Materiais piezocompósitos laminados são compostos por camadas de material piezelétrico, metálico e compósito (matriz epóxi com fibras de carbono ou de vidro), que possibilitam obter vantagens em relação aos materiais piezelétricos convencionais, permitindo obter características superiores que não podem ser conseguidas pelos seus componentes de forma isolada como, por exemplo, maior flexibilidade e resistência mecânica ou menor peso. Sob esse enfoque, este trabalho tem por objetivo o desenvolvimento de Estruturas Piezocompósitas Laminadas (EPLA) que consistem basicamente em estruturas multicamadas, através do projeto da sua resposta transiente e harmônica visando aplicações dinâmicas. Entre as potenciais aplicações dessas estruturas, tem-se atuadores, motores, sonares e dispositivos de coleta de energia (\"energy harvester\"), sendo de muito interesse a melhora das suas características dinâmicas e o seu desempenho. O projeto dinâmico de uma EPLA é complexo, porém pode ser sistematizado utilizando o Método de Otimização Topológica (MOT). O MOT é um método baseado na distribuição de material num domínio de projeto fixo com o objetivo de extremizar uma função de custo sujeita às restrições inerentes do problema, combinando algoritmos de otimização e de elementos finitos. A formulação de MOT para o projeto dinâmico de EPLA pretende determinar tanto a topologia ótima dos materiais nas diferentes camadas quanto o sinal de polarização do material piezelétrico e o ângulo da fibra na camada compósita, tendo como finalidade a maximização da amplitude de vibração em pontos determinados (em atuadores) ou da geração de energia elétrica a partir de excitações mecânicas (em coletores de energia). Além disso, é formulado um problema combinando os enfoques harmônico e transiente com o intuito de customizar a resposta da EPLA, de modo que, o nível da resposta seja o mesmo perante diferentes tipos de onda de excitação (transdutores multi-entrada). O trabalho inclui as etapas de projeto, simulação, fabricação e caracterização de protótipos. / Laminated piezocomposite materials are composed by layers of piezoelectric, metal and composite material (epoxy matrix with carbon or glass fiber), which have advantages over conventional piezoelectric materials, because of their superior characteristics, which cannot be achieved by any of its components isolated, for example, more flexibility and strength and less weight. Under this approach, this work aims at the development of Laminated Piezocomposite Structures (LAPS) what primarily consist of multi-layer structures, through the transient and harmonic response design aiming at dynamic applications. Among the potential applications of these structures it can be cited actuators, motors, sonar devices and energy harvester, being of great interest the improvement of its dynamic characteristics and performance. The dynamic design of a LAPS is complex however it can be systematized by using the Topology Optimization Method (TOM). The TOM is a method based on the distribution of material in a fixed design domain with the aim of extremizing a cost function subject to constraints inherent to the problem by means of combining the optimization algorithms and the finite element method (FEM). The TOM formulation for the LAPS dynamic project aims to determine together the optimal topology of the materials for different layers, the polarization sign of the piezoelectric material and the fiber angle of the composite layer, in order to maximize the vibration amplitude at certain points (in actuators), or the generation of electrical energy from mechanical excitations (in energy harvesters). In addition, a TOM problem combining harmonic and transient approaches is formulated with the purpose of customizing EPLA response so that the response level is the same for different excitation waveforms (multi-entry transducers). The work includes design, simulation, manufacturing and characterization of prototypes.

