Turbomachine blade, a rotor, a low pressure turbine, and a turbomachine fitted with such a blade

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United States of America Patent

PATENT NO 8951017
SERIAL NO

13190809

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Abstract

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The invention relates to a turbomachine blade made of composite material and presenting a root with a bulb-shaped end suitable for engaging in a slot of a rotor disk. In characteristic manner, the end of the root of the blade is provided, beside one of its front faces, with a projecting portion having two symmetrical fins about the axial midplane of the root, each fin having a bearing face suitable for limiting tilting of the blade relative to the rotor disk about the axial direction.

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Patent Owner(s)

Patent OwnerAddress
HERAKLESFRENCH HORN

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Cordier, Damien Les Ecrennes, FR 2 33
Habarou, Georges Le Bouscat, FR 15 427
Mateo, Julien Carigan de Bordeaux, FR 13 280
Soupizon, Jean-Luc Vaux Le Penil, FR 43 413

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