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DEPT. OF ELECTRIC
 ENGINEERING

 

FACULTY OF
 ENGINEERING

 

UNIVERSITY OF
 BOLOGNA

 

 

 

SOLID ROTOR AND
SECOTOR I.M.

PM DC LINEAR
ACTUATOR

MAGNETIC
 LEVITATION

REDUCTION OF
TORQUE RIPPLE

LINEAR
 MOTOR

BIBLIOGRAPHY

 

SOLID-ROTOR AND SECTOR INDUCTION MOTORS

 

 Polyphase induction motor with solid-iron slotless rotor offers undoubted advantages in terms of construction simplicity and strength over conventional induction motors, even though its efficiency is much lower. This solid-rotor motor is especially suited for applications that require frequent starts.

Several Authors have studied this solid-rotor induction machine using analytical methods for a two-dimensional representation, by using either cylindrical or Cartesian co-ordinate systems. The studies have been generally restricted to the sinusoidal steady-state operation, even if an analysis in terms of the two-reaction theory has been developed. The major difficulty for a satisfactory analysis of the solid rotor machine derives from the necessity to take saturation into account. In fact, owing to the relatively small skin-depth, the rotor is usually highly saturated. In the literature saturation effects are either neglected or else procedures based on the choice of a trial and error value for the average iron reluctivity are adopted. In the latter case reference is usually made to the BI-H curve. This curve relates the fundamental amplitude of B to the amplitude of H (which is assumed to be sinusoidal) and is derived from the normal magnetisation characteristic B-H.

The finite element method, on the other hand, allows the reluctivity of each individual iron element to be evaluated. If the distortion introduced by the odd harmonic components of magnetizing current is ignored, the sinusoidal steady-state operation may be studied by the use of complex numbers. If this is not done it becomes necessary to solve a time dependent problem.

In this research, the three-phase induction motor with smooth solid-rotor has been studied by a two-dimensional finite element analysis. A machine with this kind of rotor is particularly suitable for investigation by the finite element method, since the machine geometry (as observed in a reference frame on the stator) does not vary with the rotor motion.

 Features of the study: 

Ø      Complete representation of the magnetic behaviour of the iron in the machine
Ø
      
Analysis of the machine as a whole
Ø
      
Determination of the magnetic field for a given system of supply voltages.
Ø
      
Prediction of the performance under voltage-forced operation.
Ø
      
Calculation of every steady-state operating point as the asymptotic solution of the electromagnetic field partial differential equation for a fixed constant speed and for a given symmetric system of sinusoidal supply voltages.
Ø
      
Comparison of the calculated electrical and mechanical quantities with experimental results.

 

PM DC Linear actuators

 

 The linear actuators are increasingly em­ployed as direct actuators in servo sys­tems replacing the more conven­tional mechanical systems. The use of per­manent magnets on the slider offers several advantages associ­ated with the absence of electri­cal connections and heating effects due to copper losses. In addi­tion, the use of a slotless armature results in a simplified construc­tion. The design of these linear actuators is optimised for maxi­mum force to total mass ratio and for maxi­mum force to moving mass ratio. In order to analyse the dynamic behaviour a mathematical model based on a simplified field analysis is developed. Numerical simu­lations of the step response of a positioning servo system are now under investigation.
 


Fig. 1- Schematic drawing of the PM DC linear actuator.

According to these considerations a very simple and low cost PM DC linear actuator is investigated which consists of a slotless armature and a permanent magnet slider, as represented in Fig. 1.

It has been verified that the magnetic circuit geometry allows the magnet to operate at low demagnetising field if the Ampere-turns of the armature winding are compensated. For this purpose, in addition to the winding distributed over the working length, two coils are placed at the ends of the actuator. The compensation of the armature Ampere-turns is very important to achieve high thrust values. The compensating coils can be replaced by distributed windings leading to geometries which can drive two sliders.


Simple linear models are not suitable to predict the performance of the linear actuator shown in Fig. 1 as the stroke length is much larger than the magnet length and the winding current is increased beyond the rated value. Numerical techniques such as the finite-element method can be used to determine accurately the actuator performance, taking the non-linear behaviour of the iron circuit and magnet material into account.


