Fiber optic self-multiplexing amplified ring transducer and force transfer sensor with pressure compensation

• US 5,637,865 A
• Filed: 06/11/1996
• Issued: 06/10/1997
• Est. Priority Date: 10/31/1994
• Status: Expired due to Fees

• Current Assignee: the united states of america as represented by the secretary of the navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Tang, Po-Yun, Bullat, David M.
• Primary Examiner(s): Le, Que
• Application Number:
  US08/668,620
• Time in Patent Office: 364 Days
• Field of Search: 250/227.14, 250/227.16, 250/227.17, 250/231.19, 250/227.24, 385/13, 385/75, 73/650, 73/862.29, 73/862.3, 73/862.31, 340/556, 340/566
• US Class Current: 250/227.14
• CPC Class Codes: G01D 5/35335 Aspects of emitters or receivers used by an interferometer in an optical fibre sensor arrangement using multiple sensor devices using multiplexing techniques G01D5/35383
• CPC Class Codes: G01D 5/35348 using stimulated emission to detect the measured quantity
• CPC Class Codes: G01L 1/243 using means for applying force perpendicular to the fibre axis
• CPC Class Codes: G01L 1/247 using distributed sensing elements, e.g. microcapsules along a single optical fibre G01L1/242

Abstract

A fiber optic sensor is also disclosed for measuring or detecting the prece of an environmental field condition such as under-water acoustic perturbations. The sensor includes a force transfer transducer, which is enclosed within a shell, with a pressure equalizer for equalizing the interior and exterior shell pressures. An optical fiber is coiled about the transducer. An optical detector detects stress or strain in the optical fiber, resulting from external perturbations. The sensor is able to operate at various depths or altitudes. Pressure equalization enables the isolation of dynamic external perturbations from other pressure variations. For this purpose, a pressure equalizing valve may be used to allow the equalization of slow changes in static pressures, and the detection of higher frequency perturbations which might emanate from a target source.

Claims

1. A sensor comprising:

a force transfer transducer;

an optical fiber fixed to said force transfer transducer;

a detector operably coupled to said fiber for detecting strain induced in said optical fiber by said transducer;

a shell containing said transducer; and

a pressure equalizer for substantially equalizing pressure within said shell with respect to pressure outside said shell.

2. The sensor of claim 1 wherein said equalizer allows said detector to respond only to forces having a rate of change beyond a threshold level.

3. The sensor of claim 2 wherein said rate is a rate above a threshold level.

4. The sensor of claim 1 wherein said transducer transforms said forces into said strain on said optical fiber.

5. The sensor of claim 1 wherein said transducer is a force transfer column.

6. The sensor of claim 1 wherein said transducer is comprised of elastomeric material.

7. The sensor of claim 1 wherein said transducer converts acoustic energy to radial displacement of said transducer.

8. The sensor of claim 1 wherein said optical fiber is coiled about said transducer at least one time.

9. The sensor of claim 1 wherein said optical fiber is fixed to said transducer at first and second locations.

10. The sensor of claim 1 wherein said optical fiber is continuously bonded to said transducer throughout its length.

11. The sensor of claim 1 wherein said detector includes:

a light source that is optically connected to one terminal end of said optical fiber for injecting an optical signal therein; and

a photodetector optically connected to another terminal end of said optical fiber; and

wherein

said detector measures strain in said optical fiber caused by acoustic perturbations outside said shell and correlates said strain to the intensity of said perturbations.

12. The sensor of claim 1 wherein:

said force transfer transducer includes a force transfer column comprised of a generally cylindrical hollow mandrel formed of resilient material responsive to force from acoustic perturbations outside said shell.

13. The sensor of claim 12 wherein said mandrel is made of a flexible polyurethane elastomer that transfers compressive forces acting on said force transfer column into tensile forces acting on said optical fiber.

14. The sensor of claim 11 wherein said optical fiber includes a length of single monomode fiber.

15. The sensor of claim 11 wherein said shell includes a generally hollow structure formed of compliant material for transferring force from said perturbations to said transducer.

16. The sensor of claim 11 wherein said pressure equalizer includes at least one dash pot damper valve.

17. The sensor of claim 11 wherein said transducer includes a collar disposed between said force transfer column and said optical fiber.

18. The sensor of claim 17 wherein said collar comprises a split cylindrical shell fitted around a portion of said force transfer column and maintains uniformity in the transfer of force from said force transfer column to said optical fiber.

19. The sensor of claim 11 wherein said light source comprises a laser.

20. The sensor of claim 1 wherein a stress σ

applied to said force transfer transducer induces an axial strain ε

_f in said optical fiber; and

wherein said axial strain ε

_f is expressed by the following equation;

space="preserve" listing-type="equation">ε

.sub.f =-[1/(1+α

)].(ν

.σ

/E),

where ν and

E represent the Poisson'"'"'s ratio and the Young'"'"'s modulus of said force transfer transducer, respectively, and α

is a correction factor.

21. The sensor of claim 20 wherein said correction factor α

is expressed by the following equation;

space="preserve" listing-type="equation">α

=(1-ν

).(E.sub.f. t.sub.c)/[E. (A/π

) .sup.1/2 ],

where E_f and t_c represent the Poisson'"'"'s ratio and the effective thickness of said optical fiber, respectively, and A is the cross-sectional area of said force transfer transducer.

22. The sensor of claim 21 wherein said force transfer transducer is cylindrically shaped with a circular cross section having a radius R, wherein said optical fiber is coiled about said transducer n times, and wherein said correction factor α

is expressed by the following equations;

space="preserve" listing-type="equation">α

=(1-ν

).(E.sub.f. t.sub.c)/(E.R)

and

space="preserve" listing-type="equation">t.sub.c =(n-1)A.sub.f /h (n≧

100)

where A_f is the cross sectional area of said optical fiber, and h is the height of said collar.

23. The sensor of claim 21 wherein a load transfer f is effected between said force transfer transducer and said optical fiber;

and

wherein said load transfer f is expressed by the following equation;

space="preserve" listing-type="equation">f=-(ν

.E.sub.f.A.sub.f.F)/[(1+α

).E.A],

where F is a compressive force applied to said force transfer column.

24. The sensor of claim 20 wherein said axial strain ε

_f can be measured by means of the phase shift Δ

Θ

of a signal transmitted through said optical fiber and the following equation;

space="preserve" listing-type="equation">ε

.sub.f =[(1/L) (Δ

L/Δ

τ

)[Δ

θ

/360°

f.'"'"'],

where L is the length of said optical fiber, Δ

L is the change in the length of said optical fiber, Δ

τ

is a time increment, and f'"'"' is the frequency of said signal.

25. The sensor of claim 23 wherein a fixation collar having a height h is interposed between said force transfer transducer and said optical fiber;

wherein said force transfer transducer is cylindrically shaped and has a radius R; and

wherein said axial strain ε

_f is determined by the following equation

space="preserve" listing-type="equation">ε

.sub.f =(-F.ν

)/{π

R[RE+[(n-1).A.sub.f.E.sub.f.(1-ν

)/(h]]}.