Current limit controller for an air bag deployment system

• US 5,734,317 A
• Filed: 07/01/1996
• Issued: 03/31/1998
• Est. Priority Date: 07/01/1996
• Status: Expired due to Term

• Current Assignee: Freescale Semiconductor, Inc. (NXP Semiconductors NV)
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Gray, Randall C., Bennett, Paul T.
• Primary Examiner(s): Swarthout, Brent A.
• Assistant Examiner(s): TRIEU, VAN THANH
• Application Number:
  US08/674,067
• Time in Patent Office: 638 Days
• Field of Search: 340/436, 340/438, 340/514, 280/734, 280/735, 180/271, 180/282, 307/10.1
• US Class Current: 340/436
• 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 air bag deployment system (10) generates the proper current to activate a squib (74) and deploy an air bag. A separate capacitor (48) powers circuitry in a drive limit controller (54) for providing a variable voltage drive to a MOS device (68) to regulate squib (74) firing current. A switch circuit (38) supplies gate current to a transistor (46) such that an electrical connecting path allows a capacitor (22) to charge a capacitor (48). During squib (74) firing and air bag deployment, the switch circuit (38) provides electrical isolation between the decaying voltage stored on the capacitor (22) that powers the squib (74) current and the capacitor (48) that provides current regulation to the squib (74) from the drive limit controller (54).

Claims

1. An air bag deployment system, comprising:

a switch circuit having a first terminal and a second terminal;

a transistor having a base terminal coupled to the first terminal of the switch circuit, a collector terminal coupled to the second terminal of the switch circuit for receiving a first energy, and an emitter terminal for receiving a second energy;

a drive limit controller having a voltage terminal coupled to the emitter terminal of the transistor, a first input terminal, a second input terminal, and an output; and

a transistor having a gate coupled to the output of the drive limit controller, a drain terminal coupled to the second terminal of the switch circuit, and a source terminal that provides the first energy as a deployment energy in the air bag deployment system.

2. The air bag deployment system of claim 1 wherein the switch circuit controls the transistor to provide an isolation path during squib firing, the isolation path being from the first conducting electrode to the second conducting electrode of the transistor when the transistor is nonconducting.

3. The air bag deployment system of claim 1 wherein the switch circuit controls the transistor to provide an isolation path during diagnostics, the isolation path being from the first conducting electrode to the second conducting electrode of the transistor when the transistor is nonconducting.

4. The air bag deployment system of claim 1 further comprising a semiconductor device and a resistor coupled in series and each separately coupled to the drive limit controller.

5. The air bag deployment system of claim 4 wherein the resistor provides a voltage change in accordance with a current change in the semiconductor device, and

the drive limit controller provides a voltage to a gate of the semiconductor device in response to the voltage change.

6. The air bag deployment system of claim 1, further comprising a resistor having a first terminal and a second terminal, wherein the first terminal of the resistor is coupled to the source terminal of the metal oxide semiconductor transistor and to the first input terminal of the drive limit controller, and the second terminal of the resistor is coupled to the second input terminal of the drive limit controller.

7. The air bag deployment system of claim 1, further comprising a first capacitor having a first terminal coupled to the collector terminal of the transistor and a second capacitor having a first terminal coupled to the emitter terminal of the transistor.

8. The air bag deployment system of claim 7 wherein the first capacitor stores energy for firing a squib.

9. The air bag deployment system of claim 7 wherein the second capacitor provides a voltage for the drive limit controller.

10. An electrical conduction path for an air bag deployment system, comprising:

a switch circuit having a first terminal for receiving a first stored energy and a second terminal for receiving a second stored energy; and

a transistor having a control electrode coupled to the first terminal of the switch circuit, and a current conducting electrode coupled to the second terminal of the switch circuit, wherein the transistor provides an electrical conduction path controlled by the switch circuit, the transistor being off during deployment of an air bag for separating the first stored energy from the second stored energy.

11. The electrical conduction path of claim 10 further comprising a first capacitor and a second capacitor, wherein the transistor couples the first capacitor to the second capacitor.

12. The electrical conduction path of claim 11 wherein the second capacitor charges the first capacitor through the transistor.

13. The electrical conduction path of claim 12 further comprising a squib, wherein the squib receives charge from the second capacitor.

14. The electrical conduction path of claim 12 further comprising a drive limit controller, wherein the drive limit controller receives charge from the first capacitor.

15. The electrical conduction path of claim 11 wherein the transistor isolates the first capacitor from the second capacitor during a diagnostics check.

16. An integrated circuit for air bag deployment, comprising:

a transistor having a control electrode and a first and a second conducting electrode;

a switch circuit having a first terminal coupled to the control electrode of the transistor and a second terminal coupled to the first conducting electrode of the transistor; and

a high side current circuit having a first input and a second input, wherein the first input of the high side current circuit is coupled to the first conducting electrode of the transistor and the second input of the high side current circuit is coupled to the second conducting electrode of the transistor, and the transistor isolates the first input from the second input of the high side current circuit when the second terminal of the switch circuit receives a signal for air bag deployment.

17. The integrated circuit of claim 16, further comprising a first capacitor coupled to the first conducting electrode and a second capacitor coupled to the second conducting electrode.