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Studies on Current Hysteresis Controllers and Low Order Harmonic Suppression Techniques for IM Drives with Dodecagoal Voltage Space Vectors

Electronic Theses of Indian Institute of Science

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Title Studies on Current Hysteresis Controllers and Low Order Harmonic Suppression Techniques for IM Drives with Dodecagoal Voltage Space Vectors
 
Creator Azeez, Najath Abdul
 
Subject Induction Motor Drives
Dodecagonal Voltage Space Vectors
Current Hysteresis Controller
Voltage Source Inverters
Harmonic Suppression
Voltage Space Vector Induction Mortor Drives
Electric Motors
Multilevel Voltage Source Inverters
Electric Inverters
Induction Motors
Hysteresis Controller
IM Drive
Electrical Engineering
 
Description Multilevel inverters are very popular for medium and high-voltage induction motor (IM) drive applications. They have superior performance compared to 2-level inverters such as reduced harmonic content in output voltage and current, lower common mode voltage and dv/dt, and lesser voltage stress on power switches. To get nearly sinusoidal current waveforms, the switching frequency of the conventional inverters have to be in¬creased. This will lead to higher switching losses and electromagnetic interference. The problem in using lower switching frequency is the introduction of low order harmonics in phase currents and undesirable torque ripple in the motor. The 5th and 7th harmonics are dominant for hexagonal voltage space-vector based low frequency switching. Dodecagonal voltage space-vector based multilevel inverters have been proposed as an improvement over the conventional hexagonal space vector based inverters. They achieve complete elimination of 5th and 7th order harmonics throughout the modulation range. The linear modulation range is also extended by about 6.6%, since the dodecagon is closer to circle than a hexagon.
The previous works on dodecagonal voltage space vector based VSI fed drives used voltage controlled PWM (VC-PWM). Although these controllers are more popular, they have inferior dynamic performance when compared to current controlled PWM (CC¬PWM). VSIs using current controlled PWM have excellent dynamic response, inherent short-circuit protection and are simple to implement. The conventional CC-PWM tech¬niques have large switching frequency variation and large current ripple in steady-state.
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As a result, there has been significant research interest to achieve current controlled VSI fed IM drives with constant switching frequency. Two current error space vector (CESV) based hysteresis controllers for dodecagonal voltage space-vector based VSI fed induction motor drives are proposed in this work. The proposed controllers achieve nearly constant switching frequency at steady state operation, similar to VC-SVPWM based VSI fed IM drives. They also have fast dynamic response while at the same time achieving complete elimination of fifth and seventh order harmonics for the entire modulation range, due to dodecagonal voltage vector switching.
The first work proposes a nearly constant switching frequency current error space vector (CESV) based hysteresis controller for an IM drive with single dodecagonal voltage space vectors. Parabolic boundaries computed offline are used in the proposed controller. An open-end winding induction motor is fed from two inverters with asymmetrical DC link voltages, to generate the dodecagonal voltage space vectors. The drive scheme is first studied at different frequencies with a space vector based PWM (SVPWM) control, to obtain the current error space vector boundaries. The CESV boundary at each frequency can be approximated with four parabolas. These parabolic boundaries are used in the proposed controller to limit the CESV trajectory. Due to symmetries in the parabolas only two set of parabola parameters, at different frequencies, need to be stored. A generalized next vector selection logic, valid for all sectors and rotation direction, is used in the proposed controller. For this an axis transformation is done in all sectors, to bring the CESV trajectory to the ï¬rst sector. The sector information is obtained from the estimated fundamental stator phase voltage. The proposed controller is extensively studied using vector control at different frequencies and transient conditions. This controller maintains nearly constant switching frequency at steady state operation, similar to VC-SVPWM inverters, while at the same time achieving better dynamic performance and complete elimination of 5th and 7th order harmonics throughout the modulation range.
