Hybrid Brush Pocket Damper Seals for Turbomachinery

Author:

Laos Hector E.1,Vance John M.1,Buchanan Steven E.1

Affiliation:

1. Department of Mechanical Engineering, Texas A&M University, College Station, Texas 77843-3123

Abstract

Pocket damper seals perform a dual function: both sealing the pressurized gas around a rotating shaft and providing large amounts of vibration damping. The annular cavity between the labyrinth seal teeth is subdivided into separate annular cavities around the circumference of the rotor by partitioning walls. Also, the upstream and downstream teeth have different radial clearances to the rotor. These seals have been shown to provide a remarkable amount of direct damping to attenuate vibration in turbomachinery, but they generally leak more than conventional labyrinth seals if both seals have the same minimum clearance. Conversely, brush seals allow less than half the leakage of labyrinth seals, but published test results show no significant amount of damping. They are considered to be a primary choice for the seals in new aircraft engine designs because of their low leakage. This paper will describe a recently invented hybrid brush/pocket damper seal that combines high damping with low leakage. Previous brush seal results were studied and calculations were made to select a brush seal to combine with the pocket damper design. The result is a hybrid seal with high damping and low leakage. A special design feature can also allow active vibration control as a bonus benefit. A computer code written for the original pocket damper seal was modified to include the brush element at the exit blade. Results from the computer code indicate that the hybrid seal can have less leakage than a six bladed (or 6 knives) labyrinth seal along with orders of magnitude more damping. Experimental evaluations of the damping and leakage performance of the hybrid seal are being conducted by the authors. The experimental work reported here tested the damping capability of the new hybrid brush seal by exciting the seal journal through an impedance head. A conventional six-bladed labyrinth seal of the same working dimensions was also tested. The brush hybrid pocket damper seal is found to leak less than the labyrinth seal while producing two to three times more damping than the original pocket damper seal (orders of magnitude more than the conventional labyrinth). [S0742-4795(00)01102-9]

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference21 articles.

1. Thomas, H. , 1958, “Instabile Eigenschwingungen von Turbinenla¨ufern angefacht durch die Spaltstro¨mungen Stopfbuschen und Beschauflungen,” Bull de L’AIM, 71, pp. 1039–1063.

2. Alford, J. S. , 1965, “Protecting Turbomachinery from Self-Excited Rotor Whirl,” ASME J. Eng. Power, 87, pp. 333–344.

3. Childs, D. W., 1978, “The Space Shuttle Main Engine High Pressure Fuel Turbopump Rotordynamic Instability Problem,” ASME J. Eng. Power, Jan., pp. 48–57.

4. Childs, D., 1993, Turbomachinery Rotordynamics, Phenomena, Modeling and Analysis, John Wiley and Sons, New York.

5. Von Pragenau, G. L., 1992 “From Labyrinth Seals to Damping Seals/Bearings,” presented at the Fourth International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-4), Honolulu, Hawaii, pp. 277–285.

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