Permanent magnet synchronous motors (PMSMs) are an alternative in critical applications where high-speed operation,
compactness and high efficiency are required. In these applications it is highly desired to dispose of an on-line, reliable and
cost-effective fault diagnosis method. Fault prediction and diagnosis allows increasing electric machines performance and
raising their lifespan, thus reducing maintenance costs, while ensuring optimum reliability, safe operation and timely
maintenance. Consequently this thesis is dedicated to the diagnosis of magnetic and electrical faults in PMSMs.
As a first step, the behavior of a healthy machine is studied, and with this aim a new 2D finite element method (FEM) modelbased
system for analyzing surface-mounted PSMSs with skewed rotor magnets is proposed. It is based on generating a
geometric equivalent non-skewed permanent magnet distribution which accounts for the skewed distribution of the practical
rotor, thus avoiding 3D geometries and greatly reducing the computational burden of the problem.
To diagnose demagnetization faults, this thesis proposes an on-line methodology based on monitoring the zero-sequence
voltage component (ZSVC). Attributes of the proposed method include simplicity, very low computational burden and high
sensibility when compared with the well known stator currents analysis method. A simple expression of the ZSVC is
deduced, which can be used as a fault indicator parameter. Furthermore, mechanical effects arising from demagnetization
faults are studied. These effects are analyzed by means of FEM simulations and experimental tests based on direct
measurements of the shaft trajectory through self-mixing interferometry. For that purpose two perpendicular laser diodes are
used to measure displacements in both X and Y axes. Laser measurements proved that demagnetization faults may induce
a quantifiable deviation of the rotor trajectory.
In the case of electrical faults, this thesis studies the effects of resistive unbalance and stator winding inter-turn short-circuits
in PMSMs and compares two methods for detecting and discriminating both faults. These methods are based on monitoring
and analyzing the third harmonic component of the stator currents and the first harmonic of the ZSVC.
Finally, the Vold-Kalman filtering order tracking algorithm is introduced and applied to extract selected harmonics related to
magnetic and electrical faults when the machine operates under variable speed and different load levels. Furthermore,
different fault indicators are proposed and their behavior is validated by means of experimental data. Both simulation and
experimental results show the potential of the proposed methods to provide helpful and reliable data to carry out a
simultaneous diagnosis of resistive unbalance and stator winding inter-turn faults.
The latest advances in electric and electronic aircraft technologies from the point of view of an "all-electric" aircraft are presented herein. Specifically, we describe the concept of a "more electric aircraft" (MEA), which involves removing the need for on-engine hydraulic power generation and bleed air off-takes, and the increasing use of power electronics in the starter/generation system of the main engine. Removal of the engine hydraulic pumps requires fully-operative electrical power actuators and mastery of the flight control architecture. The paper presents a general overview of the electrical power generation system and electric drives for the MEA, with special regard to the flight controls. Some discussion regarding the interconnection of nodes and safety of buses and protocols in distributed systems is also presented.
Harry Rowe Mimno Award for the March 2007 AESS Magazine Paper: “Moving Towards A More Electric Aircraft”