IP Library Granted Patent US 12,466,291
Granted Patent B1
US 12,466,291 · App. 17/893,527 · Granted Nov 11, 2025

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

Inventors: Lewis Romeo Hom (Mountain View, CA); Carlos Cardona (Mountain View, CA); Geoffrey Alan Long (Montara, CA)
Assignee: Wisk Aero LLC
B60L58/18B60L53/22B60L53/62B60L58/12G01R31/396H02J7/0013B60L2200/10
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Quick Facts
Patent No.
US 12,466,291
App. No.
17/893,527
Granted
Nov 11, 2025
Kind
B1
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.

Claims (56)

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 charging power based on the updated sets of one or more custom charging parameters;

operating, by the charger interface, the charger to provide the updated total charging power to the plurality of power converters; and

operating, by the charger interface, 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.

13 . The method of claim 12 , wherein determining, for each of the plurality of battery submodules, the set of one or more custom charging parameters for the battery submodule includes optimizing a recharging process for the battery submodule.

14 . The method of claim 13 , wherein optimizing the recharging process includes determining a balance between maximizing recharging speed and minimizing battery degradation.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 23, 2025
From: HOM, LEWIS ROMEO; CARDONA, CARLOS; LONG, GEOFFREY ALAN
To: WISK AERO LLC
Reel/Frame 071214/0078 →
Continuity (1)
Provisional Application 63236027 · Aug 23, 2021
References Cited (60)
US 8485464B2 · Kroo · 2013 [cited by applicant]
US 8733690B2 · Bevirt et al. · 2014 [cited by applicant]
US 9764833B1 · Tighe et al. · 2017 [cited by applicant]
US 10110033B1 · Hom et al. · 2018 [cited by applicant]
US 10333328B1 · Hom et al. · 2019 [cited by applicant]
US 10673252B2 · Hom et al. · 2020 [cited by applicant]
US 10868430B1 · Hom et al. · 2020 [cited by applicant]
US 20040107013A1 · Fuller et al. · 2004 [cited by applicant]
US 20110254502A1 · Yount et al. · 2011 [cited by applicant]
US 20130015819A1 · Nakashima et al. · 2013 [cited by applicant]
US 20130126680A1 · Hamke et al. · 2013 [cited by applicant]
US 20160244158A1 · Fredericks et al. · 2016 [cited by applicant]
US 20170353042A1 · Liu · 2017 [cited by applicant]
US 20180339595A1 · Chang · 2018 [cited by applicant]
US 20220115878A1 · Khozikov · 2022 [cited by examiner]
US 20220115897A1 · Ijaz · 2022 [cited by examiner]
EP 3251882B1 · 2019 [cited by applicant]
“Archer Aviation Inc's Invalidity Contentions”, Case No. 3:21-CV-02450-WHO, Oct. 11, 2021, 42 pages. [cited by applicant]
“Battery Charger Multi XS 25000, XS 25000 Multi XT 14000, XT 14000”, CTEK, Available Online at: https://docs.rs-online.com/15d2/0900766b81335f57.pdf, Feb. 27, 2020, 8 pages. [cited by applicant]
“Li-Ion BMS Cell-Board Processor”, Lithiumate EL01, 2011, 14 pages. [cited by applicant]
“Li-Ion BMS Controller Processor”, Lithiumate EL02, 2011, 9 pages. [cited by applicant]
“Lithium Ion Battery Monitoring System”, Analog Devices AD7280A, 2011, 48 pages. [cited by applicant]
“Lithium Power BMS Manual”, GTBMS005A-MC8, Harbin Guantuo Power Equipment Co., Ltd., Jul. 22, 2009, 12 pages. [cited by applicant]
“Owner's Guide : RXV Elite Freedom”, EZGO: A Textron Company, 2017, 60 pages. [cited by applicant]
“Pipistrel Alpha Electro Information Pack”, Pipisrel, Revision 05, Oct. 2017, pp. 1-23. [cited by applicant]
“Strings, Parallel Cells, and Parallel Strings”, OrionBMS, Available Online at: https://www.orionbms.com/manuals/pdf/parallel_strings.pdf, pp. 1-17. [cited by applicant]
“This Week@ NASA”, NASA TV, Jun. 17, 2016, 2 pages. [cited by applicant]
“U-Changer XP Rev 2 User Manual”, Valence—Advanced Energy Systems, Document Version 4.8, Nov. 2011, 61 pages. [cited by applicant]
“Vahana, the Self-Piloted, eVTOL Aircraft from A3 by Airbus, Successfully Completes First FullScale Test Flight”, Airbus, Feb. 2, 2018, 3 pages. [cited by applicant]
“WattsUP, the New 2-Seat Electric Trainer”, Pipistrel Aircraft—News, Available Online at: http://www.pipistrel.si/news/wattsup-the-new-2seat-electric-trainer-took, 2 pages. [cited by applicant]
