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INTRODUCTION TO OPTICAL FIBRE COMMUNICATIONS(Fibre Structure and Wavelength Fundamentals)
1.0 Introduction
An optical telegraph was built by Claude Chappe in 1790s in France. In 1870, John
Tyndall demonstrated the principle of guiding light through internal reflections. In 1880,
Alexander Graham Bell invented the photophone, which used unguided light to carry speech.
A major breakthrough leading to high capacity optical communications was achieved
with the invention of laser in 1960. The laser acted as a narrowband source of optical radiation
suitable for use as a carrier of information. In 1966, Charles K. Kao at Standard
Telecommunications Laboratories, England fabricated a low loss glass fibre, giving a loss of
1000 dB/km or so. Such a fibre could transmit light for a short distance only. But Kao suggested
that purer glass materials would permit the use of fibre for longer transmission lengths. Kao had
shown that it would be possible to transmit light signals over long distance using glass fibre and
modulated infrared light. In 1970 Corning glass works, U.S.A. developed a low loss fibre giving
a loss of 20dB/Km. This was the second major breakthrough to make optical communication a
practical reality. By 1972, losses were reduced to 4dB/km. Today, the best fibres have a loss of
< 0.2 dB/km.
The information travels from the transmitter to the receiver over the information channel.
There are basically two types of information channels: unguided or guided channels.
Atmosphere is an unguided type of channel over which waves can propagate. Guided channels
are those which guide the electromagnetic waves through them. Two wire lines, coaxial cable,
waveguide and optic fibre are the examples of Guided information channels. Guided channels
have the advantages of privacy, no weather dependence and the ability to convey messages
within, under and around physical structures.
An optical fiber is a thin strand of glass or plastic serving as the transmission medium
over which the information passes. The basic fiberoptic system is a link connecting optical
transmitter and receiver.
Transmitter
It converts an electrical signal into a light signal. The source is either a lightemitting
diode or laser diode which does the actual conversion. The drive circuitry changes the electrical
signal fed to the transmitter into a form suitable for the source.
FiberOptic Cable
It is the medium for carrying the light. The cable includes the fibers and its protective
coverings.
Receiver
It accepts the light and converts it back into an electrical signal. The generator amplifies,
reshapes the signal before passing it on.
The range of wavelengths in the visible region extends from 0.4 m to 0.7 m. Thevisible range is not suitable for light transmission through glass fiber. In this region, the waves
are attenuated to such an extent that only short transmission links are possible. Losses in the
ultraviolet region are even greater. It is the infrared region from 0.8 m to 1.6 m which is
used for fiber optic transmission.
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1.1Advantages of Fibers
1.1.1 Wide Bandwidth
The information carrying capacity which increases with the bandwidth of the
transmission medium, is very large in fibers. The bandwidth available on a pair of single mode
fibers is in the order of several GHz. Thus, thousands of circuits can be carried on the fibers
whether the information is voice, data or video or a combination of these.
1.1.2 Low Loss
Bandwidth is an effective indication of the rate at which information can be sent. Loss
indicates how far the information can be sent. As a signal travels along a transmission path the
signal loses strength. This loss of strength is known as attenuation. In a copper cable,
attenuation increases with the modulation frequency: the higher the frequency of the information
signal, the greater is the loss. In an optical fibre, attenuation is flat: loss is the same at any
signaling frequency until a very high frequency. Thus, the problem of loss is much more in a
copper cable as information carrying capacity increases.
Fig.1 shows the loss characteristics Vs the channel bandwidth for fibres, and coaxial
cable. Loss in coaxial cable increases with frequency, whereas loss in the optical cable remainsflat.
Fig. 1Attenuation versus Frequency (BW)
The loss at very high frequencies in the optical fibre does not result from additional
attenuation of the light by the fibre. The loss is caused by loss of information, not by optical
power, but due to the variation of the optical power. At very high frequencies, distortion causes
a reduction or loss of this information.
