946 resultados para CAD-CAM


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Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

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Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

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Pós-graduação em Psicologia - FCLAS

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This paper presents a Computer Aided Diagnosis (CAD) system that automatically classifies microcalcifications detected on digital mammograms into one of the five types proposed by Michele Le Gal, a classification scheme that allows radiologists to determine whether a breast tumor is malignant or not without the need for surgeries. The developed system uses a combination of wavelets and Artificial Neural Networks (ANN) and is executed on an Altera DE2-115 Development Kit, a kit containing a Field-Programmable Gate Array (FPGA) that allows the system to be smaller, cheaper and more energy efficient. Results have shown that the system was able to correctly classify 96.67% of test samples, which can be used as a second opinion by radiologists in breast cancer early diagnosis. (C) 2013 The Authors. Published by Elsevier B.V.

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Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

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Modeling is a step to perform a finite element analysis. Different methods of model construction are reported in literature, as the Bio-CAD modeling. The purpose of this study was to perform a model evaluation and application using two methods of Bio-CAD modeling from human edentulous hemi-mandible on the finite element analysis. From CT scans of dried human skull was reconstructed a stereolithographic model. Two methods of modeling were performed: STL conversion approach (Model 1) associated to STL simplification and reverse engineering approach (Model 2). For finite element analysis was used the action of lateral pterygoid muscle as loading condition to assess total displacement (D), equivalent von-Mises stress (VM) and maximum principal stress (MP). Two models presented differences on the geometry regarding surface number (1834 (model 1); 282 (model 2)). Were observed differences in finite element mesh regarding element number (30428 nodes/16683 elements (model 1); 15801 nodes/8410 elements (model 2). D, VM and MP stress areas presented similar distribution in two models. The values were different regarding maximum and minimum values of D (ranging 0-0.511 mm (model 1) and 0-0.544 mm (model 2), VM stress (6.36E-04-11.4 MPa (model 1) and 2.15E-04-14.7 MPa (model 2) and MP stress (-1.43-9.14 MPa (model 1) and -1.2-11.6 MPa (model 2). From two methods of Bio-CAD modeling, the reverse engineering presented better anatomical representation compared to the STL conversion approach. The models presented differences in the finite element mesh, total displacement and stress distribution.

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Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

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Pós-graduação em Design - FAAC

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The high competitiveness and the search for newtechnologies that differentiate the product from the project,require the use of new digital tools. The computer aideddesign - Computed Aided Design (CAD), with electronicmodeling, simulation, structural analysis and production,performed in a virtual environment through the applicationof specific software, are available but their use is stilllimited. There are various software available in languagesand extensions to industrial production which, from 3Dmodeling, they can manage through Computer NumericalControl - Computed Numerical Control (CNC) machiningcenters, laminating, stamping, mold making and otherprocesses productive. This project aims to encouragecreativity and entrepreneurship in the community throughthe provision of technology computer aided design - CAD,with a view to implementation of machining technology.

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Recent developments in piston engine technology have increased performance in a very significant way. Diesel turbocharged/turbo compound engines, fuelled by jet fuels, have great performances. The focal point of this thesis is the transformation of the FIAT 1900 jtd diesel common rail engine for the installation on general aviation aircrafts like the CESSNA 172. All considerations about the diesel engine are supported by the studies that have taken place in the laboratories of the II Faculty of Engineering in Forlì. This work, mostly experimental, concerns the transformation of the automotive FIAT 1900 jtd – 4 cylinders – turbocharged – diesel common rail into an aircraft engine. The design philosophy of the aluminium alloy basement of the spark ignition engine have been transferred to the diesel version while the pistons and the head of the FIAT 1900 jtd are kept in the aircraft engine. Different solutions have been examined in this work. A first V 90° cylinders version that can develop up to 300 CV and whose weight is 30 kg, without auxiliaries and turbocharging group. The second version is a development of e original version of the diesel 1900 cc engine with an optimized crankshaft, that employ a special steel, 300M, and that is verified for the aircraft requirements. Another version with an augmented stroke and with a total displacement of 2500 cc has been examined; the result is a 30% engine heavier. The last version proposed is a 1600 cc diesel engine that work at 5000 rpm, with a reduced stroke and capable of more than 200 CV; it was inspired to the Yamaha R1 motorcycle engine. The diesel aircraft engine design keeps the bore of 82 mm, while the stroke is reduced to 64.6 mm, so the engine size is reduced along with weight. The basement weight, in GD AlSi 9 MgMn alloy, is 8,5 kg. Crankshaft, rods and accessories have been redesigned to comply to aircraft standards. The result is that the overall size is increased of only the 8% when referred to the Yamaha engine spark ignition version, while the basement weight increases of 53 %, even if the bore of the diesel version is 11% lager. The original FIAT 1900 jtd piston has been slightly modified with the combustion chamber reworked to the compression ratio of 15:1. The material adopted for the piston is the aluminium alloy A390.0-T5 commonly used in the automotive field. The piston weight is 0,5 kg for the diesel engine. The crankshaft is verified to torsional vibrations according to the Lloyd register of shipping requirements. The 300M special steel crankshaft total weight is of 14,5 kg. The result reached is a very small and light engine that may be certified for general aviation: the engine weight, without the supercharger, air inlet assembly, auxiliary generators and high pressure body, is 44,7 kg and the total engine weight, with enlightened HP pump body and the titanium alloy turbocharger is less than 100 kg, the total displacement is 1365 cm3 and the estimated output power is 220 CV. The direct conversion of automotive piston engine to aircrafts pays too huge weight penalties. In fact the main aircraft requirement is to optimize the power to weight ratio in order to obtain compact and fast engines for aeronautical use: this 1600 common rail diesel engine version demonstrates that these results can be reached.

