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:
Apr. 26, 2022

Filed:

Aug. 28, 2020
Applicant:

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

Inventors:

Kevin Morris, Hawkesbury, CA;

Nicholas Brodeur, Beaconsfield, CA;

Pascal Flynn-Robitaille, Laval, CA;

Mathieu Beland, Mirabel, CA;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/02 (2006.01); B64D 1/10 (2006.01); B64C 39/08 (2006.01); B64C 1/00 (2006.01); B64C 1/22 (2006.01); B64C 1/14 (2006.01); B64D 27/24 (2006.01); B64C 39/02 (2006.01); B64D 41/00 (2006.01); G05D 1/10 (2006.01); E05F 15/00 (2015.01);
U.S. Cl.
CPC ...
B64D 1/10 (2013.01); B64C 1/0009 (2013.01); B64C 1/1415 (2013.01); B64C 1/22 (2013.01); B64C 29/02 (2013.01); B64C 39/024 (2013.01); B64C 39/08 (2013.01); B64D 27/24 (2013.01); B64D 41/00 (2013.01); E05F 15/00 (2013.01); G05D 1/102 (2013.01); B64C 2201/02 (2013.01); B64C 2201/042 (2013.01); B64C 2201/108 (2013.01); B64C 2201/128 (2013.01); B64C 2201/141 (2013.01); E05Y 2201/422 (2013.01); E05Y 2900/502 (2013.01);
Abstract

An autonomous cargo delivery aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a biplane orientation. The aircraft includes a fuselage having an aerodynamic shape with a leading edge, a trailing edge and first and second sides. First and second wings are coupled to the fuselage proximate the first and second sides, respectively. A distributed thrust array includes a first pair of propulsion assemblies coupled to the first wing and a second pair of propulsion assemblies coupled to the second wing. A flight control system is operably associated with the distributed thrust array and configured to independently control each of the propulsion assemblies. The first side of the fuselage includes a door configured to provide access to a cargo bay disposed within the fuselage from an exterior of the aircraft with a predetermined clearance relative to the first pair of propulsion assemblies.


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