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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 (author) / ALVANOS IOANNIS (author)
2019-01-23
Patent
Electronic Resource
English
| European Patent Office | 2018
CERAMIC MATRIX COMPOSITE TURBINE VANE AND METHOD FOR MAKING
| European Patent Office | 2020