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Test results for rotordynamic coefficients of anti-swirl self-injection sealsTest 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.
Document ID
19940029674
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kim, C. H.
(Korean Inst. of Science and Technology Seoul, Republic Of Korea)
Lee, Y. B.
(Korean Inst. of Science and Technology Seoul, Republic Of Korea)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Publication Information
Publication: NASA. Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1993
Subject Category
Mechanical Engineering
Accession Number
94N34180
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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