NASA NTRS · 20120010615
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 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.
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Prill, Lisa A., Schaff, Jeffery R., Shi, Jun. 2012-06-26. Ceramic matrix composite turbine engine vane. https://ntrs.nasa.gov/citations/20120010615
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