Applicazione di tecniche Laser a scansione nel rilevamento 3D di provini di conglomerato bituminoso

Obiettivo della tesi, oltre ad una descrizione della tecnica laser a scansione ed alla presentazione di alcune realizzazioni tipiche in ambito terrestre, è relazionare su una esperienza effettuata di recente su una applicazione particolare, il rilievo tridimensionale di campioni di pavimentazioni stradali in conglomerato bituminoso per documentarne la tessitura tramite parametri classici e nuovi indicatori resi possibili dal dato tridimensionale. L’attività di tesi si è concentrata soprattutto nei problemi della fase di acquisizione.

3D probability tomography: theoretical developments and applications to high-resolution geophysical prospecting

The theory of the 3D multipole probability tomography method (3D GPT) to image source poles, dipoles, quadrupoles and octopoles, of a geophysical vector or scalar field dataset is developed. A geophysical dataset is assumed to be the response of an aggregation of poles, dipoles, quadrupoles and octopoles. These physical sources are used to reconstruct without a priori assumptions the most probable position and shape of the true geophysical buried sources, by determining the location of their centres and critical points of their boundaries, as corners, wedges and vertices. This theory, then, is adapted to the geoelectrical, gravity and self potential methods. A few synthetic examples using simple geometries and three field examples are discussed in order to demonstrate the notably enhanced resolution power of the new approach. At first, the application to a field example related to a dipole–dipole geoelectrical survey carried out in the archaeological park of Pompei is presented. The survey was finalised to recognize remains of the ancient Roman urban network including roads, squares and buildings, which were buried under the thick pyroclastic cover fallen during the 79 AD Vesuvius eruption. The revealed anomaly structures are ascribed to wellpreserved remnants of some aligned walls of Roman edifices, buried and partially destroyed by the 79 AD Vesuvius pyroclastic fall. Then, a field example related to a gravity survey carried out in the volcanic area of Mount Etna (Sicily, Italy) is presented, aimed at imaging as accurately as possible the differential mass density structure within the first few km of depth inside the volcanic apparatus. An assemblage of vertical prismatic blocks appears to be the most probable gravity model of the Etna apparatus within the first 5 km of depth below sea level. Finally, an experimental SP dataset collected in the Mt. Somma-Vesuvius volcanic district (Naples, Italy) is elaborated in order to define location and shape of the sources of two SP anomalies of opposite sign detected in the northwestern sector of the surveyed area. The modelled sources are interpreted as the polarization state induced by an intense hydrothermal convective flow mechanism within the volcanic apparatus, from the free surface down to about 3 km of depth b.s.l..

Kryoelektronenmikroskopie von Proteinen: 3D-Struktur (12 A) des Hämocyanins der Schnecke Haliotis

Zusammenfassung:Die Quartärstruktur des respiratorischen Proteins Hämocyanin (Isoform HtH1) aus der marinen Schnecke Haliotis tuberculata wurde vermittels Kryoelektronen-mikroskopie und 3D-Rekonstruktion untersucht. Das Molekül ist zylinderförmig, hat einen Durchmesser von ca. 35 nm und besteht aus einer Zylinderwand und einem internen Kragenkomplex. Dieser wiederum besteht aus einem Collar und einem Arc.Die kryoelektronenmikroskopischen Aufnahmen von in glasartigem Eis fixierten HtH1-Molekülen brachte eine enorme Verbesserung der Anzahl der zur Verfügung stehenden Ansichtswinkel gegenüber den negativkontrastierten Molekülen, die auf Karbonfilm präpariert waren.Die 3D-Rekonstruktion des HtH1 mittels Aufnahmen bei drei verschiedenen Defo-kuswerten verbesserte die Auflösung noch einmal deutlich gegenüber den Rekon-struktionen, die aus Aufnahmen bei einem festen Defokuswert gemacht wurden, und zwar auf 12 Å. Das Molekül besitzt eine D5-Symmetrie.Aus dieser bisher genausten Rekonstruktion eines Molluskenhämocyanins aus EM-Bildern ließen sich folgende neue Strukturdetails ableiten:· Ein Untereinheitendimer konnte als Repeating Unit im Dekamer des HtH1 beschrieben werden.· Das Untereinheitendimer konnte aus der 3D-Dichtekarte isoliert werden. Es be-steht eindeutig aus 16 Massen, die funktionellen Domänen entsprechen. Zwei dieser Massen bilden den Collar, zwei den Arc und 12 das Wandsegment.· Die gegenläufige Anordnung der beiden Untereinheiten innerhalb dieses Unte-reinheitendimers konnten bestätigt und auf zwei Möglichkeiten eingeschränkt werden.· Die Zahl der alternativen Anordnungen der 16 funktionellen Domänen (HtH1-a bis HtH1-h) im Untereinheitendimer konnten von 80 auf 2 eingeengt werden.· Es konnte über molekulares Modellieren mithilfe einer publizierten Kristallstruk-tur eine 3D-Struktur fastatomarer Auflösung der funktionellen Domäne HtH1-g berechnet werden.· Die funktionelle Domäne HtH1-g konnte als Domänenpaar plausibel in die 3D?Dichtekarte des Untereinheitendimers eingepasst werden, und zwar in die beiden Massen des Arc.Aus der elektronenmikroskopisch gewonnenen Dichtekarte wurde mit Hilfe des

