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
51
www.smartavionics.com
Summary of Contents for PB-4
Page 6: ...www smartavionics com vi...
Page 12: ...www smartavionics com 6...
Page 20: ...www smartavionics com 14...
Page 34: ...www smartavionics com 28...
Page 40: ...www smartavionics com 34...
Page 56: ...www smartavionics com 50...
Page 62: ...www smartavionics com 56...
Page 68: ...www smartavionics com 62...
Page 70: ...www smartavionics com 64...
Page 74: ...www smartavionics com 68...
Page 78: ...www smartavionics com 72...