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The document provides comprehensive answers related to optical communication and networks, covering critical angle calculations, total internal reflection in prisms, optical bands and windows, classification of optical fibers, and various fiber parameter calculations. It also discusses fiber fabrication methods such as MCVD and the double crucible method, along with notes on optical switches, photonic crystal fibers, and optical circulators. Key concepts include numerical aperture, acceptance angle, and the significance of different fiber types and their applications.

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0% found this document useful (0 votes)
40 views30 pages

Iat 1

The document provides comprehensive answers related to optical communication and networks, covering critical angle calculations, total internal reflection in prisms, optical bands and windows, classification of optical fibers, and various fiber parameter calculations. It also discusses fiber fabrication methods such as MCVD and the double crucible method, along with notes on optical switches, photonic crystal fibers, and optical circulators. Key concepts include numerical aperture, acceptance angle, and the significance of different fiber types and their applications.

Uploaded by

dhotreraju515
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
You are on page 1/ 30

Comprehensive Answers for Optical

Communication and Networks

1. Critical Angle Calculation


Question: A certain fiber-optic cable has the following characteristics: n1 = 1.46 and n2 = 1.43. What is
the value of critical angle (θc)?

Answer:
The critical angle is given by the formula:
θc = sin⁻¹(n2/n1)

Substituting the values:


θc = sin⁻¹(1.43/1.46)
θc = sin⁻¹(0.9795)
θc = 78.65°

The critical angle is approximately 78.65 degrees.

2. Total Internal Reflection in Prism


Question: A 45-45-90 prism is immersed in alcohol n=1.45. What is minimum RI of prism so that ray of
light incident on short faces is totally reflected at the long phase of prism?

Answer:
For total internal reflection to occur at the long face (hypotenuse) of the prism, the angle of incidence
must exceed the critical angle.

In a 45-45-90 prism, light hitting the short face perpendicular will strike the hypotenuse at 45°.

The critical angle between the prism and alcohol must be less than 45° for total internal reflection:
θc = sin⁻¹(n₂/n₁) < 45°

Where n₂ = 1.45 (alcohol) and n₁ = prism RI

sin⁻¹(1.45/n₁) < 45°


1.45/n₁ < sin(45°)
1.45/n₁ < 0.7071

Page 1 of 30
n₁ > 1.45/0.7071
n₁ > 2.05

Therefore, the minimum refractive index of the prism must be greater than 2.05.

3. Optical Bands and Windows


Question: Explain optical bands and windows. Which band is known as extended C band?

Answer:
Optical bands refer to specific wavelength ranges used in optical communication systems. These bands
are designated as follows:

1. O band (Original): 1260-1360 nm


2. E band (Extended): 1360-1460 nm
3. S band (Short): 1460-1530 nm
4. C band (Conventional): 1530-1565 nm
5. L band (Long): 1565-1625 nm
6. U band (Ultralong): 1625-1675 nm

Optical windows refer to wavelength regions with low attenuation in silica fibers:

First window: 800-900 nm (multimode fiber)


Second window: 1260-1360 nm (O-band)
Third window: 1530-1565 nm (C-band)
Fourth window: 1565-1625 nm (L-band)

The Extended C band refers to the wavelength range of approximately 1530-1570 nm, which is an
expansion of the conventional C band to accommodate more DWDM channels. It's highly valued because
it offers low attenuation and can be efficiently amplified by Erbium-Doped Fiber Amplifiers (EDFAs).

4. Classification of Optical Fibers


Question: How do you classify optical fibers based on number of modes and RI profile? Elaborate with
diagrams and color codes.

Answer:
Optical fibers are classified based on two main criteria:

A. Based on Number of Modes:

1. Single-Mode Fibers (SMF)

Page 2 of 30
Core diameter: 8-10 μm
Cladding diameter: 125 μm
Only one mode (fundamental mode) propagates
Typically color-coded yellow
Used for long-distance communication

2. Multi-Mode Fibers (MMF)

Core diameter: 50-62.5 μm


Cladding diameter: 125 μm
Multiple modes propagate simultaneously
Typically color-coded orange (62.5 μm) or aqua/teal (50 μm)
Used for shorter distances due to modal dispersion

B. Based on Refractive Index Profile:

1. Step Index Fiber (SI)

Abrupt change in refractive index between core and cladding


Can be either single-mode or multimode

2. Graded Index Fiber (GI)

Gradual decrease in refractive index from center to cladding


Almost exclusively multimode
Reduces modal dispersion compared to step-index multimode

This creates four main types of optical fibers:

1. Single-Mode Step Index Fiber


2. Multi-Mode Step Index Fiber
3. Single-Mode Graded Index Fiber (rare)
4. Multi-Mode Graded Index Fiber

5. Normalized Frequency and Guided Modes


Question: A multimode step index fiber with a core diameter of 80 μm and a relative index difference of
1.5% is operating at a wavelength of 0.85 μm. If the core refractive index is 1.48, estimate: (a) the
normalized frequency for the fiber; (b) the number of guided modes.

Answer:

(a) Normalized Frequency (V-parameter):

Page 3 of 30
The normalized frequency V is given by:
V = (2πa/λ) × n₁ × √(2Δ)

Where:

a = core radius = 80/2 = 40 μm


λ = operating wavelength = 0.85 μm
n₁ = core refractive index = 1.48
Δ = relative index difference = 1.5% = 0.015

Substituting:
V = (2π × 40 μm / 0.85 μm) × 1.48 × √(2 × 0.015)
V = (2π × 47.06) × 1.48 × √0.03
V = 295.73 × 1.48 × 0.1732
V = 75.86

(b) Number of Guided Modes:

For a step-index fiber, the number of guided modes M is approximately:


M ≈ V²/2

Substituting:
M ≈ (75.86)²/2
M ≈ 5754.95/2
M ≈ 2877 modes

Therefore, the fiber supports approximately 2877 guided modes.

