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. 11, 2024

Filed:

May. 01, 2023
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Carlos Alexander Fenny, Fort Worth, TX (US);

Rohn Lee Olson, Hurst, TX (US);

Andrew James Zahasky, North Richland Hills, TX (US);

Assignee:

TEXTRON INNOVATIONS INC., Providence, RI (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/02 (2006.01); B64C 1/06 (2006.01); B64C 3/10 (2006.01); B64C 3/16 (2006.01); B64C 11/28 (2006.01); B64C 27/08 (2023.01); B64C 27/12 (2006.01); B64C 27/50 (2006.01); B64C 29/00 (2006.01); B64C 39/02 (2023.01); B64C 39/06 (2006.01); B64D 27/24 (2006.01); B64D 31/00 (2006.01); B64C 1/00 (2006.01); B64C 39/00 (2023.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64C 29/02 (2013.01); B64C 1/068 (2013.01); B64C 3/10 (2013.01); B64C 3/16 (2013.01); B64C 11/28 (2013.01); B64C 27/08 (2013.01); B64C 27/12 (2013.01); B64C 27/50 (2013.01); B64C 29/0025 (2013.01); B64C 39/024 (2013.01); B64C 39/06 (2013.01); B64C 39/062 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B64C 2001/0045 (2013.01); B64C 39/029 (2020.01); B64D 27/026 (2024.01);
Abstract

An aircraft comprises a fuselage, first and second wing segments each having a leading edge and a trailing edge, a plurality of spokes coupling the fuselage to the first and second wing segments, one or more motors disposed within or attached to the plurality of spokes, and three or more propellers proximate to a leading edge of the plurality of spokes, distributed along the plurality of spokes, and operably connected to the motors to provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight and provide thrust whenever the aircraft is in forward flight. When the aircraft is in vertical takeoff and landing and stationary flight, the fuselage is approximately vertical. When the aircraft is in forward flight, the fuselage is approximately in the direction of the forward flight and extends forward beyond the leading edges of the first wing segment and the second wing segment.


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