Invention Grant
US09322286B2 Turbine nozzle for a turbomachine 有权
用于涡轮机的涡轮喷嘴

Turbine nozzle for a turbomachine
Abstract:
A turbine nozzle for a turbomachine, the nozzle including two coaxial platforms interconnected by radial vanes, an inner platform being connected to an annular partition that is festooned or crenellated and on which there is fastened an annular support carrying elements made of abradable material. The support is capable of sliding circumferentially over the partition between a mounting-and-dismounting position and a position for locking the support on the partition.
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