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Malaysian Institute of Aviation Technology 
DIGITAL TECH (MECH) 
AKD 21102 
CHAPTER 7 
FIBER OPTIC 
Revision 00 Issue 01 Module 5.4
Malaysian Institute of Aviation Technology 
LEARNING OUTCOME 
• Data transmission over electrical wire propagation 
• Fiber optic data bus 
• Fiber optic related terms 
• Advantages and disadvantages of fiber optic 
• Terminations: cleaving, stripping, splicing and 
termination losses 
• Couplers, control terminals, remote terminals 
• Application of fiber optics in aircraft system 
Revision 00 Issue 01 Module 5.4
Malaysian Institute of Aviation Technology 
Malaysian Institute of Aviation Technology 
BASIC COMMUNICATION SYSTEM 
Transmitter Information 
Channel Receiver 
•Information travels 
•Message is 
generated and 
from transmitter to the Message is 
receiver over this extracted from 
put into channel. the information 
suitable form channel and put 
for transfer •Divided in 2 into its final form 
over the categories: 
information 1)Unguided channel. 
channel - atmosphere 
2)Guided channel 
- copper, fiber optic 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
Malaysian Institute of Aviation Technology 
WHAT IS FIBER OPTIC? 
• Fiber optics (optical fibers) are long, thin 
strands of very pure glass about the 
diameter of a human hair. They are 
arranged in bundles called optical cables 
• Used to transmit high-speed transmission 
of data using light over long distances. 
• Transmission depend on the optical 
property of total internal reflection 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
A bundle of optical fibers 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
Revision 00 Issue 01 Module 5.10 
STRUCTURE
Malaysian Institute of Aviation Technology 
STRUCTURE 
• Core - Thin glass centre of the fiber where the 
light travels 
• Cladding - Outer optical material surrounding 
the core that reflects the light back into the core 
• Buffer coating - Plastic coating that protects the 
fiber from damage and moisture 
• Hundreds or thousands of these optical fiber are 
arranged in bundles in optical cables. The 
bundles are protected by the cable's outer 
covering, called a jacket 
Revision 00 Issue 01 Module 5.4
Malaysian Institute of Aviation Technology 
Revision 00 Issue 01 Module 5.10 
STRUCTURE
Malaysian Institute of Aviation Technology 
TOTAL INTERNAL REFLECTION 
• Core(n1) and cladding(n2) have different 
refraction index (n). n1 is always greater than n2 
(n1>n2) 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
TOTAL INTERNAL REFLECTION 
• “When the angle of incidence exceeds a critical 
value, light cannot get out of the glass; instead, 
the light bounces back in.” 
• Numerical aperture (NA) 
– measure of maximum core angle for light rays to be 
reflected down the fibre by total internal reflection 
– Snell’s law : NA= sin θ = √(n2 1 
– n2) 
2 
where n1 = refractive index of the core 
n2 = refractive index of the cladding 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
TOTAL INTERNAL REFLECTION 
Total internal reflection of light in a multi-mode optical fiber. 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
TYPES OF MODE 
• 2 types of mode : single-mode fiber and multi-mode fiber 
1. Single-mode fiber 
– Small core diameter(5-10μm) with an operating wavelength of 
around 1.5μm 
– Transmitter source : Laser diode (LD) 
– Only 1 incident angle i.e only 1 path and at same velocity, 
eliminating distortion due to pulse lapping 
– providing the least signal attenuation and the highest transmission 
speeds, large bandwidth (typically 500 - 1500 MHz.km) and longer 
distance. 
– Data is sent at multi-frequency (WDM Wave-Division- Multiplexing) 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
2. Multi-mode fiber 
TYPES OF MODE 
– large diameter core (typically 100μm) with operating wavelength 
around 1μm. 
