AFT aero and systems notes Flashcards
What are the 4 types of reaction engines?
Rocket
Ram Jet
Pulse Jet
Gas Turbine
What is a rocket?
Self contained air and fuel in pressurised container
What is a ram jet? What entry and exhaust duct type does it have?
No moving parts, requires large forward speed to operate
Divergent entry duct
Convergent exhaust duct
What is a pulse jet?
Similar to Ram jet but on intermittent cycle
What is a gas turbine?
Turbine driven compressor. Does not require forward airspeed to compress the air entering the engine
What is maximum thrust of a gas turbine limited by?
The maximum turbine temperature
If there was a large increase in gas temperature from the air intake to the turbine, what happens to the volume of gas, acceleration of the air and thrust produced?
Volume of gas increases
Acceleration of air increases
Thrust produced increases
What happens to thrust as air temperature increases?
Thrust decreases
What happens to thrust as altitude increases?
Thrust decreases due to less dense air
What happens to thrust if the mass air flow decreases?
Thrust decreases
What is the thrust formula?
Thrust = (Mass airflow X Jet exhaust velocity) - Aircraft forward speed
Describe a basic pure turbo jet.
One or more compressors driven by set of turbine wheels.
What is a spool?
Compressor at the front of an engine and its accompanying set of turbine wheels at the rear
How does a pure turbo jet deliver its thrust?
Reaction to the rearwards acceleration of exhaust gases after it has passed through the turbine sections of the engine
What happens to the static pressure at the exhaust outlet of pure turbo jet compared to the intake?
Roughly double
What is the EPR?
Engine pressure ratio.
Static pressure at the exhaust outlet compared to that at the intake
What indication does the EPR give to pilots?
Thrust output
What would a blocked EPR cause to the gauge?
Cause it to overread
Describe the basic high by-pass jet (turbo fan)
Not all air passes through the engine core and combustion chamber. Large fan (N1) is at the front of the compressor and driven by extra turbine at rear of engine
What is the by-pass ratio?
Ratio of air which bypasses the engine core compared to the air which passes through the core
What is the formula for the by-pass ratio?
By-pass ratio = (By-pass mass flow) / (Engine core mass flow)
What would an engine sound like, efficiency be with a high by-pass ratio?
Quieter and more efficient
Where is the majority of thrust produced in a high by-pass ratio engine?
From the by-pass fan air
Where is the majority of thrust produced in a low by-pass ratio engine?
From the jet exhaust