“XTI Aircraft Tri Fan 600”, Electric VTOL News, 11 pages. [cited by applicant]
“XTI TriFan 665 Flies!”, The Electric VTOL News, May 8, 2019, 8 pages. [cited by applicant]
U.S. Appl. No. 15/885,303 , “Non-Final Office Action”, Apr. 19, 2018, 5 pages. [cited by applicant]
U.S. Appl. No. 15/885,303 , “Notice of Allowance”, Jul. 27, 2018, 5 pages. [cited by applicant]
U.S. Appl. No. 16/135,851 , “Non-Final Office Action”, Nov. 28, 2018, 5 pages. [cited by applicant]
U.S. Appl. No. 16/135,851 , “Notice of Allowance”, Feb. 19, 2019, 5 pages. [cited by applicant]
U.S. Appl. No. 16/405,218 , “Non-Final Office Action”, Oct. 17, 2019, 7 pages. [cited by applicant]
U.S. Appl. No. 16/405,218 , “Notice of Allowance”, Jan. 23, 2020, 5 pages. [cited by applicant]
U.S. Appl. No. 16/856,605 , “Non-Final Office Action”, Jun. 25, 2020, 5 pages. [cited by applicant]
U.S. Appl. No. 16/856,605 , “Notice of Allowance”, Aug. 19, 2020, 6 pages. [cited by applicant]
Andrea , “Battery Management Systems for Large Lithium-Ion Battery Packs”, Artech House, 2010, 303 pages. [cited by applicant]
Bertorelli , “Airbus Announces Electric Aircraft”, Avweb, Apr. 26, 2014, 1 page. [cited by applicant]
Bodson et al., “Control Allocation with Load Balancing”, American Institute of Aeronautics and Astronautics, Aug. 10-13, 2009, pp. 1-13. [cited by applicant]
Bordignon , “Constrained Control Allocation for Systems with Redundant Control Effectors”, Virginia Polytechnic Institute and State University ProQuest Dissertations Publishing, Dec. 19, 1996, 260 pages. [cited by applicant]
Chin et al., “Battery Evaluation Profiles for X-57 and Future Urban Electric Aircraft”, American Institute of Aeronautics and Astronautics/Institute of Electrical and Electronics Engineers Electric Aircraft Technologies… [cited by applicant]
Chin et al., “Battery Performance Modeling on Maxwell X-57”, American Institute of Aeronautics and Astronautics, 2019, pp. 1-15. [cited by applicant]
Clarke et al., “X-57 Power and Command System Design”, Institute of Electrical and Electronics Engineers Transportation Electrification Conference and Expo, Jun. 22-24, 2017, 8 pages. [cited by applicant]
Cobb , “Four-Seat Sun Flyer in the Works”, The Aircraft Owners and Pilots Association, Jul. 23, 2017, 3 pages. [cited by applicant]
Grady , “Pipistrel Introduces Alpha Electro”, Apr. 14, 2015, 1 page. [cited by applicant]
Harkegard , “Efficient Active Set Algorithms for Solving Constrained Least Squares Problems in Aircraft Control Allocation”, Proceedings of the 41st Institute of Electrical and Electronics Engineers Conference on Decisi… [cited by applicant]
Huber , “Electric Sun Flyer Plans Fall First Flight”, Available Online at: https ://www.ainonline.com/aviation-news/general-aviation/2017-07-26/electric-sun-flyer-plans-fal1-first-flight, Jul. 26, 2017, 2 pages. [cited by applicant]
Johansen et al., “Control Allocation—A Survey”, Nov. 2, 2012, 22 pages. [cited by applicant]
Merheb et al., “Active Fault Tolerant Control of Octorotor UAV Using Dynamic Control Allocation”, The 2014 International Conference on Intelligent Unmanned Systems, Sep. 2014, 6 pages. [cited by applicant]
Moore , “The Joby S2 VTOL Concept : Exploring the New Degrees of Design Freedom of Distrusted Electric Propulsion”, Vertifile, Nov.-Dec. 2014, pp. 22-24. [cited by applicant]
Niles , “Pipistrel Flies WATTsUP Electric Trainer”, AVweb, Aug. 24, 2014, 1 page. [cited by applicant]
Rapoport , “Airbus Pivots Electric Aircraft Plans”, Archer-NDCA-00171664, Apr. 1, 2017, 1 page. [cited by applicant]
Stoll et al., “Conceptual Design of the Joby S2 Electric VTOL PAV”, Aviation Technology, Integration, and Operations Conference, Jun. 16-20, 2014, pp. 1-6. [cited by applicant]
Szondy , “E-Fan Electric Aircraft makes First Public Flight”, Archer-NDCA-00171660, Apr. 30, 2014, 4 pages. [cited by applicant]
Yoney , “Pipistrel Taurus Electro G2 takes to the Skies, Goes on Sale”, Archer-NDCA-00171840, Feb. 25, 2011, 5 pages. [cited by applicant]
Zhou et al., “Reconfigurable Control Allocation Technology Using Weighted Least Squares for Nonlinear System in Unmanned Aerial Vehicle”, Session: IS-4: Intelligent Adaptation and Model Identification, Jun. 25, 2012, pp… [cited by applicant]