– Transmitter source : light emitting diode (LED) 
– Support hundreds or thousands of light rays traveling at different 
velocities i.e. many angles of incident 
– Problem: pulse broadening causing limitation on bandwidth 
– 2 type of multi-mode : Step index and Graded Index 
– Easier to launch optical power and facilitate the connecting of similar fibre 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
DATA TRANSMISSION 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
DATA TRANSMISSION 
Multi-mode (graded index) 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
TERMINOLOGY 
• Attenuation : signal loss within a fibre and measure in 
decibels per kilometer (dB/km) 
• Star coupler : passive optical coupler which allows the 
light signals from each fibre stub to be coupled with 
other fibre stub and then into subsystems 
• Wavelength Division Multiplexing (WDM) : signal of 
different wavelengths are sent down the fibre all together 
• Passive optical sensor : optical sensor which do not 
require electrical supplies or any electronic processing. 
Used to monitor leading and trailing edge flap, spoilers, 
ailerons, rudder etc 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
FIBER OPTIC COMMUNICATION 
SYSTEM 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
TERMINOLOGY: TRANSMISSION 
• Optical Source - used to generate light signal. Can be 
either light-emitting diode (LED) or an injection- laser 
diode (ILD) 
• Transmitter - Produces and encodes the light signals 
• Optical fiber - Conducts the light signals over a distance. 
Light pulses move easily down the fiber- optic line 
because of a principle known as total internal reflection. 
• Optical regenerator - May be necessary to boost the light 
signal (for long distances) 
• Optical receiver - Receives and decodes the light 
signals. Can be either photodiode or phototransistor 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
OPTICAL SOURCES 
• LD advantages over LED: 
– Signal can be modulated at very high speed 
– Produce greater optical power (used for long haul 
communication cable) 
– Have higher coupling efficiency of the optical cable 
– Does not suffer from signal broadening due to pulse lapping 
• LED advantages over LD 
– Higher reliability 
– Better linearity 
– Lower cost 
– More user (used for metro/urban population and point-to-point 
connection) 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
ADVANTAGES OF FIBER OPTIC 
• SPEED: Fiber optic networks operate at high speeds i.e. 
up into the gigabits 
• BANDWIDTH: large carrying capacity 
• DISTANCE: Signals can be transmitted further without 
needing to be "refreshed" or strengthened. 
• RESISTANCE: Greater resistance to electromagnetic, 
electrical isolation, low cross talk (interference) 
• MAINTENANCE: Fiber optic cables costs much less to 
maintain. 
• PHYSICAL: Smaller size and weight than coaxial or 
copper cable buses 
• USER : able to accommodate more user 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
FIBER OPTIC VS COPPER 
The optical fiber cable in the foreground has the equivalent information-carrying 
capacity of the copper cable in the background 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
DISADVANTAGES OF FIBER OPTIC 
• Connectors have to be of high integrity 
• No DC power transmission 
• Minimum bend radii required 
• Care when handling - no excessive 
pulling, pinching or crimping 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
MAINTENANCE 
1. Repairing the cable by inserting an in-line 
splice 
- 2 type of splicing : fusion and mechanical 
- Cleaving : The controlled breaking of a 
fiber so that its end surface is smooth. 
2. Termination 
3. Testing 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
FUSION SPLICING 
• 4 Basic steps 
1.Stripping: removing the cladding using plastic clad silica 
(PCS) and cleaning of fiber using alcohol solution 
2. Cleaving: cutting of edge surface at 900 using cleaver and 
fiber is clean again using alcohol solution 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
• 4 Basic steps 
3. Fusion process : 
FUSION SPLICING 
– Sleeves are places on the fiber and the 2 ends of the fiber 
need to be connected are place on the micro core. 
– Testing of compatibility (acceptable angle of cutting), free of 
foreign object debris (FOD) and alignment of two fiber optics 
are carried out by the micro core splicing machine. 
– Errors occurred, correctional action is taken. 
