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Test results for rotordynamic coefficients of anti-swirl self-injection seals

Authors :
Kim, C. H
Lee, Y. B
Source :
NASA. Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1993.
Publication Year :
1994
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1994.

Abstract

Test results are presented for rotordynamic coefficients and leakage for three annular seals which use anti-swirl self-injection concept to yield significant improvement in whirl frequency ratios as compared to smooth and damper seals. A new anti-swirl self-inection mechanism is achieved by deliberately machining self-injection holes inside the seal stator mechanism which is used to achieve effective reduction of the tangential flow which is considered as a prime cause of rotor instability in high performance turbomachinery. Test results show that the self-injection mechanism significantly improves whirl frequency ratios; however, the leakage performance degrades due to the introduction of the self-injection mechanism. Through a series of the test program, an optimum anti-swirl self-injection seal which uses a labyrinth stator surface with anti-axial flow injections is selected to obtain a significant improvement in the whirl frequency ratio as compared to a damper seal, while showing moderate leakage performance. Best whirl frequency ratio is achieved by an anti-swirl self-injection seal of 12 holes anti-swirl and 6 degree anti-leakage injection with a labyrinth surface configuration. When compared to a damper seal, the optimum configuration outperforms the whirl frequency ratio by a factor of 2.

Subjects

Subjects :
Mechanical Engineering

Details

Language :
English
Database :
NASA Technical Reports
Journal :
NASA. Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1993
Publication Type :
Report
Accession number :
edsnas.19940029674
Document Type :
Report