Blade tip clearance control for a turbine engine...

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 25/08 (2006.01) F01D 11/08 (2006.01) F01D 25/24 (2006.01) F02C 7/24 (2006.01)

Patent

CA 2641963

Etage de turbine dans une turbomachine, comprenant une roue à aubes tournant à l'intérieur d'un anneau d'étanchéité (22) porté par un carter (24) de la turbine, et une tôle annulaire de protection thermique montée entre le carter (24) et l'anneau (22), caractérisé en ce que la tôle annulaire de protection thermique est formée de plusieurs plaques incurvées (54, 56) montées bout à bout et fixées par des pions (70) sur le carter (24).

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