Cerâmicas piezelétricas possibilitam posicionamento e sensoriamento de precisão ou captação de energia mecânica valendo-se do efeito piezelétrico, capaz de converter energia mecânica em elétrica ou o contrário. Para aprimorar ou estender as aplicações dessas cerâmicas, mecanismos flexíveis podem ser acoplados a elas, formando um Dispositivo Piezelétrico Flextensional (DPF). No projeto desse tipo de estrutura, o conceito de Material com Gradação Funcional (MGF) é interessante, já que esses materiais apresentam variações graduais de suas propriedades efetivas, permitindo a alternância entre um material mais flexível e um mais rígido de acordo com a intensidade de deslocamento desejada em cada região da estrutura. Assim, neste trabalho, implementa-se o Método de Otimização Topológica (MOT) no projeto de estruturas gradadas com o intuito de identificar as vantagens e desvantagens da utilização do conceito de MGF em DPF. Esse método combina algoritmos de otimização e o Métodos dos Elementos Finitos (MEF) para distribuir material dentro de um domínio fixo através de um modelo de material, que no presente caso é o de Material Isotrópico Sólido com Penalização (MISP) adaptado a MGF. Na fabricação desses dispositivos otimizados, utiliza-se a Sinterização por Jato de Plasma (SJP) para a obtenção de tarugos gradados que são submetidos a processos de eletro-erosão e de corte a laser. Por fim, para a verificação dos resultados numéricos, utiliza-se um vibrômetro para aferir os deslocamentos dos protótipos de atuadores fabricados. / Piezoelectric devices enable precision positioning and sensing or mechanical energy harvesting based on the piezoelectric effect. In flextensional piezoelectric devices, flexible coupling structures are attached to ceramics to improve or extend the application possibilities. On the design of this kind of structure, the concept of Functionally Graded Materials (FGM) can be interesting, since it allows gradual variations of its effective properties along some direction by mixing two or more materials. Thus, in order to identify the advantages and disadvantages of using FGM, graded flexible coupling structures that maximize the performance of piezoelectric devices are obtained by implementing the Topology Optimization Method (TOM). This method combines optimization algorithms and the Finite Element Method (FEM) to distribute material inside a fixed domain. In this work, the formulation is based on the Solid Isotropic Material with Penalization (SIMP) material model adapted for the FGM concept, which can represent continuous change in material properties along the domain. Resulting optimal graded topologies of coupling structures are presented and compared with homogeneous structures. Finally, graded devices are manufactured through Spark Plasma Sintering (SPS) technique in order to be characterized, validating numerical results. The numerical results demonstrate the TOM efficacy in designing functionally graded piezoelectric devices and show, by its implementation, significant gains in graded mechanisms performance when compared with analogous homogeneous. Furthermore, the feasibility of proposed manufacturing process is confirmed, allowing the fabrication of prototypes with expected behavior.

Esta tese de Doutorado busca contribuir na formação de subsídios científicos tanto para o projeto de uma prótese antropomórfica para membros superiores, quanto para a criação de um ambiente de treinamento, ou seja, um ambiente virtual de ação e realimentação das sensações, que poderá incorporar os mecanismos, atuadores, sensores ou estimuladores desenvolvidos. Ao final desta pesquisa, foram projetados e testados os mecanismos, sensores e alguns dispositivos de realimentação que farão parte do desenvolvimento de uma prótese de mão, a Mão de São Carlos, que possuirá características antropomórficas, para reproduzir os movimentos naturais da mão humana com um controle simplificado para o paciente. A motivação principal deste trabalho é diminuir o índice de rejeição das próteses para membros superiores, facilitando seu processo de treinamento e controle / This Doctoral thesis should contribute to the gathering of scientific subsidies for the project of a multifunction anthropomorphic upper limb prosthesis, in special the artificial hand, and for the creation of a training software, i.e., a software for the sensory's action and feedback. At the end of this research, the mechanisms, sensors, actuators and some feedback devices were designed and tested, that will be part of the development of a hand prosthesis, the São Carlos Hand, which will possess anthropomorphic characteristics, a simplified control for the patient and will reproduce the natural movements of the human hand. The main motivation of this work is to reduce the rejection index of the upper limb prosthesis, facilitating training process and control

O principal objetivo do controle de vibrações é a sua redução ou minimização, através da modificação automática da resposta estrutural. Em muitas situações isto é necessário para promover a estabilidade estrutural, e para alcançar o alto desempenho mecânico necessário em diversas áreas técnicas, tais como a engenharia aeroespacial, civil e mecânica, bem como a biotecnologia, inclusive em escala micro e nano mecânica. Uma alternativa é o uso de estruturas inteligentes, que são o resultado da combinação de sensores e atuadores integrados em uma estrutura mecânica, e um método de controle adequado. O principal objetivo deste trabalho é o desenvolvimento de rotinas computacionais para a simulação, via método dos elementos finitos, do controle ativo de estruturas inteligentes de cascas, placas e vigas delgadas de material compósito laminado com camadas de material piezoelétrico como sensores e/ou atuadores. Caracterizam esta pesquisa a utilização do elemento GPL-T9 de três nós e seis graus de liberdade mecânicos por nó, mais um grau de liberdade elétrico por camada piezoelétrica, assim como a avaliação de dois métodos de controle, o Proporcional-Integral-Derivativo (PID) e o Regulador Quadrático Linear ou Linear Quadratic Regulator (LQR), incluindo o LQR Modal, e a otimização da localização de pastilhas piezoelétricas através de um Algoritmo Genético (AG). Várias aplicações são apresentadas e os resultados obtidos são comparados aos disponíveis na literatura especializada. / The main objective of vibration control is its reduction or even its minimization by the automatic modification of the structural response. Sometimes this is necessary to increase structural stability and to attain a high mechanical behavior in several areas such as aerospace, civil and mechanical engineering, biotechnology, including macro, micro and nanomechanical scales. An alternative is to use a smart structure, which results of the combinations of integrated sensors and actuators in a mechanical structure and a suitable control method. Development of a computational code to simulate, using finite elements, the active control in smart structures such as slender shells, plates and beams of composite materials with embedded piezoelectric layers acting as actuators and sensors is the main objective of this work. This research is characterized by the use of the GPL-T9 element with three nodes and six mechanical degrees of freedom and one electrical degree of freedom per piezoelectric layer, by the evaluation of two control methods, the Proportional Integral Derivative (PID) and the Linear Quadratic Regulator (LQR), including the Modal LQR, and, finally by the optimization of piezoelectric patches placement using a Genetic Algorithm (GA). Several examples are presented and compared with those obtained by other authors.