Slope stability analysis by multi-temporal DEMs and 3D modelling: The 2002 and 2007 Stromboli landslide events

Natural hazard related to the volcanic activity represents a potential risk factor, particularly in the vicinity of human settlements. Besides to the risk related to the explosive and effusive activity, the instability of volcanic edifices may develop into large landslides often catastrophically destructive, as shown by the collapse of the northern flank of Mount St. Helens in 1980. A combined approach was applied to analyse slope failures that occurred at Stromboli volcano. SdF slope stability was evaluated by using high-resolution multi-temporal DTMMs and performing limit equilibrium stability analyses. High-resolution topographical data collected with remote sensing techniques and three-dimensional slope stability analysis play a key role in understanding instability mechanism and the related risks. Analyses carried out on the 2002–2003 and 2007 Stromboli eruptions, starting from high-resolution data acquired through airborne remote sensing surveys, permitted the estimation of the lava volumes emplaced on the SdF slope and contributed to the investigation of the link between magma emission and slope instabilities. Limit Equilibrium analyses were performed on the 2001 and 2007 3D models, in order to simulate the slope behavior before 2002-2003 landslide event and after the 2007 eruption. Stability analyses were conducted to understand the mechanisms that controlled the slope deformations which occurred shortly after the 2007 eruption onset, involving the upper part of slope. Limit equilibrium analyses applied to both cases yielded results which are congruent with observations and monitoring data. The results presented in this work undoubtedly indicate that hazard assessment for the island of Stromboli should take into account the fact that a new magma intrusion could lead to further destabilisation of the slope, which may be more significant than the one recently observed because it will affect an already disarranged deposit and fractured and loosened crater area. The two-pronged approach based on the analysis of 3D multi-temporal mapping datasets and on the application of LE methods contributed to better understanding volcano flank behaviour and to be prepared to undertake actions aimed at risk mitigation.

Scanner 3D con proiettore e videocamera

In questa dissertazione viene descritto un sistema sviluppato per ottenere una rappresentazione a tre dimensioni in real time di una superficie. Il sistema si avvale di alcune tecniche di ottimizza- zione e di trattamento dell’immagine e sfrutta dispositivi comuni e di facile reperibilita`: una videocamera e un proiettore.

OGRE: analisi di un motore grafico 3D

In questa tesi descriveremo e analizzeremo il motore grafico OGRE, acronimo di Object-Oriented Graphics Rendering Engine. La scelta di analizzare proprio questo motore grafico è legata a diverse considerazioni. Innanzitutto, OGRE è rilasciato con licenza open source e quindi rende disponibile il suo codice sorgente. Questo è molto importante, in un contesto di studio e sperimentazione come quello universitario, perché permette di comprendere e analizzare anche il funzionamento interno del motore grafico. Inoltre, OGRE è un progetto maturo e stabile con una vasta comunità di sviluppatori e utilizzatori alle spalle. Esiste molta documentazione a riguardo, tra wiki, libri e manuali, e un forum molto attivo per la richiesta di aiuto e consigli. A conferma, sia della bontà del progetto che delle ottime prestazioni del motore grafico, basta dire che OGRE è utilizzato anche da applicazioni commerciali, come videogame, editor 3D e simulatori. Infine, la caratteristica che contraddistingue OGRE da tutti gli altri motori grafici è il fatto di essere "solamente" un motore di rendering puro. Ciò significa che qualsiasi funzionalità non direttamente legata al rendering, come ad esempio la gestione degli input dell'utente, non è supportata da OGRE. Anche se questo può sembrare un difetto, in realtà ciò permetterà di concentrarci solamente sugli aspetti legati al rendering che, in un motore grafico, costituiscono la parte fondamentale.

Realisierung einer 3D-Kreuzkorrelationsanlage zur Untersuchung von Struktur und Dynamik hochkonzentrierter Kolloide

