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. 28, 2022

Filed:

Mar. 27, 2019
Applicant:

Walmart Apollo, Llc, Bentonville, AR (US);

Inventors:

John J. O'Brien, Farmington, AR (US);

Samantha M. O'Brien, Bella Vista, AR (US);

Trey Bishop, Bentonville, AR (US);

Todd Mattingly, Bentonville, AR (US);

Assignee:

Walmart Apollo, LLC, Bentonville, AR (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 15/12 (2006.01); B64D 27/20 (2006.01); B64C 39/02 (2006.01); F04D 29/54 (2006.01); F04D 19/00 (2006.01); F04D 29/38 (2006.01);
U.S. Cl.
CPC ...
B64C 15/12 (2013.01); B64C 39/024 (2013.01); B64D 27/20 (2013.01); B64C 2201/027 (2013.01); B64C 2201/108 (2013.01); F04D 19/002 (2013.01); F04D 29/384 (2013.01); F04D 29/545 (2013.01);
Abstract

A propeller-less unmanned aerial vehicle having a body having a plurality of channels, an inlet formed in the body and configured to allow air flow to enter the plurality of channels from an exterior of the body, an anechoic chamber formed in the body and coupled to the plurality of channels, a rotor comprising a plurality of angled fins located in the anechoic chamber, a control system configured to direct air flow within the plurality of channels, and one or more circular tubes coupled to the exterior of the body and in communication with the plurality of channels. The air flows into the body through the inlet, into the plurality of channels and the anechoic chamber, and exits through the one or more circular tubes to provide lift and directional control to the propeller-less unmanned aerial vehicle.


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