Air bag deployment system and method for monitoring same

• US 6,305,708 B2
• Filed: 06/29/1998
• Issued: 10/23/2001
• Est. Priority Date: 06/29/1998
• Status: Expired due to Term

• Current Assignee: NXP USA, Inc. (NXP Semiconductors NV)
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Davis, Benjamin R., DeLong, Ronald V.
• Primary Examiner(s): Culbreth, Eric
• Assistant Examiner(s): Lum, L.
• Application Number:
  US09/106,160
• Publication Number:
  US 20010013696A1
• Time in Patent Office: 1,212 Days
• Field of Search: 280/735, 280/737, 280/734, 102/201
• US Class Current: 280/735
• CPC Class Codes: B60R 2021/01095 optical
• CPC Class Codes: B60R 21/01 Electrical circuits for triggering passive safety arrangements, e.g. airbags, safety belt tighteners, in case of vehicle accidents or impending vehicle accidents electrical circuits for transmission of signals between steering wheel and the vehicle itself B60R16/027; for electrically actuating belt retractor locking means B60R22/343
• 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
• CPC Class Codes: B60R 21/26 characterised by the inflation fluid source or means to control inflation fluid flow arrangement or mounting thereof to the vehicle B60R21/20; blasting cartridges for producing gas under pressure in general F42B3/04; initiators or igniters therefor F42B3/10

Abstract

An air bag deployment system (20) includes a microcontroller (21), an inflator (23), and an inflator sensor (24). The inflator sensor (24) is adjacent to the inflator (23) and monitors the firing of the inflator (23). The inflator sensor (24) monitors the firing of a squib (36) of the inflator (23). The inflator sensor (24) transmits an inflator firing signal to the microcontroller (21) when the squib (36) of the inflator (23) is activated. In the absence of the inflator firing signal, a backup firing signal is generated by the microcontroller (21) and is transmitted to a backup squib (37).

Claims

1. An air bag deployment system, comprising:

an inflator; and

an inflator sensor directly connected to the inflator for acoustically monitoring a surface of the inflator to determine if a squib within the inflator is activated.

2. The air bag deployment system of claim 1, further comprising a control circuit coupled to the inflator.

3. The air bag deployment system of claim 1, wherein the inflator sensor is a microphone.

4. The air bag deployment system of claim 1, wherein the inflator sensor is an acoustic sensor for sensing acoustic energy produced by the activation of the squib.

5. A method for monitoring an air bag system, comprising:

transmitting a firing signal to an inflator of the air bag system;

monitoring a surface of the inflator to determine if a pyrotechnic material within the inflator has ignited; and

using an inflator sensor of the air bag system to monitor the inflator and detect ignition, wherein the inflator sensor is directly connected to the inflator.

6. The method of claim 5, wherein monitoring the surface of the inflator includes acoustically monitoring the surface of the inflator by sensing acoustic energy produced by the ignition of the pyrotechnic material.

7. The method of claim 5, further including:

activating a squib of the inflator when the firing signal is received by the inflator; and

transmitting a backup firing signal to the inflator in the absence of the firing signal from the inflator sensor.

8. An air bag deployment system, comprising:

an inflator; and

an inflator sensor directly connected to the inflator for thermally monitoring a surface of the inflator to determine if a pyrotechnic material within the inflator has ignited.

9. The air bag deployment system of claim 8, wherein the inflator sensor is a thermal sensor for sensing thermal energy produced by the igniting of the pyrotechnic material within the inflator.

10. An air bag deployment system, comprising:

an inflator; and

an inflator sensor adjacent to the inflator for sensing light produced by firing of a squib within the inflator.

11. The air bag deployment system of claim 10, further comprising:

a control circuit coupled to the inflator sensor; and

a laser coupled to the control circuit and adjacent to the inflator.

12. The air bag deployment system of claim 10, wherein the inflator sensor is a photo diode.

13. The air bag deployment system of claim 10,

wherein the light has a frequency and the inflator has a wall and comprises an optical window in the wall of the inflator, wherein the optical window is transparent at the frequency of the light produced by the firing of the squib and the inflator sensor receives the light through the optical window.

14. The air bag deployment system of claim 10, wherein the inflator sensor is a light sensor for sensing light produced by igniting of a pyrotechnic material within the inflator.

15. The air bag deployment system of claim 10, wherein the inflator sensor is spaced apart from the inflator.

16. A method for sensing activation of an inflator, comprising:

activating a squib of an inflator; and

optically monitoring a chamber within the inflator to determine if a pyrotechnic material within the inflator has ignited.

17. The method of claim 16, wherein optically monitoring includes sensing light produced by the igniting of the pyrotechnic material.

18. The method of claim 16, further including:

transmitting a firing signal to the inflator to activate the squib;

transmitting an inflator firing signal in response to sensing the light to indicate ignition of the pyrotechnic material; and

transmitting a backup firing signal to activate a backup squib to ignite the pyrotechnic material in the absence of the inflator firing signal.

19. The method of claim 16, further including activating a backup squib if activating of the squib fails.