Fiber laser welding (FLW) was used to join advanced high strength steel (AHSS) and high strength steel (HSS); specifically two dual-phase (DP) steels, with ultimate tensile strengths above 980 MPa and with different chemistries (DP980 Rich and DP980 Lean), and a high strength low alloy (HSLA) steel, with an ultimate tensile strength of 450MPa (HSLA450). The welding speed and power were varied to develop a process envelope for minimizing weld concavity. In order to attain welds free of weld concavity a balance of speed and power was required; weld concavity could be reduced by lowering power and increasing speed. Welds with amounts of concavity ranging from 15 % to 35 % were characterized with respect to hardness, tensile and fatigue testing. Tensile results revealed that DP steel was sensitive to weld concavity while HSLA450 was not. At stress amplitudes enduring beyond 1000 cycles, welded specimens exhibited lower fatigue resistance compared to the base metal. Concavity reduced the fatigue life of DP980 steels, where increasing the amount of concavity further reduced the fatigue resistance, while the fatigue resistance of HSLA steel welds was not sensitive to weld concavity. Hardness profiling of the welds revealed that HAZ softening was present in the DP980 steel welds. The amount of HAZ softening was normalized; allowing for comparison of different steels. Welds made by FLW demonstrated reduced softening compared other laser welding types because FLW was capable of welding with lower heat input. A difference in the FZ hardness was observed between the DP980 steels because of the difference in carbon content of the steels; where higher carbon content resulted in higher FZ hardness. Additionally the high cooling rate in FLW created higher fusion zone hardness than the values predicted by Yurioka’s model based on arc welding. Examination of the microstructure revealed that the soft zone of DP980 Lean steel possessed severely tempered martensite and untransformed ferrite while DP980 Rich generated a structure with a mixture of tempered martensite, untransformed ferrite and a small fraction of non-tempered martensite. This difference in HAZ softening was attributed to the alloying content of the DP980 Rich steel the higher alloying content of DP980 Rich steel formed a stable austenite that could exist near the Ac1 temperature and enabled the formation of new martensite in the soft zone. The effects of HAZ softening were apparent in tensile testing where the DP980 Lean steel, which exhibited higher softening, demonstrated by a severe reduction in elongation while the DP980 Rich steel, which had higher resistance to softening, attained elongation comparable to its base metal. HSLA450 exhibited a slight reduction in elongation due to the hardening of the fusion zone. The welded DP980 Rich and HSLA450 steels consistently failed within the base metal, while the DP980 Lean steel failed in the soft zone. The welded DP980 Rich steel also demonstrated limiting dome heights comparable to the base metal while the severe softening in the DP980 Lean led to premature fracture in the soft zone, yielding a larger reduction in the limiting dome height.

Fiber laser welding (FLW) was used to join advanced high strength steel (AHSS) and high strength steel (HSS); specifically two dual-phase (DP) steels, with ultimate tensile strengths above 980 MPa and with different chemistries (DP980 Rich and DP980 Lean), and a high strength low alloy (HSLA) steel, with an ultimate tensile strength of 450MPa (HSLA450). The welding speed and power were varied to develop a process envelope for minimizing weld concavity. In order to attain welds free of weld concavity a balance of speed and power was required; weld concavity could be reduced by lowering power and increasing speed. Welds with amounts of concavity ranging from 15 % to 35 % were characterized with respect to hardness, tensile and fatigue testing. Tensile results revealed that DP steel was sensitive to weld concavity while HSLA450 was not. At stress amplitudes enduring beyond 1000 cycles, welded specimens exhibited lower fatigue resistance compared to the base metal. Concavity reduced the fatigue life of DP980 steels, where increasing the amount of concavity further reduced the fatigue resistance, while the fatigue resistance of HSLA steel welds was not sensitive to weld concavity. Hardness profiling of the welds revealed that HAZ softening was present in the DP980 steel welds. The amount of HAZ softening was normalized; allowing for comparison of different steels. Welds made by FLW demonstrated reduced softening compared other laser welding types because FLW was capable of welding with lower heat input. A difference in the FZ hardness was observed between the DP980 steels because of the difference in carbon content of the steels; where higher carbon content resulted in higher FZ hardness. Additionally the high cooling rate in FLW created higher fusion zone hardness than the values predicted by Yurioka’s model based on arc welding. Examination of the microstructure revealed that the soft zone of DP980 Lean steel possessed severely tempered martensite and untransformed ferrite while DP980 Rich generated a structure with a mixture of tempered martensite, untransformed ferrite and a small fraction of non-tempered martensite. This difference in HAZ softening was attributed to the alloying content of the DP980 Rich steel the higher alloying content of DP980 Rich steel formed a stable austenite that could exist near the Ac1 temperature and enabled the formation of new martensite in the soft zone. The effects of HAZ softening were apparent in tensile testing where the DP980 Lean steel, which exhibited higher softening, demonstrated by a severe reduction in elongation while the DP980 Rich steel, which had higher resistance to softening, attained elongation comparable to its base metal. HSLA450 exhibited a slight reduction in elongation due to the hardening of the fusion zone. The welded DP980 Rich and HSLA450 steels consistently failed within the base metal, while the DP980 Lean steel failed in the soft zone. The welded DP980 Rich steel also demonstrated limiting dome heights comparable to the base metal while the severe softening in the DP980 Lean led to premature fracture in the soft zone, yielding a larger reduction in the limiting dome height.

