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. 31, 2026

Filed:

Dec. 23, 2024
Applicant:

Thomas W. Melcher, Mesa, AZ (US);

Inventor:

Thomas W. Melcher, Mesa, AZ (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64U 10/20 (2023.01); B64U 30/12 (2023.01); B64U 30/24 (2023.01); B64U 30/26 (2023.01); B64U 30/297 (2023.01); B64U 50/19 (2023.01); B64U 70/50 (2023.01); B64U 101/60 (2023.01);
U.S. Cl.
CPC ...
B64U 10/20 (2023.01); B64U 30/12 (2023.01); B64U 30/24 (2023.01); B64U 30/26 (2023.01); B64U 30/297 (2023.01); B64U 50/19 (2023.01); B64U 70/50 (2023.01); B64U 2101/60 (2023.01);
Abstract

An aircraft has a boom, a propulsion assembly coupled to a first end of the boom, and a first wing coupled to a second end of the boom. The first wing can be coupled to the boom by a (first) articulated joint. The propulsion assembly can be coupled to the boom by a (second) articulated joint. The articulated joints can provide various adjustments between the wing(s) and the boom (e.g., stowed, deployed, anhedral, dihedral, sweep, angle of attack, collective pitch control, the cyclic pitch control, etc.) and between the propulsion system and the boom (e.g., to move between vertical flight and horizontal flight). A payload can be connected to the boom with one of the articulated joints whereby the articulated joint adjusts a position of the payload during flight to maintain desired flight characteristics and stabilize the payload.


Find Patent Forward Citations

Loading…