Avaliação da colagem de suportes utilizados para fixar cabos elétricos em aeronaves

The most usual method to fix supports that hold the vast majority of electrical cables on an aircraft is accomplished by using, for this purpose, rivets. However, this procedure may some cause some inconveniences such as the need of effecting holes in the structure that is intended to fix these supports, thus decreasing resistance of the structure. In order to have an alternative to seek an increase in the performance of structured materials, the aircraft industry, like other industries, have been studying the use of collage as a method of replacing this usual forms. Against this backdrop, this paper aims to assess the strength and durability of a joint bonded using the adhesive EA9394, manufactured by company Henkel Corporation, and perform a careful survey of the mechanical performance of riveted structures, taking into account different types of conditioning environment and thus create a database that can be used by the aerospace industry

Análise macro e micrográfica da liga AA-356 conforme a taxa de resfriamento

The present work aims to study the characteristics of the alloy Al - 7 % Si - 0 , 3Mg ( AA356 ) , more specifically characterize the macrostructure and microstructure and mechanical properties of the alloy ingots AA356 obtained in metal molds and sand molds for power studying the structures through the difference of cooling rates . This alloy is explained by the fact of referring league has excellent combination of properties such as low solidification shrinkage and good fluidity, good weldability , high wear resistance , high strength to weight ratio, has wide application in general engineering , and particularly in the automotive and aerospace engineering . In this work we will verify this difference in properties through two different cooling rates . We monitor the solid solidification temperatures by thermocouples building with them the cooling curve as a tool that will aid us to evaluate the effectiveness of the grain refining because it achieved with some important properties of the alloy as the latent heat of solidification fraction the liquid and solid temperatures, the total solidification time, and identify the presence of inoculants for grain refinement. Thermal analysis will be supported by the study of graphic software “Origin “will be achieved where the cooling curve and its first derivative that is the cooling rate. Made thermal analysis, analysis will be made in macrographs ingots obtained for observation of macrostructures obtained in both types of ingots and also analysis of micrographs where sampling will occur in strategic positions ingots to correlate with the microstructure. Finally will be collecting data from Brinell hardness of ingots and so then correlating the properties of their respective ingots with cooling rate. We found that obtained with cast metal ingots showed superior properties to the ingots obtained with sand mold

Influência do condicionamento ambiental sobre as propriedades viscoelásticas de compósitos aramida/epóxi

The increasing application of structural composites in the aerospace industry is mainly due to its low specific weight coupled with its excellent mechanical properties when in service. As a result of climatic variations that pass the aircraft is of paramount importance to study the influence of weathering on this type of material when subjected to such changes. The purpose of this work is to evaluate the mechanical behavior of specimens of kevlar fiber /epoxy matrix composites, by dynamic mechanical thermal analysis (DMA) and interlaminar shear strength tests (ILSS), after passing through three environmental conditioning: saline fog, hygrothermal and ultraviolet radiation. From the results, we concluded that the laminate was molded supplied homogeneously, not presenting problems such as porosity, delaminations or cracks inside. After a period of 625 hours of exposure to hygrothermal conditioning, we observed a 1,2% maximum of absorption of moisture. Samples subjected to the conditioning by UV irradiation (600 hours) and salt spray showed a reduction of about 24,30% and 32,30%, respectively, on the shear strength (ILSS). In DMA analysis is not observed significant changes on the glass transition temperature. However, when considering the storage modulus of the samples conditioned by UV radiation (1200 hours), salt spray and hygrothermal conditioning there is an increase of 5,34% , 7,19% and 5,57% respectively

Projeto e concepção de um quadcopter utilizando o controle PID

The present work refers to the design, conception and development of a quadcopter based on PID controllers, a widespread microcontroller on the market was being implemented, the Arduino. Also made use of LabVIEW programming tool from National Instruments company for the quadcopter control and telemetry. For the control, LabVIEW software acquired the joystick commands, making the necessary adjustments to the perfect interpretation by microcontroller on the quadcopter and adjusts the parameters of PID controllers. For telemetry, data relating to quadcopter behavior are received, interpreted and presented in an intuitive user interface. In the first part of this graduate work presents the theoretical background on the subject, with a brief history about the quadcopters, followed by the main projects in the academic and commercial matters. Also are presented the theories of communications used in the design and PID control. Then an overview of the dynamic and mathematical model is demonstrated. Having done this, the physical and computer components required to complete the project are showed and the results are achieved consequently. Finally, a conclusion is made taking into account the results obtained. In this work will be presented the PID control of quadcopter translational movements only to roll and pitch movements