Ce travail de thèse concerne la surveillance de l’état de santé de structures complexes en service. Elle est appliquée à des éléments d’une nacelle d’avion gros porteur. Ce travail est original et s’inscrit dans le cadre d’un projet, coordonné par AIRBUS Operations SAS et porté par AIRCELLE (Groupe SAFRAN). Les principales parties de la nacelle visées par notre démarche sont le capot de soufflante (fan cowl, composite monolithique) et la structure interne fixe du capot coulissant de l’inverseur de poussée (IFS, sandwich nid d’abeille). Ces structures réalisées en matériaux composites sont sujettes à de nombreux modes de dégradation(rupture de fibres, délaminage, fissures, etc…), qui peuvent impacter la durée de vie de la nacelle. De plus elles sont exposées à de nombreuses sollicitations environnementales dont des variations thermiques importantes (de -55 °C à +120°C). L’objectif de ce travail est la mise en place d’un système SHM visant à suivre l’état de santé de ces structures afin de détecter l’apparition de tels endommagements et de les localiser avant qu’ils ne conduisent à une dégradation de la structure; ceci de manière à permettre une maintenance prédictive. Des capteurs et actionneurs piézoélectriques (PZT) sont collés sur la structure et sont utilisés pour générer des ondes de Lamb et effectuer des mesures. La démarche SHM proposée s’appuie sur des mesures successives en partant d’un état initial considéré comme sain, puis en réalisant régulièrement des mesures de suivi. La différence entre des signaux mesurés pour deux états est analysée afin d’en extraire des caractéristiquessensibles à l’apparition de dommages. Après validation, des PZT ont été collés sur le fan cowl et l’IFS ainsi que sur des coupons et un banc d’essai approprié a été conçu afin de valider notre démarche. Du fait que l’on est amené à travailler sur des différences de signaux, des algorithmes de détection, basés sur les testsd’hypothèses statistiques et l’Analyse en Composantes Principales (ACP), ont dû être développés et validés. Ceci a d’abord été testé pour la détection de dommages contrôlés introduits d’abord dans des coupons, puis dans le fan cowl et dans l’IFS. Des algorithmes robustes (y compris aux variations de température) de localisation de ces dommages, basés sur l’extraction des temps de vol des ondes de Lamb, ont été développés et validés sur les structures étudiées. Une approche de quantification des incertitudes sur la localisation par inférence Bayésienne a été proposée en complément de la démarche déterministe implémentée. / This work aims at designing a Structural Health Monitoring (SHM) system for complex composite structures, with an application to elements of aeronautical nacelles. This work is original and is in the framework of a project, coordinated by AIRBUS Operations SAS and headed by AIRCELLE (SAFRAN Group). The main parts of the nacelle concerned with our approach are the fan cowl (composite monolithic) and the inner fixed structure (IFS, sandwich structure with honeycomb core) of the thrust reverser. These structures made from composite materials are subjected to many damages types which can affect nacelle’s useful life (fiber breaking, delamination, crack, etc…). Furthermore these structures are exposed to many environmental constraints which are for instance important thermal variations (from -55°C to +120°C). The objective of this work is to develop a SHM system aimed at detecting and localizing these damages, before the degradation of the whole structureoccurs. Piezoelectric (PZT) actuators and sensors are bonded on the structure and they are used to generate Lamb wave signals and perform measurements. The proposed SHM approach is based on successive measurements starting from an initial state, considered as healthy and regularly conducting follow-up. The difference in signals measured between two states is analyzed in order to extract some damages-sensitivesfeatures. After validation, PZT elements were glued to the fan cowl and to the IFS as well as on representative coupons and a suitable test bench is designed in order to validate our approach. Since one has to work on difference in signals, damage detection algorithms based on statistical hypothesis testing and PrincipalComponent Analysis (PCA) have been developed and validated. This was first tested for the detection of controlled damages introduced in coupons, and thereafter on the fan cowl and IFS. Robust damage localization algorithms (including with temperature variations) based on Time-of-flight (ToF) extraction from difference in signals, were developed and validated for these structures. A Bayesian approach for uncertainties quantification in the damage localization is also developed, leading to more accuracy in the damage localization results.