6. Numerical Aperture and Acceptance Angle


Question: What is Numerical Aperture and Acceptance angle and explain its Significance. Derive an
expression for NA in step index fiber. Which type of ray has a wider acceptance angle?

Answer:

Numerical Aperture (NA):

Numerical Aperture is a measure of the light-gathering capability of an optical fiber. It represents the
sine of the maximum angle at which light can enter the fiber and still undergo total internal reflection.

Acceptance Angle (θₐ):

Page 4 of 30
The acceptance angle is the maximum angle at which light can enter the fiber core and still be guided
through the fiber by total internal reflection.

Significance:

1. Determines the light-gathering capability of the fiber


2. Indicates coupling efficiency between light source and fiber
3. Affects the number of modes that can propagate through the fiber
4. Influences the fiber's susceptibility to bending losses

Derivation of NA for Step Index Fiber:

Consider a ray entering the fiber at angle θₐ (acceptance angle) and refracting at angle θ₁.

From Snell's law at the air-core interface:


n₀ sin(θₐ) = n₁ sin(θ₁)

Where n₀ is the refractive index of air (≈ 1).

For the ray to undergo total internal reflection at the core-cladding interface, θ₁ must exceed the critical
angle θc:
θc = sin⁻¹(n₂/n₁)

At the boundary condition (θ₁ = θc):


sin(θ₁) = sin(θc) = n₂/n₁

From the first equation:


sin(θₐ) = n₁ sin(θ₁)/n₀
sin(θₐ) = n₁(n₂/n₁)/n₀
sin(θₐ) = n₂/n₀

But we need to express this in terms of n₁ and Δ.


Recall that the relative refractive index difference is:
Δ = (n₁² - n₂²)/(2n₁²)

For small Δ:
Δ ≈ (n₁ - n₂)/n₁

Therefore:
n₂ ≈ n₁(1 - Δ)

Substituting:
sin(θₐ) = n₁(1 - Δ)/n₀
NA = n₀ sin(θₐ) = n₁(1 - Δ)

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Expanding further:
sin²(θₐ) = n₁²(1 - Δ)²/n₀²
sin²(θₐ) = n₁²(1 - 2Δ + Δ²)/n₀²

For small Δ, we can neglect Δ² term:


sin²(θₐ) ≈ n₁²(1 - 2Δ)/n₀²

Also, from the definition of Δ:


Δ = (n₁² - n₂²)/(2n₁²)
2n₁²Δ = n₁² - n₂²
n₁²(1 - 2Δ) = n₂²

Substituting:
sin²(θₐ) ≈ n₂²/n₀²

Therefore:
NA = n₀ sin(θₐ) = √(n₁² - n₂²)

For air (n₀ = 1):


NA = sin(θₐ) = √(n₁² - n₂²)

Ray with Wider Acceptance Angle:

Meridional rays (rays passing through the fiber axis) have a wider acceptance angle compared to skew
rays (rays that never cross the fiber axis). This is because meridional rays can enter at the maximum
acceptance angle and still undergo total internal reflection, while skew rays follow a helical path and
must enter at smaller angles to maintain guided propagation.

7. Fiber Parameter Calculations


Question: A multimode step index fiber has core RI of 1.5, cladding RI of 1.38, core radius 25μm at
wavelength of 1300nm. Find NA, V, solid acceptance angle and total number of modes entering the fiber.

Answer:

Numerical Aperture (NA):

NA = √(n₁² - n₂²)
NA = √(1.5² - 1.38²)
NA = √(2.25 - 1.9044)
NA = √0.3456
NA = 0.588

Page 6 of 30
Normalized Frequency (V):

V = (2πa/λ) × NA
V = (2π × 25 μm / 1300 nm) × 0.588
V = (2π × 25 / 1.3) × 0.588
V = 120.8 × 0.588
V = 71.03

Solid Acceptance Angle (Ω):

Ω = 2π(1 - cos(θₐ))
where θₐ = sin⁻¹(NA)
θₐ = sin⁻¹(0.588)
θₐ = 35.98°

Ω = 2π(1 - cos(35.98°))
Ω = 2π(1 - 0.809)
Ω = 2π × 0.191
Ω = 1.2 steradians

Total Number of Modes (M):

For a step-index fiber:


M ≈ V²/2
M ≈ (71.03)²/2
M ≈ 5045.26/2
M ≈ 2523 modes

8. Fiber Fabrication Methods


Question: Explain MCVD and Double Crucible method for fiber fabrication method with neat diagram.

Answer:

Modified Chemical Vapor Deposition (MCVD):

MCVD is a vapor-phase process used to fabricate high-quality optical fibers with precise control over
the refractive index profile.

Process Steps:

Page 7 of 30
1. A high-purity silica tube (future cladding) is mounted horizontally on a glass lathe and rotated.
2. The tube is heated by an external heat source (oxyhydrogen burner) that traverses along its length.
3. A mixture of gases (SiCl₄, GeCl₄, POCl₃, etc.) is introduced into the tube.
4. As the gases pass through the hot zone, chemical reactions occur:
SiCl₄ + O₂ → SiO₂ + 2Cl₂
GeCl₄ + O₂ → GeO₂ + 2Cl₂
5. The resulting oxides deposit as fine particles (soot) on the inner wall of the tube.
6. The deposited particles sinter to form a glass layer.
7. Multiple layers are deposited with varying dopant concentrations to achieve the desired refractive
index profile.
8. After deposition, the tube is collapsed into a solid rod (preform) by heating it to a higher
temperature.
9. The preform is then drawn into a fiber.