1.1.3 Electromagnetic Immunity
Optic fibres are insulators. No electric current flows through them, either due to the
transmitted signal or due to external radiation striking the fibre. For these reasons, fibres do not
radiate or pickup electromagnetic radiation as in copper cables. Any copper conductor acts like
an antenna, either transmitting or receiving energy.
Since fibers do not radiate or receive electromagnetic energy, they make an ideal
transmission medium. As a consequence to fibre's electromagnetic immunity, signals do not
become distorted by EMI. Fibres offer very high standards in error free transmission.
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1.1.4 Small Size
Fibres are hair thin in size. Fibers covered with protective coverings are still smaller than
the equivalent copper conductor. The small size of fibre optic cables makes them attractive for
applications where space is at a premium.
1.1.5 Light Weight
A glass fibre weighs considerably less than a copper conductor. A fibreoptic cable with
the same information carrying as a copper cable weighs less than the copper cable. Weight
savings are important in such applications as aircraft and automobiles.
1.1.6 Greater Safety
A fibre is a dielectric. It does not carry electricity. If the cable is damaged, it does not
present any spark or fire hazard, so it cannot cause explosions or fires as a faulty copper cable
can. Moreover, it does not attract lightning. The fiberoptic cable can be run through hazardous
areas.
1.1.7 Higher Security
Fibre optics is a highly secure transmission medium, because the fibres do not radiate
energy that can be received by a nearby antenna without getting detected. It is also extremelydifficult to tap a fibre.
2.0Basic Fibre Construction
2.1 An optical fibre has two concentric layers called the core and the cladding. The inner
core carries the light. The refractive index of core is slightly higher than the cladding.
The typical value of refractive index of core is between 1.48 to 1.5. The index of cladding
is 1% lower than that of the core; the typical values being 1.46 to 1.48. The difference in
index in core and cladding allows total internal reflection of light through the core.
Most fibres have an additional coating around the cladding. The primary function of
the additional coatings which are made of polymer is to protect the core and cladding from
shocks that might affect the optical or physical properties of the fiber. The coatings do not
have any optical property so as to affect light propagation within the fibre.
2.1.1 Light Propagation in Optical Fibres
The speed of light is actually the velocity of electromagnetic energy in a vacuum
such as space. The speed of light in other materials such as glass, plastic is less. The
speed of light changes when it travels from one material to another, resulting in light
changing its direction of travel. This deflection of light is called refraction. Furthermore
different wavelengths of light travel at different speeds in the same material.
2.1.2 The index of refraction denoted by n, is a dimensionless number expressing the
ratio of the velocity of light c in free space to its velocity v in a specific material :
n = c/v
The refractive indices of some selected materials are shown in Table 1 below. The index
of glass can be changed by controlling its composition.
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Table IRefractive Indices of Various Materials
Material Index (n) Light velocity(Km/s)
Vacuum 1.0 300,000
Air 1.0003 300,000
Water 1.33 225,000
Fused Quartz 1.46 205,000
Glass 1.5 200,000Diamond 2.0 150,000
Silicon 3.4 88,000
Gallium Arsenide 3.6 83,000
2.1.3 Even when light passes from one index to another, a small portion is always reflected
back into the first material. This reflection is known as Fresnel reflection. For light
passing from air to glass, reflection loss is about 0.17 dB.
The relationship between the incident and refracted ray is clearly brought out by Snell's
law which states:
n1 sin 1 = n2 sin 2
where n1, n2 are the refractive indices of the two materials and 1, 2 are the angles of
incidence and refraction respectively. Critical angle of incidence c where 2 = 90 is
c= arc Sin (n2/n1)
At angles greater than c the light is reflected back. These simple principles of reflection
and refraction form the basis of light propagation through the optical fibre. The amount
that a ray of light is refracted depends on the refractive indices of the two materials.
Light passing from a lower refractive index to a higher one is bent towards the normal,
an imaginary line perpendicular to the interface of the two materials. But light going froma higher index to a lower one refracts away from the normal, as shown in Fig.2.
