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Ceramic matrix composite airfoil segment for a gas turbine engine, corresponding structure and method of assembling
A ceramic matrix composite (CMC) airfoil segment (82) for a gas turbine engine (20) includes a box-shape fiber geometry (98A) which defines a rectilinear pressure side bond line (100P) and a rectilinear suction side bond line (100S). A corresponding structure and method of assembling are also provided.
Ceramic matrix composite airfoil segment for a gas turbine engine, corresponding structure and method of assembling
A ceramic matrix composite (CMC) airfoil segment (82) for a gas turbine engine (20) includes a box-shape fiber geometry (98A) which defines a rectilinear pressure side bond line (100P) and a rectilinear suction side bond line (100S). A corresponding structure and method of assembling are also provided.
Ceramic matrix composite airfoil segment for a gas turbine engine, corresponding structure and method of assembling
Schaufelsegment aus keramischem Faserverbundwerkstoff für ein Gasturbinentriebwerk, zugehörige Struktur und Montageverfahren
Segment d'aube en composite à matrice céramique pour moteur à turbine à gaz, structure et procédé d'assemblage associés
BERCZIK DOUGLAS M (author) / SUCIU GABRIEL L (author) / MERRY BRIAN D (author) / ALVANOS IOANNIS (author) / DYE CHRISTOPHER M (author)
2019-05-01
Patent
Electronic Resource
English
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