Ferrule segment

FR3171064A1Pending Publication Date: 2026-07-10SAFRAN AIRCRAFT ENGINES SAS
0 Cites 0 Cited by

Patent Information

Application Number
FR2025000162
Authority / Receiving Office
FR · FR
Patent Type
Applications
Current Assignee / Owner
Filing Date
2025-01-08
Publication Date
2026-07-10
Patent Text Reader

Abstract

The invention relates to a ferrule segment (20) adapted to delimit a portion of a turbomachine duct, characterized in that it comprises a sealing plate (10) arranged on a first face (201, 241) of the ferrule segment (20) and a displacement means (30), a rotary movement of the displacement means causing a translational movement of the sealing plate between a first position and a second position, in which the sealing plate (10) projects from a lateral edge (27) of the ferrule segment (20) to cover a junction (52) between the ferrule segment and a structural arm (50) of the turbomachine. Figure for the abstract: Fig 8
Need to check novelty before this filing date? Find Prior Art