Wedge for a moving turbine blade of a turbomachine

FR3172818A1Pending Publication Date: 2026-09-11SAFRAN AIRCRAFT ENGINES SAS
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Patent Information

Application Number
FR2025002394
Authority / Receiving Office
FR · FR
Patent Type
Applications
Current Assignee / Owner
Filing Date
2025-03-10
Publication Date
2026-09-11
Patent Text Reader

Abstract

This disclosure relates to a shim (50) for a movable turbine blade (40), the movable turbine blade (40) comprising a blade root (41) housed in a recess (31) of a turbine rotor disk (30), the recess (31) comprising a first cavity (311) and a second cavity (312) arranged radially separated from each other by two first bearing surfaces (32a, 32b) of the rotor disk (30) arranged circumferentially opposite each other so as to define a longitudinal opening (33) between them, the shim (50) comprising a flexible body, a first pad, a second pad and a third pad, the shim (50) being configured such that, in an assembled configuration, the first pad bears against the blade root (41), the second pad bears against the first two bearing surfaces (32a, 32b), the third stud passes through the longitudinal opening (33) into the second cavity (312). Figure 3 (abstract)
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