– After errors are corrected, fusion splicing took place. 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
FUSION SPLICING 
• Example of error during fusion process 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
• 4 Basic steps 
4. Protection : 
FUSION SPLICING 
– A sleeve for the fiber is used to protect the splicing area and 
act as a strengthening mechanism for the fiber. 
– Final testing is simulated using Optical Time Domain 
Reflectometer (OTDR). 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
• 7 Basic steps 
1. Preparing the required connector i.e. housing, body, duct 
cap and the strain relief boot 
2. Preparing the fiber 
Revision 00 Issue 01 Module 5.10 
Termination
Malaysian Institute of Aviation Technology 
• 7 Basic steps 
3. Connecting the fiber to connector 
4. Cleaving 
5. Polishing 
Revision 00 Issue 01 Module 5.10 
Termination
Malaysian Institute of Aviation Technology 
• 7 Basic steps 
6. Visual check 
7. Testing 
Revision 00 Issue 01 Module 5.10 
Termination
Malaysian Institute of Aviation Technology 
CONNECTORS 
• Type A 
- used at production breaks i.e. not regularly 
connect-disconnect 
- Multi channel, in-line (butt type) 
- Low loss 
• Type B 
– Used to connect to the LRUs; frequently 
connect-disconnect 
– Multi channel, expended beam (ball lens) 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
TERMINOLOGY OF NETWORK 
• Bus Network 
- A network topology in which all of the terminals are attached to a 
transmission medium serving as a bus 
– Commonly called data bus 
– The term is used to describe the physical linkage between stations 
on a network sharing a common communications 
– The bus can only transmit data in one direction, and if any network 
segment is severed, all network transmission ceases. 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
TOPOLOGY 
• Bus Network 
- Computer directly connected on a main communication line 
- A host on a bus network is called a station or workstation. In a bus 
network, every station receives all network traffic, and the traffic 
generated by each station has equal transmission priority. 
Only 1 computer can communicate Each computer 
communicate 
individually Revision 00 Issue 01 Module 5.10 to network
Malaysian Institute of Aviation Technology 
TERMINOLOGY OF NETWORK 
• Star Network 
- one of the most common computer network 
topologies. 
- In its simplest form, a star network consists of one 
central switch, hub or computer, which act as a 
conduit to transmit messages. 
- This consists of a central node, to which all other 
nodes are connected; this central node provides a 
common connection point for all nodes through a hub 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
• Star Network 
Revision 00 Issue 01 Module 5.10 
TOPOLOGY
Malaysian Institute of Aviation Technology 
• Advantages 
STAR NETWORK 
- Better performance 
- Isolation of devices 
- Centralization: increasing in capacity, or connecting additional 
devices to it, increases the size of the network very easily and allows 
the inspection of traffic through the network 
- Easy to detect faults and to remove parts. 
- No disruptions to the network when connecting or removing devices. 
- Installation and configuration is easy 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
• Disadvantages 
STAR NETWORK 
- High dependence of the system on the functioning of the central hub. 
Failure of the central hub renders the network inoperable 
- There is central server dependency. 
- Expensive to purchase. 
- Requires a large amount of cable to be connected. 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
• Ring Network 
- a network topology in which each node connects to exactly two 
other nodes, forming a single continuous pathway for signals 
through each node - a ring. Data travel from node to node, with 
each node along the way handling every packet. 
Revision 00 Issue 01 Module 5.10 
TOPOLOGY
Malaysian Institute of Aviation Technology 
• Advantages 
RING NETWORK 
- Very orderly network where every device has access to the token 
and the opportunity to transmit 
- Performs better than a bus topology under heavy network load 
- Does not require a central node to manage the connectivity 
between the computers 
- Quite easy to install and reconfigure since adding or removing a 
device requires moving just two connections. 
- Point to point line configuration makes it easy to identify and isolate 
faults. 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
• Disadvantages 
RING NETWORK 
- One malfunctioning workstation can create problems for the entire 
network. This can be solved by using a dual ring or a switch that 
closes off the break. 
