Ceramic matrix composite vane structure with overwrap for a gas turbine engine

摘要

A vane structure for a gas turbine engine includes an airfoil section with a platform segment adjacent to a ring. An insert is adjacent to the platform segment and an overwrap is wound around the ring and the insert.

主权项

1. A vane structure for a gas turbine engine comprising:
a ring defined about an axis; an airfoil section with a platform segment abutting said ring, said airfoil section comprising a multiple of CMC plies; an insert adjacent to said platform segment; and an overwrap wound around said ring, said insert, and a fillet portion of said multiple of CMC plies of said airfoil section in a continuous spiral, said overwrap biasing said multiple of CMC plies toward said ring.