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. 03, 2020

Filed:

Sep. 08, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

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

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

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

Randy M. Vondrell, Cincinnati, OH (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 3/32 (2006.01); B64C 29/00 (2006.01); B64C 3/38 (2006.01); B64D 29/04 (2006.01); B64D 27/08 (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 3/32 (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 wing coupled to, and extending from, the fuselage; and a hybrid-electric propulsion system. The hybrid-electric propulsion system includes a power source including a combustion engine and an electric generator; a plurality of vertical thrust electric fans integrated into the wing and oriented to generate thrust along the vertical direction, the plurality of vertical thrust electric fans arranged along a length of the wing and driven by the power source; and a forward thrust propulsor. The forward thrust propulsor it is selectively or permanently mechanically coupled to the combustion engine.


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