- Moving, adding and changing the devices can affect the network 
- Communication delay is directly proportional to number of nodes in 
the network 
- Bandwidth is shared on all links between devices 
- More difficult to configure than a Star: node adjunction = Ring 
shutdown and reconfiguration 
Revision 00 Issue 01 Module 5.10
Malaysian Institute of Aviation Technology 
APPLICATION 
• In Boeing 777 
1.Avionics local area network (LAN) 
- Aircraft Information Management System 
(AIMS) 
- Maintenance Access Terminal (MAT) 
2. Cabin LAN 
– Zone network controller 
– Cabin file server (CFS) 
Revision 00 Issue 01 Module 5.10

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Topic 7 Digital Technique Fiber optics

  • 1. Malaysian Institute of Aviation Technology DIGITAL TECH (MECH) AKD 21102 CHAPTER 7 FIBER OPTIC Revision 00 Issue 01 Module 5.4
  • 2. Malaysian Institute of Aviation Technology LEARNING OUTCOME • Data transmission over electrical wire propagation • Fiber optic data bus • Fiber optic related terms • Advantages and disadvantages of fiber optic • Terminations: cleaving, stripping, splicing and termination losses • Couplers, control terminals, remote terminals • Application of fiber optics in aircraft system Revision 00 Issue 01 Module 5.4
  • 3. Malaysian Institute of Aviation Technology Malaysian Institute of Aviation Technology BASIC COMMUNICATION SYSTEM Transmitter Information Channel Receiver •Information travels •Message is generated and from transmitter to the Message is receiver over this extracted from put into channel. the information suitable form channel and put for transfer •Divided in 2 into its final form over the categories: information 1)Unguided channel. channel - atmosphere 2)Guided channel - copper, fiber optic Revision 00 Issue 01 Module 5.10
  • 4. Malaysian Institute of Aviation Technology Malaysian Institute of Aviation Technology WHAT IS FIBER OPTIC? • Fiber optics (optical fibers) are long, thin strands of very pure glass about the diameter of a human hair. They are arranged in bundles called optical cables • Used to transmit high-speed transmission of data using light over long distances. • Transmission depend on the optical property of total internal reflection Revision 00 Issue 01 Module 5.10
  • 5. Malaysian Institute of Aviation Technology A bundle of optical fibers Revision 00 Issue 01 Module 5.10
  • 6. Malaysian Institute of Aviation Technology Revision 00 Issue 01 Module 5.10 STRUCTURE
  • 7. Malaysian Institute of Aviation Technology STRUCTURE • Core - Thin glass centre of the fiber where the light travels • Cladding - Outer optical material surrounding the core that reflects the light back into the core • Buffer coating - Plastic coating that protects the fiber from damage and moisture • Hundreds or thousands of these optical fiber are arranged in bundles in optical cables. The bundles are protected by the cable's outer covering, called a jacket Revision 00 Issue 01 Module 5.4
  • 8. Malaysian Institute of Aviation Technology Revision 00 Issue 01 Module 5.10 STRUCTURE
  • 9. Malaysian Institute of Aviation Technology TOTAL INTERNAL REFLECTION • Core(n1) and cladding(n2) have different refraction index (n). n1 is always greater than n2 (n1>n2) Revision 00 Issue 01 Module 5.10
  • 10. Malaysian Institute of Aviation Technology TOTAL INTERNAL REFLECTION • “When the angle of incidence exceeds a critical value, light cannot get out of the glass; instead, the light bounces back in.” • Numerical aperture (NA) – measure of maximum core angle for light rays to be reflected down the fibre by total internal reflection – Snell’s law : NA= sin θ = √(n2 1 – n2) 2 where n1 = refractive index of the core n2 = refractive index of the cladding Revision 00 Issue 01 Module 5.10
  • 11. Malaysian Institute of Aviation Technology TOTAL INTERNAL REFLECTION Total internal reflection of light in a multi-mode optical fiber. Revision 00 Issue 01 Module 5.10
