Experimental force coefficients for a two-bladed labyrinth seal and a four-pocket damper seal

被引:19
作者
Ransom, D [1 ]
Li, JM
San Andrés, L
Vance, J
机构
[1] Rocketdyne, Canoga Park, CA 91309 USA
[2] Elliot Co, Jeannette, PA 15644 USA
[3] Texas A&M Univ, Dept Mech Engn, College Stn, TX 77843 USA
来源
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME | 1999年 / 121卷 / 02期
关键词
D O I
10.1115/1.2833949
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Experiments are presented to identify the stiffness and damping force coefficients of a two-blade, teeth on stator labyrinth seal with diverging clearance and its modified version as a four-pocket gas damper seal. The seals Ir ere tested without journal rotation and at rotor speeds of 1500 rpm and 3000 rpm for seal supply to ambient pressure ratios ranging from 1 to 3. Calibrated impact loads excite a flexible supported housing holding rigidly the test seal. The impact loads and seal displacement and acceleration time responses are measured and recorded as frequency spectra. The instrumental variable filter method is used to identify the seal dynamic force coefficients from the measured transfer functions over a frequency range. The experiments demonstrate the four pocket gas damper seal has large (positive) direct damping coefficients and relatively small (negative) direct stiffness coefficients. The two bladed labyrinth seal exhibits positive direct stiffness and negative damping force coefficients. The leakage performance of both seals is nearly identical. The four pocket damper seal clearly outperforms the labyrinth seal in terms of rotordynamic forces. Both seals show a minimal amount of cross-coupling force effects, well within the experimental uncertainty.
引用
收藏
页码:370 / 376
页数:7
相关论文
共 18 条
[1]  
ALFORD JS, 1965, ASME, V87, P333
[2]  
Bastow P., 1976, P 1 INT C VIBR ROT M, P279
[3]  
BENCKERT H, 1980, P I MECH ENG SEPT
[4]  
Childs D., 1993, TURBOMACHINERY ROTOR, P290
[5]  
Childs D.W., 1997, P 26 TURB S TEX A M, P201
[6]  
CHILDS DW, 1978, ASME, V100, P48
[7]  
DOYLE H, 1980, NASA CP, V2133, P3
[8]  
FRITZEN C, 1985, 85DET91 ASME
[9]  
MASSMANN H, 1985, P NASA C INST ROT MA, P179
[10]  
MILLSAPS KT, 1990, P WORKSH ROT INST PR, P129