METHOD FOR MANUFACTURING AN INTER-BLADE PLATFORM WITH SACRIFICIAL EDGES

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20250115009A1
SERIAL NO

18836442

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Abstract

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A method for manufacturing an inter-blade platform of a turbomachine fan, the platform including a base including a first and a second sacrificial lateral edge having a thickness smaller than that of the central part of the base, the method including the production of a preform of the platform by three-dimensional weaving including a central part portion and two sacrificial edge portions, the thickness of which is smaller than that of the central part portion, the difference in thickness between the lateral edge portions and the central part portion being achieved by withdrawing a plurality of weft yarns located outside the central part portion and not being woven with warp yarns.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES2 BOULEVARD DU GENERAL MARTIAL VALIN PARIS 75015

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
COMMARMOT, Manon MOISSY-CRAMAYEL, FR 1 0
GALVE, Antoine MOISSY-CRAMAYEL, FR 1 0
MOUNIEN, Richard Anandavelou MOISSY-CRAMAYEL, FR 1 0
OUTTRABADY, Henri MOISSY-CRAMAYEL, FR 1 0

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