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<p dir="ltr">This research developed a lumped volume-based coupled simulation model for gear pumps and motors, which is employed to analyze a reference machine of a compensated crescent- type internal gear pump. The model is composed of simultaneous simulations of the pump fluid domain pressure, lubricating films, and dynamics of the moving components.</p><p dir="ltr">The simulation model developed includes four major novel contributions.</p><p dir="ltr">1. A coupled simulation model was developed for the reference machine which provides (a) a lumped parameter simulation of the fluid pressure within the inter-teeth volumes, (b) CFD simulations of the lubricating interfaces, and (c) a simulation of the micromotion of the pressure compensating components and gear bodies. The simulation tool is developed in C++ and constitutes the simulation core of Multics for internal gear pumps. The model achieved volumetric and mechanical predictions for the reference type of machine, which are validated via experimental investigations.</p><p dir="ltr">2. A flexible pressure solver was established to solve the pressure transience in the fluid domain in gear pumps with general CV geometry exemplified in the reference machine. The approach allows for ample freedom in defining control volumes, including possible volume discontinuities. The new formulation, derived from mass conservation, avoids the numerical evaluation of the volume derivatives so that it allows for simulating a control volume layout with sudden shape changes. The new formulation also considers the sliding motion from volume boundaries when evaluating internal flows, which improves the accuracy of the control volume pressure solutions. The effectiveness of the proposed formulation was examined by applying the method to the simulation of the reference machine. Compared with the state-of-the-art simulations, several improvements in the pressure simulation were observed : (i) the proposed formulation provides free-of-spike fluid pressure simulations, even for discontinuous volumes; (ii) the proposed formulation properly captures the flow component between volumes that is caused by the volume boundary motions, a term previously neglected, which affects the pressure evaluation accuracy, especially in gear meshing zone.</p><p dir="ltr">3. The swift film coupling algorithm proposes a novel artificial inertia damping-based method (AIDM) to simulate this coupling. The proposed method considers modifying the physical body dynamics with artificial inertia and damping values that could achieve significant numerical solver accelerations while maintaining extremely low errors. The artificial inertia and damping are determined based on the instantaneous physical system’s Jacobian so that the first-order dynamics in the solution can be conserved from the original dynamic system. The solver acceleration capability is quantified in time-discretization-based derivations, where additional guidelines for determining the artificial inertia and damping values are found. The proposed approach is used to simulate two model problems for a 1-D slider pad under periodic loading conditions, where one pad is fixed inclined and the other free to move vertically and rotate about its center. Simulation results reported an error lower than 0.01 μm in the gap height geometry prediction by the proposed AIDM approach compared to the state-of-the-art Reynolds film damping-based method (RDM). Meanwhile, the numerical solver speed improved 1000 times for the fixed incline pad problem and one hundred thousand times for the free-to-float pad problem. Derivations showed that additional acceleration potential can be achieved in realistic mechanical systems where a higher degree of freedom is present in the body motions. The error behavior of the proposed AIDM approach is discussed, showing the error is positively related to the absolute magnitude of the modification parameter ϕ used for calculating the artificial inertia and damping, and the error is related to the validity of the linearization assumption on the system dynamics.</p><p dir="ltr">4. Based on a novel experimental set-up to measure the filling characteristics of an internal gear pump under induced gaseous cavitation. An integrated simulation approach was proposed to study the incomplete filling behavior in positive displacement machines. The approach consists of (a) a 1st order predictive model for evaluating the amount of undissolved gas at the pump inlet from the circuit pressure loss, (b) a gas-equilibrium-based cavitation model for predicting the pressure transience in the pump fluid domain, (c) a lumped volume based pump flow evaluation. Experiments performed over a wide range of operating conditions validated the deployment of the first-order gas release prediction (with 8 s time constant for fluid with 6 % total air). The complete simulation approach was validated via a good match with the measured volumetric efficiency for both low-speed and high-speed conditions.</p><p dir="ltr">The reference compensated crescent-type internal gear pump (CCIGP) unit was simulated with the full scope coupled simulation model, with which the methods proposed in this thesis research were validated with experiments. Simulation results matched with volumetric efficiency as well as mechanical efficiency. The model also reports a breakdown of the energy consumption within the reference CCIGP, which promotes the understanding of the operation of the reference machine.</p>