Fig. 2Principles of Refraction
As the angle of incidence (the angle between the incident ray and the normal) increases,
the angle of refraction approaches 90 to the normal. The angle of incidence that yields
an angle of refraction (angle between the refracted ray and the normal) as 90 is known
as critical angle. If the angle of incidence increases further (beyond critical angle), thelight is totally reflected back into the first material so that it does not enter the second
material. The angles of incidence and reflection are equal.
The fibre uses a circular configuration such that n2 surrounds n1.
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2.1.4 Figure 3 shows the propagation of light through a circular fibre with refractive indices of
core and cladding being n1, n2 respectively and n1>n2. There are three possibilities of
ray striking the corecladding interface.
(a) Light ray 1 injected into the fibre and striking the coretocladding interface at an
angle greater than the critical angle. This is totally reflected back into the core.
Since the angles of incidence and reflection are equal, the reflected light will
again be reflected. The light will continue zigzagging down the length of the fibre.
(b) Light ray 2 strikes the core cladding interface at an angle less than the critical
angle. Such a ray continues travelling to cladding. It then strikes the outer
surface of the cladding at an angle greater than the critical angle of incidence, so
it is reflected back into the cladding. It will then reenter the core, pass through
the cladding on the opposite side and is reflected again into the cladding and
then to core. The cladding is usually inefficient as a light carrier, and the light in
the cladding becomes attenuated fairly rapidly. Such a ray does not contribute to
the light energy travelling to the distant end, and it is lost over distance.
(c) Light ray 3 strikes the core cladding interface at an angle less than the critical
angle, so it is refracted into the cladding, where it meets the claddingair
interface at angle less than the critical angle of incidence for claddingair. This
ray escapes into air and does not contribute to light propagation in the fibre.
Fig. 3
Light Propagation through Fibre
In the aforesaid analysis, it is made clear that the injected light should meet the
coretocladding interface at angles greater than the critical angle so that light is
totally reflected internally and travels down the length of the fibre. The
propagation of light is governed by the indices of the core and cladding and by
Snell's law. This analysis has considered only meridional rays those that pass
through the fibre axis each time they are reflected. Other rays, called Skew rays,
travel down the fibre without passing through the axis. The path of a Skew ray is
typically helical, wrapping around and around the central axis. Such a ray is
ignored.
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2.2 Optical Fibre Classification
2.2.1 The optical fibres can be classified in three ways :
Material
Size (or Mode)
Refractive Index
2.2.2 Material Classification
One way of classifying the fibres is by their material make up.
Glass fibres have a glass core and glass cladding. They are most widely used. The
glass used in fibres is ultrapure, ultratransparent silicon dioxide or fused quartz.
Impurities such as germanium, phosphorus, boron or fluorine are added to the pure
glass to achieve the desired refractive index.
Plasticclad Silica (PCS) fibres have a glass core and plastic cladding. The performance
of this type of fibre is not as good as all glass fibres.
Plastic fibres have a plastic core and plastic cladding. Plastic fibres have high lossesand very low bandwidths but are inexpensive. Plastic and PCS fibres do not have
protective coatings surrounding the cladding.
2.2.3 Classification According to Size (or Mode)
The second way to classify fibres is by the size (core diameter) or modes in fibre. Mode
is a mathematical and physical concept describing the propagation of electromagnetic
waves through media. Mode theory derives from Maxwell's equations. For the purpose
of understanding the concept we shall define the mode simply as a path that a light
ray can follow in travelling down a fibre. The number of modes supported by a fibre
ranges from 1 to over 1,00,000. Thus, an optical fibre provides a path of travels for one
or thousands of light rays depending on its size and properties.
Multimode Fibre is characterized by relatively large core diameters. Typical values of
core diameters are 50, 62.5, 80, 100 micrometers. A multimode fibre supports more
than one propagating mode.
Single Mode Fibre supports only a single propagating mode. It is characterized by
small core diameters ranging from 4 to 10 micrometers.
Fig.4 shows crosssection of the core and cladding diameters of four commonly used
single and multimode fibres.
Fig. 4
Typical Core and Cladding Diameters
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2.2.4 Classification According to Refractive Index Profile
The refractive index profile describes the relationship between the indices of the core
and cladding. There are two main relationships existing in fibre optics: Step Index and Graded
Index. The stepindex fibre is characterized by a uniform index throughout the core material.
