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:
Nov. 08, 2022

Filed:

Apr. 19, 2019
Applicant:

Darold B Cummings, Coeur D'Alene, ID (US);

Inventor:

Darold B Cummings, Coeur D'Alene, ID (US);

Assignee:

Wright Electric, Inc., Brooklyn, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64C 15/00 (2006.01); B64D 27/26 (2006.01); B64D 29/02 (2006.01); B64C 7/02 (2006.01); B64D 33/04 (2006.01); B64D 27/12 (2006.01); B64D 27/14 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
B64C 15/00 (2013.01); B64C 7/02 (2013.01); B64D 27/12 (2013.01); B64D 27/14 (2013.01); B64D 27/26 (2013.01); B64D 29/02 (2013.01); B64D 33/02 (2013.01); B64D 33/04 (2013.01);
Abstract

An aircraft having a fuselage with a nose and a flat tail at opposite ends and a pair of wings extending therefrom. A pair of nacelles are detachably connected to the top of respective ones of the wings to be spaced from the fuselage to establish an air flow space therebetween. Each wing-mounted nacelle includes a plurality of fans, a corresponding plurality of electric motors to drive the fans, and dividers that separate the fans from one another. Each wing-mounted nacelle also includes a pair of rotatable air inlet slats at an air intake end and a pair of rotatable air exhaust flaps at an air exhaust end that are rotated relative to one another to control horizontal propulsive thrust, thrust vectoring and thrust reversing of the aircraft. A third nacelle is mounted on top of the flat tail of the fuselage between a pair of horizontal turbo generators.


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