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FIBEROPTIC SENSOR TECHNOLOGY HANDBOOK

FIBEROPTIC SENSOR TECHNOLOGY HANDBOOK

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The vertical height of the various cross-hatched regions<br />

represent the loss as a function nf the wavelength<br />

arising from the various sources. Note that the<br />

minimum total attenuation at approximately 0.8 micron<br />

wavelength is approximately 10 dB/km. This is a somewhat<br />

mediocre fiber by today’s standards. The lowest<br />

four regions in Fig. 2.17 correspond to the loss due<br />

to 1 part per million by weight, in silicon oxide (Si02)<br />

glass, of the metallic impurities Cu, Ni, Fe, and Cr,<br />

from bottom to top, respectively. The peak in the<br />

vicinity of the 0.95-micron wavelength is due to the<br />

third harmonic of the hydroxyl (OH-) vibrational mode,<br />

and corresponds to roughly a 20-part-per-million impurity<br />

content. The black dots are predicted values of<br />

losses based on calorimetry-type optical absorption<br />

measurements made on the glass sample from which the<br />

fiber was drawn. The upper cross-hatched region represents<br />

the attenuation due to Rayleigh scattering while<br />

the white region is the remaining difference between<br />

the total loss versus wavelength (the uppermost curve)<br />

and the sum of the previously mentioned losses. The<br />

latter is attributed to regular bending and microbending<br />

losses.<br />

The attenuation versus wavelength curve shown<br />

in Fig. 2.18 is for a currently available very-low-<br />

5.0 . ‘.<br />

3.0 — ‘.> ‘.<br />

2.0 —<br />

‘\<br />

1.0<br />

tion. In the bent region, the ray intersects the corecladding<br />

interface at an angle 13 that is greater than<br />

‘dC and thus it will be partially transmitted out of the<br />

core and into the cladding. This will occur at each<br />

successive reflection from the outer interface and large<br />

losses may occur. Another qualitative explanation of<br />

this type of loss is as follows. In the beam propagating<br />

in the fiber, assuming plane wavefronts, if the<br />

velocity at the center of the core in the bent section<br />

were equal to the c/nl, the “proper” velocity in the<br />

core, then the velocity at the outer edge of the front<br />

would have to be higher than c/nl, which cannot occur.<br />

Radiation in the form of core-to-cladding scattering<br />

results. Finally, from the electromagnetic wave theory<br />

it may be shown that in a waveguide with a constant<br />

bend radius, all of the solutions of the wave equation<br />

represent waves that decay with<br />

along the centerline of the core.<br />

increasing distance<br />

6<br />

6< 9.<br />

e’ 70,<br />

\<br />

/<br />

/<br />

/<br />

0.5 -<br />

\<br />

Fig. 2.19 Leakage of optical power froman optical<br />

fiber at a constant-radius bend.<br />

Fig. 2.18<br />

0.6 0.7 0.8 0.9 1.0 1.1 1.2 1.3 1.4 1.5 1.6<br />

WAVELENGTH (pm)’<br />

Attenuation rate of optical power in a low-<br />

10SS optical fiber as a function of wavelength.<br />

The arrows along the abscissa indicate<br />

the wavelengths of commercially<br />

available lasers.<br />

loss, single mode fiber. The arrows along the lower<br />

abscissa correspond to the wavelengths of currently<br />

available lasers. The peak in the loss curve at the<br />

1.4-micron wavelength is due to the OH- radical, which<br />

has been reduced to a relatively low concentration<br />

level. The minimum at approximately the 1.3 micron<br />

wavelength is of special interest, not only because the<br />

attenuation rate is down to 0.5 dB/km, but also because<br />

this wavelength is very close to the zero-dispersion<br />

wavelength of Si02 which is of special interest in some<br />

applications, as will be discussed shortly. Fig. 2.18<br />

shows that extremely low attenuation rates attainable<br />

with current fiber fabrication techniques at wave -<br />

lengths where high intensity long-life, solid state<br />

laser sources are becoming commercially available. It<br />

is now up to the fiber user to devise techniques and<br />

configurations that can maintain this low loss by not<br />

introducing significant regular (macro) bending and<br />

microbending losses.<br />

Using the latter approach it is possible to<br />

compute the expected loss due to a constant bend radius.<br />

The results of such calculations are shown in Fig. 2.20,<br />

where loss curves versus bend radius are shown for<br />

singlemode fibers at the 0.83-micron wavelength having<br />

different numerical aperture (N.A.). Note the strong<br />

dependence on bend radius and N.A. Referring to Fig.<br />

2.20, consider a fiber with a numerical aperture of<br />

0.1. When a 10-meter length is wound on a l.2-cmradius<br />

mandrel, the attenuation due to bending is approximately<br />

6 dB, i.e., 75 percent of the light energy<br />

injected into the core at the input end is scattered<br />

out of the core while propagating in the ten meters<br />

to the output end. Nhen 10 meters of identical fiber<br />

are wound on a 1.0 cm radius mandrel, the attenuation<br />

due to bending will increase by a factor of about<br />

250,000 to 60 dB, so that only about one millionth of<br />

the original light remains at the end of the fiber.<br />

Just about all of the input light is scattered out of<br />

the core. On the other hand, using the 1.2 cm radius<br />

mandrel and increasing the numerical aperture (N.A.)<br />

to 0.12 reduces these attenuations to 0.16 dB and 1.6<br />

dB, respectively. Therefore, care must be taken in<br />

designing fiberoptic sensors that require bending and<br />

winding of fibers and in specifying fibers for such<br />

applications.<br />

A ray picture of the regular (constant) bend<br />

radius loss mechanfsm is shown in Fig. 2.19. Assume a<br />

ray is traveling to the right at an angle of o less<br />

than the critical angle ec in the straight fiber sec - 2-9

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