791 resultados para vibration-based structural health monitoring
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El objetivo de este trabajo es analizar las propiedades dinámicas de una presa bóveda de doble curvatura (presa de La Tajera, Guadalajara) para ajustar un modelo de elementos finitos. Para ello se han utilizado acelerómetros de alta sensibilidad sincronizados inalámbricamente. Se han obtenido las frecuencias, amortiguamientos y formas modales frente a los efectos de las acciones de tipo ambiental (viento, paso de vehículos). Se ha modelado mediante elementos finitos la presa y su cimiento incorporando el efecto del nivel del embalse. Con las propiedades dinámicas de la estructura halladas numéricamente se ha realizado un plan de medidas en los puntos que se consideraban más significativos. Tras realizar las medidas, se ha procedido al análisis de resultados mediante un Análisis Modal Operacional. Ello permite estimar los parámetros modales (frecuencias, amortiguamientos y formas modales) experimentalmente y se ha valorado el alcance de los mismos. Posteriormente viene la parte fundamental de este trabajo, que es el ajuste del modelo de elementos finitos inicial considerando el comportamiento dinámico obtenido experimentalmente. El modelo actualizado puede utilizarse dentro de un sistema de detección de daños, o por ejemplo, para el estudio del comportamiento ante un sismo considerando la interacción presa-embalse-cimiento. The purpose of this paper is to study the dynamic characteristics of a double curvature arch dam (La Tajera arch dam) for a Finite Element Model Updating. To achieve it, high sensitivity accelerometers synchronized wirelessly have been used. The system modal dampings, natural frequencies mode shapes are identified using output only identification techniques under environmental loads (wind, vehicles). Firstly, a finite element model of the dam-reservoir-foundation system was created. Once the dynamic properties of the structure were numerically obtained, a testing plan was then carried out identifying the most significant test points. After the measurements were carried out, an Operational Modal Analysis was performed to obtain experimentally the structure dynamic properties: natural frequencies, modal dampings and mode shapes. experimentally and to assess its reach. Then, the finite element model updating of the initial model was carried out to match the recorded dynamic behavior. The updated model may be used within a structural health monitoring and damage detection system or, as it is proposed on this thesis, for the analysis of the seismic response of arch dam-reservoir-foundation coupled systems
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La dinámica estructural estudia la respuesta de una estructura ante cargas o fenómenos variables en el tiempo. En muchos casos, estos fenómenos requieren realizar análisis paramétricos de la estructura considerando una gran cantidad de configuraciones de diseño o modificaciones de la estructura. Estos cambios, ya sean en fases iniciales de diseño o en fases posteriores de rediseño, alteran las propiedades físicas de la estructura y por tanto del modelo empleado para su análisis, cuyo comportamiento dinámico se modifica en consecuencia. Un caso de estudio de este tipo de modificaciones es la supervisión de la integridad estructural, que trata de identificar la presencia de daño estructural y prever el comportamiento de la estructura tras ese daño, como puede ser la variación del comportamiento dinámico de la estructura debida a una delaminación, la aparición o crecimiento de grieta, la debida a la pérdida de pala sufrida por el motor de un avión en vuelo, o la respuesta dinámica de construcciones civiles como puentes o edificios frente a cargas sísmicas. Si a la complejidad de los análisis dinámicos requeridos en el caso de grandes estructuras se añade la variación de determinados parámetros en busca de una respuesta dinámica determinada o para simular la presencia de daños, resulta necesario la búsqueda de medios de simplificación o aceleración del conjunto de análisis que de otra forma parecen inabordables tanto desde el punto de vista del tiempo de computación, como de la capacidad requerida de almacenamiento y manejo de grandes volúmenes de archivos de datos. En la presente tesis doctoral se han revisado los métodos de reducción de elementos .nitos más habituales para análisis dinámicos de grandes estructuras. Se han comparado los resultados de casos de estudio de los métodos más aptos, para el tipo de estructuras y modificaciones descritas, con los resultados de aplicación de un método de reducción reciente. Entre los primeros están el método de condensación estática de Guyan extendido al caso con amortiguamiento no proporcional y posteriores implementaciones de condensaciones dinámicas en diferentes espacios vectoriales. El método de reducción recientemente presentado se denomina en esta tesis DACMAM (Dynamic Analysis in Complex Modal space Acceleration Method), y consiste en el análisis simplificado que proporciona una solución para la respuesta dinámica de una estructura, calculada en el espacio modal complejo y que admite modificaciones estructurales. El método DACMAM permite seleccionar un número reducido de grados de