"Thanks to significant worldwide research directed at understanding and predicting structural behavior at elevated temperatures, analytical methods are available to support a rational, performance-based approach to the structural design of buildings for fire conditions. To utilize these analytical methods effectively, structural engineers need guidance on reliable and appropriate approaches to dealing with a variety of factors, including the effects of fire protection measures, temperature-dependent thermal and structural properties, elastic and inelastic behavior of structural components and assemblies, and thermal and structural response of framing connections. To meet the objective of guiding the structural engineer in appropriate analytical methods and parameter values for performance-based structural fire protection, this thesis proposes a comprehensive way of thinking about the design and analysis of structures for fire conditions. This integration of structural engineering and fire protection engineering into a functional framework is defined herein as Fire-Robust Structural Engineering (FRSE). The FRSE process, which is presented as a series of flowcharts, is designed to guide the structural engineer in executing the functions involved in the design of fire-safe structures and to help identify informational needs critical to these tasks. Currently, mechanisms for identifying possible resources to fulfill fire-related informational needs are generally organized for the convenience of the fire research community. Identification of resources that provide appropriate information for fire-robust structural engineering, such as laboratory fire test results, parametric studies of analytical methods, and other sources of guidance, is often difficult because these resources are rarely organized and presented for the benefit of structural engineers. To begin to resolve this problem, this thesis has developed a prototype information management system (IMS) based on the framework of the FRSE process. The IMS addresses the critical challenge of organizing and presenting the available knowledge and data in a format that is consistent with the perspective and informational needs of the structural engineer. The prototype version of the IMS has been implemented using a Microsoft Excel® platform. In addition to guidance in utilizing specific analytical methods and choosing appropriate parameter values, the structural engineer also requires an understanding of the input requirements and accuracy of various analytical methods in order to make informed decisions regarding which methods are appropriate for use with different structural configurations. Therefore, this thesis includes a model study as an example of a resource that could aid the structural engineer in making such decisions. The model study compares various analytical methods (simplified spreadsheet applications and advanced finite element techniques) to published laboratory test data and discusses concerns that the structural engineer must keep in mind when using each method. Conclusions are drawn regarding the appropriateness of each analytical method to the analysis of a fully restrained, spray-protected steel beam. Given this type of information, the structural engineer can make decisions regarding the types of analytical methods and the level of analytical sophistication required to solve a given design problem."

The presented work is concerned with the development and application of an ultrasonic detection scheme suitable for the monitoring of muscle dynamics with high temporal - down to 5 µs - and spatial resolution - down to 0.78 µm. A differential detection scheme has been developed to monitor the variations of the velocity of longitudinal polarized ultrasound waves travelling in contracting and relaxing muscle, compensating for variations of the path length by referencing to a frame. The observed time dependent variations of the time-of-flight of the ultrasonic waves caused by variations in the muscle and in addition by minor deformations of the enclosure are detected each separately and synchronously and are evaluated differentially. Beside of the detected increase of the speed of sound observed for contracted muscle with respect to the relaxed state of about 0.6%, the recovery time from maximum isometric contraction is quantified and relaxation processes are observed for the recovery phase following the isometric contraction. The developed ultrasonic calliper was employed to monitor both, the brain controlled and externally excited muscle dynamics with sampling intervals down to 10 ms synchronously with signals relating to the excitation. Monitored are the activation, hold, and relaxation phase for maximum voluntary isometric contraction of the gastrocnemius muscle. A so far not reported post tetanus overshoot and subsequent exponential recovery are observed. Both are attributed to the muscle as suggested by combined monitoring with EMG and are modelled with a lumped mechanical circuit containing an idealized bidirectional linear motor unit, ratchet, damper, and springs. Both, the rapid contraction and relaxation phases require a high order filter or alternatively a kernel filter, attributed to the nerve system as suggested by external electric stimulation. The respective response function is modelled by an electrical lumped circuit. Together with a reaction time and occasionally observed droops in the hold phase, both adjusted empirically, the monitored response is represented in close approximation by the combined electrical and mechanical lumped circuits. The respectively determined model parameters provide a refined evaluation scheme for the performance of monitored athletes. Valuable parameters relate to the latent period, the muscle response time, the activation and deactivation dynamics, a possible droop and other instabilities of the hold phase, and parameters characterizing the relaxation phase including the observed post tetanus overshoot and subsequent contraction. Monitored and modelled are also the different processes involved in active muscle dynamics including isotonic, isometric, and eccentric contraction or stretching. The developed technology provides time sequential observation of these processes and registration of their path in the extension and force parameter space. Under suitable conditions the closed-loop cycles of mind controlled human muscle movements proceed along characteristic lines coinciding with well identifiable elementary processes. The presentation of the monitored processes in the extension and force parameter space allows the determination of the mechanical energy expenditure for the observed different muscle actions. An elementary macroscopic mechanical model has been developed, suitable to express the basic features of the monitored muscle dynamics.

