The compressor receives energy to rotate from the turbine which is placed right after the combustion chamber, the compressor and turbine are attached to equal portions, the high energy fluid leaving the combustion chamber makes the turbine blades spin, as you can see the turbine blades have a special air foil shape which creates lift and makes it spin.
The pressure also decreases as the turbine absorbs energy from the liquid, our goal is achieved through these steps the really hot and high speed air emitted from the engine output the engine cover chamber becomes narrower towards the outlet which then results in an even greater jet speed, in short operation Synchronized combustion chamber compressors and turbines allow the aircraft to move forward.
Modern aircraft use a slightly improved turbine compressor arrangement and are called two tens, two independent turbine compressor stages are used in this section, the outer turbine compressor shaft passes through the interior concentrically, the outer turbine is made into a low energy fluid object and will run at a faster speed. lower than the turbine in the lower cross section of the lower-velocity vane this lower speed helps reduce the centrifugal pressure induced at the base thereby increasing the resistance of the propeller.
Some modern aircraft even use three ten engines, the engines we have discussed so far are more specifically referred to as turbojet engines. Turbojet engines tend to produce high noise levels, revolutionary improvements were made to these engines by installing a large fan which has a low pressure ten, the engine this type is called a turbofan engine and almost every commercial aircraft uses this engine.
