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:
Aug. 18, 2020

Filed:

Jul. 25, 2018
Applicant:

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

Inventors:

Peng Bin, Shenzhen, CN;

Peng Wang, Shenzhen, CN;

Chengyu Yin, Shenzhen, CN;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G03B 17/56 (2006.01); F16M 13/02 (2006.01); B64D 47/08 (2006.01); B64C 39/02 (2006.01); F16M 11/20 (2006.01); F16M 11/18 (2006.01); F16M 11/10 (2006.01); G03B 15/00 (2006.01); G05D 1/00 (2006.01);
U.S. Cl.
CPC ...
B64D 47/08 (2013.01); B64C 39/024 (2013.01); F16M 11/10 (2013.01); F16M 11/18 (2013.01); F16M 11/2071 (2013.01); F16M 13/02 (2013.01); F16M 13/022 (2013.01); G03B 15/006 (2013.01); G03B 17/561 (2013.01); B64C 2201/027 (2013.01); B64C 2201/127 (2013.01); B64C 2201/141 (2013.01); B64C 2201/146 (2013.01); F16M 2200/041 (2013.01); F16M 2200/042 (2013.01); F16M 2200/044 (2013.01); G05D 1/0094 (2013.01);
Abstract

A stabilizing platform for stabilizing a payload includes a frame assembly, a plurality of actuators, and a plurality of electronic speed control (ESC) units. The frame assembly includes a plurality of frame components movable relative to one another and is configured to support the payload. The plurality of actuators are configured to permit the plurality of frame components to move relative to one another. The plurality of actuators include a first actuator that is configured to control movement of the payload about a first axis and a second actuator that is configured to control movement of the payload about a second axis. Each of the plurality of ESC units is electrically coupled to a corresponding actuator of the plurality of actuators and is configured to control actuation of the corresponding actuator. At least one of the plurality of ESC units is received in the payload.


Find Patent Forward Citations

Loading…