System and method for sensing loads

• US 8,209,092 B2
• Filed: 03/23/2007
• Issued: 06/26/2012
• Est. Priority Date: 03/23/2007
• Status: Expired due to Fees

• Current Assignee: Patricia Wiener
• Original Assignee: Patricia Wiener
• Inventors: Wiener, Patricia
• Primary Examiner(s): Nguyen, Kim T
• Application Number:
  US11/726,767
• Publication Number:
  US 20080234898A1
• Time in Patent Office: 1,922 Days
• Field of Search: 701/45, 340665-668, 180/271, 180/273
• US Class Current: 701/45
• CPC Class Codes: B60R 21/01534 using electromagneticwaves, e.g. infrared
• 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
• CPC Class Codes: G01G 3/125 wherein the weighing element is an optical member
• CPC Class Codes: G01L 1/243 using means for applying force perpendicular to the fibre axis

Abstract

An optical sensing system detects pressure through attenuation of light in an optical fiber. The weight and position of a load on a mat including multiple optical fibers may be determined; for example, such a mat may be used in an automobile seat to determine theses parameters for a passenger in the seat. This information can be presented to an airbag deployment system to easily enable the airbag to be deployed or suppressed in a manner sensitive to the weight and position of the occupant. This methodology allows loads, load movement, and load position to be detected in vehicles. In applications for vehicles such as aircraft or boats, sensing weight, position and movement of cargo can warn an operator or pilot in sufficient time to correct dangerous shifts in weight within the cargo portion of the vehicle or to modify the operation of the vehicle to compensate for such shifts.

Claims

1. An optical sensing system for detecting pressure exerted by a mass through attenuation of light in an optical fiber comprising:

a first plurality of optical fibers;

a second plurality of optical fibers that is approximately parallel to the first plurality of optical fibers;

a support element against which the first and second plurality of optical fibers can move, such that a bend is created in at least one of the optical fibers in either the first or second plurality of optical fibers as a result of the pressure exerted by an object pressing against one or more of the fibers;

a first light source for sending light beams through the first plurality of optical fibers;

a second light source for sending light beams through the second plurality of optical fibers;

a first detector for measuring any attenuation in the light beams sent through at the first plurality of optical fibers; and

a second detector for measuring any attenuation in the light beams sent through the second plurality of optical fibers;

such that at least one of the first detector and the second detector measure attenuation in the at least one of the optical fibers in which a bend is created.

2. The optical sensing system of claim 1, wherein the pressure results from the weight of the mass, and further comprising:

a processor configured to derive the weight of the mass from the attenuation of the light beam in each of the at least one of the optical fibers in which a bend is created.

3. The optical sensing system of claim 2, further comprising a seat for containing the first plurality of optical fibers, the second plurality of optical fibers and the support element.

4. The optical sensing system of claim 3 wherein the seat is an automobile seat.

5. The optical sensing system of claim 2, further comprising a memory for storing information about the derived weight at a first time and at a second time.

6. The optical sensing system of claim 2, further comprising means for providing the derived weight to an airbag deployment system.

7. The optical sensing system of claim 2, wherein the processor is further configured to derive a position of the mass with respect to the support element from the attenuation of the light beam in the at least one optical fiber.

8. The optical sensing system of claim 7, further comprising means for providing the derived position to an airbag deployment system.

9. The optical sensing system of claim 2, further comprising means for setting a reference weight value.

10. The optical sensing system of claim 2, further comprising means for differentiating whether the mass has a fixed or dynamic weight.

11. A method for measuring the weight of a mass resting on an object, comprising:

providing in the object a first plurality of optical fibers and a second plurality of optical fibers which is approximately parallel to the first plurality of optical fibers such that a change in pressure on the object causes deformation of one or more of the optical fibers in either the first or second plurality of optical fibers;

providing a first light source for sending a first light beam through the first plurality of optical fibers and a second light source for sending a second light beam through the second plurality optical fibers;

measuring any attenuation of the light beam in the first plurality of optical fibers with a first detector and any attenuation of the light beam in the second plurality of optical fibers with a second detector such that the attenuation of light in the one or more deformed optical fibers is measured by at least one of the first detector and the second detector; and

deriving the weight of the mass located on the object from the attenuation of the light in the one or more deformed optical fibers.

12. The method of claim 11 further comprising deriving the position of the mass on the object from the attenuation of the light in the one or more deformed optical fibers.

13. The method of claim 12 further comprising providing the derived weight and position of the mass on the object to an airbag deployment system.

14. The method of claim 13 wherein the airbag deploys at a certain rate and to a certain extent, and further comprising controlling the rate and extent of deployment of the airbag based at least in part upon the derived weight and position.

15. The method of claim 13 wherein the object is an automobile seat.

16. The method of claim 15 further comprising detecting whether a seatbelt is in use on the automobile seat, and wherein controlling the rate and extent of deployment of the airbag is based at least in part upon whether the seatbelt is in use.

17. The method of claim 15 further comprising providing the derived weight and position of the mass on the automobile seat to a front airbag deployment mechanism.

18. The method of claim 15 further comprising providing the derived weight and position of the mass on the automobile seat to a side airbag deployment mechanism.

19. The method of claim 13 further comprising establishing thresholds for the airbag deployment system at which the airbag will deploy based at least in part upon the derived weight and position.

20. The method of claim 19 wherein the object is an automobile seat.

21. The method of claim 20 further comprising detecting whether a seatbelt is in use on the automobile seat, and wherein establishing thresholds is based at least in part upon whether the seatbelt is in use.

22. The method of claim 21 further comprising detecting the position of the automobile seat relative to the front of the automobile, and wherein establishing thresholds and controlling the rate and extent of deployment of the airbag are each based at least in part upon the detected position of the automobile seat.

23. The method of claim 12 wherein the weight of the mass is derived at a time close to the time when the position of the mass is derived.

24. The method of claim 23 further comprising providing the derived weight and position to an airbag deployment system.

25. The method of claim 23 wherein deriving the weight and position of the mass is completed in less than approximately 1 millisecond.

26. The method of claim 11 further comprising deriving the weight of the mass at a first time and at a second time.

27. The method of claim 26 further comprising deriving the difference in the mass between the first time and the second time.

28. The method of claim 26, wherein the first time is a time in which there is no mass located on the object.