  • 12. Malaysian Institute of Aviation Technology TYPES OF MODE • 2 types of mode : single-mode fiber and multi-mode fiber 1. Single-mode fiber – Small core diameter(5-10μm) with an operating wavelength of around 1.5μm – Transmitter source : Laser diode (LD) – Only 1 incident angle i.e only 1 path and at same velocity, eliminating distortion due to pulse lapping – providing the least signal attenuation and the highest transmission speeds, large bandwidth (typically 500 - 1500 MHz.km) and longer distance. – Data is sent at multi-frequency (WDM Wave-Division- Multiplexing) Revision 00 Issue 01 Module 5.10
  • 13. Malaysian Institute of Aviation Technology 2. Multi-mode fiber TYPES OF MODE – large diameter core (typically 100μm) with operating wavelength around 1μm. – Transmitter source : light emitting diode (LED) – Support hundreds or thousands of light rays traveling at different velocities i.e. many angles of incident – Problem: pulse broadening causing limitation on bandwidth – 2 type of multi-mode : Step index and Graded Index – Easier to launch optical power and facilitate the connecting of similar fibre Revision 00 Issue 01 Module 5.10
  • 14. Malaysian Institute of Aviation Technology DATA TRANSMISSION Revision 00 Issue 01 Module 5.10
  • 15. Malaysian Institute of Aviation Technology DATA TRANSMISSION Multi-mode (graded index) Revision 00 Issue 01 Module 5.10
  • 16. Malaysian Institute of Aviation Technology TERMINOLOGY • Attenuation : signal loss within a fibre and measure in decibels per kilometer (dB/km) • Star coupler : passive optical coupler which allows the light signals from each fibre stub to be coupled with other fibre stub and then into subsystems • Wavelength Division Multiplexing (WDM) : signal of different wavelengths are sent down the fibre all together • Passive optical sensor : optical sensor which do not require electrical supplies or any electronic processing. Used to monitor leading and trailing edge flap, spoilers, ailerons, rudder etc Revision 00 Issue 01 Module 5.10
  • 17. Malaysian Institute of Aviation Technology FIBER OPTIC COMMUNICATION SYSTEM Revision 00 Issue 01 Module 5.10
  • 18. Malaysian Institute of Aviation Technology TERMINOLOGY: TRANSMISSION • Optical Source - used to generate light signal. Can be either light-emitting diode (LED) or an injection- laser diode (ILD) • Transmitter - Produces and encodes the light signals • Optical fiber - Conducts the light signals over a distance. Light pulses move easily down the fiber- optic line because of a principle known as total internal reflection. • Optical regenerator - May be necessary to boost the light signal (for long distances) • Optical receiver - Receives and decodes the light signals. Can be either photodiode or phototransistor Revision 00 Issue 01 Module 5.10
  • 19. Malaysian Institute of Aviation Technology OPTICAL SOURCES • LD advantages over LED: – Signal can be modulated at very high speed – Produce greater optical power (used for long haul communication cable) – Have higher coupling efficiency of the optical cable – Does not suffer from signal broadening due to pulse lapping • LED advantages over LD – Higher reliability – Better linearity – Lower cost – More user (used for metro/urban population and point-to-point connection) Revision 00 Issue 01 Module 5.10
  • 20. Malaysian Institute of Aviation Technology Revision 00 Issue 01 Module 5.10
  • 21. Malaysian Institute of Aviation Technology ADVANTAGES OF FIBER OPTIC • SPEED: Fiber optic networks operate at high speeds i.e. up into the gigabits • BANDWIDTH: large carrying capacity • DISTANCE: Signals can be transmitted further without needing to be "refreshed" or strengthened. • RESISTANCE: Greater resistance to electromagnetic, electrical isolation, low cross talk (interference) • MAINTENANCE: Fiber optic cables costs much less to maintain. • PHYSICAL: Smaller size and weight than coaxial or copper cable buses • USER : able to accommodate more user Revision 00 Issue 01 Module 5.10
  • 22. Malaysian Institute of Aviation Technology FIBER OPTIC VS COPPER The optical fiber cable in the foreground has the equivalent information-carrying capacity of the copper cable in the background Revision 00 Issue 01 Module 5.10
