�� �� �� �������������������UNIT IV OPTICS WITH LASER AND�OPTICAL FIBRE �
CHAPTER-16
Optical Fibre
distortions, and distance between relay stations.
optical fibers are used as a dominant transmission system.
signals with minimum losses over long distances.
centre is a the core, the middle region is a cladding and the outer region is a
protective sheath.
low losses (less than 0.2 dB/km) as a consequence of which, the distance between
two successive repeaters could be as large as 250 km.
copper cables.
There are many advantages of optical fibers over conducting wires. The main advantages are:
used in communication.
(2) Not hazardous:
(3) Immune to RFI and EMI:
electromagnetic interference and radio frequency interference.
(4) Small size, light weight, flexible, and strong:
connectors and splices.
makes it strong.
(5) No crosstalk:
information propagating through the optical fiber is trapped within the fiber and cannot
leak out.
.
(6) High information-carrying capacity:
radio waves and microwaves.
(7) Low loss:
consequence of which, the distance between two successive repeaters can be as large
as 250 km.
(8) Higher data-rate transmission:
and at higher data rates than other forms of wired and wireless communications.
FUNDAMENTALS OF OPTICAL FIBERS:
What is an optical fiber?
Structure of an optical fiber:
Fig1: An optical fiber waveguide showing core, cladding, and protective jacket
(i) Core
optical beam.
composition known as cladding.
(ii) Cladding
(iii) Jacket
strength.
Fig2: Propagation of light in an optical fiber
Let
n1 = the refractive index of the core and
n2 = the refractive index of cladding (n2 < n1).
n0 = refractive index of outside medium from where the light is launched
And
θi be the angle made by light with the axis of fiber at launching end and
θr be the angle made by the refracted ray with the axis
Φ be the angle at which refracted ray strikes the core–cladding interface
If Φ > critical angle (θc), then the ray undergoes total internal reflection at the interface. As long as the angle Φ > θc the light remains within the fiber.
Applying Snell’s law at the launching face of the fiber, we get
(1)
Now, the largest value of θi will be at Φ = θc
From the right-angled triangle ABC, we have
sin θr = sin (90°– Φ) = cos Φ
From Eq. (1), we know that
By putting the value of sin θr , we get
When Φ = θc , θi = θmax
Now,
(2)
Using Snell’s law at point B or cladding boundary,
or, (because for total internal reflection, reflection angle will be 90°)
So, (3)
Using the value of cos θc from Eq. (3) in Eq. (2), we get
(4)
For the conditions when for all values of angle of incidence, total internal reflection will occur. For special condition, when n0 = 1, the maximum value of angle of incidence (θi) for the ray to be guided is given by
(5)
In the above expression, θm is known as the acceptance angle of the fiber.
16.6 FRACTIONAL REFRACTIVE INDEX CHANGE
Fractional refractive index change is defined as the ratio of the difference between the refractive indices of the core and the cladding to the refractive index of the core. It is denoted by and is given as
−=nnn121 (16.6)
The value of is always positive and less than one because n1 > n2 (always), otherwise the phenomena of total internal reflection will not be fulfilled.
16.7 NUMERICAL APERTURE
Numerical aperture (NA) is a number, which defines the light acceptance or light propagating capacity of a fiber. Sometimes, it is also known as figure of merit. Numerical aperture is defined as the sine of maximum angle (acceptance angle) from the fiber axis at which the light may enter in the core of optical fiber and propagate through it by several internal reflections. It is expressed as
NA = sin qm = nnn12220−
Usually n0 is the refractive index of the air and is given as n0 = 1. Hence, the value of NA can be given as
NA==sinqmnn1222− (16.7)
where n1 and n2 are the refractive indices of core and cladding, respectively.
Numerical aperture can also be expressed in terms of fractional refractive index change () as follows:
Fractional refractive index change is defined as the ratio of the difference between the refractive indices of the core and the cladding to the refractive index of the core. It is denoted by Δ and is given as
(6)
The value of Δ is always positive and less than one because n1> n2 (always), otherwise the phenomena of total internal reflection will not be fulfilled.
Numerical aperture (NA) is a number, which defines the light acceptance or light propagating capacity of a fiber. It is also known as figure of merit. It is expressed as
Usually n0 is the refractive index of the air and is given as n0 = 1. Hence, the value of NA can be given as
(7)
where n1 and n2 are the refractive indices of core and cladding, respectively.
Numerical aperture can also be expressed in terms of fractional refractive index change (Δ)as follows:
Since the difference in n1 and is n2 small, so we can write
Hence Δ
or, (8)
Fig 3: The double crucible method for fiber fabrication
On the basis of refractive index profile and modes propagated through core, optical fibers are classified mainly into two categories. These are as follows:
(i) Step index (SI) optical fiber
(ii) Graded index (GI) optical fiber
n(r) = n1 when r < a (where n1 > n2)
n2 when r > a
where n1 and n2 are the refractive indices of core and cladding respectively, and a is the core radius.
