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:
May. 09, 2023

Filed:

Dec. 07, 2021
Applicant:

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

Inventors:

Brent Chadwick Ross, Flower Mound, TX (US);

Steven Ray Ivans, Ponder, TX (US);

Jeffrey Paul Nissen, Fort Worth, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 5/00 (2006.01); B64C 39/02 (2023.01); B64C 39/08 (2006.01); B64U 70/20 (2023.01); B64U 80/82 (2023.01); B64C 29/02 (2006.01); B64C 29/00 (2006.01); G05D 1/10 (2006.01);
U.S. Cl.
CPC ...
B64D 5/00 (2013.01); B64C 29/0033 (2013.01); B64C 39/024 (2013.01); B64C 39/08 (2013.01); G05D 1/102 (2013.01); G05D 1/104 (2013.01); B64U 70/20 (2023.01); B64U 80/82 (2023.01);
Abstract

An aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a biplane orientation. The aircraft has an airframe including first and second wings with first and second pylons coupled therebetween. A distributed thrust array is coupled to the airframe including a plurality of propulsion assemblies coupled to the first wing and a plurality of propulsion assemblies coupled to the second wing. A UAV carrier assembly is coupled between the first and second pylons. The UAV carrier assembly has a plurality of UAV stations each configured to selectively transport and release a UAV. A flight control system is configured to control each of the propulsion assemblies and launch each of the UAVs during flight.


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