This is the second of two papers describing results of a research project directed at developing a gas-operated vibration damper for high-temperature turbomachinery applications. This part presents the experimental measurements made on a gas damper hardware and compares them with the theoretical predictions given in Part I. It is found that the isentropic theoretical model predicts the damper characteristics quite well. A maximum damping of 2310 N-s/m (13.2 lb-s/in.) was measured at a natural frequency of 118 Hz using the present design and the results suggest that significantly higher damping levels are possible with design modifications.

1.
Sundararajan, P., and Vance, J. M., 1993, “A Theoretical and Experimental Investigation of a Gas Operated Bearing Damper for Turbomachinery: Part II—Experimental Results and Comparison With Theory,” Vibration of Rotating Systems, ASME DE-Vol. 60, pp. 85–119.
2.
Sundararajan
P.
, and
Vance
J. M.
,
1995
, “
A Gas-Operated Bearing Damper for Turbomachinery: Theoretical Predictions Versus Experimental Measurements: Part I—Theoretical Model and Predictions
,”
ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER
, Vol.
117
, this issue, pp.
741
748
.
3.
Vance
J. M.
,
Cardon
B. P.
,
San Andres
L. A.
, and
Storace
A. F.
,
1993
, “
A Gas-Operated Bearing Damper for Turbomachinery
,”
ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER
, Vol.
115
, pp.
383
389
.
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