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Title: Turbomachine blade assembly

Abstract

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.

Inventors:
Issue Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1330701
Patent Number(s):
9,482,108
Application Number:
13/856,303
Assignee:
General Electric Company (Schenectady, NY) NETL
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2013 Apr 03
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Garcia Crespo, Andres Jose. Turbomachine blade assembly. United States: N. p., 2016. Web.
Garcia Crespo, Andres Jose. Turbomachine blade assembly. United States.
Garcia Crespo, Andres Jose. Tue . "Turbomachine blade assembly". United States. https://www.osti.gov/servlets/purl/1330701.
@article{osti_1330701,
title = {Turbomachine blade assembly},
author = {Garcia Crespo, Andres Jose},
abstractNote = {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.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2016},
month = {11}
}

Patent:

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