Cooling system for the downstream side of a centrifugal...

F - Mech Eng,Light,Heat,Weapons – 02 – C

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F02C 7/12 (2006.01) F01D 25/12 (2006.01) F02C 7/16 (2006.01)

Patent

CA 2594005

Turbomachine, comprenant un ensemble diffuseur - redresseur (12) comportant un flasque aval (30) relié à son extrémité aval à des moyens (36) d'injection d'air de ventilation d'une turbine et délimitant avec le rouet (18) d'un compresseur centrifuge une cavité annulaire (41) de circulation d'air de ventilation prélevé en sortie du compresseur, cette turbomachine comprenant des moyens de prélèvement d'air, sur les moyens d'injection (36), et des moyens de guidage de cet air jusqu'à la partie radialement interne de la face aval (40) du rouet.

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