Η θερμική ανάλυση είναι μια σημαντική περιοχή μελέτης και γίνεται περισσότερο σημαντική για την σχεδίαση ηλεκτρικών μηχανών εξαιτίας της ανάγκης για μείωση του όγκου των υλικών και του κόστους κατασκευής τους καθώς και για την αύξηση της απόδοσής τους. Είναι εξίσου σημαντική με την ηλεκτρομαγνητική ανάλυση μιας και η θέρμανση της μηχανής θα οριοθετήσει την ονομαστική της ισχύ καθώς και την διάρκεια ζωής της μόνωσης. Στόχος της παρούσας διπλωματικής εργασίας είναι η εύρεση της κατανομής της θερμοκρασίας στο εσωτερικό ενός ασύγχρονου τριφασικού κινητήρα στη μόνιμη κατάσταση λειτουργίας του με τη μέθοδο των συγκεντρωμένων παραμέτρων. Στο πρώτο κεφάλαιο αναφέρονται βασικές έννοιες της θερμοδυναμικής. Γίνεται αναφορά σε διάφορους συντελεστές, παρουσιάζονται οι θερμοδυναμικοί νόμοι και γίνεται σύντομη αναφορά στους μηχανισμούς μετάδοσης θερμότητας. Στο δεύτερο κεφάλαιο δίνεται η αναλυτική περιγραφή των μηχανισμών μετάδοσης θερμότητας και παρουσιάζεται ένα απλό δίκτυο μοντελοποίησης με ισοδύναμες θερμικές αντιστάσεις. Στο τρίτο κεφάλαιο παρουσιάζεται σύντομα η δομή, η αρχή λειτουργίας και οι τύποι μιας ασύγχρονης μηχανής. Εδώ επίσης αναφέρονται και οι διάφορες μορφές απωλειών ενέργειας κατά την λειτουργία μιας τριφασικής ασύγχρονης μηχανής. Παρουσιάζεται ακόμη ο υπό μελέτη κινητήρας και αναφέρονται τα θερμοστοιχεία που χρησιμοποιούνται στην πειραματική διαδικασία. Στο τέταρτο κεφάλαιο περιγράφεται η μέθοδος θερμικής ανάλυσης με χρήση ισοδυνάμου κυκλώματος θερμικών αντιστάσεων για την μόνιμη κατάσταση. Στη συνέχεια δίνεται το προτεινόμενο κύκλωμα και παρουσιάζονται αναλυτικά οι ισοδύναμες θερμικές αντιστάσεις του μοντέλου. Τέλος στο πέμπτο κεφάλαιο παρατίθενται τα αποτελέσματα της θερμικής ανάλυσης, γίνεται σύγκριση με τα πειραματικά δεδομένα θερμοκρασιακών τιμών που πάρθηκαν από τα θερμοστοιχεία και ακολουθεί η διαδικασία της παραμετροποίησης στους διάφορους συντελεστές που χρησιμοποιήθηκαν είτε υπολογίστηκαν κατά την ανάλυση. / Thermal analysis is an important design area and becoming more important part of the electric motor design process due to the push for reduced weights and costs and increased efficiency. Thermal analysis is of equal importance as the electromagnetic design of the machine, because the temperature rise of the machine eventually determines the maximum output power. The purpose of this study is to record the temperature distribution of the internal parts of an induction motor at steady state using an equivalent thermal circuit with lumped parameters. The first chapter is an introduction of the thermodynamic theory. The laws of thermodynamics are described and there is a brief report of heat transfer mechanisms. The second chapter describes analytically the heat transfer mechanisms. Also, an example of modelling using thermal equivalent resistances is given. The third chapter introduces shortly the operational principles of an induction machine. Here are also referred the various losses that occur during the rotation of an induction motor. The studied induction motor, with the modified stator winding to include thermocouples, is shown. The fourth chapter introduces the method of thermal analysis using thermal equivalent circuit with lumped parameters. The proposed model is given and its components are described in particular. At last, in the fifth chapter the results of temperature distribution are given and compared with experimental data of temperature values that are acquired using the thermocouples. Here also takes apart the parameterising of the various coefficients that were used or calculated during this study.

