Composite airfoil assembly having a dovetail portion

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12253006
APP PUB NO 20240209741A1
SERIAL NO

18088957

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Abstract

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A composite blade assembly for a turbine engine. The composite blade assembly having a core, a first skin and a second skin. The core having a composite structure. The first skin having at least one composite ply. The second skin having at least one composite ply. The first skin having a first radius. The second skin having a second radius.

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Patent Owner(s)

  • GENERAL ELECTRIC COMPANY

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bryant,, Jr Gary Willard Loveland, US 17 24
Davis, Tod Winton Liberty Township, US 16 57
Kray, Nicholas Joseph Mason, US 220 890
Kryj-Kos, Elzbieta Evendale, US 27 18

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