aircraft engine part1
DESCRIPTION
A quick introduction to brayton cycle and engines in airplanesTRANSCRIPT
How Does Engine Work ?
Part one
Why do we need Engines ?
● Mechanical Power.
● Bleed air.
● Thrust force.
Aircraft Engines Types
● Turbojet
● Turbfan
● Turboprop
Working Cycle
The principles of Engine are the same whatever
old or very modern engine.
Pressurization.
Adding Heat.
Expansion.
Brayton Cycle
Pressurization
● Here the engine does work on gas " air flow "
● It converts the kinetic energy " Velocity " into
pressure energy " static pressure".
● Also , the wok of compressor increases the total
pressure of flow.
● Compressors in this stag are to be assumed
adiabatic.
● Most of civil aircraft compressors are axial
compressors.
Pressurization Cont'd
● Now most of airplanes engines are turbofan
because of its efficiency in this flight regime for
civil big airplanes.
● The airflow is to be pressurized due to ram
effect and this is done by intake.
● Then it passes through fan which is the major
part for thrust.
● After this , flow is to be divided according to
bypass ratio=Fan secondary flow / core primary
flow by passing over splitter
Pressurization Cont'd
● The air flow is to be compressed over two
stages of compressors.
● Low pressure compressor and High pressure
compressor.
● The reason of using two compressors is to
avoid stall or surge during starting the engine.
● Now there is three spool (compressors) working
engines such as Trent series.
800Trent
Combustors
● Types of Combustion chambers
● Annular
Combustors Cont'd
● Can
Combustors Cont'd
● Can Annular
Combustors Cont'd
The benefits of can combustor is maintainability.
But the disadvantage is that if one can is to stop
working properly during flight how much the
damage will be on turbine blade because of
change of temeprature.