Multi-battery charging station which provides battery-specific charging parameters

Patent metadata

Field	Value
Publication number	US-12466291-B1
Application number	US-202217893527-A
Country	US
Kind code	B1
Filing date	Aug 23, 2022
Priority date	Aug 23, 2021
Publication date	Nov 11, 2025
Grant date	Nov 11, 2025

Abstract

Embodiments of the invention are directed to methods and systems for providing electric power with individualized charging parameters to each battery in a multi-battery system. Electric power from the single power source can be distributed in a controlled and unequal manner. Custom charging parameters can be designed for each battery. The custom charging parameters can be determined based on battery metrics gathered for that battery, and can be designed to optimize for a number of suitable priorities, such as recharging speed and battery health. As a result, each battery can be recharged according to individual needs.

First claim

What is claimed is:

1 . A system comprising:
an aircraft including:
one or more propulsion systems;
a plurality of battery submodules, where each of the plurality of battery submodules is electrically coupled to one or more of the one or more propulsion systems; and
one or more battery monitoring systems, each of which is configured to collect one or more battery metrics for a respective battery submodule of the plurality of battery submodules;
a charger configured to provide electric power the plurality of battery submodules; and a charger interface coupled to the aircraft and the charger, the charger interface including:
a processor; and
a memory coupled with the processor, wherein the memory is configured to provide the processor with instructions which when executed cause the processor to:
receive, from each of the one or more battery monitoring systems, the one or more battery metrics for the respective battery submodule of the plurality of battery submodules;
determine, for each of the plurality of battery submodules, a set of one or more custom charging parameters for the battery submodule based on the one or more battery metrics for the battery submodule;
determine a total charging power based on a plurality of sets of one or more custom charging parameters, where each set of one or more custom charging parameters corresponds to a respective battery submodule of the plurality of battery submodules;
operate the charger to provide the total charging power to a plurality of power converters;
operate the plurality of power converters to distribute the total charging power to one or more of the plurality of battery submodules according to the plurality of sets of one or more custom charging parameters;
receive, from each of the one or more battery monitoring systems, one or more updated battery metrics for the respective battery submodule of the plurality of battery submodules;
determine, for each of the plurality of battery submodules, an updated set of one or more custom charging parameters for the battery submodule based on the one or more updated battery metrics for the battery submodule;
determine an updated total charging power based on the updated sets of one or more custom charging parameters:
operate the charger to provide the updated total charging power; and
operate the plurality of power converters to distribute the updated total charging power to the plurality of battery submodules according to the updated sets of one or more custom charging parameters.

2 . The system of claim 1 , wherein the total charging power is distributed to the plurality of battery submodules unequally.

3 . The system of claim 1 , wherein each of the plurality of sets of one or more custom charging parameters include a custom current amount for a corresponding battery submodule of the plurality of battery submodules.

4 . The system of claim 3 , wherein the custom current amount is a function of time.

5 . The system of claim 3 , wherein the plurality of power converters are DC-to-DC converters, and wherein operating the plurality of power converters to distribute the total charging power to one or more of the plurality of battery submodules includes individually operating each of the plurality of power converters to modify an input electric current received from the charger into an output electric current according to the custom current amount for the corresponding battery submodule.

6 . The system of claim 5 , further comprising:
an adaptor coupled to the aircraft and the charger, wherein the adaptor including:
the charger interface; and
the plurality of power converters.

7 . The system of claim 1 , wherein determining, for each of the plurality of battery submodules, the set of one or more custom charging parameters for the battery submodule includes:
determining at least one priority for the battery submodule; and determining the set of one or more custom charging parameters that satisfy the priority.

8 . The system of claim 7 , wherein the at least one priority includes at least one of maximizing recharging speed and minimizing battery degradation.

9 . The system of claim 1 , further comprising:
a plurality of control connection lines between each of the one or more battery monitoring systems and the charger interface, between each of the power converters and the charger interface, and between the charger and the charger interface; and a plurality of power connection lines between each of the plurality of power converters and their respective battery submodules, and between the charger and each of the plurality of power converters.

10 . An adaptor comprising:
a plurality of DC-to-DC power converters; and a charger interface comprising:
a processor; and
a memory coupled with the processor, wherein the memory is configured to provide the processor with instructions which when executed cause the processor to:
determine a total charging power based on a plurality of sets of one or more custom charging parameters each including include a custom current amount, where each set of one or more custom charging parameters corresponds to a respective battery submodule of a plurality of battery submodules included in an aircraft, wherein each of the plurality of battery submodules is electrically coupled to one or more propulsion systems of the aircraft;
operate a charger to provide the total charging power to the plurality of DC-to-DC power converters; and operate the plurality of DC-to-DC power converters to distribute the total charging power to one or more of the plurality of battery submodules according to the plurality of sets of one or more custom charging parameters including individually operating each of the plurality of DC-to-DC power converters to modify an input electric current received from the charger into an output electric current according to the custom current amount.

11 . The charger interface of claim 10 , wherein the total charging power is distributed to the plurality of battery submodules unequally.

12 . A method comprising:
receiving, by a charger interface, from each of one or more battery monitoring systems, one or more battery metrics for a respective battery submodule of a plurality of battery submodules; determining, by the charger interface, for each of the plurality of battery submodules, based on the one or more battery metrics for the battery submodule, a set of one or more custom charging parameters for the battery submodule; determining, by the charger interface, a total charging power based on the plurality of sets of one or more custom charging parameters, where each set of one or more custom charging parameters corresponds to a respective battery submodule of the plurality of battery submodules included in an aircraft; operating, by the charger interface, a charger to provide the total charging power to a plurality of power converters; operating, by the charger interface, the plurality of power converters to distribute the total charging power to one or more of the plurality of battery submodules according to the plurality of sets of one or more custom charging parameters; receiving, by the charger interface, from each of the one or more battery monitoring systems, one or more updated battery metrics for the respective battery submodule of the plurality of battery submodules; and determining, by the charger interface, for each of the plurality of battery submodules, an updated set of one or more custom charging parameters for the battery submodule based on the one or more updated battery metrics for the battery submodule; determining, by the charger interface, an updated total cha

Assignees

• Wisk Aero Llc

Inventors

• Hom Lewis Romeo
• Cardona Carlos
• Long Geoffrey Alan

Classifications

• H02J7/50

  acting upon multiple batteries simultaneously or sequentially · CPC title

• H02J2105/32

  for aircrafts · CPC title

• B60L58/18 Primary

  of two or more battery modules · CPC title

• B60L2200/10

  Air crafts · CPC title

• B60L58/12

  responding to state of charge [SoC] · CPC title