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:
Mar. 17, 2020

Filed:

Sep. 21, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nicholas Joseph Kray, West Chester, OH (US);

Xiaomei Fang, Niskayuna, NY (US);

Christopher Madsen, Garching b. Munchen, DE;

Ian Francis Prentice, Cincinnati, OH (US);

Sultan Shair, Ismaning, DE;

Dong-Jin Shim, Niskayuna, NY (US);

Douglas Duane Ward, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); B29C 70/24 (2006.01); F01D 9/04 (2006.01); F01D 25/00 (2006.01); F01D 5/28 (2006.01); B29C 70/44 (2006.01); B29C 70/48 (2006.01);
U.S. Cl.
CPC ...
B29C 70/24 (2013.01); F01D 5/147 (2013.01); F01D 5/282 (2013.01); F01D 9/041 (2013.01); F01D 25/005 (2013.01); B29C 70/44 (2013.01); B29C 70/48 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2230/30 (2013.01); F05D 2240/80 (2013.01); F05D 2300/603 (2013.01); F05D 2300/6034 (2013.01); Y02T 50/672 (2013.01);
Abstract

A gas turbine engine composite article having a composite article airfoil extending outwardly to an article root to an article airfoil tip. Within the article airfoil is a core including a core airfoil attached to a core root including a core dovetail. A continuous outer three-dimensional braided layer including braided composite material tows are braided on the core and the braided layer covers the entire core airfoil and the core root. The core may be an inflatable mandrel or a composite core made of a composite material. The core may include stiffeners such as an I beam or hollow rectangular cross-section box beams. A method for making such an article includes braiding a continuous outer three-dimensional braided layer including braided composite material tows on the core including covering the entire core airfoil and the core root with the continuous outer three-dimensional braided layer.


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