Advantages:

Very high purity


Excellent control over refractive index profile
Low attenuation fibers can be produced

Disadvantages:

Relatively slow process


Limited preform size

Double Crucible Method:

The double crucible method is a direct-melting technique for fabricating optical fibers, primarily used
for multimode fibers.

Process Steps:

1. Two concentric crucibles are used: the inner one contains the core glass, and the outer one
contains the cladding glass.
2. Both crucibles are heated to melting temperatures.
3. The molten glasses flow through concentric orifices at the bottom of the crucibles.
4. The composite structure is drawn directly into a fiber.
5. By controlling the flow rates and temperatures, the core-to-cladding ratio can be controlled.

Advantages:

Continuous process (unlike preform methods)


Relatively simple setup
Good for multimode fibers

Page 8 of 30
Disadvantages:

Limited control over complex refractive index profiles


Potential for contamination at the core-cladding interface
Higher attenuation compared to vapor deposition methods

9. Optical Components Notes


Question: Write Note on a) Optical Switches b) Photonic Crystal fiber c) Optical Circulators

Answer:

a) Optical Switches:

Optical switches are devices that selectively route optical signals from input ports to output ports
without optical-to-electrical-to-optical (O-E-O) conversion.

Types of Optical Switches:

1. Mechanical Switches:

Based on physical movement of optical components


Types include moving fiber, prism/mirror, and bubble switches
Advantages: Low insertion loss, good isolation
Disadvantages: Slow switching speed (ms range), mechanical wear

2. Electro-optic Switches:

Based on electro-optic effect (refractive index change with electric field)


Materials used include lithium niobate (LiNbO₃)
Advantages: Fast switching (ns range), no moving parts
Disadvantages: High drive voltage, polarization-dependent

3. Thermo-optic Switches:

Based on refractive index change with temperature


Usually implemented in planar waveguides
Advantages: No moving parts, relatively simple fabrication
Disadvantages: Slow switching (ms range), power consumption

4. Semiconductor Optical Amplifier (SOA) Switches:

Based on gain modulation in SOAs


Advantages: Fast switching, potential for integration
Disadvantages: Signal distortion, noise addition

Page 9 of 30
Applications:

Optical cross-connects in telecommunications networks


Protection switching
Optical add-drop multiplexing
Optical packet switching
Test equipment

b) Photonic Crystal Fiber (PCF):

Photonic Crystal Fibers are a class of optical fibers with periodic microstructured arrangements of air
holes running along their entire length.

Structure:

Contains a regular array of air holes in the cladding region


Two main types:
1. Index-guiding PCFs: Solid core surrounded by a microstructured cladding
2. Photonic bandgap PCFs: Hollow core surrounded by a photonic crystal structure

Characteristics and Advantages:

1. Endlessly single-mode operation: Can maintain single-mode operation over a wide wavelength
range
2. Highly customizable dispersion: Can be tailored for specific applications
3. High nonlinearity: Useful for nonlinear optics applications
4. Large mode area: Reducing nonlinear effects for high-power applications
5. Hollow core guidance: Low nonlinearity and potential for gas-filled fiber applications

Applications:

Supercontinuum generation
Fiber lasers and amplifiers
Sensing applications
Dispersion compensation
Gas-based nonlinear optics
Telecommunications

c) Optical Circulators:

Optical circulators are non-reciprocal multi-port devices that direct light from one port to the next in a
unidirectional sequence.

Operation Principle:

Page 10 of 30
In a three-port circulator: light entering port 1 exits at port 2, light entering port 2 exits at port 3,
and light entering port 3 exits at port 1
Based on the Faraday effect (magneto-optic effect)
Uses materials like yttrium iron garnet (YIG) with permanent magnets

Characteristics:

1. Insertion loss: Typically 0.5-1.0 dB


2. Isolation: Usually >40 dB (measure of how much light is blocked in the reverse direction)
3. Return loss: Typically >50 dB
4. Polarization-dependent loss: <0.1 dB in high-quality circulators

Applications:

1. Bidirectional transmission: Allows full-duplex communication over a single fiber


2. Optical add/drop multiplexers: Efficient adding/dropping of wavelength channels
3. Optical amplifiers: Isolating input and output signals
4. Optical time-domain reflectometers (OTDRs): Separating outgoing pulse from reflected signals
5. Fiber sensors: Particularly in interferometric sensors

10. Types of Optical Fibers


Question: Explain different types of fiber with their refractive index profile and mention its dimensions
and show with neat diagram transmission of light through this fiber.

