types of jet propulsion engine
Post on 13-Sep-2014
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DESCRIPTION
There are 5 types of jet propulsion engine such as turbojet, turbofan, turboprop, turbo-shaft, and ramjet.Some types of jet propulsive engine are not cover in this slide such as pulse engine and rocket.TRANSCRIPT
TYPES OF JET
PROPULSION ENGINE
FACULTY OF MECHANICAL &
MANUFACTURING ENGINEERING
AIRCRAFT PROPULSION BDU 20203
By:
AMAL IQMAL BIN ADNAN
AD110189
2BDC
Lecture:
Dr. Mohammad Fahmi Bin Abdul Ghafir
http://dryicons.com/free-graphics/preview/blue-background
TURBOJET
ENGINE
http://purpleopurple.com/tourism/modern-wonders/concorde.html
SINGLE SPOOL TURBOJET
Optional: Afterburner, Convergent or Con/Di Nozzle
Compressors Turbine Combustion
Chamber
Inlet
•Basic turbojet engine invented by Sir Frank Whittle and Dr. Hans von Ohain •Turbojet engine is very powerful engine ever.
Nozzle/Exhaust
SINGLE SPOOL TURBOJET
WITH TWO COMPRESSORS
Axial
Compressors
Turbines
Burner
Nozzle/Exhaust Inlet
Centrifugal
Compressors
TWO SPOOL TURBOJET
Optional: Afterburner, Convergent or Con/Di Nozzle
HP
Compressors
HP Turbine
Combustor
Nozzle/Exhaust Inlet
LP
Compressors
LP Turbines
TURBOFAN
ENGINE
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SINGLE SPOOL MIXED FLOW
TURBOFAN
Optional: Afterburner, Convergent or Con/Di Nozzle
Compressors Turbines Combustion
Chamber Nozzle/Exhaust
Inlet
•At nozzle exit, fluid flow at primary and secondary nozzle are mixed.
TWO SPOOL TURBOFAN
LOW BYPASS RATIO
HP
Compressors
LP Turbines Burner
Divergent
Nozzle Air Intake
HP Turbine
LP
Compressors
THREE SPOOL TURBOFAN
LOW BYPASS RATIO
HP
Compressors
LP Turbine
Combustor
Divergent
Nozzle Air Inlet
HP Turbine
LP
Compressor
IP Turbine
IP
Compressors
VARIABLE CYCLE ENGINE
Optional: Afterburner, Convergent or Con/Di Nozzle
•A variable cycle engine (VCE) is an engine that is designed to operate efficiently under mixed flight conditions, such as subsonic, transonic and supersonic.
TWO SPOOL TURBOFAN
Fan
Nozzles Diffuser
HP
Compressors
LP Turbines
Combustion
Chamber
HP Turbine
2
1
GEARED TURBOFAN
TYPE A
HP
Compressors
LP Turbines
Burner
Diffuser
LP
Compressors
HP Turbine
Fan
Gear
Nozzles 2
1
GEARED TURBOFAN
TYPE B
HP
Compressors
LP Turbines
Combustor
Diffuser
LP
Compressors
HP Turbine
Fan
Gear
Nozzles 2
1
Centrifugal
Compressors
THREE SPOOL TURBOFAN
HP
Compressors
LP Turbines
Combustion
Chamber
Diffuser
HP Turbine
LP Fan
IP Turbine IP
Compressors
Nozzles 2
1
INTERCOOLED RECUPERATED
TURBOFAN
Optional: Intercooler, Recuperator
HP
Compressors
LP Turbines
Burner
Diffuser
HP Turbine
LP Fan
IP Turbine IP
Compressors
Intercooled
Nozzles 2
1
MIXED FLOW TURBOFAN
HP
Compressors
LP Turbines
Combustor
Mixed Nozzle Diffuser
HP Turbine
Fan
LP
Compressors
GEARED MIXED FLOW
TURBOFAN A
HP
Compressors
LP Turbines
Combustion
Chamber
Exhaust Diffuser
HP Turbine
Fan
Gear
LP
Compressors
GEARED MIXED FLOW
TURBOFAN B
HP
Compressors
LP Turbines
Burner
Nozzles
Diffuser
HP Turbine
LP Fan
LP
Compressors
Gear
Centrifugal
Compressors
THREE SPOOL MIXED FLOW
TURBOFAN
HP
Compressors
LP Turbines
Combustor
Nozzles Diffuser
HP Turbine
LP Fan
IP Turbine
IP
Compressors
TURBOPROP
ENGINE
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SINGLE SPOOL TURBOPROP
Optional: Recuperator
Compressors
Combustion
Chamber
Exhaust
Turbines
Propeller
Gear
Intake
TWO SPOOL TURBOPROP
Optional: Recuperator
HP
Compressors
LP Turbines
Burner
Exhaust
Intake
HP Turbine
Propeller
Gear
TURBOPROP
BOOSTER ON HIGH PRESSURE SPOOL
Optional: Intercooler, Recuperator, Sequential Combustion
HP
Compressors
LP Turbines
Combustor
Exhaust
Intake
HP Turbine
Propeller
Gear
TURBOPROP
BOOSTER ON LOW PRESSURE SPOOL
Optional: Intercooler, Recuperator, Sequential Combustion
HP
Compressors
LP Turbines Combustion
Chamber
Exhaust Intake
HP Turbine
Propeller
Gear
LP
Compressors
THREE SPOOL TURBOPROP
HP
Compressors
LP Turbines
Burner
Nozzle/Exhaust Intake
HP Turbine
Propeller
IP Turbine
IP
Compressors
Gear
TURBOSHAFT
ENGINE
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TURBOSHAFT ENGINE
FOR POWERING HELICOPTER
RAMJET
http://www.urban75.net/forums/threads/309th-aerospace-maintenance-and-regeneration-group-aka-plane-graveyard.298730/
http://www.wvi.com/~sr71webmaster/schematic.html
RAMJET
(A GAS TURBINE WITHOUT COMPRESSOR AND TURBINE)
Optional: Convergent or Con/Di Nozzle
•Most powerful engine and the highest thrust produces than turbojet but it work most efficiently at speeds around Mach 3.
SCRAMJET
OPERATES AT MACH 4 AND ABOVE
NOTATION
LP = Low Pressure
IP = Intermediate Pressure
HP = High Pressure
1 = Primary Nozzle
2 = Secondary Nozzle
= Low Pressure Shaft
= Intermediate Pressure Shaft
= High Pressure Shaft
REFERENCES
1. http://www.gasturb.de
2. http://muhammadhuzaim.blogspot.com/2010/06/turbin
e-engine-lessons-cont.html
3. http://www.flightlearnings.com/2010/03/06/types-of-
turbine-engines
4. http://www.ifs.tohoku.ac.jp/enerdyn/en/en_researches_
supersonic.htm
5. http://www.okieboat.com/How%20the%20ramjet%20w
orks.html
6. http://en.wikipedia.org/wiki/Variable_Cycle_Engine
7. http://spaceflight.esa.int/impress/text/pop-up/trent.html