Satellite crash sensor and method with constant and dynamic thresholds for multi-stage restraint deployment

• US 6,363,308 B1
• Filed: 10/16/2000
• Issued: 03/26/2002
• Est. Priority Date: 10/16/2000
• Status: Expired due to Term

• Current Assignee: Delphi Technologies Ip Limited (BorgWarner Incorporated)
• Original Assignee: Delphi Technologies, Inc. (BorgWarner Incorporated)
• Inventors: Potti, Shyam V., Kvapil, Brian Scott, Brogoitti, James Hill, Patterson, Sheri Lynn, Boger, Lee Charles, Martinez, Hector Daniel, Caruso, Christopher Michael
• Primary Examiner(s): Camby, Richard M.
• Application Number:
  US09/688,750
• Time in Patent Office: 526 Days
• Field of Search: 701/36, 701/45, 701/46, 701/47, 180/271, 180/273, 180/274, 180/282, 280/734, 280/735, 340/436, 340/903
• US Class Current: 701/45
• CPC Class Codes: B60R 2021/01027 Safing sensors
• CPC Class Codes: B60R 2021/01322 comprising variable thresholds, e.g. depending from other collision parameters
• CPC Class Codes: B60R 21/013 including means for detecting collisions, impending collisions or roll-over
• CPC Class Codes: B60R 21/0132 responsive to vehicle motion parameters , e.g. to vehicle longitudinal or transversal deceleration or speed value

Abstract

A satellite crash sensor for a motor vehicle occupant restraint system that provides multi-stage deploy signaling in a manner that detects a second stage deploy crash event having an initial velocity rise followed by a loss of velocity that delays the continuation of the velocity rise. The sensor derives a velocity value from an accelerometer signal. The initiation of a possible crash event is detected and a clock count indicating a time progression into the event is initiated. A constant second stage threshold value and data defining a first stage threshold varying as function of the clock count are stored. Only for a time indicated by a first predetermined value of the clock count, a second stage datum is stored if the velocity exceeds the second stage threshold value. For a longer time determined by a second predetermined clock count, the velocity value is compared with a clock count determined value of the first stage threshold and alternatively (1) a second stage deploy signal is generated if the velocity value exceeds the value of the first stage threshold and the second stage datum is stored, (2) a first stage deploy signal is generated if the velocity value exceeds the value of the first stage threshold and the second stage datum is not stored, and (3) no deploy signal is generated if the velocity value does not exceed the first stage threshold. For at least a portion of the predetermined clock count, the clock determined value of the first threshold exceeds the second threshold value.

Claims

1. A satellite crash sensor for a motor vehicle occupant restraint system, the sensor comprising:

an accelerometer for providing an acceleration signal;

means for detecting the initiation of a possible crash event and initiating a clock count indicating a time progression into the event;

means for storing a constant second stage threshold value and data defining a first stage threshold that varies as function of the clock count;

means, effective only for a time indicated by a predetermined value of the clock count, for comparing the velocity value with the second stage threshold and storing a second stage datum if the velocity exceeds the second stage threshold value;

means for comparing the velocity value with a clock count determined value of the first stage threshold and alternatively;

(1) generating a second stage deploy signal if the velocity value exceeds the value of the first stage threshold and the second stage datum is stored,

(2) generating a first stage deploy signal if the velocity value exceeds the value of the first stage threshold and the second stage datum is not stored, and

(3) generating no deploy signal if the velocity value does not exceed the first stage threshold.

2. The sensor of claim 1 in which, for at least a portion of the predetermined clock count, the clock determined value of the first threshold exceeds the second threshold value.

4. Method according to claim 1 in which, for at least a portion of the predetermined clock count, the clock determined value of the first threshold exceeds the second threshold value.

3. Method of sensing a vehicle crash and signaling desired deployment of an occupant restraint, comprising the steps:

an accelerometer for providing an acceleration signal;

detecting the initiation of a possible crash event and initiating a clock count indicating a time progression into the event;

storing a constant second stage threshold value and data defining a first stage threshold that varies as function of the clock count;

only for a time indicated by a predetermined value of the clock count, comparing the velocity value with the second stage threshold and storing a second stage datum if the velocity exceeds the second stage threshold value;

comparing the velocity value with a clock count determined value of the first stage threshold and alternatively;

(1) generating a second stage deploy signal if the velocity value exceeds the value of the first stage threshold and the second stage datum is stored,

(2) generating a first stage deploy signal if the velocity value exceeds the value of the first stage threshold and the second stage datum is not stored, and

(3) generating no deploy signal if the velocity value does not exceed the first stage threshold.

5. An occupant restraint deployment system comprising:

a first crash sensor in a passenger area of the vehicle including an first accelerometer;

a second crash sensor in a front crush zone of the vehicle including a second accelerometer;

means in the second crash sensor responsive to the second accelerometer to provide a restraint deploy signal to the first crash sensor;

means in the first crash sensor for receiving the deploy signal and accepting the deploy signal as valid only if a sampled output of the first accelerometer exceeds a first threshold and a velocity value derived from the sampled output of the first accelerometer exceeds a second threshold.