Control method for variable level airbag inflation

• US 5,999,871 A
• Filed: 08/05/1996
• Issued: 12/07/1999
• Est. Priority Date: 08/05/1996
• Status: Expired due to Term

• Current Assignee: Loopback Technologies, Inc. (Marathon Patent Group, Inc.)
• Original Assignee: Delphi Technologies, Inc. (BorgWarner Incorporated)
• Inventors: Liu, Jiyao
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): Donnelly, Arthur D.
• Application Number:
  US08/695,814
• Time in Patent Office: 1,219 Days
• Field of Search: 701/45, 701/46, 701/47, 280/738, 280/742, 280/735, 280/730.1, 280/731, 280/732, 280/736, 180/271, 180/272, 180/273, 180/282
• US Class Current: 701/45
• CPC Class Codes: B60R 21/013 including means for detecting collisions, impending collisions or roll-over

Abstract

An airbag with two or more inflators can be inflated in successive stages separated by a time interval, inflated simultaneously or some not inflated at all, depending on crash severity. The first stage inflation is controlled in accordance with a conventional algorithm for single stage deployment. Deployment time and velocity parameters used for the first stage are employed to determine the crash severity and the time interval of the next stage. There is no time delay in the case of a very severe crash, but for a moderately severe crash the time interval is proportional to the difference of the time or velocity and a selected minimum time or velocity value.

Claims

1. A method of controlling deployment of multiple stages of a vehicle inflatable restraint comprising the steps of:

sensing vehicle acceleration;

initiating a deployment algorithm for a first stage of the restraint when the sensed acceleration exceeds a threshold, and if such deployment algorithm determines that the first stave should be deployed;

producing at least one first stage deployment parameter including a deployment time between the initiation of said deployment algorithm and the deployment of said first stage;

comparing the produced first stage deployment parameter to predetermined thresholds to determine crash severity; and

determining if and when to deploy a second stage of the restraint based on the determined crash severity.

2. The method as defined in claim 1 wherein if it is determined that the second stage of the restraint should be deployed the method includes the steps of:

producing a second stage deployment parameter including a secondary deployment time between the initiation of said deployment algorithm and the deployment of said second stage;

comparing the produced second stage deployment parameter to predetermined thresholds to re-determine crash severity as of the time of deployment of the second stage; and

determining if and when to deploy a third stage of the restraint based on the re-determined crash severity.

3. The method as defined in claim 1 wherein the produced first stage deployment parameter includes the deployment time, and the method includes the steps of:

establishing a deployment time threshold defining a crash severity limit;

comparing the deployment time to the established threshold; and

determining that the second stage of the restraint should be deployed immediately if the deployment time is below the established threshold.

4. The method as defined in claim 1 wherein the produced first stage deployment parameter includes the deployment time, and the method includes the steps of:

establishing first and second deployment time thresholds defining crash severity limits;

comparing the deployment time to the first and second thresholds;

determining that the second stage should be deployed;

immediately if the deployment time is below the first thresholds and

after a delay if the deployment time is between the first and second thresholds; and

determining that the second stage should not be deployed if the deployment time is greater than the second threshold.

5. The method as defined in claim 4 wherein the delay is proportional in duration to a difference between the first threshold and the deployment time.

6. A method of controlling deployment of multiple stages of a vehicle inflatable restraint comprising the steps of:

sensing vehicle acceleration;

initiating a deployment algorithm for a first stage of the restraint when the sensed acceleration exceeds a threshold, and if such deployment algorithm determines that the first stage should be deployed;

producing a first stabe deployment time T_D corresponding to a time between initiation of said deployment algorithm and deployment of the first stage, and a first stage velocity V_D corresponding to a change in vehicle velocity at the deployment of said first stage;

establishing first and second time thresholds T_A and T_B with T_A <

T_B, and first and second velocity thresholds V_A and V_B with V_A <

V_B ;

comparing the deployment time T_D to the thresholds T_A and T_B, and comparing the velocity V_D to the thresholds V_A and V_B to determine crash severity; and

determining if and when to deploy a second stage of the restraint based on the determined crash severity.

7. The method as defined in claim 6 wherein the step of determining if and when to deploy the second stage of the restraint includes the step of:

determining to not deploy the second stage if either T_D >

T_B or V_D >

V_B thereby indicating that the crash is not severe.

8. The method as defined in claim 6 wherein the step of determining if and when to deploy the second stage of the restraint includes the step of:

determining to deploy the second stage immediately if T_D <

T_A thereby indicating that the crash is very severe.

9. The method as defined in claim 6 wherein the step of determining if and when to deploy the second stage of the restraint includes the step of:

determining to deploy the second stage after a time delay if T_A <

T_D <

T_B and V_D <

V_A, thereby indicating that the crash is moderately severe.

10. The method as defined in claim 9 wherein the time delay is proportional to T_D -T_A.

11. The method as defined in claim 9 wherein the time delay is determined by T_LIM.sbsb.--_T *(T_D -T_A)/(T_B -T_A) where T_LIM.sbsb.--_T is an empirically determined maximum delay time value.

12. The method as defined in claim 6 wherein the step of determining if and when to deploy the second stage of the restraint includes the step of:

determining to deploy the second stage after a time delay when T_A <

T_D <

T_B and V_A <

V_D <

V_B, thereby indicating that the crash is moderately severe.

13. The method as defined in claim 12 wherein the time delay is determined by the smaller value of T_LIM.sbsb.--_T *(T_D -T_A)/(T_B -T_A) or T_LIM.sbsb._V *(V_D -V_A)/(V_B -V_A) where T_LIM.sbsb.--_T and T_LIM.sbsb.--_V are empirically determined maximum delay time values.