Obtenção e caracterização térmica de compósitos nanoestruturados de resina fenol-furfurílica/CNT

Pós-graduação em Engenharia Mecânica - FEG

Estudo da fadiga em liga de alumínio aeronáutico 7475-T761

This work will address the study of fatigue conditions with constant load in an alloy of aluminum analysis 7475 - T761, so we can better understand the conditions of the aircrafts which contain this alloy in their structures. A literature review, which was discussed the concepts of fracture mechanics, fatigue, aeronautical components, chemical analysis of aluminum alloys, fatigue problems that appears in the aircrafts, metallographic analysis, and testing of optical microscopy tensile, fatigue and microhardness, surface analysis (MEV) study of the chemical composition of the alloy in question, the main causes of crashes, was performed, completing the work, analysis of data from tensile test, hardness and fatigue together with the interpretation of images of optical microscopy and scanning electron was taken. The data indicated the high mechanical strength of the alloy, along with its microstructure indicating elongated grains and high surface contour, which shows such resistance by hindering the movement of dislocations. The grooves are clearly shown in the MEV images as well as the classic with increased fatigue loading and subsequent reduction of the number of cycles to rupture behavior shown in the graphs. Therefore we observed the optimal behavior is supported by the league when subjected to fatigue loadings

Obtenção e caracterização de compósitos de benzoxazina/fibra de carbono

Pós-graduação em Engenharia Mecânica - FEG

Avaliação dos mecanismos de endurecimentoda liga AISI 300M submetida a diferentes ciclos de transformações martensíticas

Pós-graduação em Engenharia Mecânica - FEG

Sistema de gestão da qualidade numa organização pública de P&D: fatores que influenciam a certificação

Pós-graduação em Engenharia Mecânica - FEG

Estudo da cinética de degradação da resina benzoxazina e seus compósitos nanoestruturados

The benzoxaxine resin is a new class of thermoset phenolic resin, which is presenting, in the lasts decades, a great application in the aircraft industry due mainly to its excellent mechanical and thermal properties. This resin associates the mechanical properties of epoxy resin with the thermal and flame retardant properties of phenolic resin. In this context, they are considered polymers of high performance and they are excellent candidates to replace the current thermoset matrices used in the processing of high performance composites. Thus, in this study nanostructured composites Benzoxazine/CNT were produced at different concentrations of functionalized and non-functionalized CNT (0,1%; 0,5% and 1,0% w/w). The thermal stability of the benzoxazine resin and its nanostructured composites was studied using thermogravimetry (TGA) and degradation kinetic model Ozawa-Wall-Flynn (O-W-F). The thermal characterization also included differential scanning calorimetry (DSC) and dynamic-mechanical analysis, infrared spectroscopy with Fourier transform (FTIR) and scanning electron microscopy (SEM).The introduction of non-functionalized CNT at low concentrations resulted in nanostructured composites with better thermal properties in relation to the neat resin. For all cases, however, the dispersion of CNT in the matrix was ineffective

Estudo da cinética de degradação da resina benzoxazina e seus compósitos nanoestruturados

The benzoxaxine resin is a new class of thermoset phenolic resin, which is presenting, in the lasts decades, a great application in the aircraft industry due mainly to its excellent mechanical and thermal properties. This resin associates the mechanical properties of epoxy resin with the thermal and flame retardant properties of phenolic resin. In this context, they are considered polymers of high performance and they are excellent candidates to replace the current thermoset matrices used in the processing of high performance composites. Thus, in this study nanostructured composites Benzoxazine/CNT were produced at different concentrations of functionalized and non-functionalized CNT (0,1%; 0,5% and 1,0% w/w). The thermal stability of the benzoxazine resin and its nanostructured composites was studied using thermogravimetry (TGA) and degradation kinetic model Ozawa-Wall-Flynn (O-W-F). The thermal characterization also included differential scanning calorimetry (DSC) and dynamic-mechanical analysis, infrared spectroscopy with Fourier transform (FTIR) and scanning electron microscopy (SEM).The introduction of non-functionalized CNT at low concentrations resulted in nanostructured composites with better thermal properties in relation to the neat resin. For all cases, however, the dispersion of CNT in the matrix was ineffective

Aerodinámica

La Aerodinámica estudia las fuerzas que un viento relativo ejerce sobre un obstáculo sumergido en él. Desde este punto de vista tan general las aplicaciones de la Aerodinámica no se reducen exclusivamente al estudio de las fuerzas sobre aviones más o menos clásicos sino que trascienden a otros muchos campos por el efecto de arrastre que es característico de ciencias y técnicas avanzadas. La conferencia, dentro de un ciclo sobre Ingeniería Aeroespacial, se centra en la aerodinámica de objetos volantes producidos por el hombre, pero es de temer que el interés del conferenciante por otras aplicaciones se deje ver demasiado. El tema es de una gran extensión y, sobre todo, una gran complicación. Se ha repetido hasta la saciedad que para su estudio es más útil la experimentación que el raciocinio (Sir George Cayley (1733-1857).

