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:
Aug. 18, 2020

Filed:

Aug. 30, 2017
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 35/80 (2006.01); C04B 37/00 (2006.01); C04B 35/571 (2006.01);
U.S. Cl.
CPC ...
F01D 9/044 (2013.01); C04B 35/571 (2013.01); C04B 35/573 (2013.01); C04B 35/806 (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 method for assembling an airfoil with a boundary structure to form a flow path assembly is provided. The method includes machining an opening into the boundary structure. The opening is sized to receive an airfoil or other component. The method also includes machining a cutout into the boundary structure proximate the opening. A locking feature is inserted into the cutout. When the airfoil is inserted into the opening, the locking feature interlocks the airfoil with the boundary structure. To seal the airfoil with the boundary structure, the airfoil is pressed against or into the boundary structure. When the airfoil is pressed, the locking feature is compressed such that a seal is formed between the airfoil and the boundary structure to seal the flow path assembly.


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