(i) Single-mode step index (SMSI) optical fiber
(ii) Multimode step index (MMSI) optical fiber
Fig.4 (a) Structure of a single-mode optical fiber, (b) refractive index profile,
(c) input pulse, (d) pulse propagation, and (e) output pulse
(ii) Multimode Step Index Optical Fiber
Fig.5 (a) Structural view of MMSI, (b) refractive index profile, (c) input pulse,
(d) pulse propagation, and (e) output pulse
2. Graded Index Optical Fiber
In graded index optical fiber, refractive index of the core region decreases with the radial distance from the maximum value of n1 at the starting boundary (inner side) to a constant value n2 beyond the core radius (a). The index variation may be given as
Where,
Fig.6 (a) Structural view of MMGI, (b) refractive index profile, (c) input pulse
(d) pulse propagation, and (e) output pulse
(9)
Where ,a is core radius and λ is the wavelength.
(10)
Where V is referred to as V- number, known as normalized frequency of cut-off.
Where n1(r) is the varying refractive index of the core as the function of r, n2 is the refractive index of the cladding, a is the radius of the core, x is the parameter describing the refractive index profile variation, and NA(r = 0) is the numerical aperture at the centre of the fiber core.
(12)
Where λ0 is the wavelength of the light propagating in the multimode glass fiber, d = 2a is the diameter of the core, and NA is the numerical aperture.
(13)
(13a)
Where V-parameter is considerably larger than unity.
Table 1 Comparison of single-mode and multimode index fibers
Table 2 Differences between step index and graded index fibers
1. Propagation Mechanism of Meridional Rays
The meridional ray is shown in Fig.16.7 for the SI fiber.
Fig.16.7 Ray diagram of a meridional ray propagating through SI fiber
In Fig.16.7, the light ray is entering the fiber core from a medium of refractive index n0 at an angle with respect to the core–cladding interface at a normal angle Φ. If it strikes this interface at such an angle which is totally internally reflected, then meridional rays follow a zigzag path along the fiber core. These rays pass through the axis of the waveguide after each reflection.
According to Snell’s law, the minimum angle Φmin that supports the total internal reflection for the meridional ray is obtained as
Where n1 and n2 are the refractive indices of core and cladding, respectively.
The rays which are striking at core–cladding interface at angle less than Φmin will refract out of the core and will be lost in the cladding. From Fig. 16.7, it is clear that
Hence corresponding to ,we have
And correspondingly
Using Snell’s law at the air–fiber interface AB, we get
Hence, we can conclude that the rays having entrance angle θi less than θi max will be totally internally reflected at the core–cladding interface.
2. Propagation Mechanism of Skew Rays
Fig. 7 The helical path of skew rays: (a) skew ray path in core of fiber and
(b) cross sectional view of the fiber
Fig.8 The path of skew ray in the fiber core, incidenting at an angle θi
Cos Φ.
However, if the two perpendicular planes through which the ray AB traverses are considered, then γ is the angle between the core radius and the projection of the ray on the plane BRS normal to the axis of the core.
θ is the angle between the ray and the line AT drawn parallel to the core axis. Thus, to resolve the ray path AB relative to the radius BR in these two perpendicular planes requires multiplication by cos γ and sin θ.
Hence, the reflection at point B at an angle Φ may be given as
(14)
For total internal reflection
(15)
Using Snell’s law at point A, we have
(16)
Where θimax is maximum input axial angle for meridional rays and θ is the internal axial angle.
Putting the value of sin θ from Eq. (16) in Eq. (15), we get
(17)
Where θimax represents the maximum input angle or acceptance angle for skew rays. The condition at which skew rays are accepted by the fiber core can be given as
(18)
If n0 = 1 for air, then
(19)
The block diagram of an optical communication system is shown in Fig.9. The system has:
(i) Information source: It is the source of input signals which are to be transmitted through the optical fiber up to the destination.
(ii) Electrical transmitter: It is the next part of the communication system where the information signals are produced in the form of electrical signals.
(iii) Optical source: Optical source is capable of generating an optical signal at desired frequencies. Basically LASER or LEDs are used as the source of light.
Fig.9 Optical fibre communication system
(iv) Optical fiber cable: The optical signal is launched into the optical fiber which is contained inside the cable. The cable provides mechanical and environmental protection to the hair-thin optical fiber.
(v) Optical detector: At the receiving end, photo detector is the main component. It is capable of converting the received modulated wave back to the original signal, which has the same wave shape as the optical wave envelope.
