Sistemas inteligentes aplicados em monitoramento de estruturas aeronáuticas.

Este trabalho apresenta o desenvolvimento de sistemas inteligentes aplicados ao monitoramento de estruturas aeronáuticas abordando dois modelos distintos: o primeiro é a análise e classificação de imagens de ultrassom de estruturas aeronáuticas com objetivo de apoiar decisões em reparo de estruturas aeronáuticas. Foi definido como escopo do trabalho uma seção transversal da asa da aeronave modelo Boeing 707. Após a remoção de material superficial em áreas comprometidas por corrosão, é realizada a medição da espessura ao longo da área da peça. Com base nestas medições, a Engenharia realiza a análise estrutural, observando os limites determinados pelo manual de manutenção e determina a necessidade ou não de reparo. O segundo modelo compreende o método de impedância eletromecânica. É proposto o desenvolvimento de um sistema de monitoramento de baixo custo aplicado em uma barra de alumínio aeronáutico com 10 posições de fixação de porcas e parafusos. O objetivo do sistema é avaliar, a partir das curvas de impedância extraídas do transdutor PZT fixado na barra, sua capacidade de classificar a existência ou não de um dano na estrutura e, em caso de existência do dano, indicar sua localização e seu grau de severidade. Foram utilizados os seguintes classificadores neste trabalho: máquina de vetor de suporte, redes neurais artificiais e K vizinhos mais próximos.

Beluga, Delphinapterus leucas, Habitat Associations in Cook Inlet, Alaska

A review of available information describing habitat associations for belugas, Delphinapterus leucas, in Cook Inlet was undertaken to complement population assessment surveys from 1993-2000. Available data for physical, biological, and anthropogenic factors in Cook Inlet are summarized followed by a provisional description of seasonal habitat associations. To summarize habitat preferences, the beluga summer distribution pattern was used to partition Cook Inlet into three regions. In general, belugas congregate in shallow, relatively warm, low-salinity water near major river outflows in upper Cook Inlet during summer (defined as their primary habitat), where prey availability is comparatively high and predator occurrence relatively low. In winter, belugas are seen in the central inlet, but sightings are fewer in number, and whales more dispersed compared to summer. Belugas are associated with a range of ice conditions in winter, from ice-free to 60% ice-covered water. Natural catastrophic events, such as fires, earthquakes, and volcanic eruptions, have had no reported effect on beluga habitat, although such events likely affect water quality and, potentially, prey availability. Similarly, although sewage effluent and discharges from industrial and military activities along Cook Inlet negatively affect water quality, analyses of organochlorines and heavy metal burdens indicate that Cook Inlet belugas are not assimilating contaminant loads greater than any other Alaska beluga stocks. Offshore oil and gas activities and vessel traffic are high in the central inlet compared with other Alaska waters, although belugas in Cook Inlet seem habituated to these anthropogenic factors. Anthropogenic factors that have the highest potential negative impacts on belugas include subsistence hunts (not discussed in this report), noise from transportation and offshore oil and gas extraction (ship transits and aircraft overflights), and water quality degradation (from urban runoff and sewage treatment facilities). Although significant impacts from anthropogenic factors other than hunting are not yet apparent, assessment of potential impacts from human activities, especially those that may effect prey availability, are needed.

Avaliação de complexos de inclusão na inibição do aço carbono em meio ácido

A indústria de petróleo e gás apresenta sérios problemas relacionados à corrosão. Nas petroquímicas e nas instalações de refino de petróleo, as falhas em materiais estão relacionadas com a corrosão, além disso, os processos de corrosão de metais são problemas no mundo, causando ônus em processos industriais e gerando situações de risco como a corrosão de pilares metálicos em pontes ou em fuselagens de aviões. Dentre os meios corrosivos, um muito comum é o meio ácido, que será o meio estudado neste trabalho. Com todos os problemas citados, se faz necessário o estudo de inibidores de corrosão com alta eficiência, estabilidade e que, preferencialmente, não agridam o meio ambiente. Alguns inibidores de corrosão apresentam solubilidade limitada em água, sendo necessária a utilização de alguns solventes não tão amigáveis ao meio ambiente. Então, propôs-se formar um complexo de inclusão para tornar possível a solubilização de inibidores convencionais em solução aquosa, como algumas tioureias, que apresentam solubilidade limitada em água. Essa completa solubilização do inibidor de corrosão orgânico em meio aquoso é possível com a utilização de um aditivo (hospedeiro) capaz de encapsular tais moléculas (convidados) via interações não covalentes, de modo a alcançar o máximo desempenho de inibição. Para a formação do complexo de inclusão foi usado como molécula hospedeira, a α e a β hidroxipropilciclodextrina e como molécula convidada a dibenziltioureia. A intenção foi testar a melhora da ação inibidora da corrosão do aço carbono em meio de HCl 1mol.L-1 com ensaios de perda de massa, de impedância, polarização e microscopia eletrônica de varredura (MEV), além de evidenciar a formação destes complexos de inclusão através da espectroscopia de absorção vibracional no infravermelho, espectroscopia de RMN de 1H, espectroscopia de absorção no Ultra-violeta e análise térmica diferencial (DTA)

