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Propeller Performance Metrics
are measurements used to evaluate how efficiently and effectively a propeller converts engine power into thrust
Time between overhaul
5-7 years or 1,500 to 2,000 flight hours
TBO
Air resistance
acts against the rotation of the propeller blades
profile drag
Induced drag
2 types or drag
Friction
It is the force that resists motion when two surfaces touch each other
Noise
It is the sound produced when a propeller rotates and disturbs the air
Propeller Slip
Air is compressible and not solid
Propeller Thrust
is the forward force produced by a spinning propeller that pulls (or pushes) the aircraft through the air
Power Output
It is the power produced by the engine to turn the propeller and create thrust
Brake horse power (BHP)
Power measured at the engine crankshaft
Shaft horsepower (SHP)
Power delivered to the propeller shaft
Thrust horsepower (THP)
Useful power that actually moves the aircraft forward
Propulsive Efficiency
Measures how effectively a propeller converts engine shaft power into useful thrust power that moves the aircraft forward
Fuel consumption
refers to how much fuel the engine burns to produce power that turns the propeller and generates thrust.
Although the engine burns the fuel, it greatly affects how much fuel is needed to maintain flight.
Advance Ratio
It is a dimensionless parameter that represents the ratio of aircraft forward velocity to the product of propeller rotational speed and diameter.
It measures how far the propeller "advances" in one revolution.
Propeller Efficiency
is the ability of the propeller to convert engine shaft power into thrust power
Blade Pitch
is the theoretical distance a propeller would move forward in one complete revolution if it were moving through a solid material
Low pitch & high pitch
Types of blade pitch
Low pitch
has a smaller pitch angle and is commonly used during takeoff to produce maximum thrust
High pitch
has a larger pitch angle and is commonly used during cruising to improve efficiency.
Angle pitch
is the angle between the propeller blade chord line and the plane of rotation
Pitch angle is small
▪Blade cuts the air easily
▪Propeller spins faster
▪Used for takeoff
pitch angle is large
Blade pushes more air backward
Propeller spins slower
Used for cruise
Slip
It is the difference between the theoretical distance a propeller should move forward in one revolution and the actual distance the aircraft moves forward
Torque
is the twisting force produced by the engine that rotates the propeller about its axis.
In an aircraft engine, ____ is produced by the engine crankshaft and transmitted to the propeller, causing it to spin and generate thrust
Tip speed
It is the linear velocity of the propeller blade tip as it rotates around the propeller hub
Propeller diameter
Propeller rotational speed (RPM)
Tip depends on?
▪Shock waves form
▪Drag increases
▪Propeller efficiency decreases
▪Noise increases
Problems that occur when tip speed becomes too high
Flanged shaft installation
a common method used to attach a propeller to the engine crankshaft in many light aircraft
The crankshaft has a flat circular flange, and the propeller hub is bolted directly to this flange using high-strength bolts and nuts
Tapered Shaft Installation
uses a cone-shaped shaft where the propeller hub slides onto the taper and is tightened with a large nut.
When the nut is tightened, the hub grips the shaft very tightly due to the tapered friction fit.
Splined Shaft Installation
It has longitudinal grooves (splines) along its surface
Splines
propeller rotates with the shaft without slipping
a method where the engine shaft and the propeller hub have matching grooves called?