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Ceramic matrix composite turbine engine vane

Author
Schaff, Jeffery R.
Published
June 26, 2012.
Physical Description
1 electronic document
Additional Creators
Prill, Lisa A. and Shi, Jun
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
A vane has an airfoil shell and a spar within the shell. The vane has an outboard shroud at an outboard end of the shell and an inboard platform at an inboard end of the shell. The shell includes a region having a depth-wise coefficient of thermal expansion and a second coefficient of thermal expansion transverse thereto, the depth-wise coefficient of thermal expansion being greater than the second coefficient of thermal expansion.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20120010615.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 16008303