Airbag electronic control unit with central squib current limiting

• US 20060208569A1
• Filed: 03/03/2006
• Published: 09/21/2006
• Est. Priority Date: 03/18/2005
• Status: Abandoned Application

• Current Assignee: Siemens VDO Automotive Corporation (Siemens AG)
• Original Assignee: Siemens VDO Automotive Corporation (Siemens AG)
• Inventors: Morell, Scott
• Application Number:
  US11/368,081
• Publication Number:
  US 20060208569A1
• Time in Patent Office: Days
• US Class Current: 307/10.100
• CPC Class Codes: B60R 21/017 including arrangements for providing electric power to safety arrangements or their actuating means, e.g. to pyrotechnic fuses or electro-mechanic valves

Abstract

An airbag deployment circuit includes at single current regulator controlling multiple squib deployment circuits. Squib deployment circuits that do not have to deploy simultaneously are attached to the same current regulator. A current regulation switch located prior to each current regulator is closed if any of the squib deployment circuits attached to the associated current regulator need to be deployed in a crash event. A high side transistor switch and a low side transistor switch are located adjacent each squib to control activation of that squib deployment circuit. The high side transistor switch and the low side transistor switch are also closed for each of the squib deployment circuits that are to be deployed.

Claims

1. A circuit for an electronic control unit comprising:

an energy source;

a first current regulator connected to said energy source; and

a plurality of squib deployment circuits connected to said current regulator.

2. The circuit of claim 1, wherein each of said plurality of squib deployment circuits are connected to a corresponding plurality of high side transistor switches and a corresponding plurality of low side transistor switches.

3. The circuit of claim 1, wherein each of said plurality of squib deployment circuits are arranged to not have to deploy simultaneously.

4. The circuit of claim 1, wherein said plurality of squib deployment circuits comprises between two and four squib deployment circuits.

5. The circuit of claim 1, wherein said energy source is a vehicle battery.

6. The circuit of claim 1, wherein said energy source includes an energy reserve connected to said circuit with an energy reserve switch.

7. The circuit of claim 1, including a second current regulator connected in parallel to said first current regulator, and a second plurality of squib deployment circuits connected to said second current regulator.

8. The circuit of claim 7, wherein a current regulation switch is connected between said energy source and said first current regulator and a second current regulation switch is connected between said energy source and said second current regulator.

9. An electronic control unit for an airbag deployment system comprising:

an energy source; and

a plurality of current regulators each connected to said energy source with a current regulation switch, wherein said plurality of current regulators are each connected to a plurality squib deployment circuits.

10. The electronic control unit of claim 9, wherein said plurality of current regulators are connected in parallel to said energy source, and said plurality of squib deployment circuits are connected in parallel to said plurality of current regulators.

11. The electronic control unit of claim 9, wherein each of said plurality of squib deployment circuits are connected to a high side transistor switch and a low side transistor switch.

12. The electronic control unit of claim 9, wherein said plurality of squib deployment circuits associated with one of said plurality of current regulators are arranged to not have to deploy simultaneously.

13. The electronic control unit of claim 12, wherein said plurality of squib deployment circuits comprises between two and four squib deployment circuits.

14. The electronic control unit of claim 9, wherein said energy source is a vehicle battery.

15. The electronic control unit of claim 9, wherein said energy source includes an energy reserve connected to said plurality of squib deployment circuits with an energy reserve switch.

16. A method of controlling an electronic control unit for a restraint system comprising:

a) controlling current flow from an energy source to a first plurality of squib deployment circuits with a first current regulator; and

b) closing a first regulator switch to provide current to the first current regulator and the first plurality of squib deployment circuits.

17. The method of claim 16, wherein said step b) includes providing current to the first plurality of squib deployment circuits simultaneously.

18. The method of claim 16, wherein said step b) includes closing a high side transistor switch and a low side transistor switch for each of the first plurality of squib deployment circuits.

19. The method of claim 16, further comprising:

c) controlling current flow from the energy source to a second plurality of squib deployment circuits with a second current regulator; and

e) closing a second regulator switch to provide current to the second current regulator and the second plurality of squib deployment circuits.

20. The method of claim 19, wherein said step b) and said step e) include providing current to the first plurality of squib deployment circuits and the second plurality of squib deployment circuits simultaneously.