Answer:

There are several types of optical fibers, each with distinct characteristics:

1. Single-Mode Step-Index Fiber

Refractive Index Profile:

Abrupt change from core to cladding


Core RI (n₁) > Cladding RI (n₂)

Dimensions:

Core diameter: 8-10 μm


Cladding diameter: 125 μm
Buffer coating: 250-900 μm

Light Transmission:

Only one mode (fundamental mode) propagates

Page 11 of 30
Light travels in a nearly straight line along the fiber axis
No modal dispersion

2. Multi-Mode Step-Index Fiber

Refractive Index Profile:

Abrupt change from core to cladding


Core RI (n₁) > Cladding RI (n₂)

Dimensions:

Core diameter: 50-62.5 μm


Cladding diameter: 125 μm
Buffer coating: 250-900 μm

Light Transmission:

Multiple modes propagate simultaneously


Lower-order modes follow shorter paths near the axis
Higher-order modes follow longer paths with more reflections
Significant modal dispersion limits bandwidth-distance product

3. Multi-Mode Graded-Index Fiber

Refractive Index Profile:

Parabolic decrease in refractive index from center to cladding


Highest RI at core center, gradually decreasing toward cladding

Dimensions:

Core diameter: 50-62.5 μm


Cladding diameter: 125 μm
Buffer coating: 250-900 μm

Light Transmission:

Multiple modes propagate simultaneously


Light follows sinusoidal paths
Higher-order modes travel faster in lower RI regions (near cladding)
Lower-order modes travel slower in higher RI regions (near axis)
Significantly reduced modal dispersion compared to step-index multimode

4. Dispersion-Shifted Fiber (DSF)


Page 12 of 30
Refractive Index Profile:

Complex profile with depressed cladding or raised core-cladding boundary


Designed to shift the zero-dispersion wavelength to 1550 nm

Dimensions:

Core diameter: ~8 μm
Cladding diameter: 125 μm

Light Transmission:

Single-mode operation
Optimized for minimum dispersion in the C-band

5. Dispersion-Flattened Fiber (DFF)

Refractive Index Profile:

Complex multilayer profile


Multiple cladding layers with different refractive indices

Dimensions:

Core diameter: ~8 μm
Cladding diameter: 125 μm

Light Transmission:

Single-mode operation
Low dispersion over a wide wavelength range

11. Multimode Step Index Fiber Calculations


Question: If a multimode step index fiber having the core refractive index of 1.5, cladding refractive
index of 1.38, core radius of 25 µm operates at a wavelength of 1300nm. Calculate-Numerical Aperture,
Normalized frequency, Solid acceptance angle, Total no. of modes entering the fiber.

Answer:

Numerical Aperture (NA):

NA = √(n₁² - n₂²)
NA = √(1.5² - 1.38²)
NA = √(2.25 - 1.9044)
Page 13 of 30
NA = √0.3456
NA = 0.588

Normalized Frequency (V):

V = (2πa/λ) × NA
V = (2π × 25 μm / 1300 nm) × 0.588
V = (2π × 25 / 1.3) × 0.588
V = 120.8 × 0.588
V = 71.03

Acceptance Angle (θₐ):

θₐ = sin⁻¹(NA)
θₐ = sin⁻¹(0.588)
θₐ = 35.98°

Solid Acceptance Angle (Ω):

Ω = 2π(1 - cos(θₐ))
Ω = 2π(1 - cos(35.98°))
Ω = 2π(1 - 0.809)
Ω = 2π × 0.191
Ω = 1.2 steradians

Total Number of Modes (M):

For a step-index fiber:


M ≈ V²/2
M ≈ (71.03)²/2
M ≈ 5045.26/2
M ≈ 2523 modes

12. Factors Responsible for Attenuation and Dispersion


Question: What are the different factors responsible for attenuation and dispersion in optical fiber?

Answer:

Attenuation Factors:

Page 14 of 30
Attenuation in optical fibers refers to the reduction in signal power as light propagates through the
fiber. The main factors causing attenuation are:

1. Material Absorption:

Intrinsic Absorption: Due to interaction with the basic material components


Ultraviolet Absorption: Electronic transitions in silica molecules
Infrared Absorption: Vibrational resonances in silica molecules
Extrinsic Absorption: Due to impurities
OH⁻ ions (water): Strong absorption peaks at 950 nm, 1380 nm, and 2730 nm
Transition metal ions: Fe, Cu, Cr cause absorption across the spectrum
Rare earth ions: Cause narrow absorption bands

2. Scattering Losses:

Rayleigh Scattering: Fundamental scattering due to microscopic variations in density and


composition (proportional to λ⁻⁴)
Mie Scattering: Caused by irregularities comparable to the wavelength of light
Waveguide Scattering: Due to imperfections at the core-cladding interface

3. Bending Losses:

Macrobending: Losses due to large-scale bends in the fiber


Microbending: Losses due to small-scale deformations of the fiber axis

4. Connection and Splice Losses:

Fresnel reflection at fiber ends


Misalignments (axial, angular, and lateral)
Mode field diameter mismatch

Dispersion Factors:

Dispersion in optical fibers refers to the spreading of light pulses as they propagate. The main types of
dispersion are:

1. Intermodal (Modal) Dispersion:

Different modes travel with different group velocities


Only occurs in multimode fibers
Major limiting factor for bandwidth in multimode fibers

2. Intramodal (Chromatic) Dispersion:

Page 15 of 30
Material Dispersion: Variation of refractive index with wavelength
Waveguide Dispersion: Variation of propagation constant with wavelength due to waveguide
geometry
These two components combine to give the total chromatic dispersion

3. Polarization Mode Dispersion (PMD):

Different polarization components travel at different speeds


Caused by fiber asymmetry and stress
Random in nature and fluctuates with time and temperature
Significant issue for high-speed systems (>10 Gbps)

13. Fresnel Reflection and Fiber Misalignments


Question: What is Fresnel reflection and the three types of misalignments in a fiber joint?

