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Turbomachine Blade Assembly

United States Patent Application

View the Complete Application at the US Patent & Trademark Office
Embodiments of the present disclosure include a system comprising a turbomachine blade assembly having a blade portion, a shank portion, and a mounting portion, wherein the blade portion, the shank portion, and the mounting portion comprise a first plurality of plies extending from a tip of the airfoil to a base of the dovetail.
Garcia Crespo, Andres Jose (Greenville, SC)
General Electric Company (Schenectady NY)
13/ 856,303
April 3, 2013
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH & DEVELOPMENT [0001] This invention was made with Government support under grant number DE-FC26-05NT42643-DOE awarded by the Department of Energy. The Government has certain rights in the invention.