What is it about?

Several approaches can be employed in prognostics, to detect incipient failures of primary flight command electromechanical actuators (EMA), caused by progressive wear. The development of a prognostic algorithm capable of identifying the precursors of an electromechanical actuator failure is beneficial for the anticipation of the incoming failure: a correct interpretation of the failure degradation pattern, in fact, can trig an early alert of the maintenance crew, who can properly schedule the servomechanism replacement. Prognostic, though, is strictly technology-oriented as it is based on accurate analysis of the cause and effect relationships. As a consequence, it is possible that prognostics algorithms that demonstrate great efficacy for certain applications (electrohydraulic actuators, for examples) fail in other circumstances, just because the actuator is based on a different technology. The research presented in this paper proposes a prognostic technique able to identify symptoms of an EMA degradation before the actual exhibition of the anomalous behavior; to this purpose friction, backlash, coil short circuit and rotor static eccentricity failures are considered.

Featured Image

Why is it important?

It is important because proposes an innovative model-based fault detection neural technique to analyze information gathered through FFT analysis of the components under normal stress conditions. To this purpose, a proper simulation test bench was developed: results show that the method exhibit adequate robustness and a high degree of confidence in the ability to early identify an eventual malfunctioning, minimizing the risk of false alarms or unannunciated failures.

Read the Original

This page is a summary of: Model Based Analysis of Precursors of Electromechanical Servomechanism Failures, January 2015, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2015-2035.
You can read the full text:

Read

Contributors

The following have contributed to this page