[pt] Esta dissertação faz parte de um projeto mais abrangente que visa caracterizar os parâmetros ideais para perfuração e corte a laser em rochas, metais e cimentos tipicamente utilizados na indústria do petróleo. Este trabalho teve por objetivo de caracterizar cortes a laser em placas de aço. Procurou-se correlacionar a morfologia do corte e a formação de rebarbas com parâmetros operacionais, tais como densidade de potência e posição do ponto focal. O estudo foi desenvolvido para o aço SAE 1020 com e sem anteparo rochoso (Travertino). Foram avaliadas também as mudanças na microestrutura de regiões adjacentes do aço duplex 2205 para diferentes faixas de densidade de potência. Finalmente, avaliou-se também o uso do laser no corte do aço inox submerso em água. Conclui-se que existe uma formação de rebarba, que aumenta conforme a densidade de potência diminui. Por outro lado, quanto maior a densidade de potência, maior é a extensão da mudança na microestrutura do aço. O corte de aço com anteparo rochoso abre novas perspectivas para o desenvolvimento de uma ferramenta baseada em laser de alta potência para completação de poços na indústria do petróleo. / [en] This work is part of a larger project that aims to characterize the optimal parameters for laser cutting and drilling into rocks, metals and cement typically used in the oil industry. This study had as objective to characterize laser cuts in steel plates. An attempt to establish a correlation between the morphology of the cut and the burrs with operating parameters such as power density and position of the focal point. The study was developed for the SAE 1020 steel with and without rocky bulkhead (Travertine). Also, the changes in the microstructure of adjacent regions of duplex steel in 2205 for different ranges of power density were assessed and finally it was evaluated the use of laser cutting of stainless steel submerged in water. It follows that there is a burr formation, which increases as the power density decreases. On the other hand, the higher the power density, the greater is the extent of change in the steel microstructure. Cutting steel with rocky bulkhead opens new perspectives for the tool development with high power laser for well completion in the oil industry tool.

