Internal battery heating

Patent metadata

Field	Value
Publication number	US-11495839-B2
Application number	US-201816162849-A
Country	US
Kind code	B2
Filing date	Oct 17, 2018
Priority date	Oct 18, 2017
Publication date	Nov 8, 2022
Grant date	Nov 8, 2022

Abstract

An internal battery heating system includes an electrical conversion device electrically coupled to an electrochemical sub-cell or battery modules to form a heating circuit. The electrical conversion device alternately raises and lowers a voltage of the heating circuit to drive current between the heating circuit and the electrochemical sub-cell or battery modules. A controller commands the electrical conversion device to cyclically charge and discharge the electrochemical sub-cell or battery modules for internally heating the battery modules. Alternatively, a battery module may be electrically coupled to electrochemical sub-cells via pairs of switches to form a heating circuit. The pairs of switches are adapted for switching the heating circuit alternately between a parallel arrangement and a series arrangement to alternate charging and discharging of the battery module which results in internal heating of the battery module.

First claim

What is claimed is:

1. An internal battery heating system, comprising:
a heating circuit comprising:
a plurality of battery modules electrically arranged in a parallel arrangement, wherein the plurality of battery modules comprises a first battery module and at least two additional battery modules;
a single electrical conversion device switchably connected to the first battery module and the parallel arrangement via a first switch; and
a plurality of additional switches, each additional switch switchably connected to a respective one of the at least two additional battery modules;

a controller electrically and communicatively coupled with the heating circuit, wherein the controller is adapted to instruct the single electrical conversion device to alternately raise and lower a voltage from the first battery module; and
the controller is adapted to command the first switch and the plurality of additional switches for selectively preheating at least one of the at least two of additional battery modules.

2. The internal battery heating system of claim 1 , wherein the single electrical conversion device is a buck-boost DC-DC converter.

3. The internal battery heating system of claim 1 , further comprising a plurality of temperature sensors and a plurality of voltage sensors communicatively coupled with the controller for monitoring temperature and voltage of the plurality of battery modules, respectively, wherein the controller is adapted to command coordinated switching of the first switch and the plurality of additional switches based on temperatures and voltages of the plurality of battery modules.

4. The internal battery heating system of claim 1 , further comprising an indicator configured to indicate when each of the plurality of additional battery modules has been heated to a predetermined temperature.

5. The internal battery heating system of claim 1 , further comprising an electrical power terminal, wherein each of the plurality of additional switches switchably connects a respective one of the at least two additional battery modules with the electrical power terminal such that each of the at least two additional battery modules is independently heated or independently coupled to the electrical power terminal for providing electrical power.

6. The internal battery heating system of claim 1 , further comprising a control circuit, the control circuit comprising:
a timer configured for activating the internal battery heating system for a duration;
an enable switch that enables a user to activate the internal battery heating system; and
an indicator that provides an indication when the internal battery heating system is active.

7. The internal battery heating system of claim 1 , wherein the first battery module comprises a core battery powering certain components of an aircraft.

8. The internal battery heating system of claim 1 , wherein the first battery module and the at least two additional battery modules comprise a ground power cart for an aircraft.

9. An internal battery heating system, the system comprising:
a heating circuit comprising:
a buck-boost DC-DC converter switchably connected to a first battery module via a first switch;
a second battery module switchably connected to the first battery module via a second switch; and
a third battery module switchably connected to the first battery module via a third switch,
wherein the first battery module, the second battery module, and the third battery module are in a parallel arrangement; and

a controller electrically and communicatively coupled with the heating circuit,
wherein the controller is adapted to instruct the buck-boost DC-DC converter to alternately raise and lower a voltage from the first battery module,
wherein the controller is adapted to command the second switch for selectively preheating the second battery module, and
wherein the controller is adapted to command the third switch for selectively preheating the third battery module.

10. The internal battery heating system of claim 9 , further comprising one or more additionally battery modules, wherein each additional battery module is switchably connected to the first battery module via a respective additional switch.

11. The internal battery heating system of claim 9 , further comprising a plurality of temperature sensors and a plurality of voltage sensors communicatively coupled with the controller for monitoring temperature and voltage of the first battery module, the second battery module, and the third battery module, respectively, wherein the controller is adapted to command coordinated switching of the first switch, the second switch, and the third switch based on temperatures and voltages of the first battery module, the second battery module, and the third battery module.

12. The internal battery heating system of claim 9 , further comprising an indicator configured to indicate when one of the second battery module or the third battery module has been heated to a predetermined temperature.

13. The internal battery heating system of claim 9 , further comprising a control circuit, the control circuit comprising:
a timer configured for activating the internal battery heating system for a duration;
an enable switch that enables a user to activate the internal battery heating system; and
an indicator that provides an indication when the internal battery heating system is active.

14. The internal battery heating system of claim 9 , wherein the first battery module comprises a core battery powering certain components of an aircraft.

15. The internal battery heating system of claim 9 , wherein the first battery module, the second battery module, and the third battery module comprise a ground power cart for an aircraft.

16. The internal battery heating system of claim 15 , further comprising a heater-timer-enable switch for activating the internal battery heating system.

17. The internal battery heating system of claim 16 , wherein the heater-timer-enable switch comprises a networked remote access switch.

18. An internal battery heating system, comprising:
a plurality of battery modules arranged in a parallel arrangement,
wherein the plurality of battery modules comprises a core battery module and at least two additional battery modules;

a plurality of switches each switchably connecting a respective battery module of the plurality of battery modules to the parallel arrangement,
wherein the plurality of switches comprises a core switch switchably connecting the core battery module to the parallel arrangement;

a buck-boost DC-DC converter switchably connected to the parallel arrangement and the core battery module via the core switch; and
a controller electrically and communicatively coupled with the plurality of switches and the buck-boost DC-DC converter,
wherein the controller is adapted to command the core switch to connect the buck-boost DC-DC converter to the parallel arrangement and the core battery module,
wherein the controller is adapted to instruct the buck-boost DC-DC converter to alternately raise and lower a voltage from the core battery module, and
wherein the controller is adapted to command the plurality of switches, independent from the core switch, for selectively preheating one or more batteries modules of the plurality of battery modules.

19. The internal battery heating system of claim 18 , further comprising a plurality of temperature sensors and a plurality of voltage sensors communicatively coupled with the controller for monitoring temperature and vol

Assignees

• Textron Innovations Inc

Inventors

• Beuning Charles Bernard
• Chang Vernon Weng-Yew
• Starr Robby Dale

Classifications

• H01M10/482

  for several batteries or cells simultaneously or sequentially · CPC title

• H01M10/486

  for measuring temperature · CPC title

• H01M10/657

  by electric or electromagnetic means · CPC title

• H01M10/443 Primary

  in response to temperature · CPC title

• H02M3/1582

  Buck-boost converters (H02M3/1584 takes precedence) · CPC title