Improved turbojet stator blade spacing system control ring

Details Improved turbojet stator blade spacing system control ring Improved turbojet stator blade spacing system control ring

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01)

Patent

CA 2641017

Turbomachine comportant un étage d'aubes fixes à calage variable. Un anneau de commande (17) coaxial au carter (13) comporte deux tronçons (30a, 30b) assemblés par des flasques de liaison latéraux (33) fixés avec encastrement de part et d'autre des tronçons au voisinage des extrémités de ceux-ci.

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