Rotordynamic Force Coefficients for a New Damper Seal Design

Author:

Ertas Bugra H.1,Vance John M.2

Affiliation:

1. Rotating Equipment Group, Vibrations & Dynamics Laboratory, GE Global Research Center, Niskayuna, NY 12309

2. Turbomachinery Laboratory, Mechanical Engineering Department, Texas A&M University, College Station, TX 77843-3123

Abstract

The objective of the following work was to determine frequency-dependent rotordynamic force coefficients for a new annular gas damper seal design. Both rotating and nonrotating experimental tests are presented for inlet pressures at 1000psig(69bar), a frequency excitation range of 20-300Hz, and rotor speeds up to 15,200rpm. Two different testing methods were used for determining coefficients: (1) dynamic pressure response method and (2) mechanical impedance method. The dynamic pressure method required the measurement of internal seal cavity pressure modulations in combination with the vibratory motion, whereas the mechanical impedance method used the measurement of external shaker forces, accelerations, and motion of the mechanical system. In addition to the new fully partitioned damper seal (FPDS) tests, the same experiments were conducted for a conventional pocket damper seal (PDS) design. Results of the frequency-dependent force coefficients and the internal seal dynamics for the two different gas damper seals are compared. The conclusions of the tests show that the FPDS design possesses significantly more positive direct damping and direct stiffness compared to the conventional PDS. The experiments also show the measurement of same-sign cross-coupled (cross-axis) stiffness coefficients for both seals, which indicate that the seals do not produce a destabilizing influence on rotor-bearing systems.

Publisher

ASME International

Subject

Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanical Engineering,Mechanics of Materials

Reference16 articles.

1. A New Damper Seal for Turbomachinery;Vance

2. Li, J., and Vance, J. M., 1995, “Effects of Clearance and Clearance Ratio on Two and Three Bladed TAMSEALS, TRC-Seal-4–95,” Turbomachinery Laboratory Research Progress Report, Texas A&M University, College Station.

3. Experimental Force Coefficients for a Two-Bladed Labyrinth Seal and a Four Pocket Damper Seal;Ransom;ASME J. Tribol.

4. Laos, H. E. , 1999, “Rotordynamic Effect of Pocket Damper Seals,” Ph.D. dissertation, Texas A&M University, College Station.

5. Dynamic Force Coefficients of a Multiple Blade, Multiple-Pocket Gas Damper Seal: Test Results and Predictions;Li;ASME J. Tribol.

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