10 resultados para Foam Prototyping

em AMS Tesi di Laurea - Alm@DL - Università di Bologna


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Progettazione, test e creazione di schede elettroniche per lo studio dell'atmosfera in condizioni ambientali difficili.

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I materiali polimerici espansi sono utilizzati come core di pannelli compositi di tipo sandwich (tipicamente a base di polivinilcloruro, polistirene e poliuretani). Negli ultimi anni molte ricerche si sono concentrate sulla possibilità di aumentare le loro proprietà meccaniche, termiche, di resistenza agli agenti esterni, ignifughe, etc cercando contemporaneamente la diminuzione del peso e del costo (sia delle materia prime che di processo). In questo contesto, l’obiettivo di questa tesi di laurea è lo studio, la preparazione e la caratterizzazione di espansi in PVC di natura cross-linked per la produzione di pannelli compositi a sandwich potenzialmente utilizzabili in campo eolico e navale.

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The relatively young discipline of astronautics represents one of the scientifically most fascinating and technologically advanced achievements of our time. The human exploration in space does not offer only extraordinary research possibilities but also demands high requirements from man and technology. The space environment provides a lot of attractive experimental tools towards the understanding of fundamental mechanism in natural sciences. It has been shown that especially reduced gravity and elevated radiation, two distinctive factors in space, influence the behavior of biological systems significantly. For this reason one of the key objectives on board of an earth orbiting laboratory is the research in the field of life sciences, covering the broad range from botany, human physiology and crew health up to biotechnology. The Columbus Module is the only European low gravity platform that allows researchers to perform ambitious experiments in a continuous time frame up to several months. Biolab is part of the initial outfitting of the Columbus Laboratory; it is a multi-user facility supporting research in the field of biology, e.g. effect of microgravity and space radiation on cell cultures, micro-organisms, small plants and small invertebrates. The Biolab IEC are projects designed to work in the automatic part of Biolab. In this moment in the TO-53 department of Airbus Defence & Space (formerly Astrium) there are two experiments that are in phase C/D of the development and they are the subject of this thesis: CELLRAD and CYTOSKELETON. They will be launched in soft configuration, that means packed inside a block of foam that has the task to reduce the launch loads on the payload. Until 10 years ago the payloads which were launched in soft configuration were supposed to be structural safe by themselves and a specific structural analysis could be waived on them; with the opening of the launchers market to private companies (that are not under the direct control of the international space agencies), the requirements on the verifications of payloads are changed and they have become much more conservative. In 2012 a new random environment has been introduced due to the new Space-X launch specification that results to be particularly challenging for the soft launched payloads. The last ESA specification requires to perform structural analysis on the payload for combined loads (random vibration, quasi-steady acceleration and pressure). The aim of this thesis is to create FEM models able to reproduce the launch configuration and to verify that all the margins of safety are positive and to show how they change because of the new Space-X random environment. In case the results are negative, improved design solution are implemented. Based on the FEM result a study of the joins has been carried out and, when needed, a crack growth analysis has been performed.

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L’oggetto della presente tesi è sviluppare la ricostruzione virtuale di un autobus pubblicitario progettato negli anni 50, un simbolo del design italiano legato allo sviluppo industriale del secondo dopoguerra. La tesi si sviluppa inizialmente con un’attività di ricerca e documentazione legata all'autobus, con particolare attenzione alla raccolta di immagini e disegni progettuali d’epoca, punto di partenza per la ricostruzione virtuale del mezzo. Si procede quindi alla modellazione CAD della carrozzeria cercando di replicare in modo quanto più dettagliato l’originale. Dal modello ottenuto, sono stati ricavati due prototipi di diverse dimensioni e materiali: un primo di dimensioni ridotte, realizzato tramite la tecnica del rapid prototyping, ed un secondo di dimensioni maggiori, in ureol fresato. Successivamente si procede ad uno studio preliminare di ricostruzione del mezzo con lo scopo di analizzare le principali problematiche di un’eventuale futura costruzione e messa in strada del mezzo. Tale studio parte dalla normativa vigente sulla costruzione e sulle norme di circolazione degli autobus, comprendente sia le leggi italiane sia comunitarie, riguardanti le caratteristiche dimensionali, prestazionali e di sicurezza che qualsiasi autobus con licenza di circolazione deve rispettare. Quindi verrà compiuta la scelta del telaio base da utilizzare tra quelli proposti dai maggiori costruttori europei e verrà realizzato il modello CAD anche del telaio con l’obiettivo di collegarlo alla carrozzeria e ottenere così il modello completo in tutte le sue parti. Per realizzare la scocca, verranno prese in esame le soluzioni costruttive più utilizzate dai progettisti di autobus, e viene svolto un breve studio riguardo i materiali utilizzabili a tale scopo. Sulla base di tali considerazioni si procederà alla modellazione della stessa. In ultimo si procede ad un preliminare studio fluidodinamico attraverso l’analisi CFD, e ad un preliminare studio del comportamento meccanico della struttura reticolare che sostiene la carrozzeria.

