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:
May. 26, 2020

Filed:

Mar. 03, 2017
Applicant:

Samsung Electronics Co., Ltd., Gyeonggi-do, KR;

Inventors:

Sang-In Baek, Gyeonggi-do, KR;

Young-Bae Lee, Gyeonggi-do, KR;

Uy-Hyeon Jung, Gyeonggi-do, KR;

Byoung-Uk Yoon, Gyeonggi-do, KR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/50 (2006.01); B64C 27/08 (2006.01); B64C 27/48 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64C 27/50 (2013.01); B64C 27/08 (2013.01); B64C 27/48 (2013.01); B64C 39/024 (2013.01); B64C 2201/024 (2013.01); B64C 2201/027 (2013.01); B64C 2201/108 (2013.01); B64C 2201/127 (2013.01); B64C 2201/20 (2013.01);
Abstract

An unmanned aerial vehicle (UAV) is provided, which includes a main body; a plurality of frames each extending from the main body; and a plurality of thrust generating devices respectively mounted on the plurality of frames, each of the thrust generating devices including a propeller. The propeller includes a hub that provides a rotation axis of the propeller, and rotates according to an operation of the thrust generating device, and a pair of blades, each of which is pivotably mounted on the hub, and generates a thrust or lift while rotating around the rotation axis as the hub is rotated. The blades are pivotably interlocked with each other such that the blades are aligned to a folded position in which the blades are parallel with each other on the hub in a first arrangement or aligned to an expanded position in a diametric direction of a rotating region of the propeller in a second arrangement.


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