In the second work the nearly constant switching frequency current hysteresis con¬troller is extended to multilevel dodecagonal voltage space-vector based IM drives, with online computation of CESV boundaries. The multilevel dodecagonal space-vector dia¬gram has different types of triangles, and the previously proposed methods for multilevel hexagonal VSI based current hysteresis controllers cannot be used directly. The CESV trajectory of the VC-SVPWM, obtained for present triangular region, is used as the reference trajectory of the proposed controller. The CESV reference boundaries are com¬puted online, using switching dwell time and voltage error vector of each applied vector. These quantities are calculated from estimated sampled reference phase voltages, which are found out from the stator current error ripple and the parameters of the induction motor. Whenever the actual current error space vector crosses the reference CESV tra¬jectory, an appropriate vector that will force it along the reference trajectory is switched. Extensive study of the proposed controller using vector control is done at different fre¬quencies and transient conditions. This controller has all the advantages of multilevel switching like low dv/dt, lesser electromagnetic interference, lower switch voltage stress and lesser harmonic distortion, in addition to all the dynamic performance advantages of the previous controller.
The third work proposes an elegant 5th and 7th order harmonic suppression tech¬nique for open end winding split-phase induction motors, using capacitor fed inverters. Split-phase induction motors have been proposed to reduce the torque and flux ripples of conventional three-phase IM. But these motors have high 5th and 7th order harmonics in the stator windings due to lack of back-emf for these frequencies. A space-vector harmonic analysis of the split-phase IM is conducted and possible 5th and 7th order harmonic sup¬pression techniques studied. A simple harmonic suppression scheme is proposed, which requires the use of only capacitor fed inverters. A PWM scheme that can maintain the capacitor voltage as well as suppress the 5th and 7th order harmonics is also proposed. To test the performance of the proposed scheme, an open-loop v/f control is used on an open-end winding split-phase induction motor under no-load condition. Synchronized PWM with two samples per sector was used, for frequencies above 10 Hz. The har¬monic spectra of the phase voltages and currents were computed and compared with the traditional SVPWM scheme, to highlight the harmonic suppression.
The concepts were initially simulated in Matlab/Simulink. Experimental veriï¬ca¬tion was done using laboratory prototypes at low power. While these concepts maybe easily extended to higher power levels by using suitably rated devices, the control tech¬niques presented shall still remain applicable. TMS320F2812 DSP platform was used to execute the control code for the proposed drive schemes. For the ï¬rst work the output pins of the DSP was directly used to drive the inverter switches through a dead-band circuit. For the other two works, DSP outputs the sector information and the PWM signals. The PWM terminals and I/O lines of the DSP is used to output the timings and the triangle number respectively. An FPGA (XC3S200) was used to translate the sector information and the PWM signals to IGBT gate signal logic. A constant dead-time of 1.5 µs was also implemented inside the FPGA. Opto-isolated gate drivers with desaturation protection (M57962L) were used to drive the IGBTs. The phase currents and DC bus voltages were measured using hall-effect sensors. An incremental shaft position encoder was also connected to the motor to measure the angular velocity. The switches were realized using 1200 V, 75 A IGBT half bridge modules.Gopakumar, K2017-11-30T20:03:50Z2017-11-30T20:03:50Z2017-12-012013Thesishttp://etd.iisc.ernet.in/handle/2005/2846http://etd.ncsi.iisc.ernet.in/abstracts/3698/G26023-Abs.pdfen_USG26023
oai:etd.ncsi.iisc.ernet.in:2005/28472018-01-09T06:58:05Zhdl_2005_35Experimental and Numerical Investigation on Friction Welding of Thixocast A356 Aluminium AlloySingh, Shailesh KumarAluminium AlloysThixocast A356 Aluminium AlloysFriction WeldingSemisolid Processed AlloysA356 AlloySemi-solid Metal FormingThixocasting TechnologyAl-Si Casting AlloysMaterials EngineeringThe challenges of weight reduction and good strength in automotive industry have drawn considerable interest in thixocasting technologies. Joining of such components with conventional fusion welding creates voids, hot cracking, distortion in shape, and more importantly evolution of dendritic microstructure that ultimately would lead to inferior mechanical properties of the weld region. Thus, the purpose of making thixocast component is lost. The friction welding which is a solid state joining process can avoid defects associated with melting and solidification in a typical fusion weld and can be a promising alternative. This process produces a weld under compressive force at the contact of workpieces rotating or moving relative to one another to produce heat and plastically displacing material from the faying surfaces. Research on semisolid processing has its origin in the early 1970s. However, from the literature survey on semisolid processing it is clear that, till date, not much work has been done in field of joining of semisolid processed components. In the area of solid state welding, in particular, it is not at all explored. In view of this, the present work is focused on exploration of joining of Thixocast A356 Aluminium alloy component by friction welding and comparison of its performance with friction weld of conventionally cast sample of the same alloy. The study is carried out experimentally as well as numerically. Moreover, the material behaviour of thixocast component at elevated temperature in solid state is also described with the help of processing maps and constitutive modelling.
