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:
Sep. 13, 2022

Filed:

Sep. 06, 2019
Applicant:

Industrial Technology Research Institute, Hsinchu, TW;

Inventors:

Yuh-Fwu Chou, Zhubei, TW;

Ho-Cheng Lin, Taipei, TW;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H01M 8/04858 (2016.01); H01M 16/00 (2006.01); H01M 8/04302 (2016.01); B60L 3/00 (2019.01); B60L 50/75 (2019.01); B60L 58/40 (2019.01);
U.S. Cl.
CPC ...
H01M 8/04888 (2013.01); H01M 8/04302 (2016.02); H01M 8/04895 (2013.01); H01M 16/006 (2013.01); B60L 3/0046 (2013.01); B60L 3/0053 (2013.01); B60L 50/75 (2019.02); B60L 58/40 (2019.02); B60L 2200/10 (2013.01); H01M 2250/20 (2013.01); H02J 2300/30 (2020.01);
Abstract

A power supply device disposed on an aircraft to provide a power to the aircraft is provided. The aircraft has an average required power value. The power supply device includes a secondary battery, a transformer and a fuel cell. The transformer is coupled between the secondary battery and the aircraft. The fuel cell is coupled to the aircraft and is adapted to provide a first output current to the aircraft. The transformer has an output voltage set value. When the first output end voltage of the fuel cell is lower than the output voltage set value, the transformer provides a second output current of the secondary battery to the aircraft. The output voltage set value is in a voltage range with a fuel cell output power between the maximum power value of characteristic curve of the fuel cell and the average required power value of the aircraft.


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