Plot of the flux density distribution

 

Main Contribution

 

Ø      Two-dimensional Finite Element field analysis
Ø
      
Determination of the effects of the iron core saturation on the thrust versus slider position curve
Ø
      
Calculation of the peak force during temporary overload conditions
Ø
      
Calculation of the transformer and dynamic coefficients of the machine
Ø
      
Definition of the dynamic model of the linear actuator
Ø
      
Compensating coils replaced by distributed windings leading to geometries which can drive two sliders
Ø
      
Comparative analysis

 

MAGNETIC LEVITATION SYSTEMS
FOR HIGH SPEED GROUND TRANSPORTATION

 

 The research concerns the analysis of the vertical dynamics of an electrodynamic levitation system using superconducting coils and a passive and/or damping system.

In high speed magnetically levitated vehicles the levitation systems based on repulsive forces are statically stable but dynamically have zero or low damping characteristics. In order to damp the vertical oscillations, passive damping systems, constituted by short circuited coils placed under the levitation coil, can be used. However, pas­sive damping systems usually do not provide the re­quired ride quality. Then, the damping effect on the me­chanical oscillation of the vehicle should be improved by using an additional active damping system.

The performance of combined active and passive damping system has been evaluated. The active damping has been performed by a coil current control using mechanical or electrical transducers. It has been observed that, in general, the control system based on mechanical transducers performs better than that based on electrical transducers.

In the research, the analysis of a control system for active damping which does not require vertical position, velocity or acceleration measurement is presented. The control system operation is based on sensing the current in the damping coil and regulating the supply voltage according to a suitable control law. The stability analysis has been performed.


Fig. 1 - Schematic cross-section of the levitation system
 with damping coils.

The effectiveness of the levitation system is verified by calculating the response to a step track disturbance and analysing the Power Spectral Density (PSD) of the vertical acceleration due to a random track disturbance.

Fig. 2 shows a plot of the flux distribution due to the superconducting coil current assuming the conducting sheet to behave as a perfect diamagnetic material for high values of the vehicle speed.


Fig. 2 - Plot of the flux distribution due to the superconducting coil,
 z = 0.25 m, d=0.10 m.


Fig. 3 - Vertical acceleration PSD for A=1.25 10-6 m and v = 100 m/s.

Main contributions

 

Ø      Performance evaluation of combined active and passive damping
Ø      Active damping performed by a coil current control using mechanical or electrical transducers
Ø      Analysis of a control system for active damping which does not require vertical position, velocity or acceleration measurement
Ø      Control system operation based on sensing the current in the damping coil and regulating the supply voltage according to a suitable control law
Ø
      
Stability analysis
Ø      Evaluation of the effectiveness of the levitation system by analysing the Power Spectral Density (PSD) of the vertical acceleration .

 

PERMANENT MAGNET ACTUATORS: REDUCTION OF THE TORQUE RIPPLE BY A MULTI-OBJECTIVE MINIMIZATION TECHNIQUE

 

The demand for high performance Permanent Magnet (PM) motors is continuously increasing in industrial applications because of their high efficiency and power density. The machine inherently has a torque ripple which causes vibrations and noises. This deteriorates the performance of position control systems and speed control systems at low speed. As a consequence, it is important to find out methods for reducing the torque ripple to acceptable values.

With reference to sinusoidal PM machines with surface-mounted magnets, there are mainly two contributions to the torque ripple. The first one is the cogging torque which arises from the interaction of the magnets with the stator teeth. As a result, the torque is generated by the tendency of the rotor to align with the stator at positions where the permeance of the magnetic circuit is maximized. The second contribution is the torque ripple caused by the presence of harmonics in the air-gap flux density distribution of the magnets, which leads to non-sinusoidal components of the Electromotive Force (EMF).

Many studies concerning the analysis of the cogging torque have been carried out. The most effective solutions proposed for the cogging torque reduction are the adjustment of the magnet arc width relative to the slot pitch, the shifting of the pole pairs and the skewing of either the stator slots or the rotor magnets. Other methods which have been proposed for reducing the cogging torque include the presence of dummy slots or dummy teeth in the stator laminations, and the shaping of rotor magnets.

The influence of field harmonics on the induced EMF may also be reduced acting on the stator winding distribution or adopting a fractional number of slots per pole. The skewing of stator slots and rotor magnets can also be used to reduce the harmonic content of the induced EMF. However, the impact of all these techniques cannot be considered separately for the two contributions to the total torque ripple. A tight relationship between the two contributions exists. The solutions employed to reduce the cogging torque also affect the torque ripple produced by the harmonic content of the induced EMF. As a consequence, the problem of the torque ripple reduction should be considered on the whole and in most cases a compromise has to be made to minimize the total torque ripple.

