Produzione di idrogeno "on-board" mediante deidrogenazione catalitica di kerosene

L’H2 è attualmente un elemento di elevato interesse economico, con notevoli prospettive di sviluppo delle sue applicazioni. La sua produzione industriale supera attualmente i 55 ∙ 1010 m3/anno, avendo come maggiori utilizzatori (95% circa) i processi di produzione dell’ammoniaca e quelli di raffineria (in funzione delle sempre più stringenti normative ambientali). Inoltre, sono sempre più importanti le sue applicazioni come vettore energetico, in particolare nel settore dell’autotrazione, sia dirette (termochimiche) che indirette, come alimentazione delle fuel cells per la produzione di energia elettrica. L’importanza economica degli utilizzi dell’ H2 ha portato alla costruzione di una rete per la sua distribuzione di oltre 1050 km, che collega i siti di produzione ai principali utilizzatori (in Francia, Belgio, Olanda e Germania). Attualmente l’ H2 è prodotto in impianti di larga scala (circa 1000 m3/h) da combustibili fossili, in particolare metano, attraverso i processi di steam reforming ed ossidazione parziale catalitica, mentre su scala inferiore (circa 150 m3/h) trovano applicazione anche i processi di elettrolisi dell’acqua. Oltre a quella relativa allo sviluppo di processi per la produzione di H2 da fonti rinnovabili, una tematica grande interesse è quella relativa al suo stoccaggio, con una particolare attenzione ai sistemi destinati alle applicazioni nel settore automotivo o dei trasposti in generale. In questo lavoro di tesi, svolto nell’ambito del progetto europeo “Green Air” (7FP – Transport) in collaborazione (in particolare) con EADS (D), CNRS (F), Jonhson-Matthey (UK), EFCECO (D), CESA (E) e HyGEAR (NL), è stato affrontato uno studio preliminare della reazione di deidrogenazione di miscele di idrocarburi e di differenti kerosene per utilizzo aereonautico, finalizzato allo sviluppo di nuovi catalizzatori e dei relativi processi per la produzione di H2 “on board” utilizzando il kerosene avio per ottenere, utilizzando fuel cells, l’energia elettrica necessaria a far funzionare tutta la strumentazione ed i sistemi di comando di aeroplani della serie Airbus, con evidenti vantaggi dal punto di vista ponderale e delle emissioni.

Debonding and crack propagation in cracked steel beams strengthened with CFRP and subjected to cyclic loads.

The reinforcement methods used to restore or increase the bearing capacity of metal structures are based on the application of steel plates to be bolted or welded to the original structure, which can cause problems to the integrity of the original structure. These difficulties can be overcome with the introduction of fiber-reinforced composite materials. FRPs are characterized by high strength to weight ratio, and they are very resistant to corrosion. In this dissertation a cracked steel I-beam reinforced with Carbon Fiber-Reinforced Polymer will be studied by performing a numerical evaluation of the structure with the commercial Finite Element Method software ABAQUS. The crack propagation will be computed using XFEM, while the debonding of the reinforcement layer will be found by considering a cohesive contact interface between the beam and the CFRP plate. The results will show the efficiency of the strengthening method in increasing the load carrying capacity of the cracked beam, and in reducing the crack opening of the initial notch.

Time-dependent behaviour of reinforced concrete slabs

In this thesis is studied the long-term behaviour of steel reinforced slabs paying particular attention to the effects due to shrinkage and creep. Despite the universal popularity of using this kind of slabs for simply construction floors, the major world codes focus their attention in a design based on the ultimate limit state, restraining the exercise limit state to a simply verification after the design. For Australia, on the contrary, this is not true. In fact, since this country is not subjected to seismic effects, the main concern is related to the long-term behaviour of the structure. Even if there are a lot of studies about long-term effects of shrinkage and creep, up to date, there are not so many studies concerning the behaviour of slabs with a cracked cross section and how shrinkage and creep influence it. For this reason, a series of ten full scale reinforced slabs was prepared and monitored under laboratory conditions to investigate this behaviour. A wide range of situations is studied in order to cover as many cases as possible, as for example the use of a fog room able to reproduce an environment of 100% humidity. The results show how there is a huge difference in terms of deflections between the case of slabs which are subjected to both shrinkage and creep effects soon after the partial cracking of the cross section, and the case of slabs which have already experienced shrinkage effects for several weeks, when the section has not still cracked, and creep effects only after the cracking.

Laser shock peening treatment to control and moderate fatigue crack growth in aircraft structure based on residual stress engineering approach

Laser Shock Peening (LSP) is a surface enhancement treatment which induces a significant layer of beneficial compressive residual stresses of up to several mm underneath the surface of metal components in order to improve the detrimental effects of the crack growth behavior rate in it. The aim of this thesis is to predict the crack growth behavior in metallic specimens with one or more stripes which define the compressive residual stress area induced by the Laser Shock Peening treatment. The process was applied as crack retardation stripes perpendicular to the crack propagation direction with the object of slowing down the crack when approaching the peened stripes. The finite element method has been applied to simulate the redistribution of stresses in a cracked model when it is subjected to a tension load and to a compressive residual stress field, and to evaluate the Stress Intensity Factor (SIF) in this condition. Finally, the Afgrow software is used to predict the crack growth behavior of the component following the Laser Shock Peening treatment and to detect the improvement in the fatigue life comparing it to the baseline specimen. An educational internship at the “Research & Technologies Germany – Hamburg” department of AIRBUS helped to achieve knowledge and experience to write this thesis. The main tasks of the thesis are the following: •To up to date Literature Survey related to “Laser Shock Peening in Metallic Structures” •To validate the FE model developed against experimental measurements at coupon level •To develop design of crack growth slowdown in Centered Cracked Tension specimens based on residual stress engineering approach using laser peened strip transversal to the crack path •To evaluate the Stress Intensity Factor values for Centered Cracked Tension specimens after the Laser Shock Peening treatment via Finite Element Analysis •To predict the crack growth behavior in Centered Cracked Tension specimens using as input the SIF values evaluated with the FE simulations •To validate the results by means of experimental tests