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Ceramic Matrix Composite Vane Subelement Burst TestingBurst tests were performed on Ceramic Matrix Composite (CMC) vane specimens, manufactured by two vendors, under the Ultra Efficient Engine Technology (UEET) project. Burst specimens were machined from the ends of 76mm long vane sub-elements blanks and from High Pressure Burner Rig (HPBR) tested specimens. The results of burst tests will be used to compare virgin specimens with specimens that have had an Environmental Barrier Coating (EBC) applied, both HPBR tested and untested, as well as a comparison between vendors.
Document ID
20060051738
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Brewer, David N. (Army Research Lab. Cleveland, OH, United States)
Verrilli, Michael (General Electric Aircraft Engines Cincinnati, OH, United States)
Calomino, Anthony (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2006
Subject Category
Composite Materials
Report/Patent Number
GT2006-90833
Report Number: GT2006-90833
Meeting Information
Meeting: Turbo Expo 2006
Location: Barcelona
Country: Spain
Start Date: May 8, 2006
End Date: May 11, 2006
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 22-714-30-19
Distribution Limits
Public
Copyright
Public Use Permitted.

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