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The present dissertation relates to methodologies and technics about industrial and mechanical design. The author intends to give a complete idea about the world of design, showing the theories of Quality Function Deployment and TRIZ, of other methods just like planning, budgeting, Value Analysis and Engineering, Concurrent Engineering, Design for Assembly and Manufactoring, etc., and their applications to five concrete cases. In these cases there are also illustrated design technics as CAD, CAS, CAM; Rendering, which are ways to transform an idea into reality. The most important object of the work is, however, the birth of a new methodology, coming up from a comparison between QFD and TRIZ and their integration through other methodologies, just like Time and Cost Analysis, learned and skilled during an important experience in a very famous Italian automotive factory.

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Lo scopo del lavoro è quello di verificare tramite software CAD l’influenza dei principali parametri chirurgici e anatomici sul Range Of Motion (ROM). Sono stati costruiti 5 modelli, uno di articolazione sana(Senza Protesi), uno di protesi Convenzionale e tre di protesi Conservative o a Conservazione (Totale, Media e Bassa Conservazione). Per tutti i modelli sono state simulate le rotazioni di base e i cosiddetti movimenti critici, ovvero quei movimenti a rischio di lussazione. Le prove sono state eseguite per teste da 28-,32-,36-,40mm di diametro, e con la coppa orientata di 45° in abduzione e 15° gradi in antiversione prima e successivamente di 45° e 0°. Inoltre, per verificare l’influenza dell’offset sul ROM, sono stati costruiti e simulati i movimenti per altri 5 modelli che non conservassero il vincolo del mantenere l’offset anatomico. Variando il diametro della testa si registrano differenze apprezzabili in termini di ROM solo per i movimenti di Estensione e Abduzione per il modello di Protesi Convenzionale e di Abduzione per il modello a Bassa Conservazione. Variando il livello di resezione del collo si è visto come per i modelli di protesi a Media Conservazione, Bassa Conservazione e Convenzionale si misurano angoli superiori a quello del riferimento tratto dalla Letteratura. Diversamente per il modello di Protesi a Totale Conservazione i valori ottenuti per alcuni movimenti sono inferiori, poiché limitati da un contatto di tipo c-b. Le simulazioni dei movimenti critici confermano la tendenza di un ROM accettabile per i modelli di protesi a Bassa Conservazione e di protesi Convenzionale, i quali forniscono escursioni angolari sempre superiori a quelle prese come riferimento dalla Letteratura. Invece, le protesi a Totale e Media Conservazione forniscono valori inferiori al riferimento per i movimenti di Pivot e Roll, essendo limitati dall’antiversione della coppa (movimenti di ExtraRotazione e contatto c-b). Variando la posizione della coppa a 45°/0° i due movimenti Critici Pivot e Roll migliorano per i modelli a Totale e Media Conservazione, tornando in linea con il riferimento. Riguardo l’offset si nota come più si avvicina a quello anatomico che misura 46,2mm (da 37 a 44mm), più si riscontra un aumento in termini di ROM.

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Progetto di due turbine eoliche di piccola potenza per alimentare utenze remote. Sia la turbina ad asse verticale che quella ad asse orizzontale sono state dimensionate andando ad ottimizzare il funzionamento per un vento di 7.5 m/s ed un carico dato da un alternatore da 500W. Entrambe le turbine sono poi state modellate al CAD e sono stati realizzati i disegni costruttivi di alcuni elementi delle stesse.

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Modellazione al CAD di un aliante sviluppato in Germania nei primi decenni dello scorso secolo e studio preliminare di fattibilità della motorizzazione del velivolo.