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:
Feb. 22, 2022

Filed:

Mar. 25, 2019
Applicant:

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

Inventors:

Kyle B Clark, Underhill, VT (US);

Herman Wiegman, Essex Junction, VT (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60L 15/20 (2006.01); B64D 31/00 (2006.01); B64D 27/24 (2006.01); B60L 58/12 (2019.01); B64C 29/00 (2006.01); H04L 67/125 (2022.01);
U.S. Cl.
CPC ...
B60L 15/2045 (2013.01); B60L 58/12 (2019.02); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B60L 2200/10 (2013.01); B64C 29/0091 (2013.01); H04L 67/125 (2013.01);
Abstract

A system for maintaining attitude control under degraded or depleted energy source conditions using multiple electric propulsors includes a plurality of propulsors, at least an energy source providing electric power to the plurality of propulsors and a vehicle controller communicatively coupled to each propulsor and configured to calculate initial power levels for the plurality of propulsors, the initial power levels including an initial power level for each propulsor, determine an energy output capacity of the least an energy source under load, calculate, by the vehicle controller, an aggregate potential demand of the plurality of propulsors as a function of the initial power levels, determine that electric potential is insufficient to match the aggregate potential demand, and for each initial power level generate a reduced power level, the reduced power level less than the initial power level and direct a corresponding propulsor to consume electrical power at the reduced power level.


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