Ventilated turbine rotor
Patent Information
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- SAFRAN AIRCRAFT ENGINES SAS
- Filing Date
- 2024-11-21
- Publication Date
- 2026-05-22
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Abstract
Claims
18.
19. presenting a volume accessible with a tool from the upstream side of the flange (80). Turbine, in particular a low pressure turbine, comprising a rotor according to any one of the preceding claims. Method for mounting a turbine rotor according to any one of claims 1 to 18, the method comprising: - shrink fitting of the flange (80) on the ferrule (60) by cooperation, on the one hand, between a first shrink fitting surface (87) of the flange (80) with a first complementary shrink fitting surface (67) of the ferrule (60), and on the other hand between an axial stop shoulder (64) of the ferrule (60) with a complementary axial stop shoulder (84) of the flange (80), - shrink-fitting of the disc (20) onto the flange (80) by cooperation between a second shrink-fitting surface (88) of the flange (80) and a second complementary shrink-fitting surface (28) of the disc (20), - fixing the radial flange (61) of the ferrule (60) against an upstream face of the disc (20) by bolting. [Fig. 1] 16 15 2c in RG. 4 [Fig. 5] FIG. 5 [Fig. 6A] FIG. 6A [Fig. 6B]