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Turbine engine turbine blade made of a ceramic-matrix composite with recesses made by machining
A turbine engine turbine blade of ceramic matrix composite. The root of the blade includes a single densified fiber preform including at least one recess made by machining, each point of the root of the blade being situated at a distance from a free surface of the root that is no greater than twice the maximum penetration distance into the preform of densification gas for densifying the preform, and the distal portion of the root of the blade includes a distal wall that is continuous and in a single piece.
Turbine engine turbine blade made of a ceramic-matrix composite with recesses made by machining
A turbine engine turbine blade of ceramic matrix composite. The root of the blade includes a single densified fiber preform including at least one recess made by machining, each point of the root of the blade being situated at a distance from a free surface of the root that is no greater than twice the maximum penetration distance into the preform of densification gas for densifying the preform, and the distal portion of the root of the blade includes a distal wall that is continuous and in a single piece.
Turbine engine turbine blade made of a ceramic-matrix composite with recesses made by machining
LE HONG SON (author) / SOUPIZON JEAN-LUC (author) / TRICONNET NICOLAS CHRISTIAN (author) / EBERLING-FUX NICOLAS (author) / ROUSSILLE CLEMENT (author)
2015-11-17
Patent
Electronic Resource
English
CERAMIC MATRIX COMPOSITE BLADE TRACK FOR A GAS TURBINE ENGINE
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