Method and apparatus for sensing seat occupant weight

• US 6,557,424 B1
• Filed: 02/15/2000
• Issued: 05/06/2003
• Est. Priority Date: 02/24/1999
• Status: Expired due to Fees

• Current Assignee: Siemens VDO Automotive Corporation (Siemens AG)
• Original Assignee: Siemens VDO Automotive Corporation (Siemens AG)
• Inventors: Morell, Scott M.
• Primary Examiner(s): NOLAND, THOMAS
• Application Number:
  US09/503,826
• Time in Patent Office: 1,176 Days
• Field of Search: 738/620.45, 738/625.43, 738/625.41, 73/11.3, 702/101, 701/36, 280/735, 280/734, 280/730.1
• US Class Current: 73/862.045
• CPC Class Codes: B60R 21/01516 using force or pressure sensing means
• CPC Class Codes: B60R 21/0152 using strain gauges
• CPC Class Codes: G01G 19/4142 for controlling activation of safety devices, e.g. airbag systems electrical circuits for triggering safety arrangements in case of vehicle accidents B60R21/015

Abstract

A system for measuring the weight of a seat occupant is used to control airbag deployment. The system includes a seat bottom that receives a vertical seat occupant weight force. The seat is divided into four quadrants, a front right quadrant, a left front quadrant, a left rear quadrant, and a right rear quadrant. Each quadrant includes a sensor that generates a weight signal corresponding in magnitude to the seat occupant weight in the respective quadrant. Each weight signal is comprised of a vertical force component and an error component induced by braking or deceleration forces acting on the seat bottom in a non-vertical direction. The sensors are orientated within their respective quadrants such that two sensors generate a positive error reading and two sensors generate a negative error reading. When the weight signals from each quadrant are added together to determine the total seat occupant weight, the error is eliminated as the positive and negative error components cancel each other out. The seat occupant weight is determined by adding the vertical force components from each of the weight signals together.

Claims

1. A method for determining the weight of a seat occupant comprising the steps of:

(a) providing a vertical occupant force against a seat bottom;

(b) generating a first weight signal having a first vertical force component and a positive error component induced by application of a non-vertical force to the seat bottom;

(c) generating a second weight signal having a second vertical force component and a negative error component induced by the non-vertical force;

(d) combining the first and second weight signals;

(e) canceling error induced by the non-vertical force by adding the positive and negative error components; and

(f) adding the first and second vertical force components to determine seat occupant weight.

2. The method according to claim 1 wherein the seat bottom includes at least a first seat portion and a second seat portion with step (b) further defined as generating the first weight signal to correspond to a portion of seat occupant weight on the first seat portion and with step (c) further defined as generating the second weight signal to correspond to a portion of seat occupant weight on the second seat portion.

3. The method according to claim 2 wherein step (b) further includes providing a first sensor mounted within the first seat portion for generating the first weight signal and step (c) further includes providing a second sensor mounted within the second seat portion for generating the second weight signal.

4. The method according to claim 3 wherein step (b) further includes providing the first sensor with a first strain gage having a first orientation within the first sensor to produce a positive error in response to application of the non-vertical force to the seat bottom and step (c) further includes providing the second sensor with a second strain gage having a second orientation, opposite from the first orientation, within the second sensor to produce a negative error in response to application of the non-vertical force to the seat bottom.

5. The method according to claim 1 including the steps of generating a third weight signal having a third vertical force component and a positive error component induced by the non-vertical force and generating a fourth weight signal having a fourth vertical force component and a negative error component induced by the non-vertical force prior to step (d) and wherein step (d) further includes combining the first, second , third, and fourth weight signals and wherein step (f) further includes adding the first, second, third, and fourth vertical force components to determine seat occupant weight.

6. The method according to claim 5 wherein the seat bottom includes at least a first quadrant, a second quadrant, a third quadrant, and a fourth quadrant and including the steps of generating the first weight signal to correspond to a portion of seat occupant weight on the first quadrant in step (b), generating the second weight signal to correspond to a portion of seat occupant weight on the second quadrant in step (c), generating the third weight signal to correspond to a portion of seat occupant weight on the third quadrant, and generating the fourth weight signal to correspond to a portion of seat occupant weight on the fourth quadrant.

7. The method according to claim 6 including the steps of providing a first sensor mounted within the first quadrant for generating the first weight signal during step (b), providing a second sensor mounted within the second quadrant for generating the second weight signal during step (c), providing a third sensor mounted within the third quadrant for generating the third weight signal, and providing a fourth sensor mounted within the fourth quadrant for generating the fourth weight signal.

8. The method according to claim 7 including the steps of providing the first sensor with a first strain gage having a first orientation within the first sensor to produce a positive error in response to application of the non-vertical force to the seat bottom, providing the second sensor with a second strain gage having a second orientation, opposite from the first orientation, within the second sensor to produce a negative error in response to application of the non-vertical force to the seat bottom, providing the third sensor with a third strain gage having the first orientation within the third sensor to produce a positive error in response to application of the non-vertical force to the seat bottom, and providing the fourth sensor with a fourth strain gage having the second orientation within the fourth sensor to produce a negative error in response to application of the non-vertical force to the seat bottom.