Answer:

Fresnel Reflection:

Fresnel reflection refers to the partial reflection of light that occurs at the interface between two media
with different refractive indices. In fiber optics, Fresnel reflection occurs at:

1. The interface between the fiber end and air


2. The interface between two fibers in a joint or connection

The reflection coefficient (R) for normal incidence is given by:


R = [(n₁ - n₂)/(n₁ + n₂)]²

Where n₁ and n₂ are the refractive indices of the two media.

For a typical silica fiber (n = 1.46) to air (n = 1) interface:


R = [(1.46 - 1)/(1.46 + 1)]² = [0.46/2.46]² = 0.035 or 3.5%

This means that approximately 3.5% of incident light power is reflected back at each fiber-air interface.
In telecommunications, this reflection can cause:

1. Power loss
2. Return loss/echo
3. Instability in laser sources
4. Interference in bidirectional systems

Minimizing Fresnel Reflection:

Page 16 of 30
1. Index matching gel: Fills the gap with a material of similar refractive index
2. Angled physical contact (APC) connectors: The fiber end is polished at an angle
3. Anti-reflection coatings on fiber ends
4. Fusion splicing: Direct fusion of fibers eliminates the interface

Three Types of Misalignments in Fiber Joints:

Misalignments in fiber joints lead to coupling losses. The three primary types are:

1. Longitudinal (Axial) Misalignment:

Gap between the fiber ends along the axis


Causes divergence of the beam between fibers
Loss increases with increasing gap distance
Loss formula: Loss (dB) ≈ -10 log[1/(1 + Z²/w²)]
where Z is the gap distance and w is the mode field radius

2. Lateral (Transverse) Misalignment:

Offset between the fiber cores perpendicular to the fiber axis


Most critical alignment parameter, especially for single-mode fibers
Loss formula: Loss (dB) ≈ -10 log[exp(-d²/w²)]
where d is the offset distance and w is the mode field radius

3. Angular Misalignment:

Tilt between the fiber axes


Creates a direction mismatch between the output and input fields
Loss formula: Loss (dB) ≈ -10 log[exp(-(πnw sin θ/λ)²)]
where n is the refractive index, w is the mode field radius, θ is the angle, and λ is the wavelength

In practical fiber connections, a combination of these misalignments typically occurs, and their effects
add up to determine the total connection loss.

14. Pulse Spreading in Intermodal Dispersion


Question: Derive the expression for pulse spreading in intermodal dispersion.

Answer:

Derivation of Pulse Spreading in Intermodal Dispersion:

Page 17 of 30
Intermodal dispersion occurs in multimode fibers where different modes travel at different group
velocities, causing a single input pulse to spread as it propagates.

Let's derive the expression for the maximum pulse spread due to intermodal dispersion:

Step 1: Consider the time taken by a ray traveling along the fiber axis.
The axial ray travels a distance L at a velocity v₁ = c/n₁, where c is the speed of light in vacuum and n₁ is
the core refractive index.

Time taken by axial ray:


t₁ = L / v₁ = L × n₁ / c

Step 2: Consider the time taken by the most extreme ray that undergoes total internal reflection at the
critical angle.
This ray follows a zigzag path, traveling at an angle θ₁ to the fiber axis, where θ₁ is related to the critical
angle θc by:
θ₁ = 90° - θc

The path length for this ray over a fiber length L is:
L' = L / cos(θ₁)

Time taken by the extreme ray:


t₂ = L' / v₁ = (L / cos(θ₁)) × (n₁ / c) = (L × n₁) / (c × cos(θ₁))

Step 3: Calculate the maximum time difference (pulse spreading):


Δt = t₂ - t₁
Δt = (L × n₁ / c) × (1/cos(θ₁) - 1)

From the critical angle relationship:


sin(θc) = n₂/n₁
cos(θ₁) = sin(θc) = n₂/n₁

Substituting:
Δt = (L × n₁ / c) × (n₁/n₂ - 1)

For a relative refractive index difference Δ = (n₁ - n₂)/n₁:


n₂ = n₁(1 - Δ)

Substituting:
Δt = (L × n₁ / c) × (n₁/[n₁(1-Δ)] - 1)
Δt = (L × n₁ / c) × (1/(1-Δ) - 1)
Δt = (L × n₁ / c) × (Δ/(1-Δ))

For small values of Δ (typically <0.01):


Δt ≈ (L × n₁ / c) × Δ

Page 18 of 30
This is the expression for the maximum pulse spreading due to intermodal dispersion in a step-index
multimode fiber.

RMS Pulse Broadening:


In practical systems, we often use RMS (root mean square) pulse broadening instead of maximum
spreading:
σ = (L × n₁ / c) × (Δ/√12) (for step-index fibers)
σ = (L × n₁ / c) × (Δ/√8) (for parabolic-index fibers)

15. Dispersion Shifted and Flattened Fibers


Question: Explain Dispersion shifted fiber and Dispersion flattened fiber.

Answer:

Dispersion-Shifted Fiber (DSF):

Dispersion-shifted fiber is a type of single-mode optical fiber designed to have zero chromatic
dispersion at the 1550 nm wavelength, which coincides with the minimum attenuation window of silica
fibers.

Principle:
In standard single-mode fibers, zero dispersion occurs naturally at around 1310 nm, while minimum
attenuation occurs at 1550 nm. By modifying the refractive index profile, the zero-dispersion
wavelength can be "shifted" to 1550 nm.

