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Ceramic matrix composite vane structure for a gas turbine engine and corresponding low pressure turbine
A vane structure (64A, 64B) for a gas turbine engine (20) according includes a multiple of ceramic matrix composite (CMC) airfoil sections (70) integrated between a CMC outer ring (66) and a CMC inner ring (68). A corresponding low pressure turbine (46) is also provided.
Ceramic matrix composite vane structure for a gas turbine engine and corresponding low pressure turbine
A vane structure (64A, 64B) for a gas turbine engine (20) according includes a multiple of ceramic matrix composite (CMC) airfoil sections (70) integrated between a CMC outer ring (66) and a CMC inner ring (68). A corresponding low pressure turbine (46) is also provided.
Ceramic matrix composite vane structure for a gas turbine engine and corresponding low pressure turbine
Statorbeschaufelung aus keramischem Faserverbundwerkstoff für ein Gasturbinentriebwerk und zugehörige Niederdruckturbine
Aubage statorique en composite à matrice céramique pour moteur à turbine à gaz et turbine basse pression associée
SUCIU GABRIEL L (Autor:in) / ALVANOS IOANNIS (Autor:in) / MERRY BRIAN D (Autor:in) / DYE CHRISTOPHER M (Autor:in)
18.04.2018
Patent
Elektronische Ressource
Englisch
Ceramic matrix composite vane structure for a gas turbine engine and corresponding method of forming
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