Realisierung einer 3D-Kreuzkorrelationsanlage zur Untersuchung von Struktur und Dynamik hochkonzentrierter Kolloide Im Rahmen dieser Arbeit wird eine neuartige 3D-Kreuzkorrelationsanlage zur mehrfachstreufreien Untersuchung des diffusiven Verhaltens hochkonzentrierter kolloidaler Suspensionen vorgestellt. Hierzu werden zwei Lichtstreuexperimente gleichzeitig am gleichen Streuvolumen und mit dem gleichen Streuvektor durchgeführt. Aus der so gewonnenen Kreuzkorrelationsfunktion kann das dynamische Verhalten der Kolloide bestimmt werden. Für die Diffusion der Partikel spielen neben der direkten Wechselwirkung elektroviskoser Effekt und die hydrodynamische Wechselwirkung eine entscheidende Rolle. Insbesondere bei hohen Konzentrationen kann keiner der drei Effekte vernachlässigt werden. Die zu messenden Unterschiede in den Diffusionskoeffizienten sind sehr klein. Daher wurde der experimentelle Aufbau detailliert charakterisiert. Hierbei konnten theoretische Überlegungen hinsichtlich des Nachpulsens und der Totzeit der verwendeten Si-Avalanche-Photodioden überprüft werden. Der Kurzzeitselbstdiffusionskoeffizient hochkonzentrierter geladener kolloidaler Suspensionen wurde gemessen. Um die Daten bei hohen Konzentrationen korrekt zu normieren, wurde der elektroviskose Effekt bei geringen Konzentrationen ausführlich untersucht. Hierbei zeigte sich, dass der elektroviskose Einzelteilcheneffekt zu einer monotonen Abnahme des Diffusionskoeffizienten bei abnehmender Ionenstärke führt. Anhand der volumenbruchabhängigen Daten des Kurzzeitselbstdiffusionskoeffizienten konnte zum ersten Mal gezeigt werden, dass die hydrodynamische Wechselwirkung einen geringeren Einfluss auf die Diffusion hat, falls das direkte Wechselwirkungspotential ein Coulomb-Potential anstelle eines Harte-Kugel-Potentials ist.

Metodi di ottimizzazione morfologica nel progetto preliminare di propulsori aeronautici avanzati

The aim of this Doctoral Thesis is to develop a genetic algorithm based optimization methods to find the best conceptual design architecture of an aero-piston-engine, for given design specifications. Nowadays, the conceptual design of turbine airplanes starts with the aircraft specifications, then the most suited turbofan or turbo propeller for the specific application is chosen. In the aeronautical piston engines field, which has been dormant for several decades, as interest shifted towards turboaircraft, new materials with increased performance and properties have opened new possibilities for development. Moreover, the engine’s modularity given by the cylinder unit, makes it possible to design a specific engine for a given application. In many real engineering problems the amount of design variables may be very high, characterized by several non-linearities needed to describe the behaviour of the phenomena. In this case the objective function has many local extremes, but the designer is usually interested in the global one. The stochastic and the evolutionary optimization techniques, such as the genetic algorithms method, may offer reliable solutions to the design problems, within acceptable computational time. The optimization algorithm developed here can be employed in the first phase of the preliminary project of an aeronautical piston engine design. It’s a mono-objective genetic algorithm, which, starting from the given design specifications, finds the engine propulsive system configuration which possesses minimum mass while satisfying the geometrical, structural and performance constraints. The algorithm reads the project specifications as input data, namely the maximum values of crankshaft and propeller shaft speed and the maximal pressure value in the combustion chamber. The design variables bounds, that describe the solution domain from the geometrical point of view, are introduced too. In the Matlab® Optimization environment the objective function to be minimized is defined as the sum of the masses of the engine propulsive components. Each individual that is generated by the genetic algorithm is the assembly of the flywheel, the vibration damper and so many pistons, connecting rods, cranks, as the number of the cylinders. The fitness is evaluated for each individual of the population, then the rules of the genetic operators are applied, such as reproduction, mutation, selection, crossover. In the reproduction step the elitist method is applied, in order to save the fittest individuals from a contingent mutation and recombination disruption, making it undamaged survive until the next generation. Finally, as the best individual is found, the optimal dimensions values of the components are saved to an Excel® file, in order to build a CAD-automatic-3D-model for each component of the propulsive system, having a direct pre-visualization of the final product, still in the engine’s preliminary project design phase. With the purpose of showing the performance of the algorithm and validating this optimization method, an actual engine is taken, as a case study: it’s the 1900 JTD Fiat Avio, 4 cylinders, 4T, Diesel. Many verifications are made on the mechanical components of the engine, in order to test their feasibility and to decide their survival through generations. A system of inequalities is used to describe the non-linear relations between the design variables, and is used for components checking for static and dynamic loads configurations. The design variables geometrical boundaries are taken from actual engines data and similar design cases. Among the many simulations run for algorithm testing, twelve of them have been chosen as representative of the distribution of the individuals. Then, as an example, for each simulation, the corresponding 3D models of the crankshaft and the connecting rod, have been automatically built. In spite of morphological differences among the component the mass is almost the same. The results show a significant mass reduction (almost 20% for the crankshaft) in comparison to the original configuration, and an acceptable robustness of the method have been shown. The algorithm here developed is shown to be a valid method for an aeronautical-piston-engine preliminary project design optimization. In particular the procedure is able to analyze quite a wide range of design solutions, rejecting the ones that cannot fulfill the feasibility design specifications. This optimization algorithm could increase the aeronautical-piston-engine development, speeding up the production rate and joining modern computation performances and technological awareness to the long lasting traditional design experiences.