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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.

Patent No.:

US 12741736 B1

PDFFull Text
Date of Patent:
Sep. 22, 2026

Filed:

Apr. 25, 2023

Aeronautical vehicle and method of transitioning between flight modes for an aeronautical vehicle

Applicant:

Technische Universiteit Delft, Delft, NL;

Inventor:

Bart Diane Walter Remes, Delft, NL;

Assignee:

TECHNISCHE UNIVERSITEIT DELFT, Delft, NL;

Attorney:

Tutunjian & Bitetto, P.C.

Primary Examiner:

Jessica B Wong

Int. Cl.
CPC ...
B64C 3/56 (2006.01); B64C 29/00 (2006.01); B64U 10/20 (2023.01); B64U 20/50 (2023.01); B64U 30/293 (2023.01); B64U 30/12 (2023.01);
U.S. Cl.
CPC ...
B64C 3/56 (2013.01); B64C 29/00 (2013.01); B64U 10/20 (2023.01); B64U 20/50 (2023.01); B64U 30/293 (2023.01); B64U 30/12 (2023.01);
Abstract

An aeronautical vehicle performs horizontal flight and/or vertical flight, and has a fuselage, a wing assembly having a first wing part and a second wing part rigidly coupled to one another, a rotor assembly, a horizontal thruster, and an attitude control system. The wing assembly is arranged rotatably with respect to the fuselage to rotate about a vertical pivot axis between a stow position and an active position. The rotor assembly includes two vertical thrust rotors arranged on a rotor support rotatably with respect to the fuselage to rotate the rotor assembly between a stow position and an active position. In a horizontal flight mode the wing assembly is in the active position and the rotor assembly is in the stow position, and in a vertical flight mode the wing assembly is in the stow position and the rotor assembly is in the active position.

Find Patent Forward Citations

Remes, Bart Diane Walter. (2026). Aeronautical vehicle and method of transitioning between flight modes for an aeronautical vehicle (U.S. Patent No. 12741736). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12741736

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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