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. 30, 2026

Filed:

May. 06, 2025
Applicant:

General Electric Company, Evendale, OH (US);

Inventors:

Paul Hadley Vitt, Liberty Township, OH (US);

Thomas William Vandeputte, Scotia, NY (US);

Harjit S. Hura, Cincinnati, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F01D 5/141 (2013.01); F02C 3/04 (2013.01); F05D 2240/303 (2013.01); F05D 2240/304 (2013.01);
Abstract

An airfoil assembly for a gas turbine engine includes at least two airfoils. Each airfoil of the at least two airfoils includes a leading edge, a trailing edge, a pressure side extending between the leading edge and the trailing edge, and a suction side opposite the pressure side. Each airfoil defines a chord line extending from the leading edge to the trailing edge along the pressure side, a suction side tangency point, a first reference line extending from the leading edge perpendicular to the chord line, a second reference line extending from the leading edge to the suction side tangency point, a camber line angle defined between the first reference line and the second reference line, and a solidity based on an axial width of the at least two airfoils and a pitch between adjacent ones of the at least two airfoils.


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