Suspension systems and wheels play a critical role in vehicle dynamics performance of a car in areas such as ride comfort and handling. Lumped parameter models (LPMs) are commonly used for assessing the performance of vehicle suspension systems. However, there is a lack of clarity with regard to the relative capabilities of different LPM configurations. A comprehensive comparative study of three most commonly used LPMs of increasing complexity has been carried out in the current work. The study reported here has yielded insights into the capabilities of the considered LPMs in predicting response time histories which may be used for assessing ride comfort. A shortcoming of available suspension system models appears to be in representation of harsh situations such as jounce movement which cause full compression of springs leading to ‘jerks’ manifested as high values of rate of change of acceleration of sprung mass riding on a wheel. In the current research work, a modified nonlinear quarter-car model is proposed to account for the contact force that results in jerk-type response. The numerical solution algorithm is validated through the simulation of an impact test on a car McPherson strut in a Drop Weight Impact Testing Tower developed in CAR Laboratory, CPDM. This is followed by a detailed comparison of HCM and QCM to examine their suitability for such analysis. For decades, wheel bearings in vehicles have been designed using simplified analytical approaches based on Hertz contact theory and test data. In the present work, a hybrid approach has been developed for assessing the load bearing capacity of a wheel ball bearing set. According to this approach, the amplitude of dynamic wheel load can be obtained from a lumped parameter analysis of a suspension system, which can then be used for detailed static finite element analysis of a wheel bearing system. The finite element modelling approach has been validated by successfully predicting the load bearing capacity of an SKF ball bearing set for an acceptable fatigue life. For the first time, using a powerful commercial explicit finite element analysis tool, a detailed dynamic analysis has been carried of a deep groove ball bearing with a rotating inner race. The analysis has led to a consistent representation of complex motions consisting of rotations and revolutions of rolling elements, and generated insights into the stresses developed in the various components such as balls and races. In conclusion, a simple yet effective fuzzy logic-based yaw control algorithm has been presented in the current research. According to this algorithm, two inputs i.e. a yaw rate error and a driver steering angle are used for generating an output in the form of an additive steering angle which potentially can aid a driver in avoiding straying from an intended path.

