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. 29, 2019

Filed:

Jun. 22, 2016
Applicant:

Amazon Technologies, Inc., Seattle, WA (US);

Inventors:

Brian C. Beckman, Newcastle, WA (US);

Vedran Coralic, Seattle, WA (US);

Gur Kimchi, Bellevue, WA (US);

Assignee:

Amazon Technologies, Inc., Seattle, WA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 39/02 (2006.01); B64C 27/20 (2006.01); B64C 1/40 (2006.01); G10K 11/178 (2006.01); B64C 27/46 (2006.01); B64C 27/473 (2006.01); B64C 11/00 (2006.01); B64C 11/20 (2006.01);
U.S. Cl.
CPC ...
G10K 11/178 (2013.01); B64C 11/00 (2013.01); B64C 11/20 (2013.01); B64C 27/46 (2013.01); B64C 27/473 (2013.01); B64C 39/024 (2013.01); G10K 11/17883 (2018.01); B64C 2201/027 (2013.01); B64C 2201/108 (2013.01); B64C 2220/00 (2013.01); B64C 2230/14 (2013.01); G10K 2210/1281 (2013.01); G10K 2210/3216 (2013.01); G10K 2210/3229 (2013.01); Y02T 50/166 (2013.01);
Abstract

The present disclosure is directed to controlling, reducing, and/or altering sound generated by an aerial vehicle, such as an unmanned aerial vehicle ('UAV'), while the aerial vehicle is airborne. For example, one or more transducers, such as piezoelectric thin-film transducers, or carbon nanotube transducers may be applied or incorporated into or on the surface of propeller blades that are used to aerially navigate the aerial vehicle. As the propeller blade rotates and generates sound, the transducers may be activated to generate one or more anti-sounds that cancel, reduce, or otherwise modify the sound generated by the rotation of the propeller blade. The anti-sound combines with the sound and causes interference such that the combined, or net-effect, is an overall cancellation, reduction, or other modification of the sound.


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