3. History of Jet Engines
• Sir Isaac Newton in the 18th century was the first to theorize that
a rearward-channeled explosion could propel a machine forward at a great
rate of speed. This theory was based on his third law of motion.
As the hot air blasts backwards through the nozzle the plane moves forward.
• Henri Giffard built an airship which was powered by the first aircraft engine,
a three-horse power steam engine. It was very heavy, too heavy to fly.
• In 1874, Felix de Temple, built a monoplane that flew just a short hop
down a hill with the help of a coal fired steam engine.
• Otto Daimler in the late 1800's, invented the first gasoline engine.
4. • In 1903, the Wright Brothers flew, "The Flyer", with a 12 horse power
gas powered engine.
• From 1903, the year of the Wright Brothers first flight,
to the late 1930s the gas powered reciprocating internal-combustion engine
with a propeller was the sole means used to propel aircraft.
• It was Frank Whittle, a British pilot, who designed the first turbo jet engine
in 1930.The first Whittle engine successfully flew in April, 1937.
This engine featured a multistage compressor, and a combustion chamber,
a single stage turbine and a nozzle.
• The first jet airplane to successfully use this type of engine was the
German Heinkel He 178 invented by Hans Von Ohain.
It was the world's first turbojet powered flight.
5. The W2/700 engine flew in the
Gloster E.28/39, the first British
aircraft to fly with a turbojet
engine, and the Gloster Meteor.
6.
7.
8.
9. A jet engine is an engine that
discharges a fast moving jet of fluid to
generate thrust in accordance with
Newton's third law of motion.
11. Working principle
Jet engines are also called as gas turbines. The
engine sucks air in at the front with a fan. A
compressor raises the pressure of the air. The
compressed air is then sprayed with fuel and an
electric spark lights the mixture. The burning gases
expand and blast out through the nozzle, at the
back of the engine. As the jets of gas shoot
backward, the engine and the aircraft are thrust
forward.
TURBO JET ENGINES
12.
13. Major components
• Air intake
• Compressors
• Combustors
• Turbines
• Nozzles
• Fuel system
• Cooling system
16. Fan-The fan is a first component in a turbo fan.
The large spinning fan sucks in large quantity of
air. Most of the fan blades are made up of titanium.
It then speeds this air up and splits it into two
parts. One part continues through the “core” or
center of the jet engine, where it is acted upon by
other jet engine components.
AIR INTAKE
17. The second part “bypasses” the core of the
jet engine. It goes through a duct which
surrounds the core to the back of jet engine
where it produces much of force that propels
the airplane forward. This cooler air helps to
quiet the jet engine as well as adding thrust
to the jet engine.
18.
19. Compressor - The compressor is the first
component in the jet engine core.
The compressor is made up of fans with many
blades and attached to a shaft. The compressor
squeezes the air that enters it into progressively
smaller areas, resulting in an increase in the air
pressure. This results in an increase in the energy
potential of the air. The squashed air is forced into
the combustion chamber.
20.
21. Combustor - In the combustor the air is mixed with fuel
and then ignited. There are as many as 20 nozzles
to spray fuel into the air stream. The mixture of air and
fuel catches fire. This provides a high temperature,
high-energy airflow. The fuel burns with the oxygen
in the compressed air, producing hot expanding gases.
The inside of the combustor is often made of ceramic
materials to provide a heat-resistant chamber.
The heat can reach 2700°.
22. Turbine - The high-energy airflow coming
out of the combustor goes into the turbine,
causing the turbine blades to rotate. The turbines
are linked by a shaft to turn the blades in the
compressor and to spin the intake fan at the front.
This rotation takes some energy from the high-energy
flow that is used to drive the fan and the compressor.
The gases produced in the combustion chamber move
through the turbine and spin its blades.
23. The turbines of the jet spin around thousands of
times. They are fixed on shafts which have
several sets of ball-bearing in between them.
24. Nozzle - The nozzle is the exhaust duct of the
jet engine. This is the jet engine part which actually
produces the thrust for the plane. The energy depleted
airflow that passed the turbine, in addition to the colder
air that bypassed the engine core, produces a force
when exiting the nozzle that acts to propel the engine,
and therefore the airplane, forward. The combination of
the hot air and cold air are expelled and produce an
exhaust, which causes a forward thrust.
25. The nozzle may be preceded by a mixer, which
combines the high temperature air coming from the jet
engine core with the lower temperature air that was
bypassed in the fan. The mixer helps to make the jet
engine quieter.
28. Turbo pumps are centrifugal pumps which are spun
by gas turbines and are used to raise the propellant
pressure above the pressure in the combustion
chamber so that it can be injected and burnt.
Turbo pumps are very commonly used with rockets,
but ramjets and turbojets also have been known to use
them.
Turbopumps
29. Due to temperature limitations with the gas turbines,
jet engines do not consume all the oxygen in the air
('run stochiometric'). Afterburners burn the remaining
oxygen after exiting the turbines, but usually do so
inefficiently due to the low pressures existing at this
part of the jet engine; however this gains thrust, which
can be useful.
Afterburners (reheat)
30. Thrust reversal, also called reverse
thrust, is the temporary diversion of
an aircraft engine's exhaust or
changing of propeller pitch so that
the thrust produced is directed
forward, rather than aft. This acts
against the forward travel of the
aircraft, providing deceleration.
Thrust reversers
31.
32.
33. Apart from providing fuel to the engine,
the fuel system is also used to control
propeller speeds, compressor airflow
and cool lubrication oil. Fuel is usually
introduced by an atomized spray, the
amount of which is controlled
automatically depending on the rate of
airflow.
Feul system
34. . It also increases the energy extracted
by the turbine which drives the
compressor even faster and so there is
an increase in air flowing into the
engine as well.
35. Cooling air then passes through complex
passages within the turbine blades. After
removing heat from the blade material,
the air (now fairly hot) is vented, via
cooling holes, into the main gas stream.
Cover plates are incoperated on blades
Cooling system
36. This acts as a centrifugal compressor to
pressurize the cooling air before it enters
the blade. Another solution is to use an
ultra-efficient turbine rim seal to
pressurize the area where the cooling air
passes across to the rotating disc.
