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. 03, 2022

Filed:

Jun. 14, 2021
Applicant:

Zhejiang University, Hangzhou, CN;

Inventors:

Yao Zheng, Hangzhou, CN;

Junyin Chen, Hangzhou, CN;

Changping Du, Hangzhou, CN;

Guanghua Song, Hangzhou, CN;

Rui Yang, Hangzhou, CN;

Zhixian Ye, Hangzhou, CN;

Zekun Zhang, Hangzhou, CN;

Assignee:

Other;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B60L 8/00 (2006.01); B60L 58/18 (2019.01); H02J 7/35 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B60L 8/003 (2013.01); B60L 58/18 (2019.02); B64C 39/024 (2013.01); H02J 7/35 (2013.01); B60L 2200/10 (2013.01); B60L 2210/10 (2013.01); B60L 2240/547 (2013.01); B60L 2260/24 (2013.01); B64C 2201/042 (2013.01);
Abstract

The present disclosure discloses an energy management system suitable for a solar-powered unmanned aerial vehicle and a control method thereof, which are used for an aerospace vehicle energy system. The system comprises a photovoltaic module, an MPPT controller, a first DC-DC circuit, a battery pack, a first anti-reverse circuit, a second DC-DC circuit, a second anti-reverse circuit, an ESC, a BLDC, an on-board controller, a communication link and a voltage stabilizing module. During cruising, the battery pack directly supplies power to the ESC through the first anti-reverse circuit; when high-power power output is needed, the battery pack supplies power to the ESC through the second DC-DC circuit and the second anti-reverse circuit in sequence, wherein the output voltage of the second DC-DC circuit and the accelerator signal input of the ESC are controlled by the on-board controller.


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