Turbine engine rotor comprising at least one disk reinforced...

B - Operations – Transporting – 23 – P

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B23P 15/04 (2006.01) F01D 5/02 (2006.01)

Patent

CA 2551342

Rotor de turbomachine comprenant au moins un disque pourvu d'un anneau constitué par exemple d'une bobine de fil de carbure de silicium ou d'alumine enrobé de métal. Selon l'invention, l'anneau composite (18) est logé dans une cavité annulaire close définie par exemple en usinant une gorge (16) dans une partie élargie (14) du disque et en la refermant par une plaque annulaire (20) après mise en place de l'anneau.

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