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:
Oct. 17, 2023

Filed:

Dec. 23, 2021
Applicant:

Electra Aero, Inc., Falls Church, VA (US);

Inventors:

Christopher B. Courtin, Somerville, MA (US);

Mark Drela, Cambridge, MA (US);

Robert John Hansman, Jr., Cambridge, MA (US);

John S. Langford, III, Falls Church, VA (US);

Oliver Masefield, Stans, CH;

Assignee:

Electra Aero, Inc., Manassas, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/28 (2006.01); B64C 11/00 (2006.01); B64C 9/18 (2006.01); B64D 27/24 (2006.01); B64C 3/58 (2006.01); B64C 9/24 (2006.01); B64C 9/00 (2006.01);
U.S. Cl.
CPC ...
B64C 9/28 (2013.01); B64C 3/58 (2013.01); B64C 9/18 (2013.01); B64C 9/24 (2013.01); B64C 11/00 (2013.01); B64D 27/24 (2013.01); B64C 2009/005 (2013.01);
Abstract

A system and method for lift augmentation of an aircraft having a wing with a leading edge and a trailing edge extending along a wingspan, a plurality of thrust-producing devices connected to the bottom of said wing, at least one flap connected to an inboard portion of said wing proximate the trailing edge, and an aircraft roll control device connected to said wing, wherein the improvement comprises a plurality of slipstreams associated with a plurality of thrust producing devices and a flap adaptable to deflect from a chord of the inboard portion of the wing.


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