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. 26, 2024

Filed:

Sep. 02, 2021
Applicant:

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

Inventors:

Kevin Morris, Hawkesbury, CA;

Nicholas Brodeur, Beaconsfield, CA;

Carlos Fenny, Fort Worth, TX (US);

Assignee:

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

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 11/00 (2006.01); B64C 11/46 (2006.01); B64U 10/20 (2023.01); B64U 30/297 (2023.01); B64U 50/14 (2023.01); B64U 50/19 (2023.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 11/001 (2013.01); B64C 11/46 (2013.01); B64U 10/20 (2023.01); B64U 30/297 (2023.01); B64U 50/14 (2023.01); B64U 50/19 (2023.01);
Abstract

An autonomous thrust vectoring ring wing pod is disclosed. A plurality of distributed propulsion element (thruster) layout within a self-articulating ring wing pod allows the pod to selectively control its thrust vector by controlling each propulsion element in the pod. This arrangement allows autonomous and independent control of the tilting of the ring wing relative to the aircraft. The ring wing pod acts as both a nacelle to house the propulsion elements as well as a lifting surface when in wing-borne flight. The autonomous thrust vectoring ring wing pod also provides superior aircraft attitude control in wing-borne flight, thus negating the need for conventional surface controls.


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