Les machines électriques synchrones à aimants permanents sont susceptibles de rencontrer un disfonctionnement suite à un échauffement non maîtrisé. L’objectif de cette étude est de développer un modèle thermique générique et prédictif pouvant simuler diverses situations d’intérêts: régime permanent, régime transitoire, mode dégradé, entrefer immergé, haute vitesse. Pour cela, la méthode nodale est utilisée pour développer le modèle thermique générique. En parallèle, un banc d’essai et un prototype sont conçus pour valider le modèle. L’étude de sensibilité des résultats du modèle à certains paramètres montrent que certains coefficients de convection, certaines conductances de contact et la conductivité thermique radiale du bobinage ont une influence considérable sur les résultats du modèle. Cependant ces paramètres sont mal connus, car ils sont issus des formules empiriques ou des abaques. Grâce au prototype et au modèle développé, ces paramètres sont identifiés. Trois méthodes d’identification sont testées pour aboutir à une stratégie d’identification: les algorithmes génétiques, la méthode de Gauss-Newton et la méthode de Levenberg-Marquardt. Plusieurs essais sont effectués sur le prototype instrumenté. La mesure des températures à des lieux précis du prototype permet d’identifier les paramètres mal connus et de valider le modèle. / Permanent magnet synchronous machines are likely to break down due to poorly controlled heating. The goal of this study was to develop a generic and predictive thermal model to calculate the temperature of machines during the design phase simulating temperatures at various states. These states include: steady state, transient state, fault mode, axial circulating of a cooling fluid in the air-gap and high speed. The lumped parameter method was used to develop this generic thermal model. Meanwhile, a test bench and a prototype instrumented with thermocouples were manufactured to validate the model at the same time. Sensitivity studies of the results of the model to some parameters demonstrated that some convective coefficients, contact conductances and the thermal conductivity of the winding in the radial direction influenced the model. However, these parameters are poorly known, because empirical formulas or abacus are used to calculate them. Using, the prototype and the developed model, these parameters were identified. Three methods of identification were tested in order to find a strategy for the identification: the genetic algorithms method, the Gauss-Newton method and the Levenberg-Marquardt method. Many tests were done on the prototype. The measure of the temperatures on the specific place allows to identify these parameters and to validate the model.

Ultrasonic transducers are used in many fields of daily life, e.g. as parking aids or medical devices. To enable their usage also for mass applications small and low- cost transducers with high performance are required. Capacitive, micro-machined ultrasonic transducers (CMUT) offer the potential, for instance, to integrate compact ultrasonic sensor systems into mobile phones or as disposable transducer for diverse medical applications. This work is aimed at providing fundamentals for the future commercialization of CMUTs. It introduces novel methods for the acoustic simulation and characterization of CMUTs, which are still critical steps in the product development process. They allow an easy CMUT cell design for given application requirements. Based on a novel electromechanical model for CMUT elements, the device properties can be determined by impedance measurement already. Finally, an end-of-line test based on the electrical impedance of CMUTs demonstrates their potential for efficient mass production.

Evaluation of the performance of a product and its components under impact loading is one of the key considerations in design. In order to assess resistance to damage or ability to absorb energy through plastic deformation of a structural component, impact testing is often carried out to obtain the 'Force - Displacement' response of the deformed component. In this context, it may be noted that load cells and accelerometers are commonly used as sensors for capturing impact responses. A drop-weight impact testing set-up consisting of a moving impactor head with a lightweight piezoresistive accelerometer and a strain gage based compression load cell mounted on it is used to carry out the impact tests. The basic objective of the present study is to assess the accuracy of responses recorded by the said transducers, when these are mounted on a moving impactor head. In the present work, a novel approach of theoretically evaluating the responses obtained from this drop-weight impact testing set-up for different axially loaded specimen has been executed with the formulation of an equivalent lumped parameter model (LPM) of the test set-up. For the most common configuration of a moving impactor head mounted load cell system in which dynamic load is transferred from the impactor head to the load cell, a quantitative assessment is made of the possible discrepancy that can result in load cell response. Initially, a 3-DOF (degrees-of-freedom) LPM is considered to represent a given impact testing set-up with the test specimen represented with a nonlinear spring. Both the load cell and the accelerometer are represented with linear springs, while the impacting unit comprising an impactor head (hammer) and a main body with the load cell in between are modelled as rigid masses. An experimentally obtained