Structure and Refractive Index Profile:

Core with a triangular or trapezoidal index profile


Often includes a depressed-index inner cladding layer
Complex profile compared to standard single-mode fiber

Fabrication Techniques:

Modified CVD process with careful dopant control


Typically uses germania (GeO₂) and silica (SiO₂) with precise concentration gradients

Characteristics:

Zero dispersion at approximately 1550 nm


Low attenuation (≈0.2 dB/km)
Effective area similar to standard single-mode fiber

Limitations:

Page 19 of 30
Enhanced nonlinear effects at 1550 nm due to coincidence of zero dispersion and operating
wavelength
Four-wave mixing becomes problematic in DWDM systems
The ITU-T G.653 standard defines specifications for DSF

Dispersion-Flattened Fiber (DFF):

Dispersion-flattened fiber is designed to have low chromatic dispersion over a wide wavelength range,
typically covering the S, C, and L bands (1460-1625 nm).

Principle:
By carefully designing the refractive index profile, both material and waveguide dispersion components
can be controlled to achieve a flat dispersion characteristic across multiple wavelength bands.

Structure and Refractive Index Profile:

More complex profile than DSF


Often includes multiple cladding layers with different refractive indices
Common designs feature a central core, depressed inner cladding, and raised outer ring

Fabrication Techniques:

Multi-layer deposition techniques (MCVD, OVD)


Precise control of multiple dopant concentrations

Characteristics:

Low dispersion (typically <3-4 ps/nm/km) over a wide wavelength range


Small dispersion slope
Allows operation across multiple transmission bands
Enables broadband WDM transmission

Applications:

Broadband DWDM systems


Systems using multiple transmission bands
Metro and long-haul networks with mixed bit rates

The ITU-T G.655 standard defines specifications for non-zero dispersion-shifted fibers (NZDSF), which
are a variant that maintains small but non-zero dispersion to mitigate nonlinear effects while keeping
dispersion relatively flat.

16. Comparison of Fiber Types

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Question: Compare i) Intermodal and intramodal dispersion. ii) Step index fiber and Graded index fiber.

Answer:

i) Comparison of Intermodal and Intramodal Dispersion:

Parameter Intermodal Dispersion Intramodal (Chromatic) Dispersion

Pulse spreading due to different


Pulse spreading due to wavelength-dependent
Definition propagation times of different
propagation characteristics of a single mode
modes

Occurrence Only in multimode fibers In all fiber types (single-mode and multimode)

Different modes follow different Wavelength components of a pulse travel at


Mechanism
paths with different lengths different speeds

Two components: material dispersion and


Components Only one type (modal)
waveguide dispersion

Magnitude Much larger (typically 10-30 ns/km) Much smaller (typically 1-20 ps/nm/km)

Wavelength Relatively independent of


Strongly wavelength-dependent
Dependence wavelength

- Operating at zero-dispersion wavelength


- Using graded-index profile
Mitigation - Dispersion-shifted fibers
- Using single-mode fiber
- Dispersion compensation

Effect on Major limiting factor in multimode


Major limiting factor in single-mode fibers
Bandwidth fibers

Mathematical
Δt ≈ (L×n₁/c)×Δ D = d(1/vg)/dλ = -λ/c × d²n/dλ²
Expression

ii) Comparison of Step Index Fiber and Graded Index Fiber:

Parameter Step Index Fiber Graded Index Fiber

Refractive Index Abrupt change between core and Gradual decrease from center to
Profile cladding cladding (usually parabolic)

Zigzag paths with discrete


Light Propagation Continuous bending (sinusoidal paths)
reflection angles

Modal Dispersion Higher (multimode step-index) Significantly reduced (by factor of ~100)

Bandwidth-
20-50 MHz·km 1-2 GHz·km
Distance Product

Numerical
Constant across core Varies with radial distance from center
Aperture

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Parameter Step Index Fiber Graded Index Fiber

Fabrication
Simpler to manufacture More complex doping profile required
Complexity

Cost Generally lower Generally higher

- Short-distance communication - LAN and building backbone networks


Typical
- Industrial controls - Campus networks
Applications
- Sensing - High-speed data links

Straight line segments with


Ray Paths Smooth sinusoidal curves
reflections

All modes equally guided


Mode Distribution Higher-order modes partially suppressed
regardless of launch angle

Generally higher (more forgiving to Slightly lower but more efficient power
Coupling Efficiency
alignment) distribution

More spreading, distinct mode Less spreading, modes arrive at similar


Pulse Response
groups times

17. Multimode Fiber Link Problem


Question: A 6Km link consists of multimode step with core of refractive index 1.5 and relative refractive
index difference 1%, estimate:
a. Delay difference between fastest and slowest mode
b. RMS pulse spreading due to intermodal dispersion
c. Maximum bitrate that may be obtained without substantial errors on the link
d. Bandwidth length product

Answer:

Given information:

Fiber length L = 6 km
Core refractive index n₁ = 1.5
Relative refractive index difference Δ = 1% = 0.01

a. Delay difference between fastest and slowest mode:

The maximum time delay between modes is given by:


Δt = (L × n₁ / c) × (Δ/(1-Δ))

Where c is the speed of light in vacuum (3 × 10⁸ m/s).