libertad significativos para la dinámica del fenómeno que se quiere estudiar como son los puntos de aplicación de la carga, localizaciones de los cambios estructurales o puntos donde se quiera conocer la respuesta, de forma que al implementar las modificaciones estructurales, se ejecutan los análisis necesarios sólo de dichos grados de libertad sin pérdida de precisión. El método permite considerar alteraciones de masa, rigidez, amortiguamiento y la adición de nuevos grados de libertad. Teniendo en cuenta la dimensión del conjunto de ecuaciones a resolver, la parametrización de los análisis no sólo resulta posible, sino que es también manejable y controlable gracias a la sencilla implementación del procedimiento para los códigos habituales de cálculo mediante elementos .nitos. En el presente trabajo se muestra la bondad y eficiencia del método en comparación con algunos de los métodos de reducción de grandes modelos estructurales, verificando las diferencias entre sí de los resultados obtenidos y respecto a la respuesta real de la estructura, y comprobando los medios empleados en ellos tanto en tiempo de ejecución como en tamaño de ficheros electrónicos. La influencia de los diversos factores que se tienen en cuenta permite identificar los límites y capacidades de aplicación del método y su exhaustiva comparación con los otros procedimientos. ABSTRACT Structural dynamics studies the response of a structure under loads or phenomena which vary over time. In many cases, these phenomena require the use of parametric analyses taking into consideration several design configurations or modifications of the structure. This is a typical need in an engineering o¢ ce, no matter the structural design is in early or final stages. These changes modify the physical properties of the structure, and therefore, the finite element model to analyse it. A case study, that exempli.es this circumstance, is the structural health monitoring to predict the variation of the dynamical behaviour after damage, such as a delaminated structure, a crack onset or growth, an aircraft that suffers a blade loss event or civil structures (buildings or bridges) under seismic loads. Not only large structures require complex analyses to appropriately acquire an accurate solution, but also the variation of certain parameters. There is a need to simplify the analytical process, in order to bring CPU time, data .les, management of solutions to a reasonable size. In the current doctoral thesis, the most common finite element reduction methods for large structures are reviewed. Results of case studies are compared between a recently proposed method, herein named DACMAM (Dynamic Analysis in Complex Modal space Acceleration Method), and different condensation methods, namely static or Guyan condensation and dynamic condensation in different vectorial spaces. All these methods are suitable for considering non-classical damping. The reduction method DACMAM consist of a structural modification in the complex modal domain which provides a dynamic response solution for the reduced models. This process allows the selection of a few degrees of freedom that are relevant for the dynamic response of the system. These d.o.f. are the load application points, relevant structural points or points in which it is important to know the response. Consequently, an analysis with structural modifications implies only the calculation of the dynamic response of the selected degrees of freedom added, but with no loss of information. Therefore, mass, stiffness or damping modifications are easily considered as well as new degrees of freedom. Taking into account the size of the equations to be solved, the parameterization of the dynamic solutions is not only possible, but also manageable and controllable due to the easy implementation of the procedure in the standard finite element solvers. In this thesis, the proposed reduction method for large structural models is compared with other published model order reduction methods. The comparison shows and underlines the efficiency of the new method, and veri.es the differences in the response when compared with the response of the full model. The CPU time, the data files and the scope of the parameterization are also addressed.
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We present an optical sensing methodology to estimate the fatigue damage state of structures made of carbon fiber reinforced polymer (CFRP), by measuring variations on the surface roughness. Variable amplitude loads (VAL), which represent realistic loads during aeronautical missions of fighter aircraft (FALSTAFF) have been applied to coupons until failure. Stiffness degradation and surface roughness variations have been measured during the life of the coupons obtaining a Pearson correlation of 0.75 between both variables. The data were compared with a previous study for Constant Amplitude Load (CAL) obtaining similar results. Conclusions suggest that the surface roughness measured in strategic zones is a useful technique for structural health monitoring of CFRP structures, and that it is independent of the type of load applied. Surface roughness can be measured in the field by optical techniques such as speckle, confocal perfilometers and interferometry, among others.