The profile shows a sharp step at the junction of the core and cladding. In contrast, the graded
index has a nonuniform core. The index is highest at the centre and it gradually decreases
until it matches that of the cladding.
There are basically three types of fibres according to above classification:
1. Multimode stepindex or simply stepindex fibre.
2. Multimode gradedindex or gradedindex fibre.
3. Singlemode stepindex fibre (commonly called singlemode fibre).
2.2.5 Step Index Fibre
The multimode stepindex fibre is the simplest type. The core diameter ranges from
100 to 970 micrometers. It includes all glass, PCS and all plastic constructions. This type of
fibre is the most wide ranging but it is inefficient from the point of view of information carrying
capacity.
The fibre propagates a number of modes. The path lengths of different modes are
different as different rays take a shorter or longer time to travel the length of the fibre depending
on their angle with the fibreguided axis. The ray that travels straight down the center of the
core without reflecting arrives at the other end first, other rays arrive later. Thus, though all the
rays enter the fibre at the same time but arrive at the distant end at different times. This results
into spreading of light in time or simply pulse spreading.
This spreading of light is called modal dispersion. Modal dispersion results from the
varying modal path lengths in the fibre. Typical values of modal dispersion in multimode step
index fibres range from 15 to 30 ns/km, length of fibre. Modal dispersion is the main limiting
factor for transmitting higher data rates on step index fibres.
2.2.6 Graded Index Fibre
The modal dispersion can be reduced by using gradedindex fibre. The gradedindex
(or GRIN) fibre has a core material whose refractive index varies with distance from the fibre
axis. The structure is illustrated in Fig.8.
Fig. 5GRIN Fibre
Index is maximum at the core center and decreases gradually towards the core
cladding interface. The light travels faster in a medium of lower index of refraction (v = c/n). So
the farther the light ray is from the core axis, the greater is its speed. Because the index is
Minimum density
Maximum density
Minimum density
End view Side view Index profile
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continuously changing across the axis, the light ray is bent or continually redirected towards the
fibre axis in an almost sinusoidal fashion as shown in Fig.6.Fig. 6
Ray Paths along a GRIN fibre
Those rays that follow the longest path by travelling near the outside of the core have a
faster average velocity. The light travelling near the axis of the core has the slowest average
velocity. As a result of this, all rays tend to reach the end of the fibre at the same time. The
typical value of modal dispersion for GRIN fibre is 1 ns/km or less.
Typical sizes of multimode GRIN fibres are 50/125, 62.5/125 and 85/125. This type of
fibre has wide applications requiring wide bandwidths.
2.2.7 Single Mode Fibre
One way of reducing the modal dispersion by using a GRIN fibre. Another way in which
modal dispersion is completely eliminated is by reducing the core diameter until the fibre
propagates only one more efficiently. This type of fibre is known as mono or more popularly
single mode fibre. The single mode fibre has a very small core diameter of only 4 to 10
micrometer. The cladding diameter is standardized at 125 micrometer, as in GRIN fibres.
The point at which a singlemode fibre propagates only one mode depends on the
wavelengths of light carried. Different fibre designs have a specific wavelength, called the cutoff
wavelength, above which it carries only one mode. A fibre designed for singlemode operation
at 1300 nm has a cutoff wavelength of around 1200 nm.
The operation of the singlemode fibre is quite complex. In singlemode fibre the optical
energy is not confined to the core alone. Some of the optical energy of the mode travels in the
cladding as shown in Fig.7.
Fig. 7Light through (Multi & Single Mode Fibres
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The diameter of the light appearing at the end of the fibre is larger than the core
diameter. This diameter is known as Mode Field Diameter. Since the optical energy in a
singlemode fibre travels in the cladding as well as in the core, the cladding need to be more
efficient to carry light energy unlike the multimode fibres where the flow of energy in cladding is
undesirable. The singlemode fibres have a very large bandwidth of the several gigahertz and
allow transmission up to tens of kilometers.
