Diffuser-stator assembly for a gas turbine

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

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F01D 9/02 (2006.01) F23R 3/10 (2006.01)

Patent

CA 2594266

Ensemble diffuseur-redresseur (10) pour turboréacteur ou turbopropulseur d'avion, le diffuseur (12) comprenant des flasques annulaires (22, 24) reliés par des aubes (26) et le redresseur (14) comprenant des viroles cylindriques (28, 30) reliées par des aubes (32), les flasques annulaires et les viroles cylindriques étant formés de tôles auxquelles les aubes (26, 32) sont assemblées par brasure.

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