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. 23, 2025

Filed:

Apr. 25, 2025
Applicant:

General Electric Company, Evendale, OH (US);

Inventors:

Brandon Wayne Miller, Evendale, OH (US);

Egbert Geertsema, Evendale, OH (US);

Arthur W. Sibbach, Boxford, MA (US);

Andrew Hudecki, Evendale, OH (US);

Timothy Richard Depuy, Evendale, OH (US);

John C. Schilling, Evendale, OH (US);

Frank Worthoff, Evendale, OH (US);

Tsuguji Nakano, Evendale, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 5/28 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 5/141 (2013.01); F01D 5/282 (2013.01); F01D 25/24 (2013.01); F05D 2240/303 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/961 (2013.01); F05D 2300/603 (2013.01);
Abstract

A gas turbine engine comprises a fan, a core turbine engine coupled to the fan, a fan case housing the fan and the core turbine engine, a plurality of outlet guide vanes extending between the core turbine engine and the fan case, and an acoustic spacing. Acoustic spacing comprises a distance between the fan and the plurality of outlet guide vanes, and in combination with the use of airfoils with leading edge protectors for both various stages of blades and vanes, the engine effectively reduces noise emissions, enhances aerodynamic efficiency, and improves structural durability.


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