15.1 FUNDAMENTALS👌🏼 Flashcards
Explain potential energy and formula
- energy at rest/energy that is stored
- PE = mgh
Explain kinetic energy and formula
- energy in motion
- KE = 1/2 x mass x velocity^2
Newton’s first law
- law of inertia
Newton’s second law
- F=ma
- interplay between force and motion
E.g thrust proportional to mass of airflow through engine x acceleration of air through engine
Newton’s third law
- law of action and reaction
Explain the Brayton cycle
-thermodynamic cycle of gas turbine engine that produces thrust
- has 4 stages (intake, compression, expansion and exhaust)
Explain what occurs at intake (suck)?
- air enters at constant volume.
- Leaves intake at increased pressure and a decrease in volume.
Explain compressor (squeeze) ?
- air received from intake at slightly increased pressure, with slight decrease in volume
- air leaves compressor with increased pressure and decrease in volume
Explain expansion (bang)?
- takes place in combustion chamber
- pressure remain constant, but marked increase in volume
- expanding gases turn turbine which converts velocity energy to mechanical energy.
Explain exhaust (blow) section?
- convergent duct
- converts expanding volume and decreasing pressure of gases to a final high velocity
Along the line from 0-2 what change of state occurs
Isentropic compression
Pressure increases, volume decreases
Process from 2 to 3 what change of state occurs
Isobaric heating
What change of state in lines 3 to 5
Isentropic expansion
What occurs from process 0-5
Isobaric heat release into nozzle
Formula for force
F = ma
What is the formula for work done
W = force x distance
Formula for power
- power = Force x distance/time
- power = work/time
What is the unit for power
Watt
What is 1Nm/s in W
1
What is the 1Nm in Joules
1
What is the difference between speed and velocity
Speed refers to how fast a object is moving
Velocity refers to speed and direction
Explain acceleration
-Rate of change of velocity
-change in velocity (m/s) / time (s)
-m/s^2
What are the 2 different types of aircraft engines
- Piston type engines
- Gas turbine engines
Which engines performance decrease at higher altitudes
Piston engines
Are piston engines or gas type engines more fuel efficient
Piston engines
Which engine can operate at very high altitudes
- gas turbines engines
Explain turbojet engines
- high aircraft speeds but very loud
- has problems with noise and fuel consumption in speed range of 0.8 Mach
Pros: simple design, very high speeds
Cons: high fuel consumption, loud, poor performance at low speeds
Explain turbofan engine
- high aircraft speeds possible with good engine efficiency
- produces around 80% thrust
- quieter and better fuel consumption
Explain a spool arrangement
- consists of a turbine driving a compressor through a shaft
Explain twin-spool arrangement?
- high pressure turbine driving the high pressure compressor
- low pressure turbine driving the low pressure compressor and fan
Explain 3 spool arrangement
- high pressure turbine driving high pressure compressor
- Intermediate pressure turbine driving intermediate compressor
- low pressure turbine driving the fan
Advantages of turbo fan engine
- fuel efficient
- quieter
- streamlined appearance
Disadvantages of turbofan
- heavy
- large
Explain turboprop engines
- produce shaft horsepower only, which is used to drive propeller
- extra turbines
- reduction gearbox to drive propeller
Advantages of turboprop engine
- very fuel efficient
- efficient at mid-range speed and altitude
Disadvantages of turboprop engine
- limit forward airspeed
- gearing systems are heavy and can break down
Explain turboshaft engine
- produces shaft power to drive machinery
- requires small, powerful, lightweight engine
- e.g. APU supply electric and pneumatic power
Advantages of turboshaft engine
- higher power to weight ratio
- smaller than piston engines
Disadvantages of turboshaft engine
- loud
- gear systems are complex and can break down
Explain ‘cold section’
Parts of engine from the inlets up through compressors/diffusers
Explain ‘hot section’
- refers to ares past the compressors from combustion chamber through exhaust
What is the unit of force in the English system measured in
- lbs (pounds)