Engines - Vibration (GE)


More... Transient High Vibration Indication
Airborne Vibration Monitoring System

The Airborne Vibration Monitoring System monitors engine vibration levels. The vibration indications are displayed on the secondary engine display. The vibration source indication (the rotor with the highest vibration level) is also displayed. If the vibration monitoring system cannot determine the source (FAN, LPT or N2), broadband (BB) is displayed for the affected engine. Broadband vibration is the average vibration detected.

The Airborne Vibration Monitoring System is primarily intended for engine condition monitoring, but it is also a useful tool for isolating and determining corrective action for engine anomalies.

Each engine has a primary and backup accelerometer connected through a signal conditioner tracking filter, to the vibration display on the secondary engine display. The accelerometer signal is filtered into separate frequencies, which represent engine Broadband and tracked vibration for the FAN, LPT and N2 rotors.

The Airborne Vibration Monitoring System is a trend type, primarily intended for engine condition monitoring, but it is also a useful tool for isolating and determining corrective action for engine anomalies; each engine has its own vibration characteristics and normal values at different thrust settings.

When the level of the vibration exceeds 2.5 units the vibration indications for both engines is displayed automatically, and the engine vibration and pointer remain white.

Certain engine malfunctions can result in airframe vibrations from a windmilling engine. As the airplane transitions from cruise to landing, there can be multiple, narrow regions of altitudes and airspeeds where the vibration level can become severe. In general, airframe vibrations can best be reduced by descending and reducing airspeed. However, if after descending and reducing airspeed the existing vibration level is unacceptable, and if it is impractical to further reduce airspeed, the vibration level may be reduced to a previous, lower level by a slight increase in airspeed.

System Failure

If the filter fails, engine vibration is displayed and identified as broad band (BB).

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