Refrigeración de LED's mediante "Heat Pipes"

El enfriamiento tradicional de los LEDs, mediante disipadores térmicos, se ve muchas veces comprometido al tener que disponer estos elementos refrigeradores justo en el punto de generación de la luz. Para evitar, en la medida de lo posible, este hecho, se presenta como una de las posibles alternativas el empleo de los ?Heat Pipes?. Los Heat Pipes son unos dispositivos autónomos, que permiten refrigerar los focos calientes, trasladando el calor generado por ellos a disipadores térmicos situados en zonas más accesibles y menos comprometidas. Los Heat Pipe, basados en técnicas termodinámicas, tienen un uso muy extendido en la tecnología aeroespacial. Son actualmente la solución ideal en aplicaciones de bombeo de calor y refrigeración de componenetes electricos y electrónicos. Con tamaños reducidos, pueden alcanzar flujos de refrigeración de 300 - 400 W/cm2. En esta comunicación se presenta y analiza este tipo de refrigeración aplicada a LED¿s utilizados en iluminación y alumbrado. La refrigeración de LEDs propuesta está compuesta por el Heat Pipe adosado por un extremo a la cara posterior del diodo LED, y por el otro, a una cierta distancia, al disipador térmico. La temperatura alcanzada por el LED dependerá del tipo y características del Heat Pipe así como de las cualidades del disipador térmico utilizado. También se utilizan en combinación con refrigeradores termoeléctricos (células de Peltier) cuando se desea controlar la temperatura de los dispositivos por debajo de la temperatura ambiental.

Caos en evolución no lineal de ondas de Alfven usando un modelo resistivo

Interacciones no lineales de ondas de Alfvén existen tanto para plasmas en el espacio como en laboratorios, con efectos que van desde calentamiento hasta conducción de corriente. Un ejemplo de emisión de ondas de Alfvén en ingeniería aeroespacial aparece en amarras espaciales. Estos dispositivos emiten ondas en estructuras denominadas “Alas de Alfvén”. La ecuación derivada no lineal de Schrödinger (DNLS) posee la capacidad de describir la propagación de ondas de Alfvén de amplitud finita circularmente polarizadas en un plasma frío. En esta investigación, dicha ecuación es truncada con el objetivo de explorar el acoplamiento coherente, débilmente no lineal y cúbico de tres ondas cerca de resonancia. De las tres ondas, una es linealmente inestable y las otras dos son amortiguadas. Por medio de la utilización de este modelo se genera un flujo 4D formado por tres amplitudes y una fase relativa. En trabajos anteriores se analizó la transición dura hacia caos en flujos 3D.2005). Se presenta en este artículo un análisis teórico y numérico del comportamiento del sistema cuando la tasa de crecimiento de la onda inestable es muy próxima a cero y considerando amortiguamiento resistivo, es decir se satisface una relación cuadrática entre amortiguamientos y números de onda. Al igual que en los trabajos anteriores, se ha encontrado que sin importar cuan pequeña es la tasa de crecimiento de la onda inestable existe un dominio paramétrico, en el espacio de fase, donde aparecen oscilaciones caóticas que están ausentes para una tasa de crecimiento nula. Sin embargo diagramas de bifurcación y dominios de estabilidad presentan diferencias con respecto a lo estudiado anteriormente.

Adaptive scheme for Accurate orbit propagation

Two extensions of the fast and accurate special perturbation method recently developed by Peláez et al. are presented for respectively elliptic and hyperbolic motion. A comparison with Peláez?s method and with the very efficient Stiefel- Scheifele?s method, for the problems of oblate Earth plus Moon and continuous radial thrust, shows that the new formulations can appreciably improve the accuracy of Peláez?s method and have a better performance of Stiefel-Scheifele?s method. Future work will be to include the two new formulations and the original one due to Peláez into an adaptive scheme for highly accurate orbit propagation