Discrete strain sensor

• US 4,947,693 A
• Filed: 07/13/1989
• Issued: 08/14/1990
• Est. Priority Date: 07/28/1987
• Status: Expired due to Term

• Current Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Original Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Inventors: Caserta, Anthony, Szuchy, Nicholas C.
• Primary Examiner(s): Raevis, Robert
• Application Number:
  US07/379,374
• Time in Patent Office: 397 Days
• Field of Search: 73/800, 73/705, 73/655, 250/231 R, 250/231 P, 250/227, 356/32, 356/34, 356/35
• US Class Current: 73/800
• CPC Class Codes: G01L 1/243 using means for applying force perpendicular to the fibre axis
• CPC Class Codes: G01L 1/245 using microbending

Abstract

A fiber optic load sensor and method of forming the same are disclosed for sensing the load applied to a structural surface. The sensor comprises a length of fiber optic material disposed adjacent to the surface. The fiber optic material is connectable to a light source and to a light detector. The fiber optic material includes at least one curved portion deformable in response to the applied load. The curved portion is dimensioned such that the light passing through the fiber optic material is attenuated in linear relation to the deformation of the curved portion in response to the load applied to the surface.

Claims

1. A fiber optic load senosr for sensing a load applied to a corresponding structural surface, comprising a length of fiber optic material of a selected thickness attachable to the surface, said fiber optic material being connectable to a light source and to a light detector, said fiber optic material having curved portions, said curved portions each having a curve length and curve period, said curved portions each being deformable so that the curve radius and curve period are variable in response to the load applied to the surface, said fiber optic material thickness and curve radius being selected such that light passing through said fiber optic material is actuated in linear relation to the instantaneous deformation of the fiber over a substantial range of load applied to the surface.

2. The sensor as recited in claim 1 wherein said fiber optic material includes a plurality of curved portions, each of said curved portions each having substantially the same shape.

3. The sensor as recited in claim 1 wherein said fiber optic material is formed to have a generally sinusoidal shape.

4. The sensor as recited in claim 1 wherein said curved portions each have a bend radius dimensioned so as to attenuate light passing therethrough in linear relation to deformation of said curved portions in response to the load applied to the surface.

5. The sensor as recited in claim 1 wherein said fiber optic material is approximately 400 microns thick.

6. The sensor as recited in claim 1 wherein said fiber optic material is approximately 600 microns thick.

7. The sensor as recited in claim 1 wherein said fiber optic material is approximately 1000 microns thick.

8. The sensor as recited in claim 1 wherein said sensor is disposed in load transfer relation with the surface where the load is to be measured.

9. The sensor as recited in claim 8 wherein said fiber optic material is embedded in the surface where the load is to be measured.

10. The sensor as recited in claim 8 wherein said fiber optic material is disposed upon the surface where the load is to be measured.

11. The sensor as recited in claim 1 wherein said fiber optic material has a uniform refractive index.

12. The sensor as recited in claim 1 wherein said curved portions each provide static attenuation of light passing therethrough, said curved portions also providing variable dynamic attenuation of light passing therethrough, said dynamic attenuation being linearly related to the deformation of said curved portions in response to the load applied to the surface.

13. The sensor as recited in claim 1 wherein light passing through said curved portions is attenuated in linear relation to the load applied to the surface.

14. The sensor as recited in claim 1 wherein said fiber optic material is connected to a steady state light source.

15. The sensor as recited in claim 1 wherein said fiber optic material is connected to a pulsed light source.

16. A fiber optic load sensor for sensing the load applied to a structural surface, comprising a length of fiber optic material attachable to the surface, said fiber optic material being connectable to a light source and to a light detector for detecting the light from the light source passing through the length of fiber optic material, said fiber optic material being formed to have a thickness and shaped as a repeating generally sinusoidal pattern permanently formed therein, said sinusoidal pattern having a curve radius and a curve period, said curve radius and said curve period being variable in response to the applied load, said fiber optic material further being formed to have a core formed of the first material and a cladding, interfacing said core and formed of a second material, said first material, second material, fiber optic material thickness and curve radius being selected such that light passing through said length of fiber optic material is attenuated in linear relationship to changes in the load applied to the fiber optic material over a substantial range of applied load.

17. The sensor as recited in claim 16 wherein the first material has a first index of refraction an said second material has a second index of refraction, and said curve radius being formed such that light transmitted from said core to said cladding varies linearly in response to changes in the curve radius.

18. The method of measuring the load applied to a length of fiber optic material comprising:

forming a length of fiber optic material of a selected thickness to have a core formed of a first material and a cladding formed of a second material, said core and said cladding forming an interface therebetween;

bending the length of fiber optic material to form a repeating generally sinusoidal pattern, said sinusoidal pattern having e curve radius and a curve period, said curve radius and curve period being variable in response to a load applied to the fiber optic material, the thickness and curve radius being selected such that the amount of light transmitted from the core to the cladding varies linearly in response to a load applied to the fiber optic material over a substantial load range.

19. The method as recited in claim 18 further comprising the step of monitoring a single mode of the ray paths of light passing through the length of fiber optic material.