  • 23. Malaysian Institute of Aviation Technology DISADVANTAGES OF FIBER OPTIC • Connectors have to be of high integrity • No DC power transmission • Minimum bend radii required • Care when handling - no excessive pulling, pinching or crimping Revision 00 Issue 01 Module 5.10
  • 24. Malaysian Institute of Aviation Technology MAINTENANCE 1. Repairing the cable by inserting an in-line splice - 2 type of splicing : fusion and mechanical - Cleaving : The controlled breaking of a fiber so that its end surface is smooth. 2. Termination 3. Testing Revision 00 Issue 01 Module 5.10
  • 25. Malaysian Institute of Aviation Technology FUSION SPLICING • 4 Basic steps 1.Stripping: removing the cladding using plastic clad silica (PCS) and cleaning of fiber using alcohol solution 2. Cleaving: cutting of edge surface at 900 using cleaver and fiber is clean again using alcohol solution Revision 00 Issue 01 Module 5.10
  • 26. Malaysian Institute of Aviation Technology • 4 Basic steps 3. Fusion process : FUSION SPLICING – Sleeves are places on the fiber and the 2 ends of the fiber need to be connected are place on the micro core. – Testing of compatibility (acceptable angle of cutting), free of foreign object debris (FOD) and alignment of two fiber optics are carried out by the micro core splicing machine. – Errors occurred, correctional action is taken. – After errors are corrected, fusion splicing took place. Revision 00 Issue 01 Module 5.10
  • 27. Malaysian Institute of Aviation Technology FUSION SPLICING • Example of error during fusion process Revision 00 Issue 01 Module 5.10
  • 28. Malaysian Institute of Aviation Technology • 4 Basic steps 4. Protection : FUSION SPLICING – A sleeve for the fiber is used to protect the splicing area and act as a strengthening mechanism for the fiber. – Final testing is simulated using Optical Time Domain Reflectometer (OTDR). Revision 00 Issue 01 Module 5.10
  • 29. Malaysian Institute of Aviation Technology • 7 Basic steps 1. Preparing the required connector i.e. housing, body, duct cap and the strain relief boot 2. Preparing the fiber Revision 00 Issue 01 Module 5.10 Termination
  • 30. Malaysian Institute of Aviation Technology • 7 Basic steps 3. Connecting the fiber to connector 4. Cleaving 5. Polishing Revision 00 Issue 01 Module 5.10 Termination
  • 31. Malaysian Institute of Aviation Technology • 7 Basic steps 6. Visual check 7. Testing Revision 00 Issue 01 Module 5.10 Termination
  • 32. Malaysian Institute of Aviation Technology CONNECTORS • Type A - used at production breaks i.e. not regularly connect-disconnect - Multi channel, in-line (butt type) - Low loss • Type B – Used to connect to the LRUs; frequently connect-disconnect – Multi channel, expended beam (ball lens) Revision 00 Issue 01 Module 5.10
  • 33. Malaysian Institute of Aviation Technology TERMINOLOGY OF NETWORK • Bus Network - A network topology in which all of the terminals are attached to a transmission medium serving as a bus – Commonly called data bus – The term is used to describe the physical linkage between stations on a network sharing a common communications – The bus can only transmit data in one direction, and if any network segment is severed, all network transmission ceases. Revision 00 Issue 01 Module 5.10
  • 34. Malaysian Institute of Aviation Technology TOPOLOGY • Bus Network - Computer directly connected on a main communication line - A host on a bus network is called a station or workstation. In a bus network, every station receives all network traffic, and the traffic generated by each station has equal transmission priority. Only 1 computer can communicate Each computer communicate individually Revision 00 Issue 01 Module 5.10 to network
  • 35. Malaysian Institute of Aviation Technology TERMINOLOGY OF NETWORK • Star Network - one of the most common computer network topologies. - In its simplest form, a star network consists of one central switch, hub or computer, which act as a conduit to transmit messages. - This consists of a central node, to which all other nodes are connected; this central node provides a common connection point for all nodes through a hub Revision 00 Issue 01 Module 5.10
