Difference Between Turbojet and Turbofan

The major difference between the turbojet and a turbofan lies in the operating mechanisms. Turbojet is a primal design of an air breathing gas turbine engine, whereas the turbofan is an advancement over it, and uses a fan to generate the thrust.

The efficiency of the turbojet is better at higher speeds only, but the efficiency if turbofan is good at all ranges of speed.

The turbojets produce much more noise than the turbofans.

The application spectrum of the turbofans is much more than the turbojets, which are mostly being used in military ships, missiles and aircrafts.

In turbojets, the thrust which causes propulsion totally depends upon the force of the exhaust gases, whereas in turbofans, bypass flow also helps in producing thrust.

Suggested: Difference Between Turbofan and Turboprop

Instructions

  • 1

    Turbojets

    Turbojets operate on the Brayton cycle. In this form of engine, cold air is inhales and is then compressed to a very high pressure, by passing it through an axial compressor, having many stages. The pressure of the air increases after every stage, and in modern models of this engine, it can reach up to 20:1.

    When the pressure of the air is increased, it also results in significant increase in temperature. The hot air is then used in the combustion process, resulting in the production of exhaust gases, having temperatures in the range of 1200 to 1250 degree centigrade.

    These hot gases are then directed to the turbine blades, which are mounted on a shaft, which is used to drive the compressor. The exhaust gases are then passed to a nozzle which increases its velocity.

    The major issues related with turbojets are that they are noisy and quite inefficient at subsonic speeds. In fact, the efficiency of the turbojets is only optimum after Mach 2.

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    Image Courtesy: airliners.net

  • 2

    Turbofans

    In this version, the shaft work is used to drive a huge fan, which results in a better air intake. Now, the air sucked by this fan is divided into two parts. One part of the air goes through the normal turbojet procedure to drive the shaft, after passing through a series of compressive stages, and the other part is used directly for propulsion.

    The ratio of the air allowed to go to the compressors to the air which is bypassed and helps directly in thrust protection is called bypass ratio. This ratio is set as per the specific requirement of the operation.

    Read More: Difference Between Subsonic and Supersonic

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