NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Plasma-sprayed zirconia gas path seal technology: A state-of-the-art reviewThe benefits derived from application of ceramic materials to high pressure turbine gas path seal components are described and the developmental backgrounds of various approaches are reviewed. The most fully developed approaches are those employing plasma sprayed zirconium oxide as the ceramic material. Prevention of cracking and spalling of the zirconium oxide under cyclic thermal shock conditions imposed by the engine operating cycle is the most immediate problem to be solved before implementation is undertaken. Three promising approaches to improving cyclic thermal shock resistance are described and comparative rig performance of each are reviewed. Advanced concepts showing potential for performance improvements are described.
Document ID
19790025154
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bill, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Nonmetallic Materials
Report/Patent Number
E-9941
AVRADCOM-TR-79-47
NASA-TM-79273
Report Number: E-9941
Report Number: AVRADCOM-TR-79-47
Report Number: NASA-TM-79273
Meeting Information
Meeting: Manufacturing Technol. Advisory Rev.
Location: Phoenix, AZ
Country: United States
Start Date: October 21, 1979
End Date: October 25, 1979
Sponsors: Soc. of Manufacturing Engr.
Accession Number
79N33325
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available