force-displacement response is assumed to be a nearly true behaviour of a specimen. By specifying an impact velocity to the rigid masses as an initial condition, numerical solution of the governing differential equations is obtained using Implicit (Newmark-beta) and Explicit (Central difference) time integration techniques. It can be seen that the model accurately reproduces the input load-displacement behaviour of the nonlinear spring corresponding to the tested component, ensuring the accuracy of these numerical methods. The nonlinear spring representing the test specimen is approximated in a piecewise linear manner and the solution strategy adopted and implemented in the form of a MATLAB script is shown to yield excellent reproduction of the assumed load-displacement behaviour of the test specimen. This prediction also establishes the accuracy of the numerical approach employed in solving the LPM system. However, the spring representing the load cell yields a response that qualitatively matches the assumed input load-displacement response of the test specimen with a lower magnitude of peak load. The accelerometer, it appears, may be capable of predicting more closely the load experienced by a specimen provided an appropriate mass of the impactor system i.e. impacting unit, is chosen as the multiplier for the acceleration response. Error between input and computed (simulated) responses is quantified in terms of root mean square error (RMSE). The present study additionally throws light on the dependence of time step of integration on numerical results. For obtaining consistent results, estimation of critical time step (increment) is crucial in conditionally stable central difference method. The effect of the parameters of the impact testing set-up on the accuracy of the predicted responses has been studied for different combinations of main impactor mass and load cell stiffness. It has been found that the load cell response is oscillatory in nature which points out to the need for suitable filtering for obtaining the necessary smooth variation of axial impact load with respect to time as well as deformation. Accelerometer response also shows undulations which can similarly be observed in the experimental results as well. An appropriate standard SAE-J211 filter which is a low-pass Butterworth filter has been used to remove oscillations from the computed responses. A load cell is quite capable of predicting the nature of transient response of an impacted specimen when it is part of the impacting unit, but it may substantially under-predict the magnitudes of peak loads. All the above mentioned analysis for a 3 DOF model have been performed for thin-walled tubular specimens made of mild steel (hat-section), an aluminium alloy (square cross-section) and a glass fibre-reinforced composite (circular cross-section), thus confirming the generality of the inferences drawn on the computed responses. Further, results obtained using explicit and implicit methodologies are compared for three specimens, to find the effect, if any, on numerical solution procedure on the conclusions drawn. The present study has been further used for investigating the effects of input parameters (i.e. stiffness and mass of the system components, and impact velocity) on the computed results of transducers. Such an investigation can be beneficial in designing an impact testing set-up as well as transducers for recording impact responses. Next, the previous 3 DOF model representing the impact testing set-up has been extended to a 5 DOF model to show that additional refinement of the original 3 DOF model does not substantially alter the inferences drawn based on it. In the end, oscillations observed in computed load cell responses are analysed by computing natural frequencies for the 3 DOF lumped parameter model. To conclude the present study, a 2 DOF LPM of the given impact testing set-up with no load cell has been investigated and the frequency of oscillations in the accelerometer response is seen to increase corresponding to the mounting resonance frequency of the accelerometer. In order to explore the merits of alternative impact testing set-ups, LPMs have been formulated to idealize test configurations in which the load cell is arranged to come into direct contact with the specimen under impact, although the accelerometer is still mounted on the moving impactor head. One such arrangement is to have the load cell mounted stationary on the base under the specimen and another is to mount the load cell on the moving impactor head such that the load cell directly impacts the specimen. It is once again observed that both these models accurately reproduce the input load-displacement behaviour of the nonlinear spring corresponding to the tested component confirming the validity of the model. In contrast to the previous set-up which included a moving load cell not coming into contact with the specimen, the spring representing the load cell in these present cases yields a response that more closely matches the assumed input load-displacement response of a test specimen suggesting that the load cell coming into direct contact with the specimen can result in a more reliable measurement of the actual dynamic response. However, in practice, direct contact of the load cell with the specimen under impact loading is likely to damage the transducer, and hence needs to be mounted on the moving head, resulting in a loss of accuracy, which can be theoretically estimated and corrected by the methodology investigated in this work.

