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Accumulator
A device to aid in unfeathering a propeller.
Aerodynamic twisting moment
An operational force on a propeller which tends to increase the propeller blade angle.
Angle of attack
The angle between the chord line of a propeller blade section and the relative wind.
Anti-icing system
A system which prevents the formation of ice on propeller blades.
Automatic propeller
A propeller which changes blade angles in response to operational forces and is not controlled from the cockpit.
Back
The curved side of a propeller airfoil section that can be seen while standing in front of the airplane.
Blade
One arm of a propeller from the hub to the tip.
Blade angle
The angle between the blade section chord line and the plane of rotation of the propeller.
Blade station
A distance from the center of the propeller hub.
Boots
Ice elimination components which are attached to the leading edge of propeller blades.
Boss
The center portion of a fixed-pitch propeller.
Centrifugal force
The force on a propeller which tends to throw the blades out from the propeller center.
Centrifugal twisting moment
The force on a propeller which tends to decrease the propeller blade angle.
Chord line
The imaginary line which extends from the leading edge to the trailing edge of a blade airfoil section.
Comparison unit
The unit in a synchronization or synchrophasing system which compares the signals of the master engine and the slave engine and sends a signal to correct the slave engine speed or blade phase angle.
Constant-speed system
A system which uses a governor to adjust the propeller blade angle to maintain a selected RPM.
Controllable-pitch propeller
A propeller whose pitch can be changed in flight by the pilot's control lever or switch.
De-icing system
An ice elimination system which allows ice to form and then breaks it loose in cycles.
Effective pitch
The distance forward that an aircraft actually moves in one revolution of the propeller.
Face
The flat or thrust side of a propeller blade.
Feather
The rotation of the propeller blades to an angle of about 90 degrees which will eliminate the drag of a wind milling propeller.
Fixed pitch propeller
A propeller, used on light aircraft, whose blade angles cannot be changed.
Frequency generator
The engine speed signal generator for some synchronization systems.
Geometric pitch
The theoretical distance that an aircraft will move forward in one revolution of the propeller.
Governor
The propeller control device in a constant-speed system.
Ground adjustable propeller
A propeller which can be adjusted on the ground to change the blade angles.
Hub
The central portion of a propeller which is fitted to the engine crankshaft and carries the blades.
Leading edge
The forward edge of a propeller blade.
Pitch
The same as geometric pitch. Often used interchangeably with blade angle.
Pitch distribution
The twist in a propeller blade along its length.
Plane of rotation
The plane in which the propeller rotates, 90 degrees to the crankshaft centerline.
Propeller
A device for converting engine horsepower into usable thrust.
Propeller disc
The disc-shaped area in which the propeller rotates.
Pulse generator
The unit which generates a speed and blade position signal in a synchrophasing system.
Reversing
Rotation of the propeller blades to a negative angle to produce a braking or reversing thrust.
Safetying
The installation of a safety device such as safety wire or a cotter pin.
Selector valve
Propeller control unit in a two position propeller system.
Shank
The thickened portion of the blade near the center of the propeller.
Slip
The difference between geometric pitch and effective pitch.
Snap ring
A component of a splined or tapered shaft installation which is used to aid in removal of the propeller.
Spider
The central component on many controllable-pitch propellers which mounts on the crankshaft and has arms on which the blades are installed.
Synchronization system
A system which keeps all engines at the same speed.
Synchrophasing system
A refined synchronization system which allows the pilot to adjust the blade relative position as they rotate.
Tachometer
The speed sensing unit of some synchronization systems.
Thrust bending force
An operational force which tends to bend the propeller blades forward.
Tip
The portion of the blade farthest from the hub.
Torque bending force
An operational force which tends to bend the propeller blades in the direction opposite to the direction of rotation.
Two position propeller
A propeller which can be changed between two blade angles in flight.