ABSTRACT Because of a great variety of tribocomponents and lubricants, the phenomenon of frictional magnetization and electrification between tribocomponents becomes more obvious. In order to understand the effects of frictional magnetization and electrification on tribology characteristics and miniature electrical control component signal, the frictional magnetization and electrification test under dry friction condition is investigated by the reciprocating electrification tester. Three material-pair types will be investigated their frictional magnetization and electrification behavior under various operating parameters, e.g. driver speed, normal load, and sliding distance. Moreover, the worn surface will be observed by the optical microscopy and SEM. Results show that the magnetization and electrification on friction surfaces increases with increasing load, and decreases with the carbon content of a material, and depends on material-pair. It is found that wear particles have been magnetized on the friction surface, even that the wear particles has been adhered to the surface caused by electro static action. Moreover, in the microscopic view, the frictional magnetization and electrification are related to both friction and wear.

Automotive engine mounts are used to support engine weight, protect engine from road inputs and isolate transmission of vibrations created by the engine, which has a drastic effect on the noise generated inside the passenger cabin. Most common types of engine mounts are elastomeric and hydraulic mounts, the former having better vibration isolation characteristics whereas the latter displays better shock isolation. Elastomeric mounts are widely used for their low initial cost, while hydraulic mounts with inertia track and decoupler are chosen for their good vibration isolation and shock excitation characteristics. However, hydraulic mounts with inertia track and decoupler are not appropriate for small segment and commercial vehicles due their high initial cost. In this thesis, the effect of the addition of a dry friction damper on the performance of elastomeric automobile engine mounts is investigated. Friction dampers are used to attenuate vibration amplitudes in many applications such as gas turbine engines, railway vehicles, space structures and civil buildings. In this study, a friction element is added to the engine mount at its axial direction and its effect is studied. Results show that, the addition of dry friction damping to the original system increases vibration isolation performance significantly at low frequencies / whereas, due to the increased stiffness of the system, at high frequencies dry friction damper has a mitigating effect on performance. In order to overcome this problem, original system parameters are modified. In the modified system a softer mount that increase vibration isolation performance at high frequencies / but, which might cause excessive static deflection due to reduced stiffness of the system is used. On the other hand, addition of dry friction damping prevents excessive static deflections due to the increased stiffness effect and also increases the performance at high frequencies due to the soft mount. Final results showed that vibration isolation performance at low frequencies increases considerably while vibration isolation performance at high frequency is similar and even slightly better than the original system with addition of dry friction damping.

Déterminer la durée de vie d'une pièce sous excitation vibratoire est l'un des enjeux majeurs dans l'ingénierie mécanique. Afin de donner une estimation fiable de la durée de vie, un calcul correct de champ de contrainte, qui est fortement lié à la forme et l'amplitude modale est obligatoire. Cependant, le calcul de réponse d'une structure assemblée est difficile, surtout avec la présence de frottement sec aux interfaces de liaisons qui entraîne un amortissement non linéaire. La recherche de la thèse commence par une identification phénoménologique de l'amortissement induit par le frottement sec avec 3 modèles analytiques, notamment la plaque sandwich, la rotule frottante et la plaque von Kármán. Après la caractérisation de l'amortissement structural au 1er et 2ème ordre, les influences des paramètres comme la pression de serrage, le rapport d'épaisseurs ainsi que le nombre de soudures sont analysés. La deuxième partie des travaux traite les problèmes d'amortissement avec une géométrie de dimension finie. La plaque de von Kármán est reprise dans l'étude et une méthode hybride de différences finies et d'éléments finis est adopté pour résoudre le couplage entre la flexion et les efforts internes. Une attention particulière est portée à la notion de modes non linéaires dans le cas de la plaque von Kármán. Les conditions nécessitant l'introduction de modes non linéaires sont identifiées. Le champ de force fictif qui est proposé dans l'étude sur la plaque von Kármán est ensuite introduit dans le cas de la plaque sandwich. Puis la propagation de glissement et l'influence de champ fictif sont étudiées. Afin de vérifier les phénomènes trouvés dans les études théoriques, une installation expérimentale est conçue et montée pour l'amortissement structural au premier ordre. Dans la dernière partie qui est basée sur les observations faites dans les études précédentes, une méthode de calcul de l'amortissement dans un environnement industriel est proposée. Cette méthode permet de donner un amortissement pour chaque mode isolé. / The determination of a component's lifetime under vibrational excitation is one of the most difficult challenges in mechanical engineering. In order to provide a reliable estimation of lifetime, a correct calculation of stress field, which depends on the modal form and its amplitude, is needed. However, the vibrational response calculation on an assembled structure is not easy, especially with the nonlinear structural damping induced by frictional contact surface. The research in the current thesis starts from the phenomenological identification of damping with the help of 3 analytical models, in particular the sandwich plate, rotational joint and von Karman plate. Structural damping of 1st and 2nd order are identified. The influence of parameters like clamping pressure, thickness ratio and number of welding points are also analyzed. The second part of the research focuses on problems with finite dimensions. The von Karman plate serves as the subject of the study and a hydride method which combines FDM and FEM is proposed to solve the coupling between defection and in-plane force field. A special attention is paid to nonlinear mode theory, the conditions under which the nonlinear mode is necessary are identified. The fictive force field proposed in the study of von Kármán plate is then applied to the sandwich plate model. The slipping's propagation as well as the influence of fictive force field are studied. To verify the existence of the found phenomena in the previous studies, an experimental setup is designed and mounted for the 1st order structural damping. In the last part of the research, which is based on the observations previously obtained from academic models, a calculation method of friction-induced damping in structures with complex geometries is proposed for the application in the industrial environment. This methods enables the estimation of damping for each isolated mode.

