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. 17, 2025

Filed:

Sep. 17, 2020
Applicants:

Fordrone Co., Ltd., Naju-si, KR;

Weon Kook Kim, Andong-si, KR;

Jin Kyo Shin, Yongin-si, KR;

Kwang Rae Kim, Seoul, KR;

Inventors:

Weon Kook Kim, Andong-si, KR;

Jin Kyo Shin, Yongin-si, KR;

Kwang Rae Kim, Seoul, KR;

Young Ju Jeong, Seoul, KR;

Gang Hyeon Lee, Gunpo-si, KR;

Assignee:

FORDRONE CO., LTD., Naju-si, KR;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/00 (2024.01); B64C 39/02 (2023.01); B64D 45/00 (2006.01); B64U 10/00 (2023.01); B64U 50/19 (2023.01); H04W 12/037 (2021.01); H04W 12/069 (2021.01);
U.S. Cl.
CPC ...
B64D 31/00 (2013.01); B64C 39/024 (2013.01); B64D 45/00 (2013.01); B64U 10/00 (2023.01); B64U 50/19 (2023.01); H04W 12/037 (2021.01); H04W 12/069 (2021.01); B64D 2045/0065 (2013.01); B64D 2045/0085 (2013.01); B64U 2201/20 (2023.01);
Abstract

Provided is an aerial vehicle including an emergency control device through power regulation. The aerial vehicle includes a power unit configured to supply power for the aerial vehicle, a flight control device configured to receive a wireless control signal from control terminal, and control a movement of the aerial vehicle based on the received control signal, and a power regulation device arranged between the power unit and the flight control device and configured to transmit the power from the power unit to the flight control device, wherein the power regulation device includes a communication unit configured to externally receive an emergency control signal through certain radio waves, a verification unit configured to verify whether the received emergency control signal is given according to a predetermined authority, and a power regulation unit configured to cut off the power supplied from the power unit to the flight control device.


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