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:
Sep. 14, 2021

Filed:

Jul. 23, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

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

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

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

Dominic Barone, Centerville, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64D 29/04 (2006.01); B64C 3/10 (2006.01); B64D 27/08 (2006.01); B64C 3/32 (2006.01); B64C 35/02 (2006.01); B64C 3/38 (2006.01); B64D 33/04 (2006.01); B64D 31/06 (2006.01); B64C 29/00 (2006.01); B64D 35/02 (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 plurality of vertical thrust electric fans driven by the power source; and a wing extending from the fuselage. The plurality of vertical thrust electric fans are arranged along a length of the wing, the wing including a variable geometry assembly extending along the length of the wing and moveable between a forward thrust position and a vertical thrust position, the variable geometry assembly at least partially covering the plurality of vertical thrust electric fans when in the forward thrust position and at least partially exposing the plurality of vertical thrust electric fans when in the vertical thrust position.


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