9. The method according to claim 8 wherein the first quadrant is defined as a right front quadrant, the second quadrant is defined as a left front quadrant, the third quadrant is defined as a left rear quadrant, and the fourth quadrant is defined as a right rear quadrant and further including the steps of combining the first and second weight signals, canceling error induced by the non-vertical force by adding the positive and negative error components, adding the first and second vertical force components to determine seat occupant weight on a front portion of the seat bottom and dividing the sum of the first and second vertical force components by the sum of the first, second, third, and fourth vertical force components to determine seat occupant weight distribution for front to rear.

10. The method according to claim 8 wherein the first quadrant is defined as a right front quadrant, the second quadrant is defined as a left front quadrant, the third quadrant is defined as a left rear quadrant, and the fourth quadrant is defined as a right rear quadrant and further including the steps of combining the first and fourth weight signals, canceling error induced by the non-vertical force by adding the positive and negative error components, adding the first and fourth vertical force components to determine seat occupant weight on a right side portion of the seat bottom and dividing the sum of the first and fourth vertical force components by the sum of the first, second, third, and fourth vertical force components to determine seat occupant weight distribution for right to left.

11. A method according to claim 1 including the steps of providing a system controller for controlling deployment of an airbag;

generating a seat occupant weight signal based on the addition of the first and second vertical force components;

transmitting the seat occupant weight signal to the controller; and

controlling a deployment force of the airbag based on the seat occupant weight.

12. The method according to claim 1 including the step of generating the first and second signals from independent sensor locations within the seat bottom.

13. A system for measuring the weight of a seat occupant comprising:

a seat bottom for receiving a substantially vertical seat occupant weight force;

at least one pair of sensors including a first sensor mounted within a first portion of said seat bottom for generating a first weight signal comprised of a first vertical force component and a positive error component induced by application of non-vertical seat forces to said seat bottom and a second sensor mounted within a second portion of said seat bottom for generating a second weight signal comprised of a second vertical force component and a negative error component induced by application said non-vertical seat forces; and

a processor for determining seat occupant weight based on said first and second weight signals wherein seat occupant weight is determined by summation of said first and second vertical force components and error induced by said non-vertical seat forces is eliminated by adding said positive and negative error components.

14. A system according to claim 13 wherein said first sensor includes a first strain gage having a first orientation for generating a positive error in response to application of said non-vertical force to said seat bottom and said second sensor includes a second strain gage having a second orientation, opposite from said first orientation, for generating a negative error in response to application of said non-vertical force to said seat bottom.

15. A system according to claim 13 wherein said at least one pair of sensors is comprised of a first and second pair of sensors, said first pair of sensors including said first and second sensors and said second pair including a third sensor mounted within a third portion of said seat bottom for generating a third weight signal comprised of a third vertical force component and a positive error component induced by said non-vertical seat forces and a fourth sensor mounted within a fourth portion of said seat bottom for generating a fourth weight signal comprised of a fourth vertical force component and a negative error component induced by application said non-vertical seat forces.

16. A system according to claim 15 wherein said first portion is defined as a right front quadrant, said second portion is defined as a left front quadrant, said third portion is defined as a left rear quadrant, and said fourth portion is defined as a right rear quadrant;

said first weight signal corresponding in magnitude to a portion of seat occupant weight on said right front quadrant, said second weight signal corresponding in magnitude to a portion of seat occupant weight on said left front quadrant, said third weight signal corresponding in magnitude to a portion of seat occupant weight on said left rear quadrant, and said fourth weight signal corresponding in magnitude to a portion of seat occupant weight on said right rear quadrant.

17. A system according to claim 13 including an airbag control module in communication with said processor wherein deployment force of an airbag is controlled by said control module based on seat occupant weight.

18. A system for measuring the weight of a seat occupant comprising:

a seat bottom for receiving a substantially vertical seat occupant weight force and being divided into a first quadrant, a second quadrant, a third quadrant, and a fourth quadrant;

a first sensor mounted within said first quadrant for generating a first weight signal comprised of a first vertical force component and a first error component induced by application of non-vertical seat forces to said seat bottom;

a second sensor mounted within said second quadrant for generating a second weight signal comprised of a second vertical force component and a second error component induced by application said non-vertical seat forces;

a third sensor mounted within said third quadrant for generating a third weight signal comprised of a third vertical force component and a third error component induced by application said non-vertical seat forces;

a fourth sensor mounted within said fourth quadrant for generating a fourth weight signal comprised of a fourth vertical force component and a fourth error component induced by application said non-vertical seat forces;

said first and third sensors being orientated within said first and third quadrants, respectively, such that said first and third error components caused by said non-vertical seat forces are generated as positive errors and said second and fourth sensors being orientated within said second and fourth quadrants, respectively, such that said second and fourth error components caused by said non-vertical seat forces are generated as negative errors; and

a processor for determining seat occupant weight based on said first, second, third, and fourth weight signals wherein error induced by said non-vertical seat forces is eliminated by adding said positive and negative errors.

19. An assembly according to claim 18 wherein said processor determines seat occupant weight is determined by summation of said first, second, third, and fourth vertical force components.

20. An assembly according to claim 19 wherein said processor includes an airbag control module wherein deployment force of an airbag is controlled by said control module based on seat occupant weight.