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Substituting the values:
Δt = (6 × 10³ × 1.5 / 3 × 10⁸) × (0.01/(1-0.01))
Δt = (9 × 10³ / 3 × 10⁸) × (0.01/0.99)
Δt = 3 × 10⁻⁵ × 0.0101
Δt = 3.03 × 10⁻⁷ seconds
Δt = 303 ns

Therefore, the delay difference between the fastest and slowest mode is approximately 303
nanoseconds.

b. RMS pulse spreading due to intermodal dispersion:

For a step-index multimode fiber, the RMS pulse broadening is:


σ = (L × n₁ / c) × (Δ/√12)

Substituting the values:


σ = (6 × 10³ × 1.5 / 3 × 10⁸) × (0.01/√12)
σ = 3 × 10⁻⁵ × (0.01/3.464)
σ = 3 × 10⁻⁵ × 0.00289
σ = 8.67 × 10⁻⁸ seconds
σ = 86.7 ns

Therefore, the RMS pulse spreading due to intermodal dispersion is approximately 86.7 nanoseconds.

c. Maximum bitrate without substantial errors:

For a digital system without equalization, a common criterion is that the RMS pulse spreading should be
less than approximately 0.1 bit periods to avoid substantial intersymbol interference:

0.1 × (1/Bitrate) ≥ σ
0.1/Bitrate ≥ 86.7 × 10⁻⁹
Bitrate ≤ 0.1/(86.7 × 10⁻⁹)
Bitrate ≤ 1.15 × 10⁶ bits/second
Bitrate ≤ 1.15 Mbps

Therefore, the maximum bitrate that may be obtained without substantial errors on the link is
approximately 1.15 Mbps.

d. Bandwidth-length product:

For multimode fibers, the bandwidth-length product is related to the RMS pulse spreading by:
B·L = 0.44/σ

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Where B is the 3-dB bandwidth, L is the fiber length (already included in σ), and σ is the RMS pulse
spreading.

Substituting the value of σ:


B·L = 0.44/(86.7 × 10⁻⁹)
B·L = 5.07 × 10⁶ Hz·km
B·L = 5.07 MHz·km

Therefore, the bandwidth-length product of the fiber is approximately 5.07 MHz·km.

18. Cutback Method of Attenuation Measurement


Question: Draw and explain block diagram of cutback method of attenuation measurement.

Answer:

The cutback method is a destructive technique used to measure the attenuation of an optical fiber with
high accuracy. It involves comparing the optical power output from a long fiber to the power output
from the same fiber after it has been cut to a much shorter length.

Block Diagram Components:

1. Light Source: Typically a laser or LED at the wavelength of interest


2. Optical Chopper (optional): To modulate the light for improved signal-to-noise ratio
3. Input Optics: Lens system to couple light into the fiber
4. Test Fiber: The fiber under test (long length)
5. Output Optics: Lens system to collect light from the fiber output
6. Optical Detector: Photodiode or power meter to measure the optical power
7. Display/Recorder: To display and record the measured power values

Measurement Procedure:

1. Initial Measurement:

The light source is coupled into the full length of the fiber (L)
The output power (P₂) is measured and recorded
Care is taken to collect all light exiting the fiber

2. Cutback Operation:

The fiber is cut to a short length (typically 1-2 meters) near the input end
The input coupling conditions must remain unchanged during cutting

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3. Reference Measurement:

The output power (P₁) from the short length is measured


This represents the input power to the original fiber

4. Attenuation Calculation:

The fiber attenuation coefficient α in dB/km is calculated using:


α = (10/L) × log₁₀(P₁/P₂)
Where L is the difference in fiber length (in km)

Advantages:

1. High accuracy (considered the reference method for attenuation measurement)


2. Eliminates coupling loss uncertainties
3. Measures the true fiber attenuation, independent of launch conditions
4. Simple calculation and straightforward procedure

Disadvantages:

1. Destructive method (fiber is cut)


2. Not suitable for field measurements or installed fibers
3. Requires careful handling to maintain launch conditions
4. Limited to laboratory environments

Variations:

1. Multiple Cutback: Several cuts are made along the fiber length to obtain multiple data points
2. Mode Filter Application: Mode filters may be used to attain equilibrium mode distribution
3. Automated Systems: Modern implementations use automated cutting and measurement
systems

19. Linear and Non-Linear Scattering Losses


Question: Explain linear and non linear scattering losses in optical fiber.

Answer:

Scattering losses in optical fibers can be categorized into linear and nonlinear types based on how they
interact with the optical power level.

Linear Scattering Losses:


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Linear scattering losses are proportional to the incident optical power and do not change the
wavelength of the scattered light. The two main types are:

1. Rayleigh Scattering:

Mechanism: Caused by microscopic variations in density and composition of the fiber material
that are much smaller than the wavelength of light.
Characteristics:
Fundamental lower limit on fiber attenuation
Wavelength dependence: Proportional to λ⁻⁴ (inversely proportional to the fourth power of
wavelength)
Cannot be eliminated completely, as it originates from the basic material structure
Scattering occurs in all directions, with some light scattered backward (backscattering)
Formula: αᵣ = C/λ⁴, where C is the Rayleigh scattering coefficient
Significance: Dominant loss mechanism in the 800-1600 nm region for modern fibers
Applications: Forms the basis for Optical Time-Domain Reflectometers (OTDRs)

2. Mie Scattering:

Mechanism: Caused by irregularities comparable to or larger than the wavelength of light, such
as:
Imperfections in core-cladding interface
Irregularities in core diameter
Strains and bubbles in fiber
Imperfect joints and splices
Characteristics:
Less wavelength-dependent than Rayleigh scattering
Can be minimized through improved fabrication techniques
More directional than Rayleigh scattering (forward-dominant)
Significance: Generally negligible in modern, high-quality fibers

Nonlinear Scattering Losses:

Nonlinear scattering losses occur at high optical power levels and result in a transfer of optical power
from one mode to other modes at the same or different frequencies. The two main types are:

