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:
Jul. 18, 2023

Filed:

Jul. 31, 2022
Applicant:

Beta Air, Llc, South Burlington, VT (US);

Inventors:

Braedon Lohe, Essex Junction, VT (US);

Cullen Jemison, Winooski, VT (US);

Andrew Giroux, Georgia, VT (US);

Tom Hughes, South Burlington, VT (US);

Assignee:

BETA AIR, LLC, South Burlington, VT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H02J 7/00 (2006.01); B60L 58/10 (2019.01); B60L 58/12 (2019.01); B64D 27/24 (2006.01); G01R 31/36 (2020.01); H01M 10/42 (2006.01); G01R 31/382 (2019.01);
U.S. Cl.
CPC ...
H02J 7/00032 (2020.01); B60L 58/10 (2019.02); B60L 58/12 (2019.02); B64D 27/24 (2013.01); G01R 31/3646 (2019.01); H01M 10/425 (2013.01); H02J 7/007 (2013.01); H02J 7/0013 (2013.01); H02J 7/0031 (2013.01); H02J 7/0047 (2013.01); H02J 7/0063 (2013.01); B60L 2200/10 (2013.01); B64D 2221/00 (2013.01); G01R 31/382 (2019.01); H01M 2010/4271 (2013.01); H01M 2220/20 (2013.01); H02J 2310/44 (2020.01);
Abstract

A system for battery management for electric aircraft batteries includes an energy storage system configured to provide energy to the electric aircraft via a power supply connection, the energy storage system including: a battery pack, a sensor configured to detect a condition parameter of the battery pack and generate a battery datum based on the condition parameter, a pack monitoring unit (PMU) configured to receive the battery datum, and a high voltage disconnect configured to terminate the power supply connection between the battery pack and the electric aircraft; a high voltage bus electrically connected to the high voltage disconnect; a primary functional display configured to display information based on battery datum; and a first controller area network (CAN) bus and a second CAN bus communicatively connected to the PMU, the high voltage bus, and the primary functional display.


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