workingofturbojet pdf v1

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    Turbojet Engine

    Applied Thermodynamics

    A jet engine having a turbine-drivencompressor and developing thrust from theexhaust of hot gases is a turbojet engine.

    This topic illustrates the working of aturbojet engine.

    Turbojet Engine

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    Turbojet Engine

    Applied Thermodynamics

    Thermodynamic Cycles

    Two Isothermal processes and two adiabaticprocesses constitute a carnot cycle.

    Two Adiabatic processes and two Constantpressure processes constitute a Brayton cycle.

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    Turbojet Engine

    Applied Thermodynamics

    Brayton cycle is represented in P-v and T-s diagrams

    Thermodynamic Cycles

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    Turbojet Engine

    Applied Thermodynamics

    Working of a Turbojet Engine

    In a turbojet engine, air enters axially into the rotor at state 1 and leaves the stator rotor assembly inAxial direction at state 2.

    Axial Flow Compressor (process 1-2)

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    Turbojet Engine

    Applied Thermodynamics

    Working of a Turbojet Engine

    Then, air enters the combustion chamber in which fuel is mixed with air.

    High energy igniter supplies necessary spark at the starting of the cycle.

    Combustion Chamber (process 2-3)

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    Turbojet Engine

    Applied Thermodynamics

    Working of a Turbojet Engine

    The burnt Air fuel mixture is expanded in an Axial flow turbine.

    The work output of turbine is equal to work input of compressor.

    So, net work done by the Turbojet engine is Zero.

    Axial Flow Turbine (process 3-4)

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    Turbojet Engine

    Applied Thermodynamics

    Working of a Turbojet Engine

    High pressure gases expand through nozzle which converts all pressure energy to Kinetic Energy.

    Nozzle (process 4-5)

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    Turbojet Engine

    Applied Thermodynamics

    Working of a Turbojet Engine

    High Velocity jet of gases coming out of Nozzle gives the necessary thrust to move the engine forward.(Newtons Third law of motion).

    Pressure Velocity variation in nozzle

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    Turbojet Engine

    Applied Thermodynamics

    Resources

    Books:

    1. Gas Turbines by Cohen and Rogers2. IC Engines and Gas Turbines by Gill Smith

    Reference Links:

    1. www.asme.org

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    Turbojet Engine

    Applied Thermodynamics

    What is the difference between Rockets and jetengines?

    Jet engines work on Newtons III law of motion

    Turbojet is an external combustion engine

    Rockets operate at higher mach number than jetengines

    Jet engines are self breathing engines

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    Turbojet Engine

    Applied Thermodynamics

    Net Work Output of Turbojet engine is

    Same as Compressor Work

    Same as turbine Work

    Zero

    Equal to Wc- Wt

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    Turbojet Engine

    Applied Thermodynamics

    Inlet temperature of air entering Turbojet depends on

    Altitude of operation of flight

    Monsoon conditions

    Climatic conditions

    It is always constant

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    Turbojet Engine

    Applied Thermodynamics

    Where do we see the application of Turbojet engine?

    Civil Aircrafts

    Submarine

    Helicopters

    Rockets

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    Turbojet Engine

    Applied Thermodynamics

    Answer Key

    14

    13

    32

    31

    Answer(s)Question No.