This paper presents a static test rig called “Octopus” designed for the validation of numerical models aimed at calculating the nonlinear dynamic response of a bladed disk with underplatform dampers (UPDs). The test rig supports a bladed disk on a fixture and each UPD is pressed against the blade platforms by wires pulled by dead weights. Both excitation system and response measurement system are noncontacting. This paper features the design and the setup of the noncontacting excitation generated by electromagnets placed under each blade. A traveling wave excitation is generated according to a desired engine order by shifting the phase of the harmonic force of one electromagnet with respect to the contiguous exciters. Since the friction phenomenon generated by UPDs introduces nonlinearities on the forced response, the amplitude of the exciting force must be kept constant at a known value on every blade during step-sine test to calculate frequency response functions. The issue of the force control is therefore addressed since the performance of the electromagnet changes with frequency. The system calibration procedure and the estimated errors on the generated force are also presented. Examples of experimental tests that can be performed on a dummy integral bladed disk (blisk) mounted on the rig are described in the end.

1.
Panning
,
L.
,
Popp
,
K.
,
Sextro
,
W.
,
Goetting
,
F.
,
Kayser
,
A.
, and
Wolter
,
I.
, 2004, “
Asymmetrical Underplatform Dampers in Gas Turbine Bladings: Theory and Application
,”
ASME
Paper No. GT2004-53316.
2.
Petrov
,
E. P.
, and
Ewins
,
D. J.
, 2007, “
Advanced Modelling of Underplatform Friction Dampers for Analysis of Bladed Disk Vibration
,”
ASME J. Turbomach.
0889-504X,
129
(
1
), pp.
143
150
.
3.
Cigeroglu
,
E.
,
An
,
N.
, and
Menq
,
C. H.
, 2009, “
Forced Response Prediction of Constrained and Unconstrained Structures Coupled Through Frictional Contacts
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
131
(
2
), p.
022505
.
4.
Firrone
,
C. M.
,
Zucca
,
S.
, and
Gola
,
M. M.
, 2009, “
Effect of Static/Dynamic Coupling on the Forced Response of Turbine Bladed Disks With Underplatform Dampers
,”
ASME
Paper No. GT2009-59905.
5.
Avalos
,
J.
, and
Mignolet
,
M. P.
, 2008, “
On Damping Entire Bladed Disk Through Dampers on Only a Few Blades
,”
ASME
Paper No. GT2008-51446.
6.
Sanliturk
,
K. Y.
,
Ewins
,
D. J.
, and
Stanbridge
,
A. B.
, 2001, “
Underplatform Dampers for Turbine Blades: Theoretical Modelling, Analysis and Comparison With Exp. Data
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
123
(
4
), pp.
919
929
.
7.
Botto
D.
,
Zucca
S.
, and
Gola
M. M.
, 2008, “
Parametric Study of the Kinematic Behaviour of the Underplatform Damper and Correlation with Experimental Data
,”
Proceedings of the ISMA
, pp.
1039
1054
.
8.
Sever
,
I. A.
, 2004, “
Experimental Validation of Turbomachinery Blade Vibration Predictions
,” Ph.D. thesis, Imperial College London, London.
9.
Götting
,
F.
,
Sextro
,
W.
,
Panning
,
L.
, and
Popp
,
K.
, 2004, “
Systematic Mistuning of Bladed Disk Assemblies With Friction Contacts
,”
ASME
Paper No. GT2004-53310.
10.
Pierre
,
C.
,
Judge
,
J.
,
Ceccio
,
S. L.
, and
Castanier
,
M. P.
, 2003, “
Experimental Investigation of the Effects of Random and Intentional Mistuning on the Vibration of Bladed Disks
,”
Proceedings of the Seventh National Turbine Engine High Cycle Fatigue Conference
, pp.
1
12
.
11.
Jones
,
K. W.
, and
Cross
,
C. J.
, 2003, “
Travelling Wave Excitation System for Bladed Disks
,”
J. Propul. Power
0748-4658,
19
, pp.
135
141
.
12.
Darren
,
H. E.
,
Filippi
,
S.
,
Castanier
,
M. P.
, et al.
, 2009, “
Testing and Calibration Procedures for Mistuning Identification and Travelling Wave Excitation of Blisks
,”
ASME
Paper No. GT2009-59671.
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