2.3 Advanced Single Mode Fibres
Apart from step profile in ordinary single mode fibre, more complex index profiles are
being used to obtain lower losses and lower dispersion in the fibres. Fig.8 shows refractive
index profiles of advanced singlemode fibres.
2.3.1 Modes in StepIndex Fibres
We have seen that the modal dispersion causes pulse spreading and overlapping. As a
result, it limits the data rate or information carrying capacity that a fibre can support. We will see
later that the modal dispersion depends on wavelength and core diameter. At this junction, we
will introduce a parameter V number. The V number is a fibre parameter that takes into account
the core diameter, wavelength propagated, and fibre numerical aperture (commonly known as
NA to be defined later). It is also called the normalized frequency.
Fig. 8Refractive Index Profiles of Advanced SingleMode Fibres
For a multimode stepindex fibre, the number of modes
N = V2/2
For a GRIN fibre, the number of modes is approximately
N = V2/4
For large values of V, many modes will propagate. Large V corresponds to a relatively
large core radius. The number of modes in a gradedindex fibre is about half that of a step
index fibre having the same core diameter and NA. A fibre with a 50 micrometer core supports
over 1000 modes.
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2.3.2 Fiber Comparisons
The performance of the fibre depends on its type. Here, the term performance means
higher bandwidth, higher information carrying capacity, and lower losses. Though it is common
to stress on high performance, i.e. low losses and high bandwidth of fibres, but one has to
choose the fibre depending on the application.
2.4 Numerical Aperture
3.0Characteristics of Optical Fibres - IntroductionLike any other medium such as the VF pair, coaxial cable or the free space in the case
of microwave systems, the optical fibre also its own transmission characteristics such as
Numerical Aperture, Modal and Material Dispersion, etc.
Numerical Aperture
Numerical aperture is defined as the "lightgathering ability" of a fibre. When an optical
ray in a medium of refractive index 'n' falls on the lateral surface of the core of optical fibre at a
maximum angle so that it can traverse throughout the fibre core length due to total internal
reflection, then n sin is called the Numerical Aperture (NA) of the fibre.
Only light injected into the fibre at angles greater than the critical angle will be propagated.
In Fig.9, a meridional ray is shown entering the end face of the core at an angle .
Fig. 9Meridional Ray in a Core
The ray will be refracted into the core at an offaxis angle. It strikes the core
cladding interface at an angle i and is totally reflected if i > c (c = Critical angle).
Numerical Aperture is a unitless quantity. We can also define the angles at which
rays will be propagated by the fibre. These angles form a cone that gives the maximumangle of light acceptance. The acceptance angle is related to the NA. A ray not falling
within the acceptance cone is lost by radiation.
Fig. 10Numerical Aperture
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The numerical aperture of a fibre is important because it gives an indication as to
how the fibre accepts and propagates light; a fibre with a low NA requires highly
directional light. Numerical apertures and acceptance angles for fibres representative of
Allglass, PCS and allplastic constructions are listed in Table 2.
Table 2Typical Numerical Apertures and Acceptance Angles
Construction n1 n2 NA Acceptance Angle
Allglass 1.48 1.46 0.24 13.9o
PCS 1.46 1.40 0.41 24.2o
Allplastic 1.49 1.41 0.48 29.0o
In general, fibres with a large bandwidth have a lower NA. They thus allow fewer
modes. Fewer modes means less dispersion and, hence, greater bandwidth. A large NA
promotes more modal dispersion, since more paths for the rays are provided.
In GRIN fibres, the NA is maximum at the centre (NA = 0.26). The NA drops off to
zero at the edge of the core. Only a ray perfectly parallel to the fibre axis will be guided if
it enters the waveguide at this point.
NA for singlemode fiber is only about 0.11. Light in a singlemode fibre is not
reflected or refracted, so it does not exit the fibre at angles. Similarly, the fibre does not
accept light rays at angles within the NA and propagates them by total internal reflection.