The benefits of intentional friction damping to reduce the occurrence of wear and premature failure of turbomachinery bladed-disk assemblies are well known and many studies on this topic have focused on the analysis and prediction of the complicated nonlinear forced response exhibited by these structures. In this research, extensions of the recently introduced multi-harmonic Hybrid Frequency-Time method are proposed for the efficient analysis of the response of realistic structures featuring displacement-dependent nonlinearities, such as the friction and impact phenomena that may occur in the presence of friction dampers or when two parts of the same structure periodically contact each other. These theoretical extensions are adapted to the study of large scale, industrial bladed-disk structures that may feature cyclic symmetry or mistuning. Two analysis techniques are developed for the modeling of displacement-dependent nonlinearities. In the first technique friction dampers are modeled as nonlinear operators representing the contact forces acting on the blades, from the simple case of monodirectional friction with constant normal load to the more complex case of three dimensional contact with variable normal load. The analysis of the forced response of several nonlinear systems illustrates the capabilities of this approach as well as the complexity of the typical behavior exhibited by friction damped structures. The second technique introduced helps analyze structures experiencing intermittent contact or friction between two parts or sub-components of the same assembly. This method is applied to the study of the forced response of several simple systems and is used with great efficiency to predict the nonlinear behavior of a beam with a crack. This approach also allows the dampers to be modeled realistically as stand-alone components appended to the bladed disk assembly. In this case the bladed disk assembly as well as the friction dampers are modeled as independent structures that interact at their contacting interfaces. This allows the use of detailed finite element models of dampers rather than having to make simplifying assumptions regarding their geometry. These two methods are applied to the study of the nonlinear forced response a realistic bladed-disk assembly featuring a wedge damper model and a structure-like damper model.

