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:
Nov. 03, 2020

Filed:

Feb. 06, 2020
Applicant:

Sz Dji Technology Co., Ltd., Shenzhen, CN;

Inventors:

Dayang Zheng, Shenzhen, CN;

Juncheng Zhan, Shenzhen, CN;

Lei Wang, Shenzhen, CN;

Wentao Wang, Shenzhen, CN;

Baigao Xu, Shenzhen, CN;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02J 7/00 (2006.01); H01M 10/42 (2006.01); H02J 7/34 (2006.01); H01M 2/34 (2006.01); H01M 10/48 (2006.01); B64C 39/02 (2006.01); G05D 1/00 (2006.01); G05D 1/10 (2006.01);
U.S. Cl.
CPC ...
H01M 10/4264 (2013.01); B64C 39/024 (2013.01); G05D 1/0088 (2013.01); G05D 1/101 (2013.01); H01M 2/34 (2013.01); H01M 10/425 (2013.01); H01M 10/482 (2013.01); H01M 10/486 (2013.01); H01M 10/488 (2013.01); H02J 7/0021 (2013.01); H02J 7/0029 (2013.01); H02J 7/0031 (2013.01); H02J 7/34 (2013.01); B64C 2201/042 (2013.01); B64C 2201/14 (2013.01); H01M 2010/4271 (2013.01); H01M 2010/4278 (2013.01); H01M 2200/00 (2013.01); H01M 2220/20 (2013.01);
Abstract

A method is provided for managing an unmanned aerial vehicle (UAV). The UAV includes a first cell unit and a second cell unit connected in parallel. The method includes: detecting, by a first control circuit, whether a failure occurs in the first cell unit; detecting, by a second control circuit, whether a failure occurs in the second cell unit; establishing a communication between the first control circuit and the second control circuit; and in response to detecting a signal indicating that a failure occurs in the first cell or the second cell from the first control circuit or the second control circuit, reducing an output power of a propulsion device of the UAV.


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