Turbine engine blade made of composite material with a bulb-shaped root

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United States of America Patent

PATENT NO 9828861
SERIAL NO

14428706

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Abstract

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A turbine engine blade made of composite material including fiber reinforcement obtained by three dimensionally weaving yarns and densified with a matrix, the blade including an airfoil and a blade root forming a single part. The blade root includes two opposite lateral flanks that are substantially plane and that are clamped between two independent pads made of composite material, which pads are fastened against the lateral flanks of the blade root to form a blade root that is bulb-shaped.

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Patent Owner(s)

Patent OwnerAddress
SNECMAPARIS FRANCE PARIS PARIS
HERAKLES [SPS]LES 5 CHEMINS - RUE DE TOUBAN LE HAILLAN 33185

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Le, Hong Son Thomery, FR 19 295

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