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A SEMINOR TOPIC ON
ELECTROMAGNETIC AIRCRAFT LAUNCHING SYSTEM
PRESENTED BY
D. PREM KUMAR
The basic concept discussing is to launch a aircraft with short take-off range
of distance on Navel Ships.
 To achieve high speeds with in 100’s of yards of ship deck is highly
complicate to a fighter jet ,such that we are using some external means of
systems to launch.
 Those systems will possess high thrust output within short period of time and
highly reliable to ship movements to high waves in the sea.
 At present the systems used are
1.Steam Launchers
2.Electric Launches
The basic concept discussing is to launch a aircraft with short take-off range
of distance on Navel Ships.
 To achieve high speeds with in 100’s of yards of ship deck is highly
complicate to a fighter jet ,such that we are using some external means of
systems to launch.
 Those systems will possess high thrust output within short period of time and
highly reliable with ship movements to high waves in the sea.
 At present the systems used are
1.Steam Launchers
2.Electric Launches
For over seven decades, the steam-powered catapult has been the standard
mechanism for launching airplanes from the decks of aircraft carriers.
Aircraft could not reach take-off speeds of over 180kmph in just a few seconds and
within a hundred feet, nor slow from landing speed to full stop in a similar time and
distance.
Cont…..
The existing steam catapults installed on U.S. carriers . Pistons within these connect
to the shuttle which tows the aircraft.
 The steam pressure forces the pistons forward, towing the shuttle and aircraft at
ever increasing speed until takeoff is achieved.
There is no doubt it works, as has been proven through the decades and in combat.
It can launch and retrieve aircraft of varying weights
at a rate of about one every minute or two and do so
simultaneously due to the angled deck.
why not continue with steam?
 It requires an enormous amount of energy to function, and it is energy-inefficient.
 It requires considerable maintenance and a large crew to keep it functioning, especially
in rough seas and potentially in combat conditions.
 It is bulky and heavy, while space is limited even on a modern carrier; it is an open-loop
system with no feedback to control its performance.
 It can only handle a limited range of aircraft types, weights and launch/landing
conditions The drawbacks includes the steam catapult requires a high volume of 1133 m3,
and a weight of 486 metric tons.
The new millennium have seen the development of an alternative technology for
launching aircraft, the electro-magnetic (EM) catapult.
 An EM launch system offers the requisite higher launch energy as well as substantial
improvements in performance, light weight, less volume & high efficiency.
The ability of an EM system to vary speed and thrust to meet the needs of the vehicle
being launched makes a single catapult suitable for a wide range of aircrafts.
1.Linear Induction Motor:
 The EMALS uses a linear induction motor (LIM), which uses electric currents to generate magnetic
fields that propel a carriage along a track to launch the aircraft.
 The linear induction motor consists of a row of stator coils with the same function as the circular
stator coils in conventional induction motor.
 When energized, the motor accelerates the carriage along the track. The EMALS 300-foot (91 m)
LIM will accelerate a 100,000-pound (45,000 kg) aircraft to 240 km/h(150 mph).
Linear Induction Motor
 During a launch, the induction motor requires a large surge of electric power that
exceeds what the ship's own continuous power source can provide. The capacitors
that are being used in this application are two 250V 12,000µF.
 Each stator delivers up to 121 MJ (34 kWh) (approximately one gasoline gallon
equivalent this is faster than steam catapults).A maximum-performance launch using
121 MJ of energy from each disk alternator slows the rotors from 6400 rpm to
5000 rpm which is a fly wheel.
 The energy is recharged with in 45sec.The system
then releases that energy up to 484 MJ
in 2–3 seconds .
Energy Storage System:
During launch, the power conversion subsystem releases the stored energy from the
disk alternators using a cycloconverter.
The cycloconverter provides a controlled rising frequency and voltage to the LIM,
energizing only the small portion of stator coils that affect the launch carriage at any
given moment.
4.Control System:
Operators control the power through a closed loop system . Hall effect sensors on the
track monitor its operation, allowing the system to ensure that it provides the desired
acceleration.
