11 resultados para Sliding friction

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


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Understanding the interaction of sea ice with offshore structures is of primary importance for the development of technology in cold climate regions. The rheological properties of sea ice (strength, creep, viscosity) as well as the roughness of the contact surface are the main factors influencing the type of interaction with a structure. A device was developed and designed and small scale laboratory experiments were carried out to study sea ice frictional interaction with steel material by means of a uniaxial compression rig. Sea-ice was artificially grown between a stainless steel piston (of circular cross section) and a hollow cylinder of the same material, coaxial to the former and of the same surface roughness. Three different values for the roughness were tested: 1.2, 10 and 30 μm Ry (maximum asperities height), chosen as representative values for typical surface conditions, from smooth to normally corroded steel. Creep tests (0.2, 0.3, 0.4 and 0.6 kN) were conducted at T = -10 ºC. By pushing the piston head towards the cylinder base, three different types of relative movement were observed: 1) the piston slid through the ice, 2) the piston slid through the ice and the ice slid on the surface of the outer cylinder, 3) the ice slid only on the cylinder surface. A cyclic stick-slip motion of the piston was detected with a representative frequency of 0.1 Hz. The ratio of the mean rate of axial displacement to the frequency of the stick-slip oscillations was found to be comparable to the roughness length (Sm). The roughness is the most influential parameter affecting the amplitude of the oscillations, while the load has a relevant influence on the their frequency. Guidelines for further investigations were recommended. Marco Nanetti - seloselo@virgilio.it

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Studio della caratterizzazione micromeccanica di provini in alluminio 6082 T6 saldati con la tecnica della rotary friction welding, tecnica innovativa nell’ambito delle tecnologie di giunzione solida, che sfrutta il principio della saldatura per attrito. Dopo un'introduzione teorica sulle principali tematiche affrontate e sui principali sistemi di misura usati, verranno effettuate micrografie dei giunti e prove di microdurezza sugli stessi. Si termina riportando i grafici delle microdurezze trovate, in modo da poter confrontare i risultati ottenuti con le caratteristiche del materiale base. Da questi si osserva che: nonostante la qualità accettabile dei giunti, le elevate temperature raggiunte durante la saldatura hanno alterato il trattamento termico del materiale base, che da T6 assume caratteristiche più simili a un T4. In altre parole il materiale saldato presenta caratteristiche micromeccaniche inferiori a quelle nominalmente assegnabili al materiale base.

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Il presente lavoro di tesi si pone come obiettivo la caratterizzazione microstrutturale di una serie di giunti realizzati tramite un innovativo processo di saldatura allo stato solido denominato Rotary Friction Welding. In tale ricerca si descrive il percorso seguito per arrivare a tale caratterizzazione partendo da una discussione delle principali tecniche di saldatura, in particolare quelle per attrito, per passare poi ad un’analisi dettagliata della fase di creazione dei giunti saldati e della successiva fase dedicata alla verifica microstrutturale. I risultati ottenuti, ci forniranno indici di confronto sulla qualità del materiale, sui processi tecnologici, sui trattamenti e su alcune fondamentali proprietà meccaniche

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Nel seguente elaborato si propone lo sviluppo di un modello agli elementi finiti (FEM) del processo di friction welding del quale, attraverso i dati rilevati da prove sperimentali di validazione termica, vengono valutati i parametri ottimali di simulazione. Ai risultati così ottenuti vengono applicati anche algoritmi per la valutazione della microstruttura e della qualità della saldatura, sviluppati originariamente per l'analisi dell'estrusione: in entrambi i casi a seguito del confronto con le analisi metallografiche dei provini è stato possibile validare ulteriormente il modello creato.

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The Scilla rock avalanche occurred on 6 February 1783 along the coast of the Calabria region (southern Italy), close to the Messina Strait. It was triggered by a mainshock of the Terremoto delle Calabrie seismic sequence, and it induced a tsunami wave responsible for more than 1500 casualties along the neighboring Marina Grande beach. The main goal of this work is the application of semi-analtycal and numerical models to simulate this event. The first one is a MATLAB code expressly created for this work that solves the equations of motion for sliding particles on a two-dimensional surface through a fourth-order Runge-Kutta method. The second one is a code developed by the Tsunami Research Team of the Department of Physics and Astronomy (DIFA) of the Bologna University that describes a slide as a chain of blocks able to interact while sliding down over a slope and adopts a Lagrangian point of view. A wide description of landslide phenomena and in particular of landslides induced by earthquakes and with tsunamigenic potential is proposed in the first part of the work. Subsequently, the physical and mathematical background is presented; in particular, a detailed study on derivatives discratization is provided. Later on, a description of the dynamics of a point-mass sliding on a surface is proposed together with several applications of numerical and analytical models over ideal topographies. In the last part, the dynamics of points sliding on a surface and interacting with each other is proposed. Similarly, different application on an ideal topography are shown. Finally, the applications on the 1783 Scilla event are shown and discussed.

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The main objective of this project is to experimentally demonstrate geometrical nonlinear phenomena due to large displacements during resonant vibration of composite materials and to explain the problem associated with fatigue prediction at resonant conditions. Three different composite blades to be tested were designed and manufactured, being their difference in the composite layup (i.e. unidirectional, cross-ply, and angle-ply layups). Manual envelope bagging technique is explained as applied to the actual manufacturing of the components; problems encountered and their solutions are detailed. Forced response tests of the first flexural, first torsional, and second flexural modes were performed by means of a uniquely contactless excitation system which induced vibration by using a pulsed airflow. Vibration intensity was acquired by means of Polytec LDV system. The first flexural mode is found to be completely linear irrespective of the vibration amplitude. The first torsional mode exhibits a general nonlinear softening behaviour which is interestingly coupled with a hardening behaviour for the unidirectional layup. The second flexural mode has a hardening nonlinear behaviour for either the unidirectional and angle-ply blade, whereas it is slightly softening for the cross-ply layup. By using the same equipment as that used for forced response analyses, free decay tests were performed at different airflow intensities. Discrete Fourier Trasform over the entire decay and Sliding DFT were computed so as to visualise the presence of nonlinear superharmonics in the decay signal and when they were damped out from the vibration over the decay time. Linear modes exhibit an exponential decay, while nonlinearities are associated with a dry-friction damping phenomenon which tends to increase with increasing amplitude. Damping ratio is derived from logarithmic decrement for the exponential branch of the decay.

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Costruzione di un modello numerico base per la simulazione del processo Rotary Friction Welding.

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This master thesis proposes a solution to the approach problem in case of unknown severe microburst wind shear for a fixed-wing aircraft, accounting for both longitudinal and lateral dynamics. The adaptive controller design for wind rejection is also addressed, exploiting the wind estimation provided by suitable estimators. It is able to successfully complete the final approach phase even in presence of wind shear, and at the same time aerodynamic envelope protection is retained. The adaptive controller for wind compensation has been designed by a backstepping approach and feedback linearization for time-varying systems. The wind shear components have been estimated by higher-order sliding mode schemes. At the end of this work the results are provided, an autonomous final approach in presence of microburst is discussed, performances are analyzed, and estimation of the microburst characteristics from telemetry data is examined.