In the research, the minimization of the torque ripple is formulated as an optimization design problem, without separating the different contributions. In order to do this a two-step design procedure has been proposed. In the first step a global minimization algorithm coupled to a one-dimensional field analysis is utilized. The minimization technique is based on the Evolution Strategy (ES) method. The minimization algorithm proposed considers the enhancement of the fundamental component of the induced EMF and the minimization of the two torque ripple contributions. A multi-objective problem is stated and solved by means of a penalty technique.

Once the design unknowns have been determined by the proposed procedure, the magnet arc width has been further optimized to minimize the cogging torque. For this purpose a two-dimensional Finite Element (FE) analysis has been used to determine the flux density distribution of the magnets.


Fig.
1 - Plot of the rotor geometry (solution A)
.


Fig.
2 -   Plot of the magnetic field (solution A)


Fig.
3 - Schematic drawing of the magnet skewing.


Fig.
4 - Prototype realized on the basis of the results
obtained for Solution B.

The example presented considers a 3-phase, 6-pole PM synchronous machine with sinusoidal EMF and magnets placed on the rotor surface. Since the stator skewing increases the complexity of machine construction, a skewed mounting of discrete magnet segments on the rotor has been considered.Two different magnet arrangements have been investigated. In the first one, the sum of the magnets’ width is smaller than the rotor periphery length. In the second one, the sum of the magnets width is equal to the rotor periphery length. Therefore, the rotor surface is completely covered by the PMs. This configuration allows the realization of the magnetic part of the rotor using a tube of a polymer bonded magnetic material and simplifies the manufacturing of the motor, since the magnet material can be directly molded onto the rotor eliminating subsequent assembly steps. In this work, the analysis will be mainly focused on the second magnet arrangement type. Experimental tests of the machine constructed by means of the design procedure described, have been done. The test results meet the design requirements.


Fig.
5 -   Cogging torque


Fig. 6 - Cogging torque curves for Solution B.

 

MAIN CONTRIBUTIONS

 

Ø    Minimization of the torque ripple, formulated as an optimization design problem
Ø    Minimization of the torque ripple without separating the different contributions
Ø    Definition of a two-step design procedure
Ø    Minimization technique based on the Evolution Strategy (ES) method.

Ø    Multi-objective problem solved by means of a penalty technique
Ø    Optimization of the magnet arc width in order to minimize the cogging torque
Ø    Use of a two-dimensional Finite Element analysis to determine the flux density distribution of the magnets.

 

Linear Induction Motors

 

Linear induction machines have been widely investigated for use in high speed ground transportation. Other applications including liquid metal pumps, magnetohydrodynamic, power generators, conveyors, baggage handling systems, as well as a variety of consumers applications have contributed to increase the interest in linear induction machines.

A particular type of linear induction motor is the T-shaped LIM. This mo­tor can find application particularly in drives for material dislocation along paths showing sudden direc­tion changes in the horizontal plane and in the vertical plane.

The secondary is composed of a T-shaped iron structure topped with four sheets of conducting material (usually aluminium). The primary includes four iron stacks facing the secondary sheets. The primary windings can be individually wounded in each stack, otherwise the coil conduc­tors leaving a slot can enter the corresponding slot of the adjacent core. In this way the number of end-windings is reduced leading to a lower copper weight and to a more compact machine. The primary voltage drops are also reduced.


Basic structure of the T-shaped linear induction motor.


Cross-section of the T-shaped LIM

 

In this type of motor the direction changes occur in a horizon­tal plane, while the slope changes occur in a vertical plane.

To reduce the magnetising current in LIM it is advisable to use small air-gap. In order to avoid interferences between fixed and moving parts, in T-shaped LIM it is possible to remove the horizontal secondary when the direction change takes place in a vertical plane or the vertical secondary when the direction change takes place in a horizontal plane. In this way the electromagnetic force is given by the contributions of two primaries at least. It should be noted also that the vertical component of the electromagnetic force between the horizontal primary and the corresponding secondary can be uti­lized as a lifting force allowing a reduction of the friction force of the moving part.

