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:
Jun. 22, 2021

Filed:

Jul. 23, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

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

Darek Tomasz Zatorski, Fort Wright, KY (US);

Dominic Barone, Centerville, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64C 29/00 (2006.01); B64C 3/38 (2006.01); B64D 29/04 (2006.01); B64C 3/10 (2006.01); B64D 27/08 (2006.01); B64C 3/32 (2006.01); B64D 35/02 (2006.01); B64D 33/04 (2006.01); B64D 31/06 (2006.01); B64D 27/02 (2006.01); B64D 27/26 (2006.01); H02K 7/18 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 3/10 (2013.01); B64C 3/32 (2013.01); B64C 3/38 (2013.01); B64C 29/0025 (2013.01); B64D 27/08 (2013.01); B64D 29/04 (2013.01); B64D 31/06 (2013.01); B64D 33/04 (2013.01); B64D 35/02 (2013.01); B64D 27/02 (2013.01); B64D 27/26 (2013.01); B64D 2027/026 (2013.01); F05D 2220/76 (2013.01); F05D 2270/093 (2013.01); H02K 7/1823 (2013.01);
Abstract

An aircraft includes a fuselage; a propulsion system including a power source and a vertical thrust electric fan oriented to generate thrust along a vertical direction and powered by the power source; and a wing extending from the fuselage and including the vertical thrust electric fan positioned at least partially therein. The wing includes a variable geometry assembly having partial wing assembly, the partial wing assembly including a frame and a first member, the partial wing assembly moveable generally along a longitudinal direction when the variable geometry assembly is moved between a forward thrust position and a vertical thrust position, the first member moveable relative to the frame to form an exhaust path for the vertical thrust electric fan.


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