WingWise
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M17

Propeller

Propeller theory, construction, pitch control, synchronising, ice protection and maintenance.

CAT A
CAT B1

Showing content mapped to EASA Part-66. Change authority in the header.

01

Propeller fundamentals

A propeller is a rotating aerofoil that converts engine torque into thrust. Geometric pitch is the distance advanced in one revolution in theory; effective pitch is the actual distance; the difference is slip. Blades are twisted (washout) so the angle of attack is roughly constant along the span because tip speed is much higher than root speed.

02

Forces on a propeller

Centrifugal twisting moment tries to reduce blade angle (fine); aerodynamic twisting moment tries to increase it (coarse). Centrifugal force is the largest static load. Torque reaction, gyroscopic precession, asymmetric blade effect (P-factor) and slipstream all affect aircraft handling.

03

Pitch control systems

Fixed pitch is efficient only at one condition. Variable-pitch/constant-speed propellers use a governor that senses RPM with flyweights and meters oil to the pitch-change mechanism to hold the selected RPM. Single-acting units use oil against a spring/counterweight; double-acting use oil on both sides. Feathering turns blades edge-on to minimise drag after an engine failure; reverse pitch provides braking on landing. Beta range gives direct blade-angle control on the ground.

04

Synchronising & synchrophasing

Synchronising matches the RPM of all propellers to remove beat noise. Synchrophasing additionally holds a fixed blade-phase relationship between propellers to minimise cabin noise and vibration. Auto-feather and negative-torque sensing systems protect against drag from a failed engine.

05

Ice protection & installation

Propeller de-icing may be electrical (heating elements bonded to blade leading edges, cycled by a timer through slip rings and brushes) or fluid (glycol slinger ring). Installation includes correct flange fitting, torque, and static/dynamic balancing to reduce vibration.

06

Inspection & maintenance

Inspect for nicks, gouges, cracks, corrosion, delamination on composite blades, and blade track. Damage is blended out within the manual's limits and re-protected; never straighten a bent aluminium blade in the field. Track is checked with a fixed reference and must be within limits (typically 1/16 in). Overhaul is calendar and hours driven; a propeller strike requires engine and propeller inspection per the manufacturer's instructions.

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