Lithium ion satellite battery charge control circuit

• US 6,034,506 A
• Filed: 01/16/1998
• Issued: 03/07/2000
• Est. Priority Date: 01/16/1998
• Status: Expired due to Fees

• Current Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Original Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Inventors: Hall, John C.
• Primary Examiner(s): Tso, Edward H.
• Assistant Examiner(s): TOATLEY, GREGORY J
• Application Number:
  US09/008,237
• Time in Patent Office: 781 Days
• Field of Search: 320/117, 320/122, 320/101
• US Class Current: 320/117
• CPC Class Codes: H02J 7/0019 using switched or multiplexed charge circuits
• CPC Class Codes: H02J 7/0024 Parallel/serial switching of connection of batteries to charge or load circuit
• CPC Class Codes: H02J 7/35 with light sensitive cells

Abstract

A charge control circuit for use with lithium ion satellite batteries that provides for both charge control and cell bypass features. The charge control circuit reconfigures the battery from a series array of cells to a parallel array of cells using switches (that are part of the battery) in order to implement the cell bypass function. The switches are preferably implemented using low resistance mechanical relays to lessen the thermal dissipation of the circuit. The charge control circuit minimizes the amount of current passing through the parallel battery circuit by breaking the battery down into sub-modules for purposes of charging, and using distributed low voltage power supplies for charging. The charge control circuit may also implement sequential charging of the battery along with bus cross strapping to ensure that the satellite electrical bus is always supported by one battery during battery recharging.

Claims

1. Lithium ion battery charging apparatus comprising:

a lithium ion battery comprising a plurality of sub-modules each containing a plurality of battery cells; and

a charge control circuit that comprises;

a plurality of first switches for connecting the battery cells of the plurality of sub-modules in parallel;

a plurality of second switches for connecting the respective battery cells of each of the plurality of sub-modules in series;

a DC to DC power supply having first and second terminals coupled to the battery cells of each of the sub-modules;

a plurality of third switches respectively coupled between the plurality of battery cells of each sub-module and the first terminal the respective DC to DC power supply;

a fourth switch coupled between the respective sub-modules;

a fifth switch respectively coupled between the second terminal of each respective DC to DC power supply and the respective sub-module; and

a sixth switch serially coupled between the charge control circuit and a load.

2. The apparatus of claim 1 which further comprises:

a second lithium ion battery comprising a plurality of sub-modules each containing a plurality of battery cells;

a second charge control circuit that each comprises;

a plurality of first switches for connecting the battery cells of the plurality of sub-modules in parallel;

a plurality of second switches for connecting the respective battery cells of each of the plurality of sub-modules in series;

a DC to DC power supply having first and second terminals coupled to the battery cells of each of the sub-modules;

a plurality of third switches respectively coupled between the plurality of battery cells of each sub-module and the first terminal the respective DC to DC power supply;

a fourth switch coupled between the respective sub-modules;

a fifth switch respectively coupled between the second terminal of each respective DC to DC power supply and the respective sub-module; and

a sixth switch serially coupled between the charge control circuit and a load; and

a cross strap switch coupled between the first and second charge control circuits.

3. Lithium ion battery charging apparatus comprising:

first and second lithium ion batteries comprising a plurality of sub-modules each containing a plurality of battery cells, and wherein the respective batteries are selectively coupled to a load;

first and second charge control circuits that each comprise;

a plurality of first switches for connecting the battery cells of the plurality of sub-modules in parallel;

a plurality of second switches for connecting the respective battery cells of each of the plurality of sub-modules in series;

a DC to DC power supply having first and second terminals coupled to the battery cells of each of the sub-modules;

a plurality of third switches respectively coupled between the plurality of battery cells of each sub-module and the first terminal the respective DC to DC power supply;

a fourth switch coupled between the respective sub-modules;

a fifth switch respectively coupled between the second terminal of each respective DC to DC power supply and the respective sub-module; and

a sixth switch serially coupled between the charge control circuit and a load; and

a cross strap switch coupled between the charge control circuits to selectively couple the first and second batteries to the load.

4. Non-aqueous battery charging apparatus for use in a satellite, comprising:

a non-aqueous battery disposect in a satellite comprising a plurality of sub-modules each containing a plurality of battery cells; and

a charge control circuit that comprises;

charging means for charging each of the cells of the plurality of sub-modules of the non-aqueous battery; and

cell bypass means including a plurality of first switches (Sa) for bypassing battery cells that are faulty, and pluralities of second and third switches (Sb, Sc) for reconfiguring the cells of the battery from a series array of cells to a parallel array of cells to permit battery charging, and wherein the plurality of second switches (Sb) configure the cells of the battery as a series array of cells that are directly connected in series with a load.

5. The apparatus of claim 4 wherein the charging means comprises a plurality of distributed power supplies respectively coupled to the plurality of sub-modules for reducing current required to charge the battery cells.

6. The apparatus of claim 4 wherein the non-aqueous battery comprises a lithium ion battery.

7. The apparatus of claim 4 wherein the charging means comprises:

a plurality of second switches for connecting the respective battery cells of each of the plurality of sub-modules in series;

a DC to DC power supply having first and second terminals coupled to the battery cells of each of the sub-modules;

a plurality of third switches respectively coupled between the plurality of battery cells of each sub-module and the first terminal the respective DC to DC power supply;

a fourth switch coupled between the respective sub-modules; and

a fifth switch respectively coupled between the second terminal of each respective DC to DC power supply and the respective sub-module.

8. Non-aqueous battery charging apparatus comprising:

a non-aqueous battery comprising a plurality of sub-modules each containing a plurality of battery cells; and

a charge control circuit that comprises;

charging means for charging each of the cells of the plurality of sub-modules of the non-aqueous battery; and

cell bypass means for bypassing battery cells that are faulty and for reconfiguring the cells of the battery from a series array of cells to a parallel array of cells to permit battery charging,

a second non-aqueous battery comprising a plurality of sub-modules each containing a plurality of battery cells, and wherein the respective batteries are selectively coupled to a load; and

a second charge control circuit that comprises;

charging means for charging each of the cells of the plurality of sub-modules of the second non-aqueous battery; and

cell bypass means for bypassing battery cells that are faulty and for reconfiguring the second battery from a series array of cells to a parallel array of cells to permit battery charging; and

a cross strap switch coupled between the respective charge control circuits;

and wherein the first and second charge control circuits cooperate to sequentially charge the respective batteries and wherein the cross strap switch is switched to ensure that the satellite electrical bus is always supported by one battery during battery recharging.