The steady-state performance of the ma­chine is evaluated by a math­ematical model that takes only the fundamental component of the primary mmf into account. This mathematical model  allows the determi­nation of the electro­magnetic force and phase currents cor­responding to a fixed speed value when a three-phase system of sinusoidal voltages is applied. The geometry of the machine and the thickness of the secondary aluminium sheet gives a force versus speed curve which shows decreasing force val­ues in  the motor operation range.

In linear induction ma­chines a balanced voltage operation determines unba­lanced cur­rents in the primary phases. As a conse­quence the thrust pulsation and the copper losses increases with re­spect to balanced current op­era­tion. The mathematical model men­tio­ned above permits the calcu­la­tion of the unbalan­ced supply volt­ages that deter­mine bal­anced currents. The technical feasibility of unsym­metric voltage con­trol in order to limit the negative current sequence is investi­gated. By using the mathemati­cal model it is then possible to deter­mine the force versus speed curve for some pre­fixed unbalanced supply voltages.


 Experimental setup: closed loop track of the T-Shape Linear Induction Motor

 

Nameplate data of the T-Shape Linear Induction Motor

3-phase, 2-pole, 50 Hz
star-connected windings
Rated current   = 14.5 A
Rated speed     = 3 m/s
Rated thrust      = 210 N

Primary stacks

stack length
      = 0.135  m
stack width       = 0.1
      m
stack height      = 0.05
    m

Secondary aluminium sheet

thickness        = 0.003
   m
width               = 0.16
     m
clearance         = 0.0015 m

 

The analysis of linear induction machines is more complicated than in conventional round-rotor induction machines owing to the so-called end-effects. Then, the machine performance is evaluated by a mathematical model which considers only the fundamental component of the primary mmfs, taking the end ef­fects into account. This mathematical model allows the determi­nation of the electro­magnetic force, the primary and the secondary currents cor­responding to a fixed speed value, when the motor is supplied by a three-phase system of sinusoidal voltages. The geometry of the machine and the thickness of the secondary aluminium sheet determine a decreasing force versus speed curve which suggests that it is possi­ble, in some cases, to regulate the motor speed by using a stator vol­tage controller. The phase-angle control of thyristors could be employed, but the use of this simple and reliable technique determines a high harmonic content and a low input power factor. These disadvantages may be re­duced or eliminated by employing AC vol­tage regulators operating in chopping mode. The AC PWM chopper may then be em­ployed to drive the T-shaped LIM allowing high performance in the motor opera­tion range as well as in the rege­nerative brea­king.

In linear induction machines, symmetric voltage operation determines unba­lanced cur­rents in the primary phases. As a consequence the copper losses increase with respect to balanced current opera­tion. The mathematical model mentio­ned above permits the calcula­tion of the thrust pulsation corresponding to unbalanced supply currents for each speed value.

It will be shown that suitable amplitude and phase displacement values of the negative sequence current component determine a practically negligible value of the thrust pul­sation.

Owing to the presence of this pulsating component, the primary and secondary systems experience large vibrations and consequently acoustic noise.

In linear induction motors a pulsating force is present even if the machine is supplied with a balanced 3-phase system of voltages owing to the open air-gap with an entry-end and an exit-end.

It has been shown that in order to increase the average value of the electromagnetic force the machine should be supplied with bal­anced currents. However, this operating condition does not correspond to a minimum for the amplitude of the pulsating force component.


Schematic drawing of the 3-phase PWM AC chopper

 

MAIN CONTRIBUTIONS

 

Ø      Analysis of the LIM performance under balanced voltages and balanced currents
Ø
      
Comparison of the average developed force and the pulsating com­ponent in the motor operating range
Ø
      
Determination of the amplitude and phase angle of the negative sequence component which completely eliminate the pulsat­ing force has been found
Ø
      
Analysis of the unsymmetric control of a 3-phase PWM AC chopper feeding the LIM
Ø
      
Realisation of the experimental setup of the T-Shaped LIM
Ø
      
Italian Patent "Motore elettrico lineare utilizzabile su qualsiasi tipo di percorso compresi quelli curvi a breve raggio e con forti variazioni di pendenza". Inventore designato Prof. Ing. Benito Brunelli, a nome Università degli Studi di Bologna. Brevetto depositato il 5 giugno 1990 al N. 3536 A/90.

 

SOLID ROTOR AND
SECOTOR I.M.

PM DC LINEAR
ACTUATOR

MAGNETIC
 LEVITATION

REDUCTION OF
TORQUE RIPPLE
LINEAR
 MOTOR
BIBLIOGRAPHY