Afin d’introduire de nouvelles fonctions dans les commandes de vol d’hélicoptère, il est nécessaire d’augmenter les bandes passantes de leurs actionneurs. La modélisation réaliste de l’ensemble du système d’actionnement, rendant compte de ses limitations de puissance et de sa consommation énergétique, ainsi que l’amélioration des technologies existantes des dispositifs d’étanchéité et de guidage sont les deux enjeux principaux permettant d’atteindre la durée de vie souhaitée à hautes fréquences. Pour supporter ce nouveau développement, ce travail s’organise en trois parties. Une première partie présente l’état de l’art des commandes de vol de l’hélicoptère. Une architecture générique d’actionneur est proposée ainsi que la terminologie associée. Une deuxième partie porte sur l’élaboration d’un modèle de connaissance détaillé à l’aide du formalisme Bond-graph pour le système d’actionnement. Un effort particulier est porté sur la standardisation des composants et de leurs interfaces dans une démarche orientée objet. La dernière partie traite concerne les dispositifs d’étanchéité et de guidage au niveau des vérins de commande de vol. Compte tenu de l’objectif d’utiliser des paliers fluides, les différentes manières de générer une force normale au sein d’un film fluide sont analysées. Puis, une étude plus approfondie des butées hydrostatiques et des paliers hybrides coniques est ensuite conduite en tenant compte des contraintes propres à l’aéronautique. L’ensemble des connaissances acquises sont appliquées à un cas concret de développement assisté par les modèles d’actionneur hautes fréquences pour le contrôle actif de rotor. / In order to introduce new functions in helicopter flight controls, it is necessary to increase the bandwidths of their actuators. A realistic modelling of the entire actuating system, taking into account its power limitations and its energy consumption, as well as the improvement of the existing sealing and guiding device technologies are the two main challenges to reach the desired high frequency without reducing dramatically the actuator lifespan. To support this new development, this work is organized in three parts. A first part presents the state of the art of the helicopter flight controls. A generic actuator architecture is proposed as well as the associated terminology. A second part deals with the development of a detailed knowledge-model using the Bond-graph formalism for the actuating system. A particular effort is made to standardize the components and their interfaces in an object-oriented approach. The last part deals with the sealing and guiding devices of flight control cylinders. Given the objective of using fluid bearings, the various ways of generating a normal force within a fluid film are analyzed. Then, a more detailed study of the hydrostatic thrust bearings and the conical hybrid bearings is then carried out taking into account the constraints specific to aeronautics. All the knowledge acquired is applied to a concrete case of development, aided by the models, of high frequency actuators for the active control of a rotor.