  • 36. Malaysian Institute of Aviation Technology • Star Network Revision 00 Issue 01 Module 5.10 TOPOLOGY
  • 37. Malaysian Institute of Aviation Technology • Advantages STAR NETWORK - Better performance - Isolation of devices - Centralization: increasing in capacity, or connecting additional devices to it, increases the size of the network very easily and allows the inspection of traffic through the network - Easy to detect faults and to remove parts. - No disruptions to the network when connecting or removing devices. - Installation and configuration is easy Revision 00 Issue 01 Module 5.10
  • 38. Malaysian Institute of Aviation Technology • Disadvantages STAR NETWORK - High dependence of the system on the functioning of the central hub. Failure of the central hub renders the network inoperable - There is central server dependency. - Expensive to purchase. - Requires a large amount of cable to be connected. Revision 00 Issue 01 Module 5.10
  • 39. Malaysian Institute of Aviation Technology • Ring Network - a network topology in which each node connects to exactly two other nodes, forming a single continuous pathway for signals through each node - a ring. Data travel from node to node, with each node along the way handling every packet. Revision 00 Issue 01 Module 5.10 TOPOLOGY
  • 40. Malaysian Institute of Aviation Technology • Advantages RING NETWORK - Very orderly network where every device has access to the token and the opportunity to transmit - Performs better than a bus topology under heavy network load - Does not require a central node to manage the connectivity between the computers - Quite easy to install and reconfigure since adding or removing a device requires moving just two connections. - Point to point line configuration makes it easy to identify and isolate faults. Revision 00 Issue 01 Module 5.10
  • 41. Malaysian Institute of Aviation Technology • Disadvantages RING NETWORK - One malfunctioning workstation can create problems for the entire network. This can be solved by using a dual ring or a switch that closes off the break. - Moving, adding and changing the devices can affect the network - Communication delay is directly proportional to number of nodes in the network - Bandwidth is shared on all links between devices - More difficult to configure than a Star: node adjunction = Ring shutdown and reconfiguration Revision 00 Issue 01 Module 5.10
  • 42. Malaysian Institute of Aviation Technology APPLICATION • In Boeing 777 1.Avionics local area network (LAN) - Aircraft Information Management System (AIMS) - Maintenance Access Terminal (MAT) 2. Cabin LAN – Zone network controller – Cabin file server (CFS) Revision 00 Issue 01 Module 5.10

Notes de l'éditeur

  1. Better performance: star topology prevents the passing of data packets through an excessive number of nodes. At most, 3 devices and 2 links are involved in any communication between any two devices. Although this topology places a huge overhead on the central hub, with adequate capacity, the hub can handle very high utilization by one device without affecting others. Isolation of devices: Each device is inherently isolated by the link that connects it to the hub. This makes the isolation of individual devices straightforward and amounts to disconnecting each device from the others. This isolation also prevents any non-centralized failure from affecting the network. Benefits from centralization: As the central hub is the bottleneck, increasing its capacity, or connecting additional devices to it, increases the size of the network very easily. Centralization also allows the inspection of traffic through the network. This facilitates analysis of the traffic and detection of suspicious behavior Installation and configuration is easy since every one device only requires a link and one input/output port to connect it to any other device(s).
  2. Due to the point to point line configuration of devices with a device on either side (each device is connected to its immediate neighbor), it is quite easy to install and reconfigure since adding or removing a device requires moving just two connections.