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The research and the activities presented in the following thesis report have been led at the California Polytechnic State University (US) under the supervision of Prof. Jordi Puig Suari. The objective of the research has been the study of magnetic actuators for nanosatellite attitude control, called magnetorquer. Theese actuators are generally divided in three different kinds: air core torquer, embedded coil and torquerod. In a first phase of the activity, each technology has been analyzed, defining advantages and disadvantages, determining manufacturing procedures and creating mathematical model and designing equation. Dimensioning tools have been then implemented in numerical software to create an instrument that permits to determine the optimal configuration for defined requirements and constraints. In a second phase of the activities the models created have been validated exploiting prototypes and proper instruments for measurements. The instruments and the material exploited for experiments and prototyping have been provided by the PolySat and CubeSat laboratories. The results obtained led to the definition of a complete designing tool and procedure for nanosatellite magnetic actuators, introducing a cost analysis for each kind of solution. The models and the tools have been maintained fully parametric in order to offer a universal re-scalable instrument for satellite of different dimension class.

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Lavoro sviluppato attraverso un’attività sperimentale svolta su un motore Diesel 1.3 Multijet, presente al banco nei laboratori hangar della Scuola di Ingegneria e Architettura, sede di Forlì. L’attività è stata incentrata sullo sviluppo di un sistema RCP (Rapid Control Prototyping) per il controllo del pattern di iniezione del motore, basato sull’analisi in tempo reale di un opportuno indice di rumore, calcolato in real time attraverso il processamento del segnale proveniente da un microfono da laboratorio affacciato al blocco motore.

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This thesis proposes a novel technology in the field of swarm robotics that allows a swarm of robots to sense a virtual environment through virtual sensors. Virtual sensing is a desirable and helpful technology in swarm robotics research activity, because it allows the researchers to efficiently and quickly perform experiments otherwise more expensive and time consuming, or even impossible. In particular, we envision two useful applications for virtual sensing technology. On the one hand, it is possible to prototype and foresee the effects of a new sensor on a robot swarm, before producing it. On the other hand, thanks to this technology it is possible to study the behaviour of robots operating in environments that are not easily reproducible inside a lab for safety reasons or just because physically infeasible. The use of virtual sensing technology for sensor prototyping aims to foresee the behaviour of the swarm enhanced with new or more powerful sensors, without producing the hardware. Sensor prototyping can be used to tune a new sensor or perform performance comparison tests between alternative types of sensors. This kind of prototyping experiments can be performed through the presented tool, that allows to rapidly develop and test software virtual sensors of different typologies and quality, emulating the behaviour of several hardware real sensors. By investigating on which sensors is better to invest, a researcher can minimize the sensors’ production cost while achieving a given swarm performance. Through augmented reality, it is possible to test the performance of the swarm in a desired virtual environment that cannot be set into the lab for physical, logistic or economical reasons. The virtual environment is sensed by the robots through properly designed virtual sensors. Virtual sensing technology allows a researcher to quickly carry out real robots experiment in challenging scenarios without all the required hardware and environment.

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Questa tesi si propone di realizzare una caratterizzazione del polimero ABS ottenuto con tecnica Fused Deposition Modeling in modo da ottenere dati utili alla realizzazione di parti strutturali tramite rapid prototyping.

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This thesis work has been carried out at Clarkson University in Potsdam NY, USA and involved the design of a low elongation wing, consisting of parts made by polylactide (PLA) using the fused deposition model (FDM) technology of Rapid Prototyping, then assembled together in a thin aluminum spar. The aim of the research is to evaluate the feasibility of collecting electrical energy by converting mechanical energy from the vibration of the wing flutter. With this aim piezoelectric stripes were glued in the inner part of the wing, as well as on the aluminum spar, as monomorphic configuration. During the phases of the project, particular attention was given to the geometry and the materials used, in order to trigger the flutter for low flow velocity. The CAD software SolidWorks® was used for the design of the wing and then the drawings were sent to the Clarkson machine shop in order to to produce the parts required by the wing assembly. FEM simulations were performed, using software MSC NASTRAN/PATRAN®, to evaluate the stiffness of the whole wing as well as the natural vibration modes of the structure. These data, in a first approximation, were used to predict the flutter speed. Finally, experimental tests in the Clarkson wind tunnel facility were carried out in order to validate the results obtained from FEM analysis. The power collected by the piezoelectrics under flutter condition was addressed by tuning the resistors downstream the electronic circuit of the piezoelectrics.