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:
Sep. 13, 2022

Filed:

Aug. 17, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

David Alan Frey, West Chester, OH (US);

Kirk Douglas Gallier, Liberty Township, OH (US);

Daniel Patrick Kerns, Mason, OH (US);

Brandon ALlanson Reynolds, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 11/00 (2006.01); F01D 25/00 (2006.01); F01D 25/24 (2006.01); C04B 35/573 (2006.01); C04B 37/00 (2006.01); C04B 35/571 (2006.01); C04B 35/515 (2006.01); C04B 35/80 (2006.01);
U.S. Cl.
CPC ...
F01D 9/044 (2013.01); C04B 35/515 (2013.01); C04B 35/571 (2013.01); C04B 35/573 (2013.01); C04B 35/80 (2013.01); C04B 37/001 (2013.01); F01D 9/041 (2013.01); F01D 11/003 (2013.01); F01D 11/005 (2013.01); F01D 25/005 (2013.01); F01D 25/24 (2013.01); C04B 2235/48 (2013.01); C04B 2237/38 (2013.01); C04B 2237/61 (2013.01); C04B 2237/84 (2013.01); F05D 2220/32 (2013.01); F05D 2230/10 (2013.01); F05D 2230/23 (2013.01); F05D 2230/31 (2013.01); F05D 2230/60 (2013.01); F05D 2250/75 (2013.01); F05D 2260/30 (2013.01); F05D 2260/36 (2013.01); F05D 2300/603 (2013.01); F05D 2300/6033 (2013.01);
Abstract

Flow path assemblies and methods for forming such flow path assemblies for gas turbine engines are provided. For example, a flow path assembly for a gas turbine engine has a boundary structure, an airfoil, and a locking feature. The boundary structure and the airfoil are formed from a composite material. The boundary structure defines an opening and a cutout proximate the opening, and the airfoil is sized to fit within the opening of the boundary structure. The locking feature is received within the cutout defined by the boundary structure to interlock the airfoil with the boundary structure.


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