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a jet engine works on the principle of newton's


Jet Engine Basic Knowledge 
It is a gas turbine engine.  The jet engine does the opposite of the Newton 3rd law.  Jet engines squeeze large amounts of air and push it backward with more force.  Due to which the air accelerates backward.  From which an energy is produced.  And provides power to the jet engine to go ahead.


Jet Engine Inner part?
The jet engine has many different rotating parts.  And each part has different speed of rotation.  If the speed of low compressor rotating is much less than the high compressor.  So engine efficiency works.  And the optimum speed of Fernt Fenn is less than that.  So we use three types of rotating system in which Front Fan Low Pressure Compressor and High Pressure Compressor rotate at all different speeds, but most of the engin manufacturer is called two speed system called Tow spool design to avoid complex.  Let's do it.  Come know about this design.



Tow Spool Design Work?
In this design, the front fan, low pressure compressure and low pressure turbine are attached to the same rod.  So it rotates with the same speed.  Whereas high pressure compressure and high pressure turbine are connected by another stick.  This rod is hollow inside.  This stick is fite with the first stick.  Thus they rotate at different speeds without disturbing each other.


Front Fan Work?
This is the first part of a big fun turbo fan.  This fan splashes the maximum amount of air and increases its speed.  Most air is called Bypass Air.  Which is pushed out.  Due to which Thrust is generated.  In most jet eingen, this fan only produces 90% Thrust.  The remaining 10% air moves towards the center of Eingen.



flow compressure work?
An axle flow compressure is first installed in the code.  It passes through a low diameter tube while reducing air.  Due to which the air pressure and temperature becomes high.  As air moves forward in the compressure.  As such the ballad of compures gets smaller.  Which makes this compureer's ballade make the air more compuresed.


Type of Blades and work?
High pressure compressure rotates at a faster rate.  In which the presur and temperature of the air is greatly increased.  Axle Flow compressure has separate parts.  There is a section of rotating ballads called Rotor Blades.  There is a section of stationary blades called Staor Blades.  One after the other.  The Gurup of all these blades is called Stage.  Rotor Blades Rotor Drum are attached and Rotor Blades are fixed with Outer casing.  The ballad is designed in such a way that the wind enters the interior following the direction of the ballade, the shape of rotor and staor is of this type.  The area of ​​flow increases in the direction of flow.  And this is because.  Because the blade is bent towards the axial direction.


Stoar Blades and Rotors blades working? 
When the air enters the Stoar Blades, the air becomes dull as the Flow Aera increases.  And some kinetic energy of the air changes into pressure energy.  Likewise when air passes through rotor blads.  So as the flow aera increases, the velocity of the air relative to the blade decreases, so the air pressure increases.  While the Rotor Blade is rotating and accelerating the air.  And so the air exits at more absolute velocity.  Therefore, after passing through the air rotor blade, both the wind velocity and pressure increase.  This wind again passes through stoar blades and rotor blades with great velocity.  Due to which the valucity and pressure of the air increases further.  This process is repeated at each stage.  The velocity and pressure of the air increases further.


How to increase air velocity?
When the air enters the Stoar Blades, the air becomes dull as the Flow Aera increases.  And some kinetic energy of the air changes into pressure energy.  Likewise when air passes through rotor blads.  So as the flow aera increases, the velocity of the air relative to the blade decreases, so the air pressure increases.  While the Rotor Blade is rotating and accelerating the air.  And so the air exits at more absolute velocity.  Therefore, after passing through the air rotor blade, both the wind velocity and pressure increase.  This wind again passes through stoar blades and rotor blades with very high velocity. This process is repeated at each stage.  And in every stage, the pressure of air increases.


Fuel Mixed with hot Compresed Air?
This compressed air then enters the Combustion Chamber.  There are many nozzles in the Combustion Chamber to spray fuel into the air.  A mixture of air and fuel is ignited by a spark plug at the time of starting.  Once the combustion process starts it burns continuously.  This high pressure high temperature and burning gases pass through turbine ballot with great speed.  Whose balladas roam.  And exhaust gases transfer the energy to the turbine.  Due to which, these gases and the temperature pressure are reduced.  The high pressure compressor rotates as the high pressure turbine rotates.  Because they are attached to a single rod.  Similarly the low pressure turbine rotates the front fan and the low pressure compressure.  Exhaust gases pass through a nozzle before exiting.  Where the remaining energy of the exhaust gases is converted into a high speed jet by a nozzle.  Due to which the engine gets thrust to proceed.


Invention of Jet Engine
 Jet Engine was invented by Frank Whittle of Britain and Hans Von Dhain of Germany. The turbo Jet Engine was patented by Frank Whittle in 1930 and Hans Von Dhain designed and ran the first operational jet engine in 1937.
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Milan Tomic

Hi. I’m Designer of Blog Magic. I’m CEO/Founder of ThemeXpose. I’m Creative Art Director, Web Designer, UI/UX Designer, Interaction Designer, Industrial Designer, Web Developer, Business Enthusiast, StartUp Enthusiast, Speaker, Writer and Photographer. Inspired to make things looks better.

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