The hot workability of thixocast and conventionally cast A356 alloy is evaluated with the help of processing maps developed on the basis of the dynamic materials model approach using the flow stress data obtained from the isothermal compression test in wide range of temperature (300-500℃) and strain rates (0.001s-1-10s-1). The domains of the processing map are interpreted in terms of the associated microstructural mechanism. On comparing the flow stress at elevated temperature of thixocast and conventionally cast A356 alloy samples, it is observed that the flow stress of the latter showed higher value at different strain level, temperature and strain rates. This indicates that the flow property of the thixocast alloy sample is better than
that of the conventionally cast one (i.e. response to plastic flow is better for the former); while at room temperature thixocast sample has higher strength. Moreover to investigate the general nature of the influence of strain, strain rate and temperature on the compressive deformation characteristics of thixocast A356 and conventionally cast A356 aluminium alloy, a comprehensive model describing the relationship of the flow stress, strain rate and temperature of the alloys at elevated temperatures is proposed by hyperbolic-sine Arrhenius-type equation and Johnson-Cook model. The validity of descriptive results based on the proposed constitutive equation is also investigated and a comparison between two constitutive models is also made. In order to numerically model the friction welding process of a thixocast A356 aluminium alloy and conventionally cast alloy of same material using a finite element method (FEM), temperature dependent physical properties, mechanical properties as well as viscoplastic constitutive equations were used in the model. A two- dimensional axisymmetric finite element model has been developed. The modelling is based on a coupled thermomechanical approach. First, a nonlinear, transient two-dimensional heat transfer model is developed to determine the temperature fields. Later, the temperature fields are used as input for a nonlinear, two-dimensional structural model in order to predict the distortions and von Mises stress. The finite element models are parametrically built using APDL (ANSYS Parametric Design Language) provided by ANSYS. The validation of the model is carried out by comparing with the experiment. Once validated, the thermomechanical model was used to perform parametric studies in order to investigate effects of various process parameters on temperature and stress distribution in the workpieces. This helps in deciding the range of parameters for friction welding experiments in order to get good weld. Both thixocast and conventionally cast samples exhibited similar temperature distribution during the friction welding process, because of identical thermophysical properties. The magnitude of von Mises stress distribution during friction welding of thixocast A356 sample is found to be lower than that of the conventionally cast sample. It is because of their different constitutive behaviour at elevated temperature. Moreover, the developed FEM model can be successfully used to predict the residual stress at various locations for different set of parameters and geometry for friction welding of thixocast and conventionally cast A356 alloy. This helps in reducing time consuming and expensive experiments on residual stress measurement.
The chosen experiments based on Taguchi L27 orthogonal array were conducted on the friction welding machine which works on the principles of continuous drive-mechanism. The experimental specimens were machined from thixocast A356 aluminium alloy connecting rods as well as conventionally cast A356 aluminium alloy ingot in the form of cylindrical bars of dimensions 85mm length and 20mm diameter. The parameters used for welding were friction pressure, rpm, forge pressure, burn-off, and upset pressure. The effects of welding parameters on performance characteristics (i.e. tensile strength and weld efficiency) were evaluated. Taguchi method was applied to investigate the influence of each parameter on strength of joints and evaluate the combination of parameters that leads to the highest weld strength. Accordingly optimum process parameters was identified which helps in achieving the tensile strength of more than parent material. The optimized process parameters for friction welding of thixocast A356 aluminium alloy are rpm = 500, friction pressure = 60, upset time = 5, upset pressure = 100 and burn off = 5. The empirical relationships were also developed to predict the tensile strength. The developed relationship can be effectively used to predict the tensile strength of welded joint with a correlation coefficient of 0.86, which