Rotor stage for a turbine engine reinforced by fibres

Details Rotor stage for a turbine engine reinforced by fibres Rotor stage for a turbine engine reinforced by fibres

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/34 (2006.01) F01D 5/02 (2006.01) F01D 21/04 (2006.01)

Patent

CA 2220987

L'invention propose un étage de rotor de turbomachine à jante (3) mince renforcée par au moins un anneau fibreux (15). Un tel étage de rotor (1) est remarquable en ce que l'anneau fibreux (15) a une hauteur h au moins égale à 1,5 fois sa largeur 1, et en ce que les anneaux fibreux (15) sont en saillie sur la paroi intérieure (22) de ladite jante (3) afin de rigidifier cette jante et de réduire la quantité de matière fibreuse à utiliser.

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