This thesis is addressed to the understanding of the mechanisms at the origin of the contact wave fields at frictional interfaces and its relationship with the local characteristics of the surfaces in contact, as well as with the global dynamics and macroscopic frictional behaviour of the system. The aim of this work is to provide insights on the generation and propagation of the waves through the contact both to avoid instabilities and to control their effect on friction. The work is organized in two main parts. The first part presents the development of a non-linear finite element analysis in large transformations of the dynamic rupture at the interface with contact friction separating two bodies (isotropic and elastic) without relative motion. A rupture is considered when an initially sticking zone shifts in sliding state. The properties of the obtained ruptures are analyzed for a flat interface between dissimilar materials in function of the nucleation energy; then the effect of the interface roughness is analyzed. The differentiated rupture inside the asperities and the conditions for coupling and uncoupling between the waves radiating in the two bodies have been also investigated. In the second part, the analysis deals with the sliding onset between two bodies in contact. The sliding between two bodies made of different isotropic elastic materials and separated by a frictional interface is simulated. The evolution along the time of the global normal and tangential forces is analyzed, relating it to the local phenomena occurring at the interface. This part tries to investigate how micro-slips at the interface, acting as distributed ruptures, trigger the macro-slips between the two bodies. The interaction between local and global dynamics is also studied. Finally a numerical parameter space study is carried out, as a function of several system parameters (contact law, friction coefficient, material damping, normal load, translational velocity and regularization time). The results show the key role of the micro-slips and precursors (detectable wave propagations that occur at tangential global force well below the critical value expected by the friction law) in triggering the macro-slip between the two bodies. Depending on their distribution and magnitude the evolution of the contact forces passes from stick-slip-like behaviour to continuous sliding. The local dynamics at the contact (wave and rupture propagation) is linked to the global behaviour of the system (stick-slip, continuous sliding, induced vibrations); the effect of the contact and system parameters on the transfer of vibrational energy between the sliding contact and the system is investigated. The numerical results obtained by the two parts of the work show a good agreement with experimental results in literature.

[pt] Neste trabalho estuda-se um sistema de acompanhamento de alvos, também conhecido como sistema de rastreamento de alvos, do tipo pan-tilt atuado por motores de corrente contínua e fixo em um corpo em movimento. Para tanto é montada uma bancada de testes e implementa-se um programa de simulação. A modelagem para o programa é feita no domínio do tempo, permitindo a utilização de equações bastante complexas para representar o sistema, o que não é possível quando se utiliza modelos no domínio da freqüência. Apesar de se modelar o sistema com corpos rígidos, flexibilidades e amortecimentos estruturais devido aos redutores de velocidade são considerados. Erros nos sensores, folgas nos redutores, atritos seco e viscoso, limites de saturação para as correntes e tensões nas armaduras dos motores também são considerados. Um método para a inclusão dos atrasos de tempo para atualização dos sinais de controle e dados obtidos pelos sensores durante a integração numérica das equações de movimento é apresentado. Para controlar o sistema utilizam-se controladores que não requerem o modelo matemático da planta, tanto na bancada de testes como no programa de simulação. Três tipos diferentes de arquitetura de controle são propostas, chamadas neste trabalho de tipo 1, tipo 2 e tipo 3. A complexidade delas aumenta à medida que mais sensores estão disponíveis no sistema. A arquitetura do tipo 1 destina-se a sistemas onde se possui apenas sensores que fornecem os erros angulares de azimute e elevação do alvo. Se, além deste sensor, também houver sensores para medir as posições angulares relativas entre os elos do mecanismo usa-se a arquitetura do tipo 2. Se houver, ainda, sensores de velocidades angulares inerciais pode-se utilizar a arquitetura do tipo 3. Por fim são apresentados resultados de experimentos e simulações onde se compara o desempenho do sistema com cada tipo de arquitetura de controle. / [en] A study on a pan-tilt type target tracking system actuated by permanent magnet DC motors and assembled in a moving body is presented in this work. To achieve such objective, an experimental test bed is constructed and a simulation program is implemented. The mechanical model is derived and simulated in time domain. This approach allows using accurate non-linear equations to represent system behavior, otherwise infeasible in frequency domain. Although the system is modeled with rigid bodies, flexibility and structural damping due to the gearboxes are considered. Sensor errors, backlash in the gearboxes, dry and viscous friction, saturation limits for armature current and tension of the motors are also considered. A method to include the time delays for the control signal updates, as well as time delays due to sensor dynamic response, during the numerical integration of the equations of motion, is presented. Controllers that require no mathematical model of the plant are employed in the experimental test bed and in the simulation program. Three different control architectures are proposed, called in this work type 1, type 2 and type 3. Their complexity increases depending on the number of available sensors. The type 1 is applied to systems with only one sensor that provides the targets angular azimuth and elevation errors. If, besides this sensor, sensors to measure the relative angular positions between the mechanism links are available type 2 architecture is used. In addition, if sensors to measure inertial angular speeds are also available, type 3 architecture can be used. Finally, experimental and numerical results, comparing system performance with each control architecture are presented.

No description available.

