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Ceramic matrix composite vane structure for a gas turbine engine and corresponding method of forming
A ceramic matrix composite (CMC) airfoil (66) for a gas turbine engine (20) includes at least one CMC ply (88) which defines a suction side (84), an outer platform (80), a pressure side (82) and an inner platform (78) with a continuous "I"-shaped fiber geometry. A corresponding vane structure (62A) and method of forming are also provided.
Ceramic matrix composite vane structure for a gas turbine engine and corresponding method of forming
A ceramic matrix composite (CMC) airfoil (66) for a gas turbine engine (20) includes at least one CMC ply (88) which defines a suction side (84), an outer platform (80), a pressure side (82) and an inner platform (78) with a continuous "I"-shaped fiber geometry. A corresponding vane structure (62A) and method of forming are also provided.
Ceramic matrix composite vane structure for a gas turbine engine and corresponding method of forming
Statorbeschaufelung aus keramischem Faserverbundwerkstoff für ein Gasturbinentriebwerk und zugehöriges Formungsverfahren
Aubage statorique en composite à matrice céramique pour moteur à turbine à gaz et procédé de façonnage associés
SUCIU GABRIEL L (Autor:in) / ALVANOS IOANNIS (Autor:in)
23.01.2019
Patent
Elektronische Ressource
Englisch
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