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Section 17.3

Propeller Pitch Control

The constant-speed propeller and governor, fine/coarse pitch, feathering and reverse.

Notes

Propeller pitch control, summary notes

Main ideas
  • A constant-speed propeller holds a selected RPM by automatically varying blade pitch: FINE (low) pitch gives high RPM for take-off and climb, COARSE (high) pitch gives low RPM for efficient cruise, like changing gear.
  • A governor controls it: spring-loaded flyweights sense engine RPM and meter (boosted) engine oil to or from the pitch-change piston in the hub. On-speed holds pitch; over-speed coarsens pitch; under-speed fines it, always driving RPM back to the set value.
  • FEATHERING turns the blades to about 90° (edge-on to the airflow) after an engine failure so the propeller stops windmilling and its drag is minimised, essential on multi-engine aircraft; springs/counterweights and accumulators drive feather/unfeather.
  • REVERSE pitch (a negative blade angle) is used on turboprops for aerodynamic braking and reverse thrust on landing; the low-pitch 'beta' range is used for ground handling.
  • Mechanisms are single-acting (oil pressure one way, a spring or counterweight the other) or double-acting (oil on both sides of the piston); a pitch-lock or feathering stop prevents unwanted movement.
  • ⚠ Exam trap: FINE pitch = high RPM (take-off), COARSE pitch = low RPM (cruise); feathering streamlines the blades (~90°) on a failed engine to cut drag; the governor's flyweights meter oil to the pitch-change piston.
Solved examples
  1. On a constant-speed prop the aircraft enters a descent and speeds up, yet the RPM stays constant. How does the governor achieve this?

    As the aircraft accelerates, the blades tend to speed up (over-speed). The governor's flyweights fly out, porting oil to increase blade pitch (coarser). The coarser blades take a bigger 'bite' of air, loading the engine more and bringing RPM back to the selected value, so RPM stays constant while pitch changes automatically.

Simulation

Constant-speed propeller & governor

Constant-Speed Propeller & GovernorFull screen ↗
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Mind map

Pitch control concept map

Propeller Pitch Control

Quiz

Propeller pitch control quiz

Propeller Pitch Control, quiz

Ref 17.38 of 17Pass 75%
  1. 1. A constant-speed propeller holds a selected RPM by:

    Varying the blade pitch as power and airspeed change
    Varying the engine fuel only
    Changing the reduction gear ratio
  2. 2. Feathering a propeller means:

    Turning the blades edge-on to the airflow
    Setting the finest pitch
    Stopping the governor
  3. 3. On a single-acting constant-speed propeller, loss of governor oil pressure usually causes the blades to move towards:

    Fine pitch
    Feather
    Reverse
  4. 4. On the rotating blade shown, force X acts radially outward along the blade. It is:

    XYZ
    Centrifugal force
    Thrust bending force
    Torque bending force
  5. 5. On the same blade, moments Y and Z act in opposite senses about the pitch axis. In practice:

    XYZ
    The centrifugal twisting moment is the larger, turning the blade to fine
    The aerodynamic twisting moment is the larger, turning the blade to coarse
    They are always equal and cancel
  6. 6. A constant-speed propeller holds a set RPM by:

    Automatically varying blade pitch
    Changing fuel flow only
    Applying a brake
  7. 7. Fine (low) pitch gives:

    High RPM, for take-off/climb
    Low RPM, for cruise
    Zero thrust
  8. 8. Coarse (high) pitch gives:

    Low RPM, for efficient cruise
    High RPM, for take-off
    Reverse thrust