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Turbine Seal Research at NASA GRCLow-leakage, long-life turbomachinery seals are important to both Space and Aeronautics Missions. (1) Increased payload capability (2) Decreased specific fuel consumption and emissions (3) Decreased direct operating costs. NASA GRC has a history of significant accomplishments and collaboration with industry and academia in seals research. NASA's unique, state-of-the-art High Temperature, High Speed Turbine Seal Test Facility is an asset to the U.S. Engine / Seal Community. Current focus is on developing experimentally validated compliant, non-contacting, high temperature seal designs, analysis, and design methodologies to enable commercialization.
Document ID
20150010376
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
Proctor, Margaret P.
(NASA Glenn Research Center Cleveland, OH, United States)
Steinetz, Bruce M.
(NASA Glenn Research Center Cleveland, OH, United States)
Delgado, Irebert R.
(NASA Glenn Research Center Cleveland, OH, United States)
Hendricks, Robert C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 10, 2015
Publication Date
November 29, 2011
Subject Category
Mechanical Engineering
Report/Patent Number
E-663258
Report Number: E-663258
Meeting Information
Meeting: NASA Seal/Secondary Air System Workshop
Location: Cleveland, OH
Country: United States
Start Date: November 29, 2011
Sponsors: NASA Headquarters
Funding Number(s)
WBS: WBS 561581.02.08.03.47.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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