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Compliant Turbomachine SealingSealing interface materials and coatings are sacrificial, giving up their integrity for the benefit of the component. Seals that are compliant while still controlling leakage, dynamics, and coolant flows are sought to enhance turbomachine performance. Herein we investigate the leaf-seal configuration. While the leaf seal is classified as contacting, a ready modification using the leaf-housing arrangement in conjunction with an interface film rider (a bore seal, for example) provides for a film-riding noncontact seal. The leaf housing and leaf elements can be made from a variety of materials from plastic to ceramic. Four simplistic models are used to identify the physics essential to controlling leakage. Corroborated by CFD, these results provide design parameters for applications to within reasonable engineering certainty. Some potential improvements are proposed.
Document ID
20110012885
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Hendricks, R. C.
(NASA Glenn Research Center Cleveland, OH, United States)
Braun, M. J.
(Akron Univ. Akron, OH, United States)
Deng, D.
(Akron Univ. Akron, OH, United States)
Hendricks, J. A.
(Diligent Design Toledo, OH, United States)
Date Acquired
August 25, 2013
Publication Date
May 1, 2011
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
54-ISROMAC-11
NASA/TM-2011-214040
E-15397-2
Meeting Information
Meeting: 11th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery
Location: Honolulu, HI
Country: United States
Start Date: February 26, 2006
End Date: March 2, 2006
Funding Number(s)
WBS: WBS 561581.02.08.03.16.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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