Method and apparatus for testing an airbag restraint system with parallel sensors

• US 5,293,153 A
• Filed: 04/09/1991
• Issued: 03/08/1994
• Est. Priority Date: 04/09/1991
• Status: Expired due to Fees

• Current Assignee: TRW Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Original Assignee: TRW Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Inventors: Abeska, Edward J., Rochette, Jeffrey R.
• Primary Examiner(s): Swarthout, Brent
• Application Number:
  US07/682,566
• Time in Patent Office: 1,064 Days
• Field of Search: 340/436, 340/438, 307/10.1, 280/734, 280/735
• US Class Current: 340/438
• CPC Class Codes: B60R 21/0176 for firing circuits using only mechanical switches as collision detecting means, in series with pyrotechnic fuses
• CPC Class Codes: G01R 31/007 using microprocessors or computers

Abstract

A method and apparatus are disclosed for testing an airbag restraint system of the type having at least two parallel connected inertia sensors connected in series with a squib across a source of electrical energy, each inertia sensor having a normally open switch and an associated parallel connected resistor. Each parallel connected inertia sensor has a series connected diode for isolating its associated inertia sensor circuit from other circuit components in the firing circuit. A microcontroller monitors at least one voltage value at a component connection while at least one parallel connected inertia sensor is isolated. The microcontroller determines a value functionally related to the resistance of at least one circuit component in the firing circuit while at least one parallel connected inertia sensor is isolated. The microcontroller compares the determined value against predetermined limits. If the determined value is not within the predetermined limits, an error indication is provided.

Claims

1. An apparatus for testing an airbag restraint system of the type having a firing circuit including at least two parallel connected inertia sensors connected in series with a squib across a source of electrical energy, each of said at least two parallel connected inertia sensors having a normally open switch and an associated parallel connected resistor, said apparatus comprising:

means for isolating at least one of the parallel connected inertia sensors of the firing circuit from the other inertia sensor of the firing circuit;

means for monitoring, in said firing circuit, at least one voltage value at a component connection while said at least one of the parallel connected inertia sensors is isolated;

means for determining from the monitored voltage value a value functionally related to the resistance of at least one circuit component of said firing circuit while said at least one of the parallel connected inertia sensors is isolated;

means for comparing the determined value against a predetermined limit; and

means for providing an error indication in response to said means for comparing.

2. The apparatus of claim 1 wherein said means for isolating includes diodes, each one of said two parallel connected inertia sensors having one of said diodes connected in series therewith so that said one of said two parallel connected inertia sensors is connected to the cathode side of said one of said diodes, the anode of each of said one of said diodes being connected to one terminal of the squib, said means for isolating further including a plurality of switching circuits, each of said one of said diodes having an associated switching circuit, each said associated switching circuit including a normally open switch, for, when closed, reverse biasing said one of said diodes.

3. The apparatus of claim 2 wherein said switching circuits include a first switching circuit connected between a source of electrical energy and the cathode of one of said diodes and a second switching circuit connected to the anode of said one of said diodes and to electrical ground for, when said first and second switching circuits are actuated, reverse biasing said one of said diodes and establishing a known test current through the parallel connected resistor associated with said one of said inertia sensors whose associated diode is reversed biased.

4. The apparatus of claim 3 wherein said means for monitoring includes means to monitor the voltage at the associated cathode of said one of said diodes and wherein said means for determining determines a value functionally related to the value of the parallel connected resistor associated with said one of said inertia sensors associated with the monitored cathode of the reversed biased diode.

5. The apparatus of claim 3 wherein said airbag restrain system includes a series connected inertia sensor having a normally open switch and a parallel connected resistor and wherein said switching circuits further include a third switching circuit connected between the source of electrical energy and the cathode of another of said one of said diodes, closure of said three switching circuits isolating said series connected inertia sensor from said parallel connected inertia sensors.

6. The apparatus of claim 3 wherein said first switching circuit includes a series connected sensing resistor of known value.

7. The apparatus of claim 5 wherein said second and third switching circuits each includes an associated series connected sensing resistor of known value.

8. An apparatus for testing an airbag restraint system of the type having a firing circuit including a safing inertia sensor having a normally open safing inertia switch and a safing resistor connected in parallel with the safing inertia switch, one terminal f the safing inertia switch connected to a source of electrical energy, a second terminal of said safing inertia switch connected to a first terminal of a squib, a first diode and a second diode each having their anode connected to a second terminal of said squib, the cathode of the first diode connected to a first parallel inertia sensor having a first normally open parallel inertia switch and a resistor connected in parallel with the first parallel inertia switch, the second terminal of said first parallel inertia switch being connected to electrical ground, a second parallel inertia sensor having a second normally open parallel inertia switch and a resistor connected in parallel with the second parallel inertia switch, one terminal of said second parallel inertia switch connected to the cathode of said second diode, the second terminal of said second parallel inertia switch being connected to electrical ground, said apparatus comprising:

a first switching network connected between said source of electrical energy and the cathode of the first diode, said first switching network including a first actuatable solid state switch connected in series with a first test resistor having a known resistance value;

a second switching network connected between the source of electrical energy and the cathode of the second diode, said second switch network including a second actuatable solid state switch connected in series with a second test resistor having a known resistance value;

a third switching network connected between the anodes of the first and second diodes and electrical ground, said third switching network including a third actuatable solid state switch connected in series with a third test resistor having a known resistance value;

means for controlling said first, second, and third solid state switches so as to selectively reverse bias said first and second diodes, and establish known test currents selectively though said parallel connected resistors of said safing sensor and the parallel connected resistors of the first and second parallel inertia sensors;

means for monitoring the voltage values of the source of electrical energy and the voltage value present at selected circuit junctions;

means for determining the resistance values of selected sensors based upon said monitored voltage values; and

means to warn the vehicle operator if the determined resistance values are not within predetermined limits.

9. A method for testing an airbag restraint system of the type having a firing circuit including at least two parallel connected inertia sensors connected in series with a squib across a source of electrical energy, each of said parallel connected inertia sensors having a normally open switch and an associated parallel connected resistor, said method comprising the steps of:

isolating at least one of the parallel connected inertia sensors of the firing circuit from the other circuit components of the firing circuit;

monitoring at least one voltage value at a component connection while said at least one of the parallel connected inertia sensors is isolated;

determining from the monitored voltage value a value functionally related to the resistance of said at least one parallel connected inertia sensor;

comparing the determined value against predetermined limits; and

providing an error indication if the determined value is not within the predetermined limits.