Comparison of different scheduling techniques for H-infinity controllers

Several approaches to designing schedule H-infinity control systems are compared. These include a controller switching approach and also parameter scheduling of an observer representation of the controller. They are illustrated by application to a Generic VSTOI. Aircraft Model (GVAM) supplied by The Royal Aerospace Establishment (RAE) at Bedford. The switched design has been tested on the simulator at RAE Bedford. The linear H-infinity designs make use of a loop-shaping followed by robust stabilisation to additive perturbations of a normalised coprime factorisation of the shaped plans. The different scheduling approaches are compared with respect to achieved robust stability levels. performance and complexity of implementation.

An experimental and computational study of the formation of a streamwise shed vortex in a turbine stage

Shear layers shed by aircraft wings roll up into vortices. A similar, though far less common, phenomenon can occur in the wake of a turbomachine blade. This paper presents experimental data from a new single stage turbine that has been commissioned at the Whittle Laboratory. Two low aspect ratio stators have been tested with the same rotor row. Surface flow visualisation illustrates the extremely strong secondary flows present in both NGV designs. These secondary flows lead to conventional passage vortices but also to an intense vortex sheet which is shed from the trailing edge of the blades. Pneumatic probe traverse show how this sheet rolls up into a concentrated vortex in the second stator design, but not in the first. A simple numerical experiment is used to model the shear layer instability and the effects of trailing edge shape and exit yaw angle distribution are investigated. It is found that the latter has a strong influence on shear layer rollup: inhibiting the formation of a vortex downstream of NGV 1 but encouraging it behind NGV 2.

Axial compressor response to inlet flow distortions by a CFD analysis

The usual approach to compressor design considers uniform inlet flow characteristics. Especially in aircraft applications, the inlet flow is quite often non uniform, and this can result in severe performance degradation. The magnitude of this phenomenon is amplified in military engines due to the complexity of inlet duct configurations and the extreme flight conditions. CFD simulation is an innovative and powerful tool for studying inlet distortions and can bring this inside the very early phases of the design process. This project attempts to study the effects of inlet flow distortions in an axial flow compressor trying to minimize the use computer resources and computational time. The first stage of a low bypass ratio compressor has been analyzed and its clean and distorted performance compared outlining the principal changes due to uneven flow distribution: drop in mass flow, increase in pressure and temperature ratios, decrease in surge margin. Three different studies have then been conducted to better understand the effects of the level, the type and the frequency of the distortion.

Vortex filament simulation of trailing vortex merger

Aircraft in high-lift configuration shed multiple vortices. These generally merge to form a downstream wake consisting of two counter-rotating vortices of equal strength. The understanding of the merger of two co-rotating trailing vortices is important in evaluating the separation criteria for different aircraft to prevent wake vortex hazards during landing and take-off. There is no existing theoretical method on the basis of which such norms can be set. The present study is aimed at gaining a better understanding of the behaviour of wake vortices behind the aircraft. Two dimensional studies are carried out using the vortex blob method and compared with Bertenyi's experiment. It is shown that inviscid two dimensional effects are insufficient to explain the observations. Three dimensional studies, using the vortex filament method, are applied to the same test case. Two Lamb-Oseen profile vortices of the same dimensions and initial separation as the experiment are allowed to evolve from a straight starting condition until a converged steady flow is achieved. The results obtained show good agreement with the experimental distance to merger. Core radius and separation behaviour is qualitatively similar to experiment, with the exception of rapid increases at first. This may be partially attributable to the choice of filament-element length, and recommended further work includes a convergence study for this parameter. Copyright © 2005 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

The use of object oriented modelling and simulation tools in constraint satisfaction for embodiment design

The software package Dymola, which implements the new, vendor-independent standard modelling language Modelica, exemplifies the emerging generation of object-oriented modelling and simulation tools. This paper shows how, in addition to its simulation capabilities, it may be used as an embodiment design tool, to size automatically a design assembled from a library of generic parametric components. The example used is a miniature model aircraft diesel engine. To this end, the component classes contain extra algebraic equations calculating the overload factor (or its reciprocal, the safety factor) for all the different modes of failure, such as buckling or tensile yield. Thus the simulation results contain the maximum overload or minimum safety factor for each failure mode along with the critical instant and the device state at which it occurs. The Dymola "Initial Conditions Calculation" function, controlled by a simple software script, may then be used to perform automatic component sizing. Each component is minimised in mass, subject to a chosen safety factor against failure, over a given operating cycle. Whilst the example is in the realm of mechanical design, it must be emphasised that the approach is equally applicable to the electrical or mechatronic domains, indeed to any design problem requiring numerical constraint satisfaction.