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:
Dec. 05, 2023

Filed:

Aug. 31, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Brendan Michael Freely, Loveland, OH (US);

Kurt David Murrow, Springboro, OH (US);

Michael James McMahon, Cincinnati, OH (US);

Andrew Breeze-Stringfellow, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/02 (2006.01); B64D 27/24 (2006.01); B64C 23/00 (2006.01); B64D 31/12 (2006.01); F04D 25/16 (2006.01);
U.S. Cl.
CPC ...
B64D 27/02 (2013.01); B64C 23/00 (2013.01); B64D 27/24 (2013.01); B64D 31/12 (2013.01); F04D 25/166 (2013.01);
Abstract

An aircraft equipped with a distributed fan propulsion system and methods of operating such aircraft are provided. In one aspect, an aircraft includes a wing having a top surface and a bottom surface. The aircraft also has a distributed propulsion system that includes a suction fan array having one or more fans mounted to the wing and a pressure fan array having one or more fans mounted to the wing. The fans of the suction fan array are each positioned primarily above the top surface of the wing and the fans of the pressure fan array are each positioned primarily below the bottom surface of the wing. The fans of the suction fan array are controllable independent of the fans of the pressure fan array so that the air pressure above and/or below the wing can be locally controlled, allowing for adjustment of lift on the wing.


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