The closed loop system allows the EMALS to maintain a constant tow force, which
helps reduce launch stresses on the plane's airframe
3.Power Conversion System:
Circuit Diagram :
The main principle used is Rail Gun Magnetic Effect which states
 The current flowing in the rails produces a magnetic flux density between the rails,
and this magnetic field interacts with the current flowing in the armature.
 The resulting Lorentz force accelerates the armature together with the projectile
along the rails.
Cont…..
 The capacitors that are being used in this application are two 250V 12,000µF which are not
capable of being fully charged by a regular power supply, to charge some voltage doublers are used
 The amount of charged stored is vary depending on weight of the armed carrier . Using PNPN SCR
triggering is applied.
 When current is flowing through the coil it generates a magnetic field around the piston that has an
opposing magnetic charge of the coil repelling it through the channel at very high speeds.
 Several switches are used in the circuit for safety including a charging switch and firing switch.
 The control system for this project will all be done through Lab View which will apply the 1.7V to
gate of the SCR to trigger the device.
 After charged with in 2-3sec the aircraft is launched up to the weight of 22,000kgs
Advantages:
 Compared to steam catapults, EMALS can control the launch performance
with greater precision, allowing it to launch more kinds of aircraft, from
heavy fighter jets to light unmanned aircraft.
 Lower operating costs.
 Require fewer people to operate.
 Deliver more percent of energy than a steam catapult's.
 90% power conversion efficiency.
disadvantages :
As in the case of EMALS ,air craft equipment is above the launch motor
which may be affected by the electro magnetic emissions (highly sensitive by
EMF).
Handling should be very careful due to high currents.
Highly skilled personal is required.
Initial cost is very high and Fault clearance take time.
Countries that are planning emals :
 United States
>EMALS was designed for and into the Gerald R. Ford-class aircraft carrier. And test runs on Feb 2020.
French
>Construction of the PANG is expected to begin around 2025 and will enter service in 2038.
 China
>According to a report in July 2017, the electromagnetic launchers used in the
Type 003 aircraft carrier. And about to launch in 2021.
 India
>The Indian Navy has shown an interest in installing EMALS for its planned CATOBAR super carrier
INS Vishal.
 United Kingdom
>UK were working on an electro-magnetic catapult (EMCAT) system for the Queen Elizabeth-class
aircraft carrier.
Applications :
StarTram is a proposed space launch system propelled
by maglev. The initial Generation 1 facility would launch
cargo only. More advanced technology would be required
for the Generation 2 system for passengers.
The name itself indicates Runway towards Stars
The idea is that by using electromagnetism to
accelerate a bullet, you can overcome the limitations
of gunpowder-style firearms, which generally top out
at muzzle velocities of about 2,000 meters per second .
Magnetic propulsion can in theory reach any speed; it is also
silent, and with no explosive gases to disperse it can have an
extremely high rate of fire.
Rail guns use magnetic fields created by high electrical
currents to accelerate a projectile to 5,400 miles an hour.
The velocity is sufficient to give the EMRG an effective
range of 110 nautical miles, or 126 miles on land.
A new warship, the large surface combatant, is
scheduled to eventually replace the Ticonderoga-class
cruisers.
Hyperloop is described as a sealed tube or
system of tubes with low air pressure through
which a pod may travel substantially free of air
resistance or friction. Virgin Hyperloop,in the
recent trial, two passengers - both company staff
- travelled the length of a 500m test track in 15
seconds, reaching 172km/h.
conclusion:
 The EMALS is a very good solution, being surprisingly small and simple , with a manageable power
electronics switching system.
 The mechanical systems does not appear to provide sufficient advantage to make the extra complexity
worthwhile, unless becomes a much more significant concern that has so far appeared.
 The EMLS offers the increased energy capability necessary to launch the next generation of
Applications in all sectors.
 The only limitation is the power handling capability and vibration resistance material.
 The challenge of this project will be to get the projectile up to a fast enough speed in a short time.
