Turbomachine blade including a platform
FR3171471A1Pending Publication Date: 2026-07-24SAFRAN 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
- 2025-01-23
- Publication Date
- 2026-07-24
Abstract
A stator blade (3) of an unshod section of a fan (26) comprising: - a foot (8); - a blade (7); - a platform (20) fixed to the blade (7) and configured to radially delimit the airflow (F) in the stator, at least one through-hole (35) being formed in the platform (20) configured to receive an inspection tool; and - at least one conduit (36) fixed to a radially internal face (20b) of the platform (20) such that a through-passage (37) of the conduit (36) extends in line with the through-hole (35), the conduit (36) being configured to guide the inspection tool to allow inspection of an area of interest (39) of the foot (8). Figure for the abstract: Fig. 3
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