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Propulsion Devices (Engines)
Air-Breathing
Use atmospheric
air (+ some fuel)
as main propellant
Rockets
Carry entire propellant
(liquid/solid fuel + oxygen)
Piston, Gas Turbine
and Ramjet Engines
Jet-engine.ppt, 10-7-01
Gas Turbine Engines (most aircraft jet engines):
• Use high-temperature gases to power a propeller or
produce direct thrust by expanding and accelerating the
exhaust gases through a nozzle.
• Three main types: Turbojet, Turbofan and Turboprop
Jet Engines – Basic Operation
• Air enters the trough the intake duct (cowl).
• Air compressed by passage through the compressor.
• Mixed with fuel in the combustion chamber.
• Fuel is ignited, Pressure and Temperature
raised
• Some of the pressure used to turn a turbine;
• Turbine shaft drives the compressor.
• Hot, high pressure air forced through a nozzle.
• The reaction force is the engine thrust.
Jet Engine – Common Types
• Turbojets:
• Turbine used to drive the compressor.
• All intake air passes through the combustion chamber and exits through the nozzle.
• All thrust produced by hot, high-speed exhaust gases.
•Turbofans (Fan-Jet):
• A large propeller in the intake cowl, in front of compressor.
• Dramatically increases the amount of air pulled in the intake.
• Only a small percentage passed through the engine, the rest of cold air is Bypassed.
• Part of the thrust through the hot exhaust gases and part by the cold bypassed air.
Produces cooler exhausts and quieter engines.
• High by-pass ratio are most commonly used in larger commercial aircraft.
•Turboprops:
• Jet engine used to turn a large propeller, which produces most (90% or more) of
the thrust. Used in smaller aircraft.
Jet Engine – Common Types
Pratt-Whitney
Engine Gallery
GE90 Engine
Jet Engine Combuster
Film cooling via convection
One annular section
Turbulent flame (fuel self-ignited)
• Use spark plug to start the engine
and re-light after flameout
Flame stabilization

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Jet engine

  • 1. Propulsion Devices (Engines) Air-Breathing Use atmospheric air (+ some fuel) as main propellant Rockets Carry entire propellant (liquid/solid fuel + oxygen) Piston, Gas Turbine and Ramjet Engines Jet-engine.ppt, 10-7-01 Gas Turbine Engines (most aircraft jet engines): • Use high-temperature gases to power a propeller or produce direct thrust by expanding and accelerating the exhaust gases through a nozzle. • Three main types: Turbojet, Turbofan and Turboprop
  • 2. Jet Engines – Basic Operation • Air enters the trough the intake duct (cowl). • Air compressed by passage through the compressor. • Mixed with fuel in the combustion chamber. • Fuel is ignited, Pressure and Temperature raised • Some of the pressure used to turn a turbine; • Turbine shaft drives the compressor. • Hot, high pressure air forced through a nozzle. • The reaction force is the engine thrust.
  • 3. Jet Engine – Common Types
  • 4. • Turbojets: • Turbine used to drive the compressor. • All intake air passes through the combustion chamber and exits through the nozzle. • All thrust produced by hot, high-speed exhaust gases. •Turbofans (Fan-Jet): • A large propeller in the intake cowl, in front of compressor. • Dramatically increases the amount of air pulled in the intake. • Only a small percentage passed through the engine, the rest of cold air is Bypassed. • Part of the thrust through the hot exhaust gases and part by the cold bypassed air. Produces cooler exhausts and quieter engines. • High by-pass ratio are most commonly used in larger commercial aircraft. •Turboprops: • Jet engine used to turn a large propeller, which produces most (90% or more) of the thrust. Used in smaller aircraft. Jet Engine – Common Types
  • 6. Jet Engine Combuster Film cooling via convection
  • 7. One annular section Turbulent flame (fuel self-ignited) • Use spark plug to start the engine and re-light after flameout Flame stabilization