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:
Jan. 20, 2026

Filed:

Oct. 09, 2024
Applicant:

General Electric Company, Evendale, OH (US);

Inventors:

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

Brandon W. Miller, Middletown, OH (US);

Keith E. Blodgett, Milford, OH (US);

William J. Solomon, Cincinnati, OH (US);

Scott Alan Schimmels, Miamisburg, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/042 (2006.01); B64D 29/00 (2006.01); F02C 7/057 (2006.01);
U.S. Cl.
CPC ...
F02C 7/042 (2013.01); B64D 29/00 (2013.01); F02C 7/057 (2013.01);
Abstract

A turbine engine including a fan having a plurality of fan blades, a nacelle that extends circumferentially about the fan, an engine intake including an engine inlet, and a variable engine intake system. The nacelle includes a fan cowl and an inlet cowl that is movable with respect to the fan cowl. The engine inlet is defined from a leading edge of the inlet cowl to the plurality of fan blades. The engine inlet defines a droop axis at the leading edge of the inlet cowl. The inlet cowl is tilted at a droop angle that is defined as an angle of the droop axis with respect to an axial plane of the turbine engine. The variable engine intake system adjusts the droop angle of the inlet cowl during operation of the turbine engine.


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