
2001
, “
Maximum Entropy Approach for Modeling Random Uncertainties in Transient Elastodynamics
,”
J. Acoust. Soc. Am.
,
109
(
5
), pp.
1979
1996
.10.1121/1.1360716
9.
El-Shafei
,
A.
,
El-Kabbany
,
A. S.
, and
Younan
,
A. A.
,
2004
, “
Rotor Balancing Without Trial Weights
,”
ASME J. Eng. Gas Turbines Power
,
126
(3), pp.
604
609
.10.1115/1.1762903
10.
Lee
,
C.-W.
,
1993
,
Vibration Analysis of Rotors
,
Kluwer
,
Dordrecht
, Netherlands.
11.
Batou
,
A.
and
Soize
,
C.
,
2012
, “
Rigid Multibody System Dynamics With Uncertain Rigid Bodies
,”
Multibody Syst. Dyn.
,
27
(
3
), pp.
285
319
.10.1007/s11044-011-9279-2
12.
Younan
,
A. A.
and
El-Shafei
,
A.
,
2008
, “
Model Calibration of Anisotropic Rotordynamic Systems With Speed Dependent Parameters
,”
ASME J. Eng. Gas Turbines Power
,
130
(4), p.
042502
.10.1115/1.2770485
You do not currently have access to this content.