 FAN  COMPRESSOR  COMBUSTOR  TURBINE  MIXER  NOZZLE.

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Presentation transcript:

 FAN  COMPRESSOR  COMBUSTOR  TURBINE  MIXER  NOZZLE

Inlet- inlet is the opening at the front of engine, it allows the outside air to enter the engine. Compressor – compressor is made up of fans with many blades, it compress the air and raises the pressure & temperature of the air, the compressed air then is delivered to the burner.

 Burner – Burning process occur here. Fuel is sprayed to the compressed air.The mixture of the fuel + air will be burned. The results is heated gas with high energy, high pressure and high temperature.  Turbine- turbine used some of the heated gas energy to turn the compressor. This energy is transferred through the shaft.  Nozzle- The balance of heated gas energy exits through the nozzle at very high speed. This causes thrust.  As the jets of gas shoot backward, the engine and the aircraft are thrust forward. (Newton 3 rd Law)

Compressor Turbine

Compressor Turbine Combustion Products Fuel Air

 ~0.3  ~ 1.0 T>2000 K

Single Can Tubular or Multi-Can Tuboannular Can-Annular Annular