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. 20, 2022

Filed:

Jun. 24, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Patrick Michael Marrinan, Mason, OH (US);

Thomas Lee Becker, Symmes Township, OH (US);

Kurt David Murrow, Liberty Township, OH (US);

Jixian Yao, Niskayuna, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 29/04 (2006.01); B64C 1/16 (2006.01); B64C 21/06 (2006.01); B64D 27/20 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
B64D 29/04 (2013.01); B64C 1/16 (2013.01); B64C 21/06 (2013.01); B64D 27/20 (2013.01); B64D 33/02 (2013.01); B64D 2033/0226 (2013.01); Y02T 50/10 (2013.01);
Abstract

An aircraft including a fuselage and an aft engine is provided. The fuselage extends from a forward end of the aircraft towards an aft end of the aircraft. The aft engine is mounted to the fuselage proximate the aft end of the aircraft and includes a fan and a nacelle. The fan is rotatable about a central axis of the aft engine and includes a plurality of fan blades. The nacelle of the aft engine surrounds the plurality of fan blades and defines a bottom portion having a forward end. Additionally, the nacelle defines a curved surface at the forward end of the bottom portion, the curved surface including a reference point where the curved surface defines the smallest radius of curvature. The nacelle further defines a normal reference line extending normal from the reference point. The normal reference line defines an angle with the central axis of the aft engine greater than zero to, e.g., allow for a maximum amount of airflow into the aft engine.


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