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:
- Publication Date:
- Research Org.:
- General Electric Co., 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)
- 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 = {},
url = {https://www.osti.gov/biblio/1330701},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2016},
month = {11}
}
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