ANY QUERIES???....
Electricity – The Soul

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Electro Magnetic Aircraft Launching System

  • 1. A SEMINOR TOPIC ON ELECTROMAGNETIC AIRCRAFT LAUNCHING SYSTEM PRESENTED BY D. PREM KUMAR
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  • 4. The basic concept discussing is to launch a aircraft with short take-off range of distance on Navel Ships.  To achieve high speeds with in 100’s of yards of ship deck is highly complicate to a fighter jet ,such that we are using some external means of systems to launch.  Those systems will possess high thrust output within short period of time and highly reliable to ship movements to high waves in the sea.  At present the systems used are 1.Steam Launchers 2.Electric Launches
  • 5. The basic concept discussing is to launch a aircraft with short take-off range of distance on Navel Ships.  To achieve high speeds with in 100’s of yards of ship deck is highly complicate to a fighter jet ,such that we are using some external means of systems to launch.  Those systems will possess high thrust output within short period of time and highly reliable with ship movements to high waves in the sea.  At present the systems used are 1.Steam Launchers 2.Electric Launches
  • 6. For over seven decades, the steam-powered catapult has been the standard mechanism for launching airplanes from the decks of aircraft carriers. Aircraft could not reach take-off speeds of over 180kmph in just a few seconds and within a hundred feet, nor slow from landing speed to full stop in a similar time and distance. Cont…..
  • 7. The existing steam catapults installed on U.S. carriers . Pistons within these connect to the shuttle which tows the aircraft.  The steam pressure forces the pistons forward, towing the shuttle and aircraft at ever increasing speed until takeoff is achieved. There is no doubt it works, as has been proven through the decades and in combat. It can launch and retrieve aircraft of varying weights at a rate of about one every minute or two and do so simultaneously due to the angled deck.
  • 8. why not continue with steam?  It requires an enormous amount of energy to function, and it is energy-inefficient.  It requires considerable maintenance and a large crew to keep it functioning, especially in rough seas and potentially in combat conditions.  It is bulky and heavy, while space is limited even on a modern carrier; it is an open-loop system with no feedback to control its performance.  It can only handle a limited range of aircraft types, weights and launch/landing conditions The drawbacks includes the steam catapult requires a high volume of 1133 m3, and a weight of 486 metric tons.
  • 9. The new millennium have seen the development of an alternative technology for launching aircraft, the electro-magnetic (EM) catapult.  An EM launch system offers the requisite higher launch energy as well as substantial improvements in performance, light weight, less volume & high efficiency. The ability of an EM system to vary speed and thrust to meet the needs of the vehicle being launched makes a single catapult suitable for a wide range of aircrafts.
  • 10. 1.Linear Induction Motor:  The EMALS uses a linear induction motor (LIM), which uses electric currents to generate magnetic fields that propel a carriage along a track to launch the aircraft.  The linear induction motor consists of a row of stator coils with the same function as the circular stator coils in conventional induction motor.  When energized, the motor accelerates the carriage along the track. The EMALS 300-foot (91 m) LIM will accelerate a 100,000-pound (45,000 kg) aircraft to 240 km/h(150 mph).
  • 12.  During a launch, the induction motor requires a large surge of electric power that exceeds what the ship's own continuous power source can provide. The capacitors that are being used in this application are two 250V 12,000µF.  Each stator delivers up to 121 MJ (34 kWh) (approximately one gasoline gallon equivalent this is faster than steam catapults).A maximum-performance launch using 121 MJ of energy from each disk alternator slows the rotors from 6400 rpm to 5000 rpm which is a fly wheel.  The energy is recharged with in 45sec.The system then releases that energy up to 484 MJ in 2–3 seconds . Energy Storage System:
  • 13. During launch, the power conversion subsystem releases the stored energy from the disk alternators using a cycloconverter. The cycloconverter provides a controlled rising frequency and voltage to the LIM, energizing only the small portion of stator coils that affect the launch carriage at any given moment. 4.Control System: Operators control the power through a closed loop system . Hall effect sensors on the track monitor its operation, allowing the system to ensure that it provides the desired acceleration. The closed loop system allows the EMALS to maintain a constant tow force, which helps reduce launch stresses on the plane's airframe 3.Power Conversion System:
  • 15. The main principle used is Rail Gun Magnetic Effect which states  The current flowing in the rails produces a magnetic flux density between the rails, and this magnetic field interacts with the current flowing in the armature.  The resulting Lorentz force accelerates the armature together with the projectile along the rails. Cont…..
