FIBEROPTIC SENSOR TECHNOLOGY HANDBOOK
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