17.1 Fundamentals Flashcards
How does a propeller generate thrust?
Pushing a large amount of air back slowly.
Define a propellor.
A device, with a rotating hub with 2 or more rotating blades to propel the aircraft.
Define a hub.
The central portion of a propeller which carries the blades.
Define a blade.
Aerofoil section that is attached to the hub.
Define the blade butt.
The base of the propeller where the root ends.
Define the blade root/shank.
The thickened portion of the blade nearest to the hub.
Define a blade station.
What’s it measured in?
A distance measured from the centre of rotation.
Measured in inches or centimetres.
Where the master reference station on a fixed pitch propeller?
Normally 75% from the centre of rotation.
Where is the master reference station on a variable pitch propeller?
50-75% from the centre of rotation.
Where are blade measurements take from?
Blade master reference station.
Define blade face?
The flat thrust producing side of a propeller blade.
Define the blade back.
The curved side of the propeller blade facing the direction of flight.
Define the blade chord line.
A line through the blade profile at the points between the face and back surfaces.
Define the plane of rotation.
What angle?
The plane in which the propeller rotates. This is 90° to the engine centreline.
Define the blade angle.
The angle between the blade chord line and the plane of rotation.
Define the pitch?
Distance advanced in one complete revolution.
Define the pitch change mechanism.
Device to alter blade angle.
Define a fine/ low pitch.
Vertical blade angles.
Define a coarse/ high pitch.
Horizontal blade angles.
Define a reverse pitch.
Turning the blades to a negative angle to produce braking or reversing thrust.
What does the dome assembly do?
Encases the pitch change mechanism.
Define a spinner.
An aerodynamic fairing that covers the centre of the propeller.
Where is a tractor propeller mounted?
In front of the wing LE or nose of the aircraft.
Where is a pusher propeller mounted?
Behind the wing trailing edge or rear of the fuselage.