indicates the strong positive relationship between predicted and experimental data. Friction welding of thixocast A356 aluminium alloy helps to achieve very fine eutectic silicon particles of the order of 0.4 at the interface due to severe plastic deformation taking place during welding. Obtaining such fine eutectic silicon particles is difficult to be achieved within few seconds of processing by any other method. The hardness variation of friction welded thixocast alloy shows higher value as compared to that of a conventionally cast sample in the heat affected zone, which indicates better weld strength of the former. This was also confirmed by the tensile strength studied and fatigue test. This indicates that weldability of cast alloys will get improved if the microstructure is modified to globular type.Chattopadhyay, Kamanio2017-11-30T20:25:10Z2017-11-30T20:25:10Z2017-12-012013Thesishttp://etd.iisc.ernet.in/handle/2005/2847http://etd.ncsi.iisc.ernet.in/abstracts/3699/G26270-Abs.pdfen_USG26270
oai:etd.ncsi.iisc.ernet.in:2005/28482018-01-09T06:56:58Zhdl_2005_27Wing in Ground EffectMondal, ParthaGround EffectGround-Cushion PhenomenonAirfoilsWingsKutta-Joukowski TheoremDiscrete Vortex Method3D Ground Effect ModelComputational Fluid DynamicsAerodynamicsDynamic Ground Effect AnalysisSinking Grid MethodologyFlow SolverInverted Ground Effect WingDynamic Ground ApproachGround Effect StudiesAerospace EngineeringThe thesis presents a two pronged approach for predicting aerodynamics of air- foils/wings in the vicinity of the ground. The ï¬rst approach is effectively a model for ground effect studies, employing an inexpensive Discrete Vortex Method for the 2D pre- dictions and the well known Numerical lifting line theory for the 3D predictions. The second one pertains to the dynamic ground effect analysis which employs the state of the art moving mesh methodology based time accurate CFD. In that sense, the thesis deals with two ends of spectrum in the ground effect analysis; one, a model to be used in the concept design phase and the other an advanced CFD tool for analysis.
The proposed model for ground effect studies is based on the well known Discrete Vortex Method (DVM). An important aspect of this method is that it employs what is referred to as the Generalized Kutta Joukowski Theorem (GKJ), meant for interaction problems with multiple vortices, for predicting the lift (and drag) within a potential flow framework. After ascertaining the correctness of using the GKJ theorem for lift prediction for airfoils in ground effect, a modified DVM is presented as a model for ground effect predictions. As per this model, knowing the free stream lift and drag (either from an ex- periment or from a RANS computation) the aerodynamics of the section in ground effect can be predicted. The model is effectively built by constraining the DVM to produce the reference lift/drag in the free stream. The accuracy of the model, particularly for the more relevant high lift sections used during take-off and landing, is systematically estab- lished for a number of test cases. Knowing the sectional ground effect, the extension to 3D analysis is very simple and this is achieved through the well known Numerical Lifting Line theory. The efficacy of the proposed method for the 3D applications is demonstrated using a high lift wing in ground effect. It is worth noting that the proposed model predicts the lift and drag very accurately, practically at no computational cost as compared to modern RANS based CFD tools requiring over 40 or 50 million volumes at a high computational cost and intense human intervention for generating the grids for every ground clearance.
The other aspect of the thesis pertains to what is referred to as the Dynamic Ground Effect. Normally the CFD computations mimic the ground effect experiments in simulat- ing the ground effect. These simulations do not maintain geometric similarity with the actual landing or take-off sequence of the aircrafts and this can only be achieved when the simulations are dynamic. Dynamics is also important in case of combat aircrafts (particularly their naval versions) with an aggressive landing and take-off. The dynamic ground effect simulations also provides a framework for simulating varied gust conditions. This dynamic simulation of the ground effect is accomplished using a novel sinking grid methodology, which allows the grids to sink in the ground as the aircraft approaches the ground along the glide path. These simulations make use of the state of the art, time accurate moving grid methods and therefore can be computationally expensive. Never- theless, the utility of such computations in terms of their ability to produce continuous data has been highlighted in the thesis. In that sense, these dynamic computations will be cheaper as compared to the static simulations to produce data at the same level of resolution.
 
Contributor Balakrishnan, N
 
Date 2017-11-30T20:42:08Z
2017-11-30T20:42:08Z
2017-12-01
2013
 
Type Thesis
 
Identifier http://etd.iisc.ernet.in/handle/2005/2848
http://etd.ncsi.iisc.ernet.in/abstracts/3700/G26283(Abs).pdf
 
Language en_US
 
Relation G26283