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:
Oct. 07, 2025

Filed:

Dec. 16, 2021
Applicant:

Aerovironment, Inc., Arlington, VA (US);

Inventors:

Joel Ifill, Los Angeles, CA (US);

Zach Taylor, Redondo Beach, CA (US);

Jason Litzinger, Canyon Lake, CA (US);

Phil Stahlhuth, Pasadena, CA (US);

Marc Berte, Leesburg, VA (US);

Assignee:

AeroVironment, Inc., Arlington, VA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 19/02 (2006.01); B64C 27/02 (2006.01); G05D 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/028 (2013.01); B64C 27/02 (2013.01); G05D 1/105 (2013.01); B64D 19/02 (2013.01);
Abstract

A method of assembling a delivery payload assembly configured to be deployed from an aircraft and travel along a flight path to a predetermined landing destination includes attaching a tail-kit assembly to a first end of a payload, the tail-kit assembly including a rotor blade assembly including a plurality of rotor blades having a central axis of rotation, and a flight control and navigation system configured to control a collective pitch angle of each of the plurality of rotor blades of the rotor blade assembly, configured to control an axial thrust force of the rotor blade assembly, the axial thrust force being at an angle with respect to the central axis of rotation of the rotor blade assembly, and configured to navigate the delivery payload assembly along the flight path to the predetermined landing destination. The method further includes removing the tail-kit assembly from the payload after the payload is delivered to the predetermined landing destination.


Find Patent Forward Citations

Loading…