17.6.1 Propeller Balancing Flashcards
What causes propeller roughness?
Bent blades, blades out of track, imbalance, loose mounting, out of tolerance blade angles, and spinner imbalance.
What are the three types of propeller balancing?
Static Balancing, Dynamic Balancing, Aerodynamic Balancing.
What is static balance?
A body is in static balance when its center of gravity lies on the axis of rotation.
How is static balancing carried out?
It is done off the aircraft using a mandrel on stable knife edges or rollers, checked in horizontal and vertical planes.
How can horizontal imbalance be corrected in fixed pitch wood propellers?
By applying varnish or paint to the light blade or adding solder to the metal tipping.
How is vertical imbalance corrected in fixed pitch wood propellers?
By adding weights to the hub.
How are fixed pitch metal propellers statically balanced?
By removing metal from the heavy side and refinishing with a protective coating.
What is the general permissible tolerance for propellers of aircraft up to 5700 kg?
2 gm (0.070 oz), but manufacturer specifications are binding.
How are metal and composite variable pitch propellers balanced?
By placing lead washers onto a balancing stud and in recesses of the hub.
What is dynamic balancing?
Balancing the propeller to reduce the moment of imbalance while the engine is running.
What are the four steps to dynamically balance a propeller?
- Obtain in-flight vibration information. 2. Ensure vibration exceeds limits. 3. Calculate mass and location to reduce vibration. 4. Install balance weight(s) and confirm vibration levels.
What is the function of a Propeller Balance Monitoring System (PBMS)?
To provide balance solutions based on data from a Magnetic Pickup Unit and Active Noise Control Unit.
What causes aerodynamic imbalance in propellers?
Differing aerodynamic loads due to variations in blade angles.
What is aerodynamic balance?
When each blade produces equal thrust, resulting in no periodic vibrations.
What is the Aerodynamic Correction Factor (ACF)?
A reference to the blade angle difference necessary for balancing thrust or torque.