3.2 Dispersion
Dispersion is a phenomenon which spreads a light pulse as it travels down the
length of an optical fibre. Dispersion is undesirable as it limits the bandwidth or
informationcarrying capacity of a fibre. The bit rate must be low enough to ensure that
pulses do not overlap. The pulse broadening increases as the square root of thedistance of transmission. The duration that must be allotted between pulses to avoid
inter-symbol interference is proportional to the length of the fibre.
There are three classes of dispersion.
1. Modal or intermodal dispersion.
2. Material dispersion.
3. Waveguide dispersion.
3.2.1 Modal Dispersion
This type of dispersion is dominant in multimode fibres. It arises due to different
velocities of different modes. Singlemode fibres are not subject to intermodal
dispersion. Gradedindex fibres greatly reduce intermodal dispersion. Phase velocity of
light in the core will be same in any direction for a S.I. fibre. A ray travelling along the
fibre axis will travel the shortest distance. A ray having an angle i with the axis which is
equal to the critical angle (i = c), will be travelling the longest path. Most S.I. glass
fibres have measured pulse spreads around 1050 ns/km. The discrepancy arise due to
mode mixing and preferential attenuation.
Mode mixing is the exchange of power between modes. Rays in one mode are
deflected (by scattering and at bends and splices) into the paths of other modes. Rays
may move from higher to lowerorder modes, and vice versa. The result of continued
mode mixing is that energy launched in any one mode travels a total zigzag path length
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that is somewhere between the shortest (axialmode) path and the longest (critical
angle) path. All rays travel nearly the same total length, reducing multimode pulse
spreading considerably. The mode mixing is not perfect, so modal distortion is the main
cause of spreading in S.I. fibres. Although mode mixing reduces the pulse spread, it is
not altogether desirable. Deflections will also direct some rays into paths at less than the
critical angle. The light will be lost, increasing the fibre attenuation.
The second source of pulse spread reduction is the greater attenuation suffered
by higher ordered modes which penetrate more deeply into the cladding, thereby
contributing less to the received pulse compared to lowerorder modes. Pulse spread
will be smaller due to negligible amplitude of higherorder modes in the received pulse.
But it is undesirable as total signal attenuation increases. It is important to note that
modal dispersion does not depend on the source wavelength or on the source
bandwidth. GRIN fibres produce much less multimode distortion than S.I. fibres.
3.2.2 Material Dispersion
It is caused due to the variation of velocity with wavelength (colour). Different
wavelengths travel at different velocities through a fibre even when all the light followsthe same path. The velocity variation caused by some property of the material gives rise
to the effect which is called material dispersion.
We know that n = c/v, where c is the speed of light in a vacuum and v the speed of
the same wavelength in the material. The index of refraction changes according to the
wavelengths. As a result each wavelength travels at a different speed through the
material. The pulses travel at different velocities, reaching the end of the fibre at slightly
different times. When summed at the output, the pulses add together, yielding an output
that is lengthened or spread relative to the input signal. This illustrates how dispersion
creates pulse distortion. The farther the pulse travels, the greater the spreading.
Distortion caused by material dispersion can be reduced by using sources with
smaller bandwidths or line widths. Optical sources radiative over a range of wavelengths
instead of the desired single wavelength or single frequency. This range is known as
line width or spectra width. The smaller the line or spectral width, the more coherent
the source emits light at a single wavelength; thus it has zero line width and is perfectly
monochromatic. Typical line widths of common sources are listed in Table 3.
Table 2Typical Source Spectral Widths
Source Line width ()Lightemitting diode (semiconductor) 20100 nm
Laser Diode (semiconductor) 15 nm
Nd : YAG laser (solid state) 0.1 nm
HeNe laser 0.002 nm
At 1.3 micrometer, the material dispersion is zero. Pulse spreading due to
material dispersion disappears at this wavelength. M is positive at wavelengths below
1.3 micrometer. M is negative and pulse spreading is positive at wavelengths about 1.3
micrometers. Material dispersion is of greater concern in singlemode fibres. In a
multimode fibre, the modal dispersion is dominant and material dispersion is of no
consequence. For SM fibres material dispersion is large in the range of 0.8 to 0.9
micrometer. Pulse spread becomes smaller for longer wavelengths and narrower source
linewidths.