1. Stimulated Brillouin Scattering (SBS):

Mechanism: Interaction between the optical field and acoustic phonons (sound waves) in the fiber
Characteristics:
Generates a backward-propagating wave (Stokes wave) shifted downward in frequency by
~10-15 GHz

Page 26 of 30
Threshold power proportional to fiber core area and inversely proportional to effective fiber
length
More significant for narrowband signals (like CW lasers)
Threshold typically around 1-10 mW in long fibers
Formula: Threshold power Pᵗʰ ≈ 21(A_eff/L_eff)(v_B/Δv)
Mitigation: Broadening the laser linewidth, using larger core fibers

2. Stimulated Raman Scattering (SRS):

Mechanism: Interaction between the optical field and molecular vibrations (optical phonons) in
the fiber
Characteristics:
Generates both forward and backward propagating waves shifted downward in frequency by
~13 THz (100 nm at 1550 nm)
Higher threshold than SBS (typically ~1 W in conventional fibers)
Broadband phenomenon affecting multiple channels in WDM systems
Can lead to power transfer from shorter to longer wavelength channels
Applications: Forms the basis for Raman amplifiers and lasers
Mitigation: Controlling total power in fiber, channel spacing management

3. Four-Wave Mixing (FWM):

Mechanism: Nonlinear interaction where three waves at frequencies f₁, f₂, and f₃ generate a fourth
wave at frequency f₄ = f₁ ± f₂ ± f₃
Characteristics:
Particularly problematic in DWDM systems with equally spaced channels
Strongly affected by fiber chromatic dispersion (minimal in zero-dispersion fibers)
Creates crosstalk and interference in multi-channel systems
Mitigation: Unequal channel spacing, operating away from zero-dispersion wavelength

Comparison of Linear vs. Nonlinear Scattering:

Characteristic Linear Scattering Nonlinear Scattering

Power Proportional to input Threshold-based, grows exponentially above


Dependence power threshold

Same wavelength as
Wavelength Shift Shifted wavelength (Stokes/anti-Stokes)
input

Occurrence Always present Only significant above power threshold

Effect on System Constant attenuation Power-dependent, can cause sudden system failure

Mitigation Improve fiber fabrication Limit optical power, manage dispersion

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Characteristic Linear Scattering Nonlinear Scattering

Affects all channels


Impact on WDM Can cause selective channel degradation
equally

20. Bending Losses and Attenuation Calculation


Question: Explain microbending and macro bending losses. How it can be minimized? An optical signal
has lost 55% of its power after travelling 3.5Km. What is attenuation in dB/km?

Answer:

Macrobending Losses:

Macrobending losses occur when an optical fiber is bent with a radius of curvature that is large
compared to the fiber diameter but small enough to cause light leakage.

Mechanism:

When a fiber is bent, the outer part of the bend must travel a longer path than the inner part
At a certain radial distance (critical radius), the mode field can no longer be confined within the
core
Light beyond this point radiates out of the fiber

Characteristics:

Increases exponentially as bend radius decreases


More significant for longer wavelengths
More severe in fibers with smaller numerical aperture
Single-mode fibers are more susceptible than multimode fibers

Formula:
The bend loss (α_bend) can be approximated as:
α_bend ∝ exp(-CR), where C is a constant and R is the bend radius

Minimization Methods:

1. Maintain minimum bend radius specifications (typically 20-40 mm for standard fibers)
2. Use bend-insensitive fibers with modified refractive index profiles
3. Use fibers with higher numerical aperture
4. Employ proper cable management practices
5. Use bend limiters and protective elements at fiber terminations

Microbending Losses:
Page 28 of 30
Microbending losses result from small-scale deformations or irregularities along the fiber axis, with
displacements comparable to or less than the fiber diameter.

Mechanism:

Small irregularities cause local changes in the core-cladding geometry


These changes cause coupling between guided modes and radiation modes
Random microscopic bends create multiple scattering points along the fiber

Sources of Microbends:

1. Mechanical pressure from cable layers or fixtures


2. Thermal contraction/expansion of buffer and jacket materials
3. Imperfections from manufacturing process
4. Environmental stress (temperature, vibration)

Characteristics:

Wavelength-dependent (increases with wavelength)


More significant in fibers with larger mode field diameter
Highly dependent on external mechanical forces
Can cause significant variation in attenuation over time

Minimization Methods:

1. Use looser buffer tubes and proper cabling design


2. Apply soft, compressible coatings around the cladding
3. Avoid non-uniform lateral pressures during installation
4. Use fibers with smaller mode field diameters
5. Employ temperature-resistant cable designs
6. Ensure proper handling during installation

Attenuation Calculation:

Problem: An optical signal has lost 55% of its power after traveling 3.5 km.

Solution:

If the signal has lost 55% of its power, then the output power (P_out) is 45% of the input power (P_in):
P_out = 0.45 × P_in

The attenuation in decibels is defined as:


Attenuation (dB) = -10 × log₁₀(P_out/P_in)
Attenuation (dB) = -10 × log₁₀(0.45)

Page 29 of 30
Attenuation (dB) = -10 × (-0.3468)
Attenuation (dB) = 3.468 dB

This is the total attenuation over the 3.5 km length.

To find the attenuation per kilometer (in dB/km):


Attenuation coefficient = Total attenuation / Length
Attenuation coefficient = 3.468 dB / 3.5 km
Attenuation coefficient = 0.991 dB/km

Therefore, the fiber has an attenuation of approximately 0.99 dB/km.

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