(vi) Electrical receiver: It is the part of the communication system where original signal is recovered in its suitable form. Usually, electronic amplifiers and signal restorers consisting of signal processor circuits are used in this section of communication system.
(20)
(21)
On the basis of several mechanisms which are responsible for signal attenuation within optical fibers, we can categorize the losses in terms of the following points:
(i) Absorption losses
(ii) Scattering losses
(iii) Bending losses
(iv) Dispersion losses
1) Absorption Losses
The absorption of light by core and cladding materials of a fiber during wave propagation is the main source of attenuation. Absorption of light is caused by the following three different mechanisms:
(i) Atomic imperfection in the glass composition
(ii) Intrinsic absorption
(iii) Extrinsic absorption
Fig. 10 The attenuation spectra for the intrinsic loss mechanism in pure GeO2—SiO2 glass
The absorption due to the strong electronic and molecular transition band is characterized by peak loss in the ultraviolet and diminishing loss as the visible region is approached.
2) Scattering Losses
(i) linear scattering losses and
(ii) non-linear scattering losses.
(a) Rayleigh and
(b) Mie scattering.
(ii) Nonlinear Scattering Losses
(22)
where d is the core diameter, λ is the operating wavelength (both are measured in μm), αdB is the fiber attenuation in db/km, and ν is the source bandwidth in GHz.
(b) Stimulated Raman scattering (SRS):
(23)
where PSRS is the threshold optical power for SRS, d is the core diameter, λ is the operating wavelength, and αdB is the fiber attenuation in decibels.
3) Bending Losses
Bending losses occur due to imperfections and deformations present in the fiber structure. Generally, there are two types of bending losses: micro bending losses and macro bending losses.
(ii) Macro bending losses:
(16.24)
where all the symbols have their usual meanings.
4)Dispersion Losses
(i) Intramodal dispersion and (ii) Intermodal dispersion.
(i)Intramodal Dispersion
(a) material dispersion and (b) waveguide dispersion.
(b) Waveguide dispersion:
(ii) Intermodal Dispersion
(25)
where n1 is the refractive index of the core and c is the velocity of light.
(26)
(27)
where n2 is the refractive index of cladding.
Fig. 12 Path taken by axial and extreme meridional ray in a perfect MMSI fiber
Putting the value of cos θ in Eq. (26), we get
(28)
The delay difference δTSI between the extreme meridional ray and the axial ray will be given as
where Δ is the relative refractive index difference. Since Δ<< 1, so it may also be given approximately by
Putting the value of Δ in terms of numerical aperture, we get
(30)
where NA is the numerical aperture of the fiber. The approximate expression for the delay difference given in Eq. (30) is usually employed to estimate the maximum pulse broadening in time due to the intermodal dispersion in an MMSI fiber.
(29)
Similarly, after 2 km of optical fiber, the output power is
Hence, after L kilometer of optical fiber, the above expression can be given as
Or,
Taking log on both sides and then multiplying by 10 gives power loss in decibel as
where α (10 log10 k) is the attenuation coefficient of the fiber in decibel/kilometer.
Therefore, (31)
Sometimes, the number of decibel loss is expressed with negative sign and hence, the above equation can also be given as
(32)
(ii) Optical fiber cables have good stable transmission characteristics. The optical attenuation due to cabling are quite usual and must be minimized within the cable design.
(iii) Optical cables have similar mechanical properties such as tension, torsion, compression, bending, squeezing, and vibration, as of electrical transmission cables. Hence, the cable strength will be improved.
(iv) Splicing and joining of optical fibers are very easy within the cable.
Fig.13 A hypothetical two-fiber cable design. The basic building block on the left-hand fiber is exactly same as it is shown on right-hand fiber
Optical fibers have wide range of applications in the field of optical communication, medical science, illumination technology, optical sensor, etc. Some important applications of optical fiber are as follows:
(i) Optical fibers are widely used in broadcast television, cable TV, remote monitoring, and surveillance.
(ii) Fibers are most commonly used for transmission of digital data.
(iii)It is frequently used in military operations such as for secret communications, command and control links on ship and aircrafts, data links for satellites, etc.
(iv) It is widely used in cable TV network and closed circuit TV (CCTV) systems.
(v) Fibers are frequently used in illumination technology.
(vi) Fibers have a variety of applications in medical services.
(vii) Fibers are frequently used for decorative applications.
(viii) A coherent bundle fiber is used, sometimes along with lens, for a long, thin imaging device called endoscope.
(ix) Fibers are used to transfer infrared energy from the source to the point of application of heat.
(x) Fibers are used to form sensors to measure physical and chemical parameters.