Turbo Jet Engines

By Kajal Vats|Updated : September 16th, 2021

Hello Aspirants!

Hope you all are Safe and Healthy!

As we already discussed  Jet Engines & their types and working in our previous article. In continuation with that here in this article, we are going to tell you all about one of the types of Jet Engine: Turbo Jet Engines.

 

Hello Aspirants!

Hope you all are Safe and Healthy!

As we already discussed  Jet Engines & their types and working in our previous article. In continuation with that here in this article, we are going to tell you all about one of the types of Jet Engine: Turbo Jet Engines.

 The Turbojet is an airbreathing type jet engine, typically used in aircraft. It produces all of its thrust by ejecting a high energy gas stream from the engine exhaust nozzle. 

Basic Components of Turbojet Engines:

  • Inlet,
  • The Gas turbine engine
  • A compressor
  • A combustion chamber
  • A turbine
  • The exhaust nozzle

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Working of a Turbojet Engine:

  • Air is drawn into the engine through the inlet and compressed and heated by the compressor.
  • Fuel is then added to the combustion chamber and ignited.
  • The burning fuel adds energy to the exhaust stream by heating and expanding the air.
  • Sufficient energy to drive the compressor is extracted from the exhaust stream by the turbine.
  • The remainder of the exhaust energy is used to produce thrust, a process that is enhanced by the geometry of the exhaust nozzle.
  • As the exhaust gas passes through the nozzle, it is accelerated to high speed as it expands thus providing propulsion.
  • The thrust produced by the engine can be selectively increased by incorporating an afterburner or re-heat into the engine design.

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Turbojets Aircraft:

  • Turbojet aircraft work on the principle of accelerating a relatively small mass of air to a high speed.
  • As optimum efficiency is achieved when the speed of the accelerated air approximates that of the aircraft, turbojet engines do not reach peak efficiency until speeds approaching Mach 2.
  • For sub-mach speeds(a ratio between true air speed & local speed of sound), a turbofan engine is significantly more efficient and also much quieter due to the greater mass and lower speed of the exhaust stream leaving the engine.

Advancements:

  • Turbojet are highly efficient for supersonic aircraft but their efficiency is very low for low speeds therefore they are used for high speeds only.

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