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. 02, 2020

Filed:

Mar. 30, 2016
Applicant:

Vantage Robotics, Llc, San Francisco, CA (US);

Inventors:

Tobin Fisher, San Francisco, CA (US);

Johannes Becker Van Niekerk, Livermore, CA (US);

Assignee:

VANTAGE ROBOTICS, LLC, San Francisco, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/02 (2006.01); B64C 39/02 (2006.01); B64D 33/08 (2006.01); B64D 27/24 (2006.01); B64C 11/20 (2006.01); H02K 9/22 (2006.01); H02K 7/14 (2006.01); H02K 5/02 (2006.01);
U.S. Cl.
CPC ...
B64C 11/02 (2013.01); B64C 11/20 (2013.01); B64C 39/024 (2013.01); B64D 27/24 (2013.01); B64D 33/08 (2013.01); H02K 5/02 (2013.01); H02K 7/14 (2013.01); H02K 9/22 (2013.01); B64C 2201/024 (2013.01); B64C 2201/042 (2013.01); B64C 2201/108 (2013.01); Y02T 50/62 (2013.01);
Abstract

A propeller drive assembly includes an electric motor having a stator and a rotor. During operation the motor generates heat. A propeller made from a thermally conductive plastic includes a hub that is secured to the rotor portion of the motor so that the heat generated within the motor is transferred by conductance through the thermally conductive hub and propeller and then, by convection, is absorbed by the surrounding air, as the propeller rotates through the air. A thermally conductive interface material can be positioned between the rotor portion of the motor and the hub of the propeller to increase the thermal efficiency of the heat transfer between the motor and the propeller. A thermally conductive grease can be used as the interface material and an O-ring seal can be provided about the rotor to prevent the grease from escaping during motor operation.


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