Compact multicore fiberoptic device for sensing components of force

• US 10,234,344 B2
• Filed: 02/03/2017
• Issued: 03/19/2019
• Est. Priority Date: 02/04/2016
• Status: Active Grant

• Current Assignee: OFS Fitel LLC (Furukawa Electric Company Limited)
• Original Assignee: OFS Fitel LLC (Furukawa Electric Company Limited)
• Inventors: Abedin, Kazi S
• Primary Examiner(s): Sohn, Seung C
• Application Number:
  US15/424,204
• Publication Number:
  US 20170227410A1
• Time in Patent Office: 774 Days
• Field of Search: 25022714
• CPC Class Codes: G01L 1/242 the material being an optical fibre
• CPC Class Codes: G01L 5/166 using photoelectric means
• CPC Class Codes: G02B 6/02042 Multicore optical fibres
• CPC Class Codes: G02B 6/32 having lens focusing means positioned between opposed fibre ends with lens being an integral part of the single fibre end G02B6/262

Abstract

A multi-axis force sensor is compact in that it comprises a single strand of optical fiber and a single, movable reflecting element having a reflecting surface separated from a fiber end-face by a gap, and yet is capable of measuring axially and/or laterally applied forces with high sensitivity. The force to be measured causes the reflecting surface to tilt, translate or deform. The single strand of fiber is configured to have multiple cores that carry multiple optical interrogation signals through an end-face of the fiber to incidence on the reflecting surface. The cores are configured so that the propagation vectors of the interrogation signals, as the signals emanate from the fiber end-face, make non-perpendicular angles with that end-face. Furthermore, the cores are configured to capture a portion of the interrogation signals back-reflected from the reflecting surface. The amount of power coupled back into each core is a function of the position of the reflecting surface, which in turn is a function of the magnitude and direction of the applied force. A deformable casing to which the force is applied may surround the reflecting element, the gap and the fiber end-face.

Claims

1. A fiberoptic device for sensing axial and/or lateral components of force comprising:

a movable reflecting surface onto which interrogation light beams are directed, wherein a position of said movable reflecting surface is responsive to at least one of said axial and lateral components of said force; and

an end-face spaced apart from said movable reflecting surface so as to form a gap therebetween; and

an optical fiber having a longitudinal axis and having a multiplicity of core regions for directing a multiplicity of said interrogation light beams, either serially or simultaneously, onto different locations of said movable reflecting surface;

said interrogation beams being directed toward said movable reflecting surface such that at least two of said interrogation beams are incident on said movable reflector reflecting surface from different directions from one another, portions of each of said interrogation beams being back-reflected from said movable reflecting surface into the same core region from which said portion emanated, and

said back-reflected portions being related to at least one of said components of said force.

2. The device of claim 1, further including:

a deformable casing surrounding said movable reflecting surface, said optical gap and said end-face, said force being applied to said deformable casing so as to deform said casing and cause said movable reflecting surface to move.

3. The device of claim 1, wherein said end-face is one of an end-face of said optical fiber and an end-face of a graded index (GRIN) lens.

4. The device of claim 3, wherein said GRIN lens has an index gradient constant (g) and has a length that is an odd multiple of ¼

pitch, where pitch=2π

/g.

5. The device of claim 1, further including a GRIN lens, wherein said interrogation beams are directed toward said movable reflecting surface via said GRIN lens so that said interrogation beams have propagation vectors with directions different from one another at said movable reflecting surface.

6. The device of claim 1, wherein at least one of said core regions is located peripherally and is twisted around said longitudinal axis so that said interrogation beams have propagation vectors with directions different from one another at said end-face.

7. The device of claim 1, wherein at least two of said core regions intersect said end-face in positions symmetrically located around said longitudinal axis and peripherally located around said end-face.

8. The device of claim 1, wherein said multiplicity of core regions includes a central core region positioned along said longitudinal axis, said central core region configured to direct a reference light beam through said end-face to said movable reflecting surface.

9. The device of claim 1, wherein said gap is filled with a material that is deformable in response to the application of at least one of said force components and is transparent to said optical interrogation beams.

10. The device of claim 1, further including an anti-reflection coating disposed on said end-face, said gap being formed between said coating and said movable reflecting surface.

11. The device of claim 1, wherein said deformable casing comprises a substance selected from a group consisting of metals, metal alloys, and polymers.

12. A force measurement system comprising a fiberoptic device for sensing said axial and lateral components of said force according to claim 1,

a light source for generating said interrogation light beams,

a photo detector for detecting said back-reflected light,

a coupling and routing device for coupling said interrogation light beams to selected core regions of said optical fiber and for coupling said back-reflected light to said photo detector, and

a computer responsive to said photo detector for calculating a magnitude and direction of at least one of said components of said force.

13. The system of claim 12 configured to couple said interrogation light beams to said selected core regions serially, one at a time.

14. The system of claim 12 configured to couple said interrogation light beams to all of said selected core regions simultaneously.

15. A fiberoptic device for sensing axial and lateral components of force comprising:

a light guiding optical element for carrying a multiplicity of interrogation optical signals and for emitting from an end-face said interrogation optical signals with propagation vectors having directions different from one another; and

a reflecting surface spaced apart from said end-face, each of said interrogation optical signals emitting from said end-face being directed to said reflecting surface,

wherein portions of each of said interrogation optical signals are back-reflected from said reflecting surface into said light guiding optical element,

wherein said back-reflected portions are related to a position of said reflecting surface with respect to said light guiding optical element.

16. The device of claim 15 further including a casing that encapsulates and holds in place said light guiding optical element and said reflecting surface.

17. The device of claim 16, wherein said position of said reflecting surface with respect to said light guiding optical element is responsive to said lateral and axial components of said force applied to said reflecting surface through said casing.

18. The device of claim 15, wherein said light guiding optical element is an optical fiber having a multiplicity of cores, one of which being a peripheral core twisted around a longitudinal axis of said optical fiber.

19. The device of claim 15, wherein said light guiding element includes an optical fiber having multiple a multiplicity of cores and a graded index (GRIN) lens attached at an end of said optical fiber.

20. The device of claim 19, wherein one of said multiplicity of cores is located at the center of said optical fiber and runs parallel to said longitudinal axis.