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3.2.3 Waveguide Dispersion
Waveguide dispersion results from the guiding structure and is important in
singlemode fibres. It occurs because guided optical energy is divided between the core
and the cladding. The energy travels at slightly different velocities in the core and
cladding because of the slightly different refractive indices of the materials.
Waveguide and material dispersions depend on the source's spectral width as
well as the length of the fibre. Waveguide dispersion is much less than material
dispersion in the range of 0.80.9 micrometer. At 1.3 micrometer, wavelength material
dispersion disappears, waveguide dispersion is significant. Just beyond this wavelength,
M becomes negative while M' stays positive. Cancellation occurs, leaving zero pulse
spread at a wavelength that is still close to 1.3 micrometer.
In SM fibre attenuation is lowest at 1550 nm, while the dispersion is lowest at
wavelength close to 1300 nm. To take advantage of lowest attenuation as well as low
dispersion at 1550 nm, singlemode fibre is constructed with a triangularshaped
refractive index variation. Such a fibre is known as dispersion shifted fibre. In order to
obtain uniformly low dispersion over a wide range of wavelengths in the region 1300 to
1600 nm, dispersion flattened fibres are used. The dispersion-flattened fibre is
constructed by appropriately tailoring the refractive index variation of the fibre. For this
depressedcladding fibre, where the core index is surrounded by a thin inner cladding
whose index is low and an outer cladding whose index is a bit higher is used.
3.2.4 Length Dependence of the Pulse Spread
The pulse broadening increases linearly with fibre length. Experiments with
multimode fibres have shown that this is true for short lengths (usually less than 1 km),
but for longer lengths, the broadening is proportional to the square root of the length.
A good fibre has little mode mixing, so equilibrium is established only after travelover a long distance. A fibre with no mode mixing would have infinite Le, and its pulse
spread would increase linearly with length. A poor fibre has a lot of mode mixing due to
scattering, micro-bends and in-homogeneities. For this fibre Le is relatively short.
Although the poor fibre has improved bandwidth, its attenuation will be much higher than
that of good fibres.
Material and waveguide dispersions are independent of mode coupling. Pulse
broadening by material and waveguide mechanisms increases linearly with path length.
3.2.5 Total Pulse Spread
The total pulse spread of a multimode fibre is determined, by the sum of the modal
distortion and the material plus waveguide (negligible) dispersions. The way in which
these two contributions are added to find the total effect, depends upon the pulse
shapes in question and the degree of precision required.
3.3 Band width
The bandwidth (BW) is defined to be the frequency at which the fibres base band
frequency response is down by 3 dB (in optical power). It is the 3 dB bandwidth of a fibre
which corresponds to reduction in modulated optic power by half. It is important to note
that optic 1.5 dB bandwidth equals the electrical 3 dB bandwidth.
f1.5dB (optic) = f3dB (electrical)
f1.5dB (optic) = 0.71 f3dB (optic)
hence, f3dB (electrical) = 0.71 f3dB (optic)
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The fibre bandwidth is generally specified as the bandwidth length product given
in megahertz or gigahertz kilometers. A bandwidth of 400 MHzkm. means that a 400
MHz signal can be transmitted for 1 km. It also means that the product of the frequency
and the length must be 400 or less (BW X L = 400). A lower frequency can be sent for a
longer distance. Conversely a higher frequency can be sent shorter distance.
3.4 Attenuation
Signal attenuation is a major factor in the design of any communication system. In anoptic system, the loss of power takes place at several points. These are the coupler,
splices and connectors and within the fibre itself. In this section, we will study the losses
associated with the fibre. Attenuation varies with the wavelength of light. The attenuation
curve of a typical fibre is shown in Fig.11.
Fig. 11Spectral Attenuation for Allglass Fibre
It can be seen that the fibre exhibits minimum attenuation at wavelength slots of around
850 nm, 1300 nm and 1550 nm. These slots are also called first window, second
window, and the third window, respectively. A typical singlemode fibre offers
attenuation of 2.02.5 dB/km. at 850 nm and 0.40.5 dB at 1300 nm and 0.250.30 at1550 nm. The operating wavelengths are so chosen as to avoid high loss regions of the
fibre attenuation curve.
