Turbomachine rotor assembly with two bladed-discs separated...

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

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F01D 5/00 (2006.01) F01D 5/06 (2006.01) F01D 5/08 (2006.01) F01D 11/00 (2006.01) F01D 11/02 (2006.01)

Patent

CA 2388778

A spacer (36) made to be installed between two permanently connected discs (31 and 32), without a bolted flange, and comprising axial thrust (43, 47) as well as outer radial thrust (45, 48) alignment surfaces (41). It comprises moreover an outer cover (37) to provide sealing and a cooling passageway, and stiffening tongues (38) which accommodate thrust loads.

Une entretoise (36) à installer entre deux disques (31 et 32) solidaires, sans bride boulonnée, et comprenant des surfaces d'alignement (41) de poussée axiale (43, 47) et de poussée radiale extérieure (45, 48). Elle comprend en outre un couvercle extérieur (37) pour assurer l'étanchéité et un passage de refroidissement, et des languettes de renfort (38) pour absorber les charges de poussée.

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