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Turbine Engine Clearance Control Systems: Current Practices and Future DirectionsThis presentation reviews the following: (i) Cause and effect of gas turbine blade tip seal wear (ii) Current clearance control practices (iii) Present approaches under investigation at GRC.
Document ID
20040000621
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Lattime, Scott B. (Ohio Aerospace Inst. Brook Park, OH, United States)
Steinetz, Bruce M. (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 21, 2013
Publication Date
September 1, 2003
Publication Information
Publication: 2002 NASA Seal/Secondary Air System Workshop
Volume: 1
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20040000616Collected Works2002 NASA Seal/Secondary Air System Workshop
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