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The Santas Justa and Rufina Gothic church (fourteenth century) has suffered several physical, mechanical, chemical, and biochemical types of pathologies along its history: rock alveolization, efflorescence, biological activity, and capillary ascent of groundwater. However, during the last two decades, a new phenomenon has seriously affected the church: ground subsidence caused by aquifer overexploitation. Subsidence is a process that affects the whole Vega Baja of the Segura River basin and consists of gradual sinking in the ground surface caused by soil consolidation due to a pore pressure decrease. This phenomenon has been studied by differential synthetic aperture radar interferometry techniques, which illustrate settlements up to 100 mm for the 1993–2009 period for the whole Orihuela city. Although no differential synthetic aperture radar interferometry information is available for the church due to the loss of interferometric coherence, the spatial analysis of nearby deformation combined with fieldwork has advanced the current understanding on the mechanisms that affect the Santas Justa and Rufina church. These results show the potential interest and the limitations of using this remote sensing technique as a complementary tool for the forensic analysis of building structures.
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Polymer FBGs have advantages for sensing because of low Young's modulus, high temperature sensitivity, large strain range and so on. They are attractive for many niche applications such as structural health monitoring of composite materials, biochemical and biomedical sensing. While polymer FBGs have been developed for some time, polymer microfibre Bragg gratings are developed only recently and have shown to introduce some interesting features, e.g. increased pressure sensitivity to pressure / force and improved response time to humidity. We will report and discuss the recent work on polymer FBG and polymer microfibre Bragg gratings as well as their applications such as accelerometer, humidity sensor and force and pressure sensor. © 2015 OSA.
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L'elaborato tratta della progettazione di un sistema di alimentazione wireless risonante per i nodi sensori, strumenti fondamentali per il controllo delle strutture(Structural Health Monitoring). Esso si concentra sulla realizzazione di un convertitore flyback risonante (con circuito di snubber incluso per il main switch) in grado di fornire una tensione di 5 Volt in uscita a fronte di una corrente media massima sul carico di 800mA data una tensione di 12 volt in ingresso. Dopo aver introdotto il concetto di Wireless Power Transfer (WPT) e i principi fisici su cui esso poggia (induzione elettromagnetica e risonanza elettromagnetica), si presentano i modelli circuitali più utilizzati in questo ambito. Una volta illustrate le conoscenze allo stato dell'arte dell'accoppiamento induttivo risonante, si analizza il comportamento del modello scelto, al fine di evidenziare i vantaggi dell'utilizzo del circuito alla frequenza di risonanza. Sono state effettuate simulazioni con il simulatore LTspice come controprova. Si passa quindi a dimensionare i vari elementi del circuito a fronte delle specifiche stabilite. Grazie ai risultati ottenuti, si procede alla stesura del Bill Of Materials. La tesi si conclude presentando i possibili campi di ricerca e sviluppo del sistema di alimentazione.
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Peer reviewed
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Peer reviewed
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Much of the bridge stock on major transport links in North America and Europe was constructed in the 1950s and 1960s and has since deteriorated or is carrying loads far in excess of the original design loads. Structural Health Monitoring Systems (SHM) can provide valuable information on the bridge capacity but the application of such systems is currently limited by access and bridge type. This paper investigates the use of computer vision systems for SHM. A series of field tests have been carried out to test the accuracy of displacement measurements using contactless methods. A video image of each test was processed using a modified version of the optical flow tracking method to track displacement. These results have been validated with an established measurement method using linear variable differential transformers (LVDTs). The results obtained from the algorithm provided an accurate comparison with the validation measurements. The calculated displacements agree within 2% of the verified LVDT measurements, a number of post processing methods were then applied to attempt to reduce this error.
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In the recent years, vibration-based structural damage identification has been subject of significant research in structural engineering. The basic idea of vibration-based methods is that damage induces mechanical properties changes that cause anomalies in the dynamic response of the structure, which measures allow to localize damage and its extension. Vibration measured data, such as frequencies and mode shapes, can be used in the Finite Element Model Updating in order to adjust structural parameters sensible at damage (e.g. Young’s Modulus). The novel aspect of this thesis is the introduction into the objective function of accurate measures of strains mode shapes, evaluated through FBG sensors. After a review of the relevant literature, the case of study, i.e. an irregular prestressed concrete beam destined for roofing of industrial structures, will be presented. The mathematical model was built through FE models, studying static and dynamic behaviour of the element. Another analytical model was developed, based on the ‘Ritz method’, in order to investigate the possible interaction between the RC beam and the steel supporting table used for testing. Experimental data, recorded through the contemporary use of different measurement techniques (optical fibers, accelerometers, LVDTs) were compared whit theoretical data, allowing to detect the best model, for which have been outlined the settings for the updating procedure.
