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FIBEROPTIC SENSOR TECHNOLOGY HANDBOOK

FIBEROPTIC SENSOR TECHNOLOGY HANDBOOK

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Fig. 5.35<br />

SIGNAL<br />

ELECTRICAL<br />

REBALANCE<br />

UPPER<br />

~1 lppoRT<br />

IER<br />

MASS<br />

DIODE<br />

LASER<br />

3dB COUPLER<br />

iii=<br />

CASE<br />

DIAPHRAGMS<br />

LOWER SUPPORT<br />

lkFIBER<br />

)1‘t’ /u<br />

m1<br />

s<br />

3dB COUPLER<br />

PHOTODIODES<br />

A two-fiber phase-change interferometric<br />

fiberoptic accelerometer.<br />

where A is the cross sectional area of the fiber, AT is<br />

the magnitude of the change of the tensile stress in<br />

each fiber, and the 2 is due to the presence of two fibers.<br />

The resulting strain AS = .4L/L is given by:<br />

AS = AT/Y = ma/2YA (5.20)<br />

attached to a spring with a spring constant k, the resonant<br />

frequency is given by:<br />

combining Eqs. (5.26) and (5.27) there is obtain-<br />

Thus,<br />

ed:<br />

fr = (1/2n)(k/m)112. (5.27)<br />

fr = (1/2n)(2YA/Lm)l/2 (5.28)<br />

As above, A = m(d/2)2. To further emphasize the dependence<br />

of the resonant frequency, fr, on the fiber parameters,<br />

Eq. (5.28) may be written as:<br />

fr = [Yd2/8mLm]1/2 (5.29)<br />

Comparing Eqs. (5.25) and (5.29) we see that the optical<br />

fiber physical parameters appear in the form Yd2/<br />

Lm. Therefore, if the expression d2/Lm in Eq. (5.25)<br />

is decreased in order to decrease ~in, the value<br />

of fr given by Eq. (5.28) is also decreased. The minimum<br />

detectable acceleration (a~n) and longitudinal<br />

resonant frequency are shown in Figs. 5.36 and 5.37 as<br />

functions of m and d. In each case the length of fibe<br />

L is taken to be one cm and the value of A is 10 -5<br />

radian. Alternately, if a mass of one gram % ~ chosen,<br />

the mass in grams on the abscissa in both Figs. 5.36<br />

and 5.37 can be replaced by the length in centimeters.<br />

3.0 t.<br />

where Y is Young’s modulus for the fiber.<br />

Consider next an optical beam propagating in<br />

one of*the fibers. Its phase shift, $ , in traveling<br />

the length L, as given in Subsection 4.2.1 and Eqs.<br />

(4.7) and (4.8), is:<br />

4 = zn~~l~o (5.21)<br />

where h. is the optical wavelength in vacuum and n is<br />

the fiber core’s refractive index. The’ quantity Aoln<br />

is the wavelength of the light in the fiber core. In<br />

general, the change in @ per fiber (twice this for two<br />

fibers) may be written as it was in Eq. (5.1), namely:<br />

A+ = 2m(nAL + LAn)/Ao (5.22)<br />

with the wave number k = 2iI/lo. For the case of a tensile<br />

strain, however, the AL term dominates and one may<br />

write:<br />

A+ = 2nnAL/~o = 2nnLAS/lo (5.23)<br />

Fig. 5.36<br />

10.0<br />

10 2.0 3.0<br />

MASS (grams)<br />

The variation of sensitivity in micrograms<br />

as a function of the mass in grams in a<br />

fiberoptic accelerometer for different<br />

sizes of fibers.<br />

Substituting into Eq. (5.23) from Eq. (5.20) and because<br />

A - n(d/2)2:<br />

A~ = 4nLma/Y~d2 (5.24)<br />

where d is the fiber diameter.<br />

- h<br />

-$<br />

d<br />

m -1-<br />

Solving Eq. (5.24) for ~n in terms of A$~n yields:<br />

amin = AoYd2A$tin/4nLm (5.25)<br />

Referring to Fig. 5.35, the effective spring<br />

force F, required to displace the mass m a distance z,<br />

along the axis of the fiber, is given by:<br />

F = -2YAz/L = -kz (5.26)<br />

from which it follows that 2YA/L = k, where k is the<br />

effective spring constant. However, when a mass m is<br />

.--— ------.-----<br />

I 1 1 1<br />

10 2.0 3.0<br />

MASS(grams)<br />

Fig. 5.37 The variation of resonant frequency as a<br />

function of the mass in a fiberoptic accelerometer<br />

for different sizes of fibers.<br />

5-13

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