Materiais compósitos são projetados e fabricados para várias aplicações de alto desempenho, incluindo componentes para os segmentos automobilístico, aeroespacial, aeronáutico, naval, de defesa, de óleo e gás, energia eólica e até equipamentos esportivos. Porém, a união por soldagem de Compósitos de Matriz Metálica de Alumínio (Al-CMM) ainda é um grande obstáculo para a maior disseminação desta classe de materiais estruturais. As mudanças microestruturais decorrentes do ciclo de soldagem e/ou do tratamento térmico afetam sensivelmente as propriedades mecânicas e físico-químicas finais da junta e do metal base nas proximidades de mesma, daí a importância de se estudar a evolução microestrutural que prospera nestas etapas. O presente trabalho caracterizou a microestrutura do compósito liga-A356/SiCp soldado por laser de fibra de Itérbio, empregando-se nessa tarefa técnicas de microscopia óptica, radiografia e microscopia eletrônica de varredura, assim como difração de raios-X e de elétrons retroespalhados, ensaio instrumentado de dureza e microtomografia computadorizada. O foco das análises realizadas restringiu-se à geometria dos cordões de solda, à expulsão de SiC particulado da zona soldada, à volatilização de elementos químicos da poça de soldagem, à formação de precipitados fragilizantes de Al4SiC4 em formato de agulhas no cordão de solda e à determinação das regiões com concentração de poros, todos estes fenômenos tendo efeitos nocivos, em maior ou menor extensão, no desempenho global da junta do Al-CMM soldada a laser, notadamente em suas propriedades mecânicas e eletroquímicas. / Microstructural materials composites are designed and manufactured for various high performance applications, including components for different industries like automobile, aerospace, aeronautical, naval, defense, oil and gas, wind energy and even sports equipment. However, the junction by welding of Aluminum Metal Matrix Composite (Al-MMC) is still a major obstacle to the further spread of this class of structural materials. The microstructural changes resulting from the welding cycle and / or post-weld heat treatment significantly affect the final mechanical and physicochemical properties of the joint and the base metal near it, hence the importance of studying the microstructural evolution that thrives in these steps. This study aims to characterize the microstructure of the composite alloy-A356 / SiCp welding by Ytterbium fiber laser, using optical microscopy, X-ray, scanning electron microscopy, X-ray diffraction, electron backscatter diffraction, instrumented test hardness and computed microtomography. The focus of the analyzes was restricted to the geometry of the weld bead, the particulate SiC expulsion of the welded zone, volatilization of chemical elements from the welding zone, formation of precipitates embrittlement of Al4SiC4 in needle shape in the weld bead and determining the concentration of regions with pores, all these phenomena have harmful effects to a greater or lesser extent, the overall performance of the joining Al-CMM laser welded, mainly in their mechanical and electrochemical properties.

Made available in DSpace on 2016-04-18T21:39:49Z (GMT). No. of bitstreams: 2 Camila Campos Dias1.pdf: 2379886 bytes, checksum: f6caa3559713f5aee5905312eed15997 (MD5) Camila Campos Dias2.pdf: 1312698 bytes, checksum: feece23943bc176a275e8b5e11dc217c (MD5) Previous issue date: 2009-01-30 / Fundo Mackenzie de Pesquisa / In this work we show a study of mode-locking stabilization in an Erbium doped fiber laser with assynchronous mode-locking generating ultra-short pulses at the rate of 10 GHz. The fiber effects are presented as well as the mode-locking techniques. Also is presented a study of energy pulse stabilization, frequency and cavity, in addition an overview of stabilization techniques. Using different cavities setups with different accumulated dispersion, we analyzed the stabilization of the pulse. The temperature effects and state of polarization were studied too and we found that the temperature has greater influence on the stability. After the results of passive approach of the stabilization, we studied two methods of active stabilization, using a feedback and proposed a new one that is a new way of controlling the frequency variations in the cavity. By the use the asynchronous mode-locking, through the cavity frequency, we control the modulator frequency. For the implementation of our proposal, there are two approaches to data acquisition, using a frequency counter or a spectrum analyzer, in this work the tests were performed with the first. / Apresentamos neste trabalho um estudo da estabilização do acoplamento de modos de um laser de fibra dopada com Érbio com modos acoplados assíncronamente operando a uma taxa de 10 GHz com pulsos ultracurtos. Os efeitos que ocorrem na fibra são apresentados assim como os métodos de acoplamento de modos que geram o trem de pulsos. Também é apresentado um estudo da estabilização da energia do pulso, freqüência e cavidade, além do histórico dos meios de estabilização. Utilizando diferentes configurações de cavidade, com diferentes dispersões acumuladas, analisamos o tempo de estabilidade do pulso. Os efeitos da temperatura e do estado de polarização também foram estudados e verificamos que a temperatura tem maior influência na instabilidade. Depois dos resultados da abordagem passiva de estabilização do acoplamento de modos, estudamos dois métodos de estabilização ativa, utilizando um feedback e propusemos um novo método de feedback que é uma nova maneira de controlar as variações de freqüência na cavidade. Como utilizamos o acoplamento de modos assíncrono, através da freqüência da cavidade, controlamos a freqüência do modulador. Para a realização da nossa proposta, existem duas abordagens de aquisição de dados, utilizando um freqüencímetro ou um analisador de espectro elétrico, sendo que os testes deste trabalho foram realizados com o primeiro.