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Parmi les méthodes les plus utilisées en inspection embarquée des structures (Structural Health Monitoring ou SHM), les techniques d’imagerie basées sur un modèle de propagation sont de plus en plus répandues. Pour les techniques d'imagerie basées sur un modèle de propagation, bien que ces techniques montent en popularité, la complexité des matériaux composites réduit grandement leur performance en détection d'endommagements comparativement aux démonstrations précédentes de leur potentiel sur des matériaux isotropes. Cette limitation dépend entre autres des hypothèses simplificatrices souvent posées dans les modèles utilisés et peut entraîner une augmentation des faux positifs et une réduction de la capacité de ces techniques à détecter des endommagements. Afin de permettre aux techniques d'imagerie basées sur un modèle d'offrir une performance équivalente à celle obtenue précédemment sur les structures métalliques, il est nécessaire d'exploiter des modèles de propagation considérant la dynamique complexe des ondes dans ce type de structures. Cette thèse présente les travaux effectués sur la modélisation de la propagation des ondes guidées dans les matériaux composites. En première partie, une amélioration simple des modèles de génération et de propagation est proposée afin de permettre de mieux reconstruire les signaux générés et propagés sur une structure composite. Par la suite, le potentiel de la technique « Excitelet » à détecter et positionner adéquatement un ou plusieurs endommagements sur un matériau, peu importe son empilement (d’un composite unidirectionnel à un matériau isotrope), est démontré tant pour le mode A[indice inférieur 0] que le mode S[indice inférieur 0]. Les résultats obtenus numériquement et expérimentalement démontrent une corrélation directe entre l'amélioration des modèles mathématiques derrière les techniques d'imagerie et la robustesse des techniques pour ce qui est de la précision sur le positionnement du dommage et du niveau de corrélation obtenu. Parmi les améliorations à la technique d'imagerie « Excitelet » proposées, une amélioration significative des résultats en imagerie est démontrée en considérant la distribution de cisaillement plan sous l’émetteur, ce qui est une nouveauté par rapport aux travaux de recherche précédents en imagerie. La performance de la technique d'imagerie via la modélisation de la propagation d'ondes guidées dans les laminés multicouches transverses isotropes est par la suite démontrée. Les équations de l'élasticité en 3D sont utilisées pour bien modéliser le comportement dispersif des ondes dans les composites, et cette formulation est par la suite implantée dans la technique d'imagerie « Excitelet ». Les résultats démontrent que l'utilisation d'une formulation mathématique plus avancée permet d'augmenter la précision quant au positionnement des dommages et à l'amplitude de la corrélation obtenue lors de la détection d'un dommage. Une analyse exhaustive de la sensibilité de la technique d’imagerie et de la propagation d’ondes aux conditions environnementales et à la présence de revêtement sur la structure est présentée en dernière partie. Les résultats obtenus montrent que la considération de la propagation complexe dans la formulation d’imagerie ainsi que la caractérisation des propriétés mécaniques « a priori » de l’imagerie améliorent la robustesse de la technique et confèrent à la technique « Excitelet » la capacité de détecter et positionner précisément un endommagement, peu importe le type de structure.
