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:
Mar. 21, 2023

Filed:

Sep. 20, 2021
Applicant:

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

Inventors:

John Richard McCullough, Weatherford, TX (US);

Paul K. Oldroyd, Azle, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/08 (2006.01); B64C 29/00 (2006.01); B64C 3/56 (2006.01); B64C 11/46 (2006.01); B64C 17/00 (2006.01); B64C 29/02 (2006.01); B64C 39/02 (2023.01); B64D 27/24 (2006.01); B64D 27/26 (2006.01); B64C 27/30 (2006.01); B64C 1/06 (2006.01); G05D 1/00 (2006.01); G05D 1/10 (2006.01); B64U 30/10 (2023.01); B64U 30/20 (2023.01); B64U 101/60 (2023.01);
U.S. Cl.
CPC ...
B64C 39/08 (2013.01); B64C 1/063 (2013.01); B64C 3/56 (2013.01); B64C 11/46 (2013.01); B64C 17/00 (2013.01); B64C 27/30 (2013.01); B64C 29/0033 (2013.01); B64C 29/02 (2013.01); B64C 39/024 (2013.01); B64D 27/24 (2013.01); B64D 27/26 (2013.01); G05D 1/0094 (2013.01); G05D 1/101 (2013.01); G05D 1/102 (2013.01); G05D 1/106 (2019.05); B64C 2211/00 (2013.01); B64D 2027/262 (2013.01); B64U 30/10 (2023.01); B64U 30/20 (2023.01); B64U 2101/60 (2023.01);
Abstract

A package delivery system uses unmanned aircraft operable to transition between thrust-borne lift in a VTOL configuration and wing-borne lift in a forward flight configuration. Each of the aircraft includes an airframe having at least one wing with a distributed thrust array coupled to the airframe. The distributed thrust array includes a plurality of propulsion assemblies configured to provide vertical thrust in the VTOL configuration and a plurality of propulsion assemblies configured to provide forward thrust in the forward flight configuration. A package delivery module is coupled to the airframe. A control system is operably associated with the distributed thrust array and the package delivery module. The control system is configured to individually control each of the propulsion assemblies and control package release operations of the package delivery module. The system includes a ground station configured to remotely communicate with the control systems of the aircraft during package delivery missions.


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