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Table of Contents
{ Abstract / Résumé }
Chapter 1
Chapter 2
Chapter 3
Chapter 4
5.1
5.2.1 : Introduction
5.2.2 : Experimental Setup
Ph.D.  /  { Web Version }  /  Chapter 5  /  { 5.2 }  /  5.2.3 : Diametric Load of low-birefringent fiber
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Chapter 6
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Chapter 8
Appendix
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5.3
5.2.4 : Diametric Load of Polarization Maintaining Fiber
5.2.5 : Study on the PM fiber strain anisotropy sensitivity
5.2.6 : Conclusions

5.2        Characterization of a Fiber Bragg Grating under Diametric Loading

5.2.3       Diametric Load of low-birefringent fiber

The model used to simulate the response of a FBG written in a low-birefringence fiber is based on the following hypotheses:

-         The applying region of diametric load is longer than the FBG length, then the state of strain can be said Plane-strain (no deformation in the direction of the fiber axis)

-         No shear stress

-         The fiber is mechanically homogeneous, isotropic and the deformations are elastic (linearity between stresses and strains)

-         The core fiber is dielectric, isotropic, homogeneous and non dispersive

From the Bragg wavelength equation, the variation of Bragg wavelength is


       

(5-12)


where

    

lB,i

  :  

Bragg wavelength for the fast and slow axis

    

ni,eff

  :  

Effective refractive index of the fast and slow axis directions

    

ni

  :  

Refractive index of the core fiber in the fast and slow axis directions

    

L

  :  

FBG period


The geometrical variation DL/L , which correspond to the deformation along the Z axis, is zero due to the Plane-strain hypothesis. Then


(5-13)


In the reference where the inverse dielectric permeability tensor e-1 is diagonal :


       

(5-14)


and then


    and   

(5-15)


where

    

e-1ij

  :  

Dielectric permeability tensor

    

ni

  :  

Refractive index of the fast and slow axis directions

    

Pij

  :  

Strain-optic tensor

    

ei

  :  

Strain

    

Sij

  :  

Elasticity tensor (S11=1/E and S12=-n/E)

    

si

  :  

Stress

    

E

  :  

Young Modulus

    

n

  :  

Poisson Ratio


The relative Bragg wavelength sensitivity depends on light polarization and might be different in the x and y direction. Combining the equations above the variation of Bragg wavelength is given by


(5-16)


The relation between si and ei are derived from the general case and the hypothesis of Plain Strain (ez = 0). In the last equation, nx and ny are approximated by n0.

For the diametric load of an optical fiber, the core is small regarding the fiber diameter, therefore the stress should be uniform in the core and equal to the stress at (x,y)=(0,0) (Fig. 5-19) [5-14]:

Fig. 5-19 : Diametric load of optical fiber (Z-direction along the fiber axis)


(5-17)


where

    

d

  :  

Fiber diameter

    

R

  :  

Fiber radius

    

t

  :  

Length of diametric applying region

    

P

  :  

Diametric load in N (P/t is the line load density)


Fig. 5-20 FBG reflectivity under diametric load from 0 N to 155 N.

Fig. 5-20 shows the experimental results for a low-birefringence fiber under diametric load. Each curve represents two measurements for a given load applied on a length of 26 mm. Each spectrum is the superposition of the two independent polarization measurements. There is no initial birefringence. For small diametric load both modes are degenerated. For higher values the two modes are clearly separated. For 155 N the separation is about 0.45nm.

Fig. 5-21 shows the measured and calculated peak reflectivity as a function of applied load for the two polarization modes. The wavelength changes are strongly different for the two modes. Slow and fast axis have sensitivities of 31.0 10-4 and -1.36 10-4 nm/N. A very good agreement between experimental and calculated values is observed.

Fig. 5-21 FBG Bragg wavelength under diametric load; circles or triangles: experimental data; solid line: calculated values.

In Fig. 5-21 the following values have been taken [5-15, 5-16] for the theoretical model:


    

P11

  =  

0.113

    

P12

  =  

0.252

    

E

  =  

64.1 GPa

    

n

  =  

0.16

    

d

  =  

125 mm

    

t

  =  

26mm

    

lB,0

  =  

1526.616 nm

    

n0

  =  

lB,0 / 1058.5 nm = 1.442245




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