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:
Jun. 23, 2026

Filed:

Oct. 26, 2022
Applicant:

Textron Systems Coporation, Hunt Valley, MD (US);

Inventors:

Matthew T. Velazquez, Mount Airy, MD (US);

James Gard Blonde, Baltimore, MD (US);

Brian Reissner Caskey, Cockeysville, MD (US);

Sean Marshall Baity, Westminster, MD (US);

Assignee:

TEXTRON SYSTEMS CORPORATION, Hunt Valley, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64U 20/80 (2023.01); B64U 10/14 (2023.01); B64U 20/50 (2023.01); B64U 30/293 (2023.01); B64U 50/18 (2023.01); B64U 50/34 (2023.01);
U.S. Cl.
CPC ...
B64U 20/80 (2023.01); B64U 10/14 (2023.01); B64U 20/50 (2023.01); B64U 30/293 (2023.01); B64U 50/18 (2023.01); B64U 50/34 (2023.01); B64U 2201/102 (2023.01); B64U 2201/104 (2023.01);
Abstract

A tactically deployable rotorcraft for targeted delivery of effects and/or sensors includes a body housing an energy subsystem, a control and communications subsystem, and a modular payload compartment for holding an effect or sensor payload, the body having a generally cylindrical outline and a plurality of arm-rotor niches therein. Arm-rotor assemblies are pivotably mounted to the body, each including an articulating arm and a rotor at a distal end, and each being pivotable between (1) a closed position in a corresponding arm-rotor niche within the outline of the body, and (2) an open position extending from the body with the rotor facing in a flight direction. The rotors are powered by the energy subsystem and controlled by the control and communications subsystem to provide powered flight to a target location for delivery of the effect or sensor payload.


Find Patent Forward Citations

Velazquez, Matthew. (2026). Modular rotorcraft and system for air-delivered effects or sensor payloads (U.S. Patent No. 12662265). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12662265

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

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