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:
Dec. 05, 2023

Filed:

Jul. 12, 2021
Applicant:

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

Inventors:

Sean Richard Donovan, Richmond, VT (US);

Nathan William Joseph Wiegman, Essex Junction, VT (US);

Tom Michael Hughes, Bristol, VT (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B60L 50/60 (2019.01); B64D 27/24 (2006.01); B60L 58/10 (2019.01); B64D 45/00 (2006.01); B64C 29/00 (2006.01);
U.S. Cl.
CPC ...
B60L 50/60 (2019.02); B60L 58/10 (2019.02); B64C 29/00 (2013.01); B64D 27/24 (2013.01); B64D 45/00 (2013.01); B60L 2200/10 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A system for disconnecting a battery from an electric aircraft upon impact. The system includes an electric aircraft and a battery assembly electrically coupled to the electric aircraft. The battery assembly is configured to include at least a sensor. The at least a sensor is configured to detect impacts to the electric aircraft. The battery assembly is configured to include a connector. The connector attaches the battery assembly to the electric aircraft. The connector includes an electrically actuating disconnection mechanism. The battery assembly is configured to include a control circuit. The control circuit is electrically connected to the electrically actuating disconnection mechanism. The control circuit is configured to detect, using the at least a sensor, an impact to the aircraft. The control sensor disconnects the connector from the electric aircraft using the electrically actuating disconnection mechanism as a function of the detection of impacts to the electric aircraft.


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