Le perçage est un procédé de fabrication répandu dans le milieu industriel. Le secteur aéronautique a recours à ce procédé pour usiner de nombreuses pièces. Les chambres de combustions en sont un exemple. Exposées à des cycles thermiques sévères, elles sont percées d’une multitude de trous de refroidissement. Chez Safran Helicopter Engines, motoriste spécialisé dans la conception de turbines à gaz pour hélicoptères, ce perçage est réalisé à l’aide d’un procédé d’usinage unique : le perçage par percussion laser à la volée. Ce procédé phare leur permet de réaliser des milliers de trous inclinés dans des tôles en matériaux réfractaires. Safran Helicopter Engines cherche à maintenir son avance dans la production de turbines en s’appuyant sur les innovations constantes du procédé de perçage. Ce travail de thèse s’est articule autour du développement d’un nouveau procédé de perçage laser. De manière à définir un procédé fiable et efficace, plusieurs stratégies de perçage sont étudiées via les possibilités offertes par un laser à fibre milliseconde de haute puissance. Les résultats obtenus laissent entrevoir des perspectives intéressantes en termes d’augmentation de cadence de production à qualité d’usinage équivalente. L’amélioration des performances a été démontrée expérimentalement sur un banc d’essais représentatif des machines de production. Des trous de 400 μm de diamètre incliné à 60o ont pu être réalisés avec un cycle de perçage raccourci au minimum d’un facteur 2. Cette thèse présente également des éléments de compréhension des phénomènes de formation d’un trou. Pour cela, une modélisation des processus thermo hydrodynamiques impliqués dans le procédé de perçage laser a été développée. Ce modèle basé sur une approche par éléments finis repose sur l’étude thermique au cours de l’interaction entre le faisceau laser et la matière. Une partie du modèle inclut les phénomènes de propagation du faisceau dans la cavité en cours de formation afin de traduire de manière plus réaliste le dépôt d’énergie. / Drilling is a well-known manufacturing process. The aeronautic industry uses this process to machine a lot of elements. Among them, we can mention turbine blades, fuel injectors, combustion chambers. The latter are exposed to serious thermal stresses. To limit their impacts, combustion chambers are drilled with multiples cooling holes. At Safran Helicopter Engines, engines manufacturer specialized in engines design for helicopters, drilling is performed with a unique machining process : on the fly laser percussion drilling. This flagship process allows drilling thousands of tilted holes on refractory materials. Safran Helicopter Engines seeks to preserve its leading position in turbo engines manufacturing by looking for steady innovative drilling process. This thesis is structured around the development of a new laser drilling process. To define a reliable and efficient process, several drilling strategies were studied through the possibilities offered by a high-power millisecond fiber laser. The presented results allow catching a glimpse of the possibilities of production improvement. The performance enhancement was established through experimentation with a test bench. Holes of 400 μm diameter with an angle of 60o were drilled with a reduced processing time thanks to this new drilling process. In this thesis, we also propose a theoretical approach describing the hole formation. A mathematical model, accounting for all the physical process taking place during the drilling process is introduced. This model is based on finite elements method and considers the laser beam propagation within the drilled holes by solving Maxwell equations

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Master's thesis deals with consideration possibility of conventional and unconvetional welding methods of wrought magnesium alloys. Methods of Friction Stir Welding, Pulsed Nd:YAG laser and Continuous Fiber laser was used to join magnesium alloy sheets AZ31, AZ61, ZE10 and ZE41. For studying influence of processing parameters on microstructure and mechanical properties were used methods of light microscopy, scanning electron microscopy, tensile tests and microhardness measurements. The results of tensile tests show that from the point of view of keeping ultimate tensile strength is the best methods for welding magnesium alloys Friction Stir Welding. Compared with Nd:YAG laser, fiber laser give better properties of welds. From comparing microstructure and mechanical properties . It wasn't found publications about Friction Stir Welding of magnesium ZE alloys or about FSW sheets with thickness only 0,8 mm and 1,6 mm.

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No description available.