NASA NTRS · 20090002573
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 spar has a first chamber essentially along the suction side and a second chamber along the pressure side opposite the first chamber.
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Shi, Jun, Ochs, Stuart S., Green, Kevin E., Jarmon, David C., Sahm, Michael K., Prill, Lisa A.. 2008-11-18. Ceramic matrix composite turbine engine vane. https://ntrs.nasa.gov/citations/20090002573
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