For internal combustion engines used in heavy-duty vehicles, increased engine efficiency and consequently reduced CO2 emissions can be obtained if the engine speed can be kept within an optimal speed range. This requires swift and frequent gear shifts where the dry friction clutch is utilized. Enhanced dry clutch simulation models and a better understanding of the involved phenomena can assist the development towards swifter gear shifts and help reduce CO2 emissions. The work presented in this thesis focuses on the modelling of dry clutch systems for heavy-duty applications and their effect on the torsional response of the driveline during transient events such as clutch engagement and disengagement. During these events it is primarily the first vibration mode of the driveline that is active and consequently it is possible to greatly reduce theof degrees of freedom (DOFs) of the powertrain model and still capture the relevant dynamics of the powertrain. The reduced set of differential equationsdescribe the torsional motion of the powertrain and the equations of motion are solved numerically in the time-domain. From a mathematical point ofview, the equations of motion turn "stiff" when the clutch is locked. This issue is resolved by utilizing numerical solution techniques suitable for stiff differential equations. In the simulations it was observed that no engine torque fluctuations were transferred through the slipping clutch. Consequently the response of the driveline is purely modal during sliding. If the gradient of the coefficient of friction is negative the modal response is possibly unstable with exponentially growing vibration amplitudes as an effect. Moreover, the way in which the clamp load evolves during clutch engagement is found to severely effect the excitation of transient vibrations during clutch synchronization. It can be shown that reducing the gradient of the evolving clamp load at the onset of sliding will reduce the amplitude of the friction induced vibrations. Reducing the torsional vibration amplitudes will help avoid the jerky motion of the vehicle during launch and increase comfort for driver and passengers. / Reduced transmission vibrations - reduced energy consumption and environmental impacts together with an increased competitiveness. Swedish Energy Agency (project No. 42100-1)

Trial and error and the use of highly time-consuming methods are often necessary for modeling, simulating and characterizing nonlinear dynamical systems. However, for the rather common special case when a nonlinear system has linear relations between many of its degrees of freedom there are particularly interesting opportunities for more efficient approaches. The aim of this thesis is to develop and validate new efficient methods for the theoretical and experimental study of mechanical systems that include significant zero-memory or hysteretic nonlinearities related to only small parts of the whole system. The basic idea is to take advantage of the fact that most of the system is linear and to use much of the linear theories behind forced response simulations. This is made possible by modeling the nonlinearities as external forces acting on the underlying linear system. The result is very fast simulation routines where the model is based on the residues and poles of the underlying linear system. These residues and poles can be obtained analytically, from finite element models or from experimental measurements, making these forced response routines very versatile. Using this approach, a complete nonlinear model contains both linear and nonlinear parts. Thus, it is also important to have robust and accurate methods for estimating both the linear and nonlinear system parameters from experimental data. The results of this work include robust and user-friendly routines based on sinusoidal and random noise excitation signals for characterization and description of nonlinearities from experimental measurements. These routines are used to create models of the studied systems. When combined with efficient simulation routines, complete tools are created which are both versatile and computationally inexpensive. The developed methods have been tested both by simulations and with experimental test rigs with promising results. This indicates that they are useful in practice and can provide a basis for future research and development of methods capable of handling more complex nonlinear systems.

There are many active and passive vibration control techniques to reduce the effect of energy on structures which emerges during an earthquake and reduce the displacement of buildings that is caused by ground acceleration. Main advantage of passive vibration control techniques over active vibration control techniques is / no external power or a sensor is required for passive vibration control devices (PVCDs) and it results in lower installation and maintenance costs. However, PVCDs require a predefined optimum damping ratio and optimum damping distribution along the structure since they are not adaptive to changing ground acceleration values. During the design of the PVCDs numerous factors such as building properties and earthquake characteristics should be considered. Dry friction damper is an example of PVCD and has an extensive usage in many different fields due to its high energy damping capacity with low cost and ease of installation. In this thesis, damping of seismic energy at buildings with dry friction dampers is investigated and a new optimization method is developed in frequency domain by employing Describing Function Method (DFM) which reduces the computational effort compared to the time domain and finite element solutions drastically. The accuracy and verification of the presented method is investigated by comparing the frequency domain results with time marching solutions. Furthermore, damper placement and slip forces on the dampers are optimized for single and multi-story buildings equipped with dry friction dampers by utilizing the developed method.