Systems and method for a composite blade with fillet transition
Abstract
A system includes a turbomachine blade segment including an airfoil with an exterior surface, and a platform coupled to the airfoil having a first side and a second side. The system also includes a concave fillet transition extending between the airfoil and the platform. The concave fillet transition includes one or more interface ply segments extending across the exterior surface of the airfoil and the first or the second side of the platform to form a continuous surface between the airfoil and the platform.
- Inventors:
- Publication Date:
- Research Org.:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1494575
- Patent Number(s):
- 10,132,170
- Application Number:
- 13/842,639
- Assignee:
- General Electric Company (Schenectady, NY)
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2013 Mar 15
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Garcia-Crespo, Andres Jose, and de Diego, Peter. Systems and method for a composite blade with fillet transition. United States: N. p., 2018.
Web.
Garcia-Crespo, Andres Jose, & de Diego, Peter. Systems and method for a composite blade with fillet transition. United States.
Garcia-Crespo, Andres Jose, and de Diego, Peter. Tue .
"Systems and method for a composite blade with fillet transition". United States. https://www.osti.gov/servlets/purl/1494575.
@article{osti_1494575,
title = {Systems and method for a composite blade with fillet transition},
author = {Garcia-Crespo, Andres Jose and de Diego, Peter},
abstractNote = {A system includes a turbomachine blade segment including an airfoil with an exterior surface, and a platform coupled to the airfoil having a first side and a second side. The system also includes a concave fillet transition extending between the airfoil and the platform. The concave fillet transition includes one or more interface ply segments extending across the exterior surface of the airfoil and the first or the second side of the platform to form a continuous surface between the airfoil and the platform.},
doi = {},
url = {https://www.osti.gov/biblio/1494575},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2018},
month = {11}
}
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