Cette thèse s'inscrit dans le cadre d'un projet international (MARS) dont le but est d'améliorer l'efficacité du transport aérien par contrôle d'écoulement. Dans ce contexte, les travaux expérimentaux présentés ici sont focalisés sur l'utilisation d'un actionneur plasma à Décharge à Barrière Diélectrique (DBD) pour contrôler l'écoulement turbulent en aval d'une marche descendante (BFS) à Reh = 30000. Deux types de décharges sont étudiés : une ac-DBD qui produit une force électrohydrodynamqiue et une ns-DBD qui produit une onde de pression. Plusieurs positions de l'actionneur sont étudiés, de façon à optimiser les effets de la décharge sur l'écoulement. A l'aide d'un système PIV stéréoscopique, une étude étendue est destinée à l'évaluation des paramètres électriques du signal. Parmi tous les résultats obtenus, la zone de recirculation est réduite de 20%. De plus, d'autres quantités moyennes telles que les composantes de Reynolds, l'énergie cinétique et l'épaisseur de la couche cisaillée ont été aussi analysées. La dernière partie de la thèse comprend une analyse dynamique des modifications produites par l'actionneur. Pour cela, les structures dominantes sont examinées par leur signature fréquentielle et par une décomposition orthogonal aux valeurs propres (POD). Tous les résultats conduisent à la définition d'un cas d'action optimal pour lequel il est obtenu une réduction maximal de la longueur de rattachement. Le lâcher tourbillonnaire est renforcé par un mécanisme de type "lock-on". / This thesis is part of an international project (MARS) to improve air transport efficiency by active flow control strategy. In this context, the presented experimental works are focused on a surface Dielectric Barrier Discharge (DBD) as a solution to control the turbulent flow separation downstream a backward-facing step (BFS) at Reh = 30000. Two different plasma discharges are investigated: an ac-DBD resulting in a electrohydrodynamic force and a ns- DBD producing a pressure wave. Thanks to the versatility of plasma discharges and in order to optimize its effects on the flow, different locations of the DBD actuator have been investigated. Furthermore, an extended parametric study regarding the input variables of the discharge has been carried out by stereoscopic PIV. Among the obtained results, the mean reattachment length has been reduced up to 20%. In addition, other averaged quantities such as Reynolds stress components, the kinetic energy and the vorticity thickness of the separated shear layer have been analyzed to provide more extended information about the effects of the DBD actuator. The last part includes a dynamical analysis of the modifications produced by an optimal actuation. For that aim, the dominant structures are investigated by their signature in the frequency domain and by proper orthogonal decomposition (POD). All the results lead to the definition of an optimal actuation for which the mean reattachment position is reduced and the vortex shedding street can be reinforced by a lock-on control mechanism.

The number of flights have increased by 80% between 1990 and 2014, and the demand for air travel continues to increase. Even though the aviation sector contributes to economical and social benefits, it still affects the climate change [1]. A first step to minimize the environmental impact is to develop more electric aircraft (MEA), where the idea is to maximize the use of electricity and improve the overall energy effciency [2]. In most of today's aircraft, large mechanical transmission shafts with a lot of components are driven by central power units, termed centralized drive systems. By the use of electromechanical actuators (EMAs), a distributed drive systems can be used instead, which increases functionality, reduces mass, maintenance and energy consumption, as well as improves manufacturing and assembly [3].  When designing electromechanical actuators, one must take into account a lot of parameters that affect each other in various ways. It is often a time-consuming job to find the most optimal choice of architecture. Parameters such as temperature, load, lifetime and effciency to mention a few. This master thesis offers a new analytical tool for EMAs of primary and secondary flight control systems for Saab Avionics Systems. The aim of the analytical tool is to characterize the parts of the system and identify important parameters in order to find the most optimal choice of architecture. The tool focus on the main mechanical components such as the three-phase synchronous permanent magnet motor, power-off brake, two-stage planetary gearbox and ball screw. The tool developed in this project generates an initial design of the EMA with optimized dimensions in order to minimize both mass and energy consumption. It functions by identifying three main groups of parameters: The input parameters: fixed values defined by the customer demands The design parameters: variables that the user can change to find the optimal choice of architecture The output parameters: resulting values of either performance or dimensions By defining few design parameters for each component, and implementing multidisciplinary design optimization (MDO), the analytical tool can find an optimized solution for each specific project in a time-efficient way. The final values of the parameters characterize the performance of the EMA.

