Chapter 8. Rotor Balancing
This chapter aims to provide an overview of the rotor balancing process.
Although the emphasis is on gyroplane rotor balancing, it is also largely
applicable to helicopter rotors. Please see the
for
details of how the sensors are attached to the aircraft and
for
details of selecting the profile that matches the orientation of the
accelerometer axes.
A tutorial document that provides an in-depth description of how to use the
PB-4 to balance a rotor is available from the Smart Avionics website.
8.1. Causes of rotor vibration
Mass imbalance is one of the causes of rotor vibration and the PB-4 system
can help you balance the rotor to eliminate that vibration. Other vibrations
may also be present. In particular, gyroplanes often suffer strong vibration at
twice the rotor frequency. This “× 2” (times 2) vibration is often much larger
than the vibration due to imbalance and so even when the rotor has been mass
balanced satisfactorily, vibration will still be noticeable to the occupants.
Fig 8.1. Rotor spectrum with large × 2 peak
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