NASA NTRS · 20120012427
Ceramic matrix composite turbine engine vane
Abstract
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 coefficient of thermal expansion (CTE) varying with depth.
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Schaff, Jeffery R., Shi, Jun. 2012-07-03. Ceramic matrix composite turbine engine vane. https://ntrs.nasa.gov/citations/20120012427
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