Les simulateurs d'accouchement sont des outils dédiés à la formation du personnel médical en gynécologie obstétrique. Le BirthSIM développé au laboratoire Ampère constitue une interface haptique de simulateur d'accouchement permettant de reproduire divers scénarios d'accouchement et de former les jeunes sages-femmes et obstétriciens aux différents gestes techniques nécessaires dans le cadre de leurs professions. Dans ce manuscrit, les récentes améliorations apportées au prototype du BirthSIM seront présentées. Parmi ces améliorations, deux sont particulièrement remarquables. La première concerne l'augmentation du nombre de degrés de liberté pilotés de l'interface. Ainsi, les travaux ayant permis le passage d'une interface ne comptant qu'un seul degré de liberté à quatre seront détaillés. Le BirthSIM est le seul simulateur d'accouchement qui intègre à la fois des actionneurs électriques et pneumatiques. La seconde évolution concerne le développement de lois de commande permettant d'améliorer le rendu haptique de l'interface. Les lois de commande retenues permettent d'asservir en position le BirthSIM, mais également de régler la raideur de l'interface. Ce réglage de raideur en coordonnées cartésiennes a pour objectif de reproduire le comportement de la tête fœtale en contact avec les tissus mous du bassin au cours d'une contraction. La loi de commande présentée dans ces travaux de thèse est une loi de commande non-linéaire synthétisée par backstepping. En effet, cette méthode permet de prendre en compte les phénomènes non-linéaires agissant sur le comportement des actionneurs pneumatiques. Cette commande, assurant le suivi d'une consigne de position et une modification de la raideur en temps réel à partir d'une stratégie de réglage de gain, a été testée à la fois en simulation et sur le prototype du BirthSIM. Les performances de cette commande sont également comparées à celles de lois de commande plus classiquement utilisées en robotique. / The childbirth simulators are developed for practitioner training in gynecology and obstetrics. The BirthSIM is a haptic interface which simulates various childbirth scenarios to teach obstetricians and midwives the technical delivery gestures. In this work, the latest improvements on the BirthSIM prototype will be presented. Two improvements are especially detailed. The first one consists in adding actuated degrees of freedom to the haptic interface. Thus, the works which have led to a new four degrees of freedom robot are presented. The BirthSIM is the only childbirth simulator which is actuated by electrical and pneumatic actuators. The aim of the second improvement is to synthesize control laws which improve the haptic rendering. The studied control laws allow the haptic interface to be controlled in position and its stiffness to be tuned in real time. This cartesian stiffness tuning is suitable to reproduce the behavior of the fetal head surrounded by the maternal pelvic muscles. The control law presented in this document have been obtained by the non-linear backstepping synthesis. Indeed, the non-linear phenomenons occurring in pneumatic cylinders can be taken into account by this method. The controller obtained in this work allows the BirthSIM end-effector to track a reference position but also allows the robot stiffness to be tuned in real time. The stiffness control is based on a gain tuning strategy. Finally, the performances have been evaluated in simulation and experimental tests. Those performances have also been compared to the other conventional compliant controllers of the robotic field.

<p>Hydrocephalus is a neurological disease characterized by abnormal accumulation of cerebral spinal fluid (CSF) in ventricle of brain. 1 in 1000 newborns are affected each year and it is life-threatening if left untreated. The golden standard of treatment is to surgically implant a shunt that divert excessive CSF away from ventricle to alleviate intraventricular pressure (ICP) in patient. Unfortunately, shunt failure rate is notoriously high because of obstruction of catheter intake pore. The obstruction is primary caused by normal and inflammatory tissue (biofilm) buildup over time. Shunt replacement surgery is typically required after only 1 year of implantation for 40% of patients. To prolong the lifespan of hydrocephalus shunt, we previously proposed and designed magnetic micro-actuators platform to remove biofilm mechanically. Removal of muscle cells and microbeads were demonstrated from wafer level devices on bench-top.</p><p> </p><p>To examine device efficacy in ventricular catheter, I developed magnetic actuator on polymer substrate. First, polyimide based flexible thin-film devices were microfabricated and integrated into a single-pore silicone catheter. A proof-of-concept self-clearing smart catheter was presented. Removal of microscopic biofilm was evaluated against bovine serum protein (BSA). Detachment of BSA up to 95% was achieved by shear stress from magnetic actuation. Next, I developed resistive deflection sensing using a metallic strain gauge, allowing device alignment with magnetic field for maximum energy delivery. In addition, auxiliary functionalities such as occlusion detection and flow rate measurement were demonstrated on catheter. Moreover, a new serpentine cantilever geometry with increased magnetic volume was proposed for improved delivery of torque and deflection. In a benchtop evaluation, we showed prolonged catheter drainage (7x) in a dynamic fluid environment containing macroscopic blood clots. Finally, using an intraventricular hemorrhage (IVH) porcine model, we observed that self-clearing catheter had longer survival than control catheter (80% vs. 0%) over the course of 6 weeks. Animals treated with magnetic actuation had significantly smaller ventricle size after 1 week of implantation.</p>