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:
Jul. 28, 2026

Filed:

Dec. 16, 2025
Applicant:

General Electric Company, Evendale, OH (US);

Inventors:

Trevor H. Wood, Clifton Park, NY (US);

Kishore Ramakrishnan, Rexford, NY (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F04D 19/00 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F04D 29/324 (2013.01); F04D 19/002 (2013.01); F05D 2200/11 (2013.01); F05D 2200/13 (2013.01); F05D 2200/14 (2013.01); F05D 2200/221 (2013.01); F05D 2220/36 (2013.01); F05D 2240/304 (2013.01);
Abstract

An airfoil assembly for turbine engines is provided. The airfoil assembly includes a plurality of airfoils and an airfoil includes a first surface defining a pressure side and a second surface defining a suction side, a plurality of first chord sections defining at least one first chord length, a plurality of second chord sections defining at least one second chord length, and a plurality of wave-shaped projections extending along the trailing edge. The plurality of wave-shaped projections each define a wave peak and a wave trough. The wave-shaped projections have an amplitude that is a proportion of an average local chord length of the airfoil. The wave-shaped projections may be designed according to a relationship to power coefficient, fan pressure ratio, and/or thrust coefficient of a turbine engine to produce an airfoil with a sculpted trailing edge feature that reduces noise during operation of the turbine engine.


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