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La mise en oeuvre de systèmes de détection de défauts à même les structures ou infrastructures en génie est le sujet d’étude du Structural Health Monitoring (SHM). Le SHM est une solution efficace à la réduction des coûts associés à la maintenance de structures. Une stratégie prometteuse parmi les technologies émergentes en SHM est fondée sur l’utilisation d’ondes ultrasonores guidées. Ces méthodes sont basées sur le fait que les structures minces agissent comme guides d’ondes pour les ondes ultrasonores. Puisque les structures aéronautiques sont majoritairement minces, les ondes guidées constituent une stratégie pertinente afin d’inspecter de grandes surfaces. Toutefois, les assemblages aéronautiques sont constitués de plusieurs éléments modifiant et compliquant la propagation des ondes guidées dans celles-ci. En effet, la présence de rivets, de raidisseurs, de joints ainsi que la variation de la nature des matériaux utilisés complexifie la propagation des ondes guidées. Pour envisager la mise en oeuvre de systèmes de détection basés sur les ondes guidées, une compréhension des interactions intervenant dans ces diverses structures est nécessaire. Un tel travail entre dans le cadre du projet de collaboration CRIAQ DPHM 501 dont l’objectif principal est de développer une banque de connaissances quant à la propagation d’ondes guidées dans les structures aéronautiques. Le travail de ce mémoire présente d’abord les résultats d’études paramétriques numériques obtenus dans le cadre de ce projet CRIAQ. Puis, afin de faciliter la caractérisation expérimentale de la propagation des ondes guidées, une seconde partie du travail a porté sur le développement d’un absorbant d’ondes guidées. Cet absorbant permet également d’envisager l’extension des régions observables par les systèmes SHM. Ce deuxième volet contribue donc également au projet CRIAQ par l’atténuation de réflexions non désirées dans l’étude menée sur les maintes structures aéronautiques nourrissant la banque de connaissances. La première partie de ce mémoire relève l’état des connaissances de la littérature sur la propagation d’ondes guidées dans les structures aéronautiques. La deuxième partie présente rapidement le formalisme derrière les ondes de Lamb ainsi que les différentes approches analytiques pour caractériser les interactions entre ondes guidées et discontinuités. Par la suite, les outils utilisés pour effectuer les simulations par éléments finis sont présentés et validés par le biais d’une phase expérimentale. La deuxième partie se termine avec la présentation des différentes structures et discontinuités étudiées dans le cadre du projet CRIAQ. Finalement, la troisième et dernière partie de ce mémoire présente les travaux numériques orientés vers la conception d’un absorbant idéal pour ondes guidées. Afin d’y parvenir, une étude paramétrique quant à la forme, les dimensions et les propriétés mécaniques de l’absorbant est entreprise. Enfin, une étude expérimentale permettant de valider les résultats numériques est présentée.
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Abstract: We present an optical sensing methodology to estimate the fatigue damage stateof structures made of carbon fiber reinforced polymer (CFRP), by measuring variations on the surface roughness. Variable amplitude loads (VAL), which represent realistic loads during aeronautical missions of fighter aircraft (FALSTAFF) have been applied to coupons until failure. Stiffness degradation and surface roughness variations have been measured during the life of the coupons obtaining a Pearson correlation of 0.75 between both variables. The data were compared with a previous study for Constant Amplitude Load (CAL) obtaining similar results. Conclusions suggest that the surface roughness measured in strategic zones is a useful technique for structural health monitoring of CFRP structures, and that it is independent of the type of load applied. Surface roughness can be measured in the field by optical techniques such as speckle, confocal perfilometers and interferometry, among others.
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Non Destructive Testing (NDT) and Structural Health Monitoring (SHM) are becoming essential in many application contexts, e.g. civil, industrial, aerospace etc., to reduce structures maintenance costs and improve safety. Conventional inspection methods typically exploit bulky and expensive instruments and rely on highly demanding signal processing techniques. The pressing need to overcome these limitations is the common thread that guided the work presented in this Thesis. In the first part, a scalable, low-cost and multi-sensors smart sensor network is introduced. The capability of this technology to carry out accurate modal analysis on structures undergoing flexural vibrations has been validated by means of two experimental campaigns. Then, the suitability of low-cost piezoelectric disks in modal analysis has been demonstrated. To enable the use of this kind of sensing technology in such non conventional applications, ad hoc data merging algorithms have been developed. In the second part, instead, imaging algorithms for Lamb waves inspection (namely DMAS and DS-DMAS) have been implemented and validated. Results show that DMAS outperforms the canonical Delay and Sum (DAS) approach in terms of image resolution and contrast. Similarly, DS-DMAS can achieve better results than both DMAS and DAS by suppressing artefacts and noise. To exploit the full potential of these procedures, accurate group velocity estimations are required. Thus, novel wavefield analysis tools that can address the estimation of the dispersion curves from SLDV acquisitions have been investigated. An image segmentation technique (called DRLSE) was exploited in the k-space to draw out the wavenumber profile. The DRLSE method was compared with compressive sensing methods to extract the group and phase velocity information. The validation, performed on three different carbon fibre plates, showed that the proposed solutions can accurately determine the wavenumber and velocities in polar coordinates at multiple excitation frequencies.