mist aero
TRANSCRIPT
AEROSPACE TECHNOLGYAEAV-433
Lec Akhter Mahmud Nafi [email protected]
Department of Aeronautical Engineering
Topics to be covered Types of Aero engine
Reciprocating Engine and their components.
Air breathing Aero engines:
Turbojet Turbo-prop Turbo-fan Hybrid Rocket Ramjet
Different Parts of Gas Turbine Engine
Intake Compressor Combustion Chamber nozzle Jet pipe Turbine Afterburner
Metallurgy of aero-engine components. Properties of Aviation fuel
Different Systems of aircraft
HydraulicPneumaticOxygenBrakeEngine controlCabin pressurizationAir conditioningEmergency SystemSafety Equipment Fire fighting System
MECHANICS AND THERMODYNAMIC PROPULSION- HILL & PETERSON (WISLEY)
AIRCRAFT GAS TURBINE ENGINE TECHNOLOGY – ERWIN TREAGER
GAS TURBINE THEORY – COHEN & ROGERSTHE JET ENGINE – ROLLS ROYCE LIMITEDAIRFRAME & POWER PLANT MECHANICS GENERAL
HAND BOOK –FAA, US DEPT OF TPTNPOWERPLANT TEXT BOOK - JEPPESENROCKET PROPULSION ELEMENTS- GEORGE SUTTON AERODYNAMICS – CLANCYMECHANICS OF FLIGHT- KERMODE
Reference Books
History Of Jet Engines
After world war II designers dreamed to invent an engine which can break the sound barrier (speed of sound) , which led to the discovery of gas turbine engines which was called as Jet engine.
With the development of gas turbine engine during second world war, New era of speed and altitude is revealed & Concept of intermediaries introduced
Dr. Hans von Ohain and Sir Frank Whittle were the pioneers behind today’s jet engines.
Introduction
• Jet engine is also called Gas Turbine Engine.
• • It works under the principle of Newton’s third
law which states that “For every acting force there is an equal and opposite force.’’
Jet Engine
• A jet engine is a machine designed for the purpose of creating large volumes of high velocity exhaust gases.
• This is done in order to overcome the aerodynamic drag of an airplane.
• In the process of producing high velocity exhaust, the engine also produces: Electrical Power Hydraulic Power Pneumatic power for air-conditioning & pressurization Hot Air for anti-icing protection
Basic Operation of a Jet Engine
The basic operations of Jet Engine are as follows:• Air enters the compressor where it is compressed.• Fuel is then added and ignited.• The resulting gas spins the gas turbine.• The turbine powers the compressor.• The gas then exists the engine at tailpipe.
The way a jet engine operates is similar to the way an automobile engine operates i.e.
• Intake• Compression• Ignition• exhaust
JET PROPULSION SYSTEM
When the work output of the gas turbine plant is used to produce high velocity jet of hot gasses and this jet is used to propel (to push or move something with a lot of force) the vehicles in which the systems are mounted, such systems are known as jet propulsion system .
Brayton Cycle
Gas turbine engines work on Brayton power cycle.
The air enters the compressor gets compressed and the compressed air enters in to the combustion chamber, where the fuel and air are mixed and burnt and passes through the turbine, exit through nozzle with high acceleration.
Brayton Cycle
Since fresh air enters the compressor at the beginning and exhaust are thrown out at the end, this cycle is an open cycle.
By replacing the combustion process by a constant pressure heat addition process, and replacing the exhaust discharging process by a constant pressure heat rejection process, the open cycle described above can be modified as a closed cycle, called ideal Brayton cycle. The ideal Brayton cycle is made up of four internally reversible processes.
• 1-2 Isentropic compression (in a compressor) • 2-3 Constant pressure heat addition • 3-4 Isentropic expansion (in a turbine) • 4-1 Constant pressure heat rejection
Brayton Cycle:
Types Of Jet Engines
ROTARY
• TURBO JET• TURBO PROP• TURBO FAN• TURBO SHAFT
ATHODYDS
• AEROTHERMODYNAMIC DUCTS ( NO ROTORS)
RAM JETPULSE JETSCRAM JET
THESE ARE NOT THE PRIME THRUST SOURCES……
Airbus A330
General Electric CF6-80E1Pratt & Whitney PW4000Rolls-Royce Trent 700 high-bypass turbofan engines
Lec Nafi
Lockheed Martin F-22 Raptor
Pratt & Whitney F119 (company designation PW5000[1]) is an afterburning turbofan engine