Experiments are presented to identify the stiffness and damping force coeff
icients of a two-blade, teeth on stator labyrinth seal with diverging clear
ance and its modified version as a four-pocket gas damper seal. The seals I
r ere tested without journal rotation and at rotor speeds of 1500 rpm and 3
000 rpm for seal supply to ambient pressure ratios ranging from 1 to 3. Cal
ibrated impact loads excite a flexible supported housing holding rigidly th
e test seal. The impact loads and seal displacement and acceleration time r
esponses are measured and recorded as frequency spectra. The instrumental v
ariable filter method is used to identify the seal dynamic force coefficien
ts from the measured transfer functions over a frequency range. The experim
ents demonstrate the four pocket gas damper seal has large (positive) direc
t damping coefficients and relatively small (negative) direct stiffness coe
fficients. The two bladed labyrinth seal exhibits positive direct stiffness
and negative damping force coefficients. The leakage performance of both s
eals is nearly identical. The four pocket damper seal clearly outperforms t
he labyrinth seal in terms of rotordynamic forces. Both seals show a minima
l amount of cross-coupling force effects, well within the experimental unce
rtainty.