TURBOMACHINE SET

FR3171258A1Pending 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
2025-01-14
Publication Date
2026-07-17
Patent Text Reader

Abstract

A turbomachine assembly comprising a first shaft (10) and a second shaft (20) extending coaxially about an axis (X), the second shaft (20) being mounted on the first shaft (10) abutting axially against an annular axial bearing shoulder (14) extending radially outward from the first shaft (10), the assembly further comprising a coupling system including a clamping nut (30) having a first tubular portion (31) and a second tubular portion (34) coaxial with respect to the axis (X), wherein the second portion (34) of the clamping nut (30) is located radially inside relative to the first portion (31) of the clamping nut (30). (See Figure 2 for more details.)
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