TURBOMACHINE ASSEMBLY INCLUDING A HOLLOW TAB FOR TURBOMACHINE ORGAN

FR3171246A1Pending Publication Date: 2026-07-17SAFRAN AIRCRAFT ENGINES SAS
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Patent Information

Authority / Receiving Office
FR · FR
Patent Type
Applications
Current Assignee / Owner
SAFRAN AIRCRAFT ENGINES SAS
Filing Date
2025-01-16
Publication Date
2026-07-17
Patent Text Reader

Abstract

The invention relates to a turbomachine assembly mounted centered on a longitudinal axis (X), the turbomachine assembly comprising a sealing tab (26), a first ring sector (15a) and a second ring sector (15b) arranged circumferentially opposite each other around the longitudinal axis, the first ring sector (15a) comprising a first groove (25; 32) 32a, 32b), which receives a first circumferential end (26d) of the sealing tab and the second ring sector (15b) comprising a second groove (25; 32b), arranged circumferentially opposite the first groove (25; 32) and which receives a second circumferential end of the sealing tab, the first and second circumferential ends (26d) of the sealing tab (26) being circumferentially opposed.According to the invention, the sealing strip is hollow, having a recessed portion extending between a first and a second opposing wall of the sealing strip. Figure for the abbreviation: Fig. 7.
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