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. 16, 2018

Filed:

Dec. 09, 2016
Applicants:

David G. Ullman, Independence, OR (US);

Vincent Homer, Independence, OR (US);

Inventors:

David G. Ullman, Independence, OR (US);

Vincent Homer, Independence, OR (US);

Assignee:

Other;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64D 31/06 (2006.01); B64C 3/32 (2006.01); B64D 29/02 (2006.01); B64C 21/00 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 3/32 (2013.01); B64C 21/00 (2013.01); B64D 29/02 (2013.01); B64D 31/06 (2013.01); Y02T 50/166 (2013.01); Y02T 50/44 (2013.01); Y02T 50/64 (2013.01);
Abstract

The Distributed Electric Ducted Fan Wing concept incorporates multiple electric ducted fans on lifting surfaces configured to provide integrated aerodynamics and propulsion resulting in enhanced aerodynamic characteristics and thus aircraft performance. The concept uses a plurality of electric ducted fans (EDFs) to not only provide thrust, but to also blow air across the upper surface of a substantial portion of the lifting surface area increasing lift at little loss in efficiency. Not only can the total lift on the surfaces be enhanced, but the lift distribution managed: to aid in aircraft control; ameliorate the effects of turbulence: reduce shed vortices; mitigate the effects of system failures; eliminate stalls; and compensate for crosswinds. This concept offers the potential for increasing electric airplane efficiency and performance, enhancing Short Takeoff and Landing (STOL) capabilities, improving passenger comfort, and reducing the structural stress and cost of aircraft.


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