Ceramic matrix composite turbine nozzle shell and method of assembly
Abstract
A method of manufacturing a ceramic matrix composite (CMC) turbine nozzle shell is provided. The method includes: assembling a primary outer nozzle platform, a primary inner nozzle platform, a core and trailing edge preform, and an airfoil-shaped body; joining the primary outer nozzle platform to a secondary outer nozzle platform of the airfoil-shaped body; and joining the primary inner nozzle platform to a secondary inner nozzle platform of the airfoil-shaped body. Composite plies circumferentially surround the airfoil-shaped body, and their longitudinal edges are cut into fingers that are folded down. The fingers are interleaved between secondary platform plies to form the secondary outer and inner nozzle platforms.
- Inventors:
- Issue Date:
- Research Org.:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1860065
- Patent Number(s):
- 11174203
- Application Number:
- 16/170,773
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Classifications (CPCs):
-
B - PERFORMING OPERATIONS B28 - WORKING CEMENT, CLAY, OR STONE B28B - SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS, SLAG, OR MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
C - CHEMISTRY C04 - CEMENTS C04B - LIME, MAGNESIA
- DOE Contract Number:
- FE0024006
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 10/25/2018
- Country of Publication:
- United States
- Language:
- English
Citation Formats
de Diego, Peter, Greene, John Ellington, Hobart, David Randall, and Murray, III, James Joseph. Ceramic matrix composite turbine nozzle shell and method of assembly. United States: N. p., 2021.
Web.
de Diego, Peter, Greene, John Ellington, Hobart, David Randall, & Murray, III, James Joseph. Ceramic matrix composite turbine nozzle shell and method of assembly. United States.
de Diego, Peter, Greene, John Ellington, Hobart, David Randall, and Murray, III, James Joseph. Tue .
"Ceramic matrix composite turbine nozzle shell and method of assembly". United States. https://www.osti.gov/servlets/purl/1860065.
@article{osti_1860065,
title = {Ceramic matrix composite turbine nozzle shell and method of assembly},
author = {de Diego, Peter and Greene, John Ellington and Hobart, David Randall and Murray, III, James Joseph},
abstractNote = {A method of manufacturing a ceramic matrix composite (CMC) turbine nozzle shell is provided. The method includes: assembling a primary outer nozzle platform, a primary inner nozzle platform, a core and trailing edge preform, and an airfoil-shaped body; joining the primary outer nozzle platform to a secondary outer nozzle platform of the airfoil-shaped body; and joining the primary inner nozzle platform to a secondary inner nozzle platform of the airfoil-shaped body. Composite plies circumferentially surround the airfoil-shaped body, and their longitudinal edges are cut into fingers that are folded down. The fingers are interleaved between secondary platform plies to form the secondary outer and inner nozzle platforms.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Nov 16 00:00:00 EST 2021},
month = {Tue Nov 16 00:00:00 EST 2021}
}
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