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3.4.1 Sources of Loss in Fibres
The losses occurring in glass fibres can be attributed to three main causes:
1. Absorption
2. Scattering
3. Geometric effects.
3.4.2 Absorption
The losses due to absorption can be divided further in two categories:(a) Intrinsic absorption
(b) Absorption due to impurities
The intrinsic absorption is a natural property of glass itself. Even the purest
glass will absorb heavily within specific wavelength regions. Intrinsic absorption is very
strong in shortwavelength ultraviolet portion of the electromagnetic spectrum. This
absorption is due to strong electronic and molecular transition bands. Fortunately, the
operating region of the fibre is far removed from UV region. Apart from UV absorption
loss, glass absorbs light in the infrared region also. The infrared absorption peaks
occur between 7 and 12 micrometer for typical glass composition, far from the region of
interest. The IR loss is associated with vibrations of chemical bonds such as the silicon
oxygen bond. Thermal energy causes the atoms to be moving constantly, so the SiO
bond is continually stretching and contracting. This vibration has a resonant frequency in
the infrared range. IR absorption contributes a small loss at the upper limit of our
range, 1.6 micrometer. In fact, IR absorption prohibits the use of silica fibres beyond 1.6
micrometer wavelength. Impurities are a major source of loss in any practical fibre. In
general, two types of impurities are particularly troublesome:
(a) Metal ions
(b) Hydroxyl ion (OH)
Metal impurities causing absorption include ions of iron, copper, cobalt, vanadium,
nickel, manganese and chromium. To maintain low losses, the level of these ions must
be less than one part per billion.
The hydroxyl ion (OH) is another most important contributor to the loss. Though
the peak OH ion absorption lies at 2.73 micrometer (outside the band of interest), the
overtones and combination bands of this peak lie within the range of interest. The most
significant OH losses occur at 1.38, 1.24 and 0.94 micrometer. Fig.11 indicates OH
absorption peaks. OH impurity is kept to less than a few parts per million during theglass fibre manufacture.
3.4.3 Scattering
Scattering is the loss of optical energy due to imperfections in the fibre and from
the basic structure of the fibre. Due to scattering, the light is scattered in all directions
which causes the loss of power in the forward direction. This loss is known as Rayleigh
scattering loss.
Rayleigh scattering takes palce due to variations in the density and composition of
glass material in the fibre. Density and compositional variations take place during
manufacture itself. Material in-homogeneities unintentionally introduced into the glass
during manufacture also cause scattering losses.
Rayleigh scattering is inversely proportional to the fourth power of the wavelength
(1/4) and it diminishes rapidly at longer wavelengths.
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3.4.4 Geometric Effects
Bending a fibre causes attenuation. Two types of bends are :
(a) Micro-bending
(b) Macro-bending
Microscope bending loss is caused due to determination of the fibre axis during
cabling process. When a fibre is sheathed within a protective cable, it sets up stresses
which cause small axial distortion (micro-bends) to appear randomly along the fibre.
Micro-bends cause some of the light to couple out of the fibre. This effect can be
eliminated by using loosetube cable construction.
Excessive bending of the cable or fibre may result in loss known as Macro-bend
loss. This loss may occur when wrapping the fibre on a spool or pulling the fibre cable
around a corner. Fibres can be bent with radius of curvature as small as 10 cm. with
negligible loss. Typically, breaking will not occur unless the bend radius is less than 150
times the fibre diameter. For example, if the diameter is 125 micrometer, the bend radius
before breaking is as little as 1.9 cm. Fig.12 illustrates Micro-bend and Macro-bend
losses. A minimum bend radius should be maintained to avoid losses. As a rule of
thumb, the minimum bend radius is five times the cable diameter for an
unstressed cable and ten times the diameter for a stressed cable. The total
attenuation of the fibre is the combination of all the loss phenomena.
Fig. 12Radiation due to Micro-bending and Macro-bending