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:
Aug. 11, 2026

Filed:

Nov. 15, 2024
Applicant:

Virginia Tech Intellectual Properties, Inc., Blacksburg, VA (US);

Inventors:

Kevin Kochersberger, Blacksburg, VA (US);

Sarthak Deshmukh, Blacksburg, VA (US);

Katie Marie Moncure, Fairfax, VA (US);

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64U 10/20 (2023.01); B64F 5/10 (2017.01); B64U 20/73 (2023.01); B64U 20/77 (2023.01); B64U 30/29 (2023.01); B64U 50/31 (2023.01); B64U 60/50 (2023.01);
U.S. Cl.
CPC ...
B64U 10/20 (2023.01); B64F 5/10 (2017.01); B64U 20/73 (2023.01); B64U 20/77 (2023.01); B64U 30/29 (2023.01); B64U 50/31 (2023.01); B64U 60/50 (2023.01);
Abstract

Various embodiments of a novel monocoque aerostructure quadcopter implemented as a vertical take-off and landing vehicle are described. In one example, a vertical take-off and landing vehicle includes a fuselage having a leading end positioned in a first horizontal plane and a trailing end positioned in a second horizontal plane that is vertically below the first horizontal plane. The vertical take-off and landing vehicle further includes a first arm assembly extending from the leading end of the fuselage in the first horizontal plane. The vertical take-off and landing vehicle further includes a second arm assembly extending from the trailing end of the fuselage in the second horizontal plane. The vertical take-off and landing vehicle further includes a first rotor assembly coupled to the first arm assembly and a second rotor assembly coupled to the second arm assembly.


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