Rapid processing of laminar composite components
US-12180120-B2 · Dec 31, 2024 · US
US9103214B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9103214-B2 |
| Application number | US-201113215292-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 23, 2011 |
| Priority date | Aug 23, 2011 |
| Publication date | Aug 11, 2015 |
| Grant date | Aug 11, 2015 |
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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.
Opening claim text (preview).
What is claimed is: 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…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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