  • 16.  The capacitors that are being used in this application are two 250V 12,000µF which are not capable of being fully charged by a regular power supply, to charge some voltage doublers are used  The amount of charged stored is vary depending on weight of the armed carrier . Using PNPN SCR triggering is applied.  When current is flowing through the coil it generates a magnetic field around the piston that has an opposing magnetic charge of the coil repelling it through the channel at very high speeds.  Several switches are used in the circuit for safety including a charging switch and firing switch.  The control system for this project will all be done through Lab View which will apply the 1.7V to gate of the SCR to trigger the device.  After charged with in 2-3sec the aircraft is launched up to the weight of 22,000kgs
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  • 18. Advantages:  Compared to steam catapults, EMALS can control the launch performance with greater precision, allowing it to launch more kinds of aircraft, from heavy fighter jets to light unmanned aircraft.  Lower operating costs.  Require fewer people to operate.  Deliver more percent of energy than a steam catapult's.  90% power conversion efficiency.
  • 19. disadvantages : As in the case of EMALS ,air craft equipment is above the launch motor which may be affected by the electro magnetic emissions (highly sensitive by EMF). Handling should be very careful due to high currents. Highly skilled personal is required. Initial cost is very high and Fault clearance take time.
  • 20. Countries that are planning emals :  United States >EMALS was designed for and into the Gerald R. Ford-class aircraft carrier. And test runs on Feb 2020. French >Construction of the PANG is expected to begin around 2025 and will enter service in 2038.  China >According to a report in July 2017, the electromagnetic launchers used in the Type 003 aircraft carrier. And about to launch in 2021.  India >The Indian Navy has shown an interest in installing EMALS for its planned CATOBAR super carrier INS Vishal.  United Kingdom >UK were working on an electro-magnetic catapult (EMCAT) system for the Queen Elizabeth-class aircraft carrier.
  • 21. Applications : StarTram is a proposed space launch system propelled by maglev. The initial Generation 1 facility would launch cargo only. More advanced technology would be required for the Generation 2 system for passengers. The name itself indicates Runway towards Stars
  • 22. The idea is that by using electromagnetism to accelerate a bullet, you can overcome the limitations of gunpowder-style firearms, which generally top out at muzzle velocities of about 2,000 meters per second . Magnetic propulsion can in theory reach any speed; it is also silent, and with no explosive gases to disperse it can have an extremely high rate of fire.
  • 23. Rail guns use magnetic fields created by high electrical currents to accelerate a projectile to 5,400 miles an hour. The velocity is sufficient to give the EMRG an effective range of 110 nautical miles, or 126 miles on land. A new warship, the large surface combatant, is scheduled to eventually replace the Ticonderoga-class cruisers.
  • 24. Hyperloop is described as a sealed tube or system of tubes with low air pressure through which a pod may travel substantially free of air resistance or friction. Virgin Hyperloop,in the recent trial, two passengers - both company staff - travelled the length of a 500m test track in 15 seconds, reaching 172km/h.
  • 25. conclusion:  The EMALS is a very good solution, being surprisingly small and simple , with a manageable power electronics switching system.  The mechanical systems does not appear to provide sufficient advantage to make the extra complexity worthwhile, unless becomes a much more significant concern that has so far appeared.  The EMLS offers the increased energy capability necessary to launch the next generation of Applications in all sectors.  The only limitation is the power handling capability and vibration resistance material.  The challenge of this project will be to get the projectile up to a fast enough speed in a short time. ANY QUERIES???....