Dans un cadre de modélisation des machines électriques, la méthode qui connaît une grande popularité, car réputée pour la qualité de ses résultats est la méthode des éléments finis. Cependant, les temps de calcul deviennent importants lorsque les modèles éléments finis sont associés à une démarche d’optimisation et de prédimensionnement dans le cadre d’un cahier des charges complexe. Les méthodes de modélisation bien souvent utilisées comme alternative aux éléments finis sont les approches de modélisation par constantes localisées. Ces dernières se prêtent bien aux différentes physiques impliquées dans le fonctionnement des machines électriques, i.e. électromagnétique, mécanique et thermique. Ainsi, les stratégies de conception optimisée d’une machine électrique utilisent ces modèles pour déterminer les propriétés et performances de cette dernière dans différentes conditions de fonctionnement. Cependant, la mise en place de ce type de modèles nécessite un temps de développement important par manque d’outils dédiés tels que ceux existants pour les éléments finis. Dans le contexte électromagnétique, les travaux de cette thèse présentent une contribution à l’approche de modélisation par réseaux de réluctances par le développement d’outils permettant leurs générations automatiques. Cette approche est intégrée dans un outil permettant le traitement automatisé d'une géométrie, fournissant un modèle précis dans un délai plus court que celui nécessaire à la construction d'un modèle dédié. L’outil, intégralement développé sur MATLAB®, a été appelé MRNsoftware (pour Mesh-based Reluctance Network Software). Ce mémoire s’organise en quatre parties. Le premier chapitre est consacré à un état de l’art détaillé sur les méthodes de modélisation par réseaux de réluctances. Dans la deuxième partie, nous abordons les méthodologies mises en place en se basant sur un maillage de l’espace d'étude par des blocs élémentaires bidirectionnels et dans le cadre d’un maillage conforme. Le maillage non conforme fera l’objet du troisième chapitre. Une interpolation des potentiels se révélera utile pour connecter les différentes branches des interfaces de non-conformité dans le maillage de l’espace d’étude. Différents découpages d’une même structure sont testés et la précision ainsi que le temps d’évaluation des modèles en réseaux de réluctances sont comparés aux modèles de référence réalisés par éléments finis. Le quatrième chapitre présente en premier lieu l’interface graphique de l’outil. Par la suite, les approches de modélisation développées seront utilisées pour réaliser les modèles de la machine linéaire à aimants permanents et la machine linéaire à commutation de flux à excitation bobinée. Ces approches de modélisation sont le fruit de la collaboration entre les laboratoires SATIE et GREAH et s’inscrivent dans la problématique générale de développement d’outils de modélisation multiphysiques de dispositifs électromagnétiques en vue de leurs dimensionnements optimisés. / In the field of electrical machine modeling, the method that is experiencing great popularity as renowned for the quality of its results is the finite element method. However, computation time becomes important when the finite element models are associated with an optimization and predesign process as part of a complex technical specification sheet. The alternate modeling solution is the lumped parameter models approach. The latter is well suited for the individual physical domains involved in the operation of electrical machines, namely electromagnetic, mechanical and thermal. The latter is well suited for the individual physical domains involved in the operation of electrical machines, namely electromagnetic, mechanical and thermal. Thus, electric machine design routines have been used to determine the properties and performance of the latter under different operating conditions. However, the implementation of these modeling approaches requires significant development time for lack of dedicated tools such as those existing for the finite element method. In the electromagnetic context, the work of this thesis presents a contribution to the reluctance network modeling approach by developing tools allowing their automatic generation. This approach is integrated into a software tool allowing the automated processing of a geometry, providing a precise model in a shorter time than that required for the construction of a dedicated model. The tool, fully developed on MATLAB®, has been called MRNsoftware (for Mesh-based Reluctance Network Software). This dissertation contains four chapters. The first chapter is devoted to a detailed state of the art on reluctance network modeling methods. In the second chapter, we discuss the methodologies implemented based on a conformal mesh of the study space by bidirectional elementary blocks. The non-conformal mesh will be the subject of the third chapter. Magnetic scalar potential interpolation will prove useful to connect the different branches of the block elements at the edge of the non-conformal interfaces. Different mesh patterns of the same structure are tested and the accuracy as well as the evaluation time of the reluctance network models are compared with the finite element reference models. The fourth chapter presents, at first, the graphical interface of the tool. Subsequently, the developed modeling techniques are used to realize the models of the permanent magnet linear machine and the linear wound excitation linear machine. These modeling approaches are the result of the cooperation between SATIE and GREAH laboratories and are part of the general endeavor of developing multiphysics modeling tools for the optimal sizing of electromagnetic devices.