The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 15, 2021

Filed:

Oct. 25, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Peter de Diego, Zirconia, NC (US);

John Ellington Greene, Greenville, SC (US);

Matthew Troy Hafner, Honea Path, SC (US);

David Randall Hobart, Cincinnati, OH (US);

James Joseph Murray, III, Mauldin, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/28 (2006.01); C04B 35/565 (2006.01); C04B 41/50 (2006.01); B32B 18/00 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); C04B 35/565 (2013.01); C04B 41/5059 (2013.01); F01D 5/282 (2013.01); F01D 5/284 (2013.01); B32B 18/00 (2013.01); B32B 2603/00 (2013.01); C04B 2235/3826 (2013.01); F05D 2230/31 (2013.01); F05D 2240/128 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A ceramic matrix composite turbine nozzle includes a primary outer nozzle platform; a primary inner nozzle platform; and an airfoil-shaped body extending between the primary inner and primary outer nozzle platforms. The body includes core plies defining a cavity; composite wrap plies circumscribing the core plies and defining an airfoil shape; a secondary outer nozzle platform in contact with the primary outer nozzle platform; and a secondary inner nozzle platform in contact with the primary inner nozzle platform. Each composite wrap ply has two layers of unidirectional fibers oriented transverse to each other and has first and second longitudinal edges. The first and second longitudinal edges are cut into fingers, which are folded in a transverse direction away from a turbine nozzle longitudinal axis and are interleaved between platform plies to define the secondary inner nozzle platform and the secondary outer nozzle platform.


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