LITHIUM-ION AIRCRAFT BATTERY WITH AUTOMATICALLY ACTIVATED BATTERY MANAGEMENT SYSTEM

• US 20110248680A1
• Filed: 04/12/2010
• Published: 10/13/2011
• Est. Priority Date: 04/12/2010
• Status: Active Grant

• Current Assignee: Concorde Battery Corporation
• Original Assignee: Concorde Battery Corporation
• Inventors: Vutetakis, David G., Timmons, John B.
• Granted Patent: US 8,179,092 B2
• Time in Patent Office: Days
• US Class Current: 320/120
• CPC Class Codes: H01M 10/0525 Rocking-chair batteries, i.e. batteries with lithium insertion or intercalation in both electrodes; Lithium-ion batteries
• CPC Class Codes: H01M 10/425 Structural combination with electronic components, e.g. electronic circuits integrated to the outside of the casing printed circuits H05K1/00
• CPC Class Codes: H01M 10/48 Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte constructional details of current conducting connections for detecting conditions inside cells or batteries, e.g. details of voltage sensing terminals, H01M50/569
• CPC Class Codes: H01M 50/204 Racks, modules or packs for multiple batteries or multiple cells
• CPC Class Codes: H01M 50/296 characterised by terminals of battery packs terminals of batteries H01M50/543
• CPC Class Codes: H01M 50/569 Constructional details of current conducting connections for detecting conditions inside cells or batteries, e.g. details of voltage sensing terminals battery terminal connectors with integrated measuring arrangements G01R31/364
• CPC Class Codes: H02J 7/0029 with safety or protection devices or circuits
• CPC Class Codes: H02J 7/0048 Detection of remaining charge capacity or state of charge [SOC]
• CPC Class Codes: H02J 7/005 Detection of state of health [SOH]
• CPC Class Codes: H02J 9/005 using a power saving mode for copiers G03G15/5004
• CPC Class Codes: Y02E 60/10 Energy storage using batteries

Abstract

A rechargeable aircraft battery assembly includes at least one lithium-ion cell having a positive cell terminal and a negative cell terminal and a battery management circuit operable to control charging and/or discharging of the lithium-ion cell. The battery management circuit is constantly off when the aircraft circuit is not engaged with the battery connector and is constantly on when the aircraft circuit is engaged with the battery connector.

Claims

1. A rechargeable battery system for supplying electrical power to an aircraft, the battery system comprising:

a. a battery assembly of such size and configuration as to be installed in an aircraft and comprising;

i. at least one lithium-ion cell having a positive cell terminal and a negative cell terminal;

ii. a battery management system having a circuit connected to the cell and operable to monitor and control the operation of the lithium-ion cell, and having an off state and an on state, the battery management circuit being connected to one of the positive and negative cell terminals by a first conductor;

iii. a battery connector having a first jumper terminal and a second jumper terminal;

iv. a second conductor connecting the battery management circuit to the first jumper terminal;

v. a third conductor connecting the second jumper terminal to the other of the positive and negative cell terminals; and

b. an external connector configured to be engaged with the battery connector and including a jumper that electrically connects the first jumper terminal to the second jumper terminal when the battery connector is engaged with the external connector;

c. wherein the battery management circuit is constantly in the off state when the external connector is not engaged with the battery connector, and the battery management circuit is constantly in the on state when the external connector is engaged with the battery connector.

2. The rechargeable battery system of claim 1 wherein the battery connector is a battery power connector and the external connector is an aircraft power connector, wherein the battery connector and external connector cooperate to provide power from the battery to the aircraft when the external connector is engaged with the battery connector.

3. The rechargeable battery system of claim 1 wherein the battery assembly further comprises a battery auxiliary receptacle.

4. The rechargeable battery system of claim 1 wherein the battery connector is a battery auxiliary receptacle and the external connector is an aircraft mating connector, wherein the battery connector and external connector cooperate to provide a communication link between the battery management system and the aircraft when the external connector is engaged with the battery connector.

5. The rechargeable battery system of claim 1 wherein the battery assembly comprises a plurality of lithium-ion cells and wherein the battery management circuit is operable to balance the capacities of the lithium-ion cells whenever the battery management circuit is in the on state.

6. A method of managing a rechargeable battery configured for connection to an external device and having one or more lithium-ion battery cells, the method comprising:

a. providing a battery management circuit;

b. preventing the supply of power from the battery cells to the battery management circuit when the rechargeable battery is disconnected from the external device; and

c. supplying power from the battery cells to the battery management circuit when the rechargeable battery is connected to the external device;

d. wherein the battery management circuit is always off when the rechargeable battery is disconnected from the external device and the battery management circuit is always on when the rechargeable battery is connected to the external device.

7. The method of claim 6 wherein the step of preventing the supply of power from the battery cells to the battery management circuit when the rechargeable battery is disconnected from the external device comprises providing an open circuit between the battery management circuit and the battery cells.

8. The method of claim 7 wherein the step supplying power from the battery cells to the battery management circuit when the rechargeable battery is connected to the external device comprises closing the open circuit.

9. The method of claim 8 wherein closing the open circuit comprises connecting an external connector to the battery that includes a jumper that closes the open circuit when the external connector is connected to the battery.

10. The method of claim 9 wherein the external connector is a power connector.

11. The method of claim 9 wherein the external connector is an auxiliary connector.

12. A battery management system for a rechargeable aircraft battery having at least one lithium-ion battery cell, the battery management system comprising:

a. a battery connector adapted to connect the rechargeable battery to an external device, the battery connector having a first contact and a second contact;

b. a battery management circuit having a first lead and a second lead, one of the leads being connected to a first terminal of the battery cell, and the other of the leads being connected to the first contact of the battery connector;

c. a conductor connecting the second terminal of the battery cell to the second contact of the battery connector;

d. an external connector comprising a jumper configured to selectively connect the first contact and the second contact when the external connector is removably connected to the battery connector; and

e. wherein power is supplied from the battery cell to the battery management circuit when the jumper connects the first contact and the second contact, and no power is supplied from the battery cell to the battery control circuit when the jumper does not connect the first contact and the second contact.

13. The battery management system of claim 12 wherein the external connector is an electrical power connector configured to connect the battery cell to the external device.

14. The battery management system of claim 12 wherein the external connector is an instrumentation connector configured to at least partially connect the battery management circuit to the external device.

15. The battery management system of claim 12 wherein the battery comprises a plurality of battery cells and wherein the battery management circuit is configured to automatically balance the capacities of the battery cells whenever power is supplied from the battery cell to the battery management circuit.

16. A rechargeable battery system for supplying electrical power to an aircraft, the battery system comprising:

a. a battery assembly of such size and configuration as to be installed in an aircraft and comprising;

i. at least one lithium-ion cell having a positive cell terminal and a negative cell terminal;

ii. a battery management system having a circuit connected to the cell and operable to monitor and control the operation of the lithium-ion cell, and having an off state and an on state;

iii. the battery management circuit being normally open until the battery assembly is connected to one of the group consisting of the aircraft electrical system and an external power source, whereupon the battery management system is automatically activated.

17. A battery management system for a rechargeable aircraft battery having at least one lithium-ion battery cell, the battery management system comprising:

a. a battery connector adapted to connect the rechargeable battery to an external device, the battery connector having a first contact and a second contact;

b. a battery management circuit being connected to the battery cell;

c. the battery management circuit being normally open until the battery assembly is connected to one of the group consisting of the aircraft electrical system and an external power source, whereupon the battery management system is automatically activated.