Relevant bibliographies by topics / AA6061

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Academic literature on the topic 'AA6061'

Author: Grafiati
Published: 4 June 2021
Last updated: 7 September 2023

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Journal articles on the topic "AA6061"

1

Agustín-Sáenz, Cecilia, Patricia Santa Coloma, Francisco J. Fernández-Carretero, Fabiola Brusciotti, and Marta Brizuela. "Design of Corrosion Protective and Antistatic Hybrid Sol-Gel Coatings on 6XXX AlMgSi Alloys for Aerospace Application." Coatings 10, no. 5 (April 30, 2020): 441. http://dx.doi.org/10.3390/coatings10050441.

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An inorganic–organic coating based on glycidyl-functionalized silica and zirconia was synthesized by sol-gel technology to protect three types of AlMgSi (6XXX series) alloys against corrosion in aerospace applications. Different parameters such as the solid content, the organic/inorganic ratio of the sols and the deposition conditions were studied with the aim to achieve a tradeoff between the corrosion protection, antistatic performance and low vacuum-induced outgassing. Those parameters directly influence the thickness and the density of the coatings, and therefore the barrier effect against corrosion and the contact electrical resistance, which are affected in opposite ways. To obtain a low contact electrical resistance, silver nanowires (NW) with a high aspect ratio were loaded in the sol-gel matrix with the aim to create a conductive path through the hybrid coating with a low concentration of NWs. The coatings were adapted for AA6063, AA6061 and AA6082, and they all showed an outstanding anti-corrosion performance in different artificial weathering tests, whereas electrochemical impedance spectroscopy permitted the identification of the most critical parameters affecting water uptake. An antistatic performance was demonstrated by the low contact electrical resistance of the coated AA6061 and AA6063 alloys, although the incorporation of NWs showed a detrimental effect on the corrosion protection compared with the unloaded coating.
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Kumar, B. Ashok, M. Muthu Krishnan, A. Felix Sahayaraj, Mohamad Reda A. Refaai, G. Yuvaraj, D. Madhesh, and Haiter Lenin Allasi. "Characterization of the Aluminium Matrix Composite Reinforced with Silicon Nitride (AA6061/Si3N4) Synthesized by the Stir Casting Route." Advances in Materials Science and Engineering 2022 (January 29, 2022): 1–8. http://dx.doi.org/10.1155/2022/8761865.

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The current work is concerned with the synthesis of aluminium (AA6061-T6) matrix composites (AMCs) reinforced with 15 and 20 weight percentages of silicon nitride (Si3N4) particulates using the indigenously fabricated electric stir casting furnace with bottom discharge arrangement. The major concern in the synthesis of AMCs of ceramic particles with the aluminium matrix is wettability in the casting route, and it was overcome by adding 2% of magnesium in the melt, proper incorporation time, and appropriate stirring speed. The microstructure and mechanical characteristics of the synthesized AMC were analyzed. Si3N4 particles in the matrix are uniformly dispersed in the optical and scanning electron micrographs (SEM). Adding reinforcement particles of Si3N4 to the AA6061 matrix increased microhardness, macrohardness, and ultimate tensile strength significantly. Microhardness and macrohardness of the AA6161/20 wt.% Si3N4 composite were 98 VHN and 91 BHN, respectively, which were 117.8% and 111.63% higher than those of the AA6061 matrix alloy, respectively. Ultimate tensile strength (UTS) of AA6061 was 159.82 MPa which was increased to 249.12 MPa in the AA6061/20 wt.% Si3N4 composite. Percent elongation of the AA6061/Si3N4 composite was reduced with the addition of Si3N4 reinforcement.
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Inagaki, Hirosuke. "Texture Development in 6000 Series Al-Mg-Si Alloys for Car Body Panels." Materials Science Forum 558-559 (October 2007): 77–84. http://dx.doi.org/10.4028/www.scientific.net/msf.558-559.77.

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Recovery, recrystallization and the formation of recrystallization textures were investigated in three representative Al-Mg-Si alloys used for car body panels. Commercial hot bands of AA6016, AA6111 and AA6061 Al-Mg-Si alloys finished at low temperatures were cold rolled to a rolling reduction of 95 % in thickness and isothermally annealed at temperatures between 250 and 500 °C. In these alloys, precipitation was completed for the most part during low temperature hot rolling, and the sizes and the amount of fine precipitates formed during this low temperature hot rolling strongly affected recrystallization and the development of recrystallization textures. As a result, in the specimens annealed at 300 °C, quite different recrystallization behavior and recrystallization textures were observed. In the AA6061 alloy, in which, among three alloys, the maximum amount of Mg2Si should be precipitated, recrystallization was significantly suppressed. This resulted in the formation of strong {110} <111> and {100} <013> recrystallization textures. Also in the AA6111 alloy, in which precipitation of a medium amount of Mg2Si was expected, recrystallization was retarded to the same extent. In this alloy, however, recrystallization textures consisted of very strong {100} <001> and rather strong {110} <111> main orientations. In theAA6016 alloy, in which the minimum amount of Mg2Si and a large amount of Si particles should be precipitated, recrystallization occurred very rapidly, forming very weak recrystallization textures. In all alloys, annealing at higher temperatures resulted in the formation of weak textures, since fine precipitates were dissolved during annealing. Thus, the solution treatment, which is a necessary step to induce bake hardening in these alloys, randomizes their recrystallization textures.
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Sun, Yu-Kai, Shih-Ying Chang, Lung-Chuan Tsao, Tung-Han Chuang, Guo-Zhan Zhang, and Chih-Yi Yeh. "Effects of Adding Active Elements to Aluminum-Based Filler Alloys on the Bonding of 6061 Aluminum Alloy and Alumina." Applied Sciences 11, no. 21 (November 6, 2021): 10440. http://dx.doi.org/10.3390/app112110440.

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In this study, AA6061/AA6061 and AA6061/alumina were directly brazed with Al10.8Si10Cu, Al10Si10Cu4Ti and Al10Si10Cu4Ti0.1RE filler alloys at 530 °C for 10 min without the use of flux. The addition of titanium and rare-earth elements into Al10.8Si10Cu alloy effectively improved the bonding shear strengths of AA6061/AA6061 and AA6061/alumina joints. The highest joint shear strengths were 61.1 and 19.2 MPa, respectively. The Al10.8Si10Cu filler alloy without titanium and rare-earth elements could not wet on the alumina and caused failure of the AA6061/alumina joint. The shear strengths of the AA6061/AA6061 and AA6061/alumina joints both strongly depended on the active element addition. Due to the high chemical activity of the rare-earth elements, they formed AlLa between the Al10Si10Cu4Ti0.1RE filler alloy and alumina. The addition of rare-earth elements into Al10Si10Cu4Ti filler alloy resulted in significant enhancement of the average bond strength of AA6061/alumina joints, from 8.0 to 14.8 MPa.
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Arsyad, H., L. H. Arma, and Januari. "The Roughness Characteristic of AA6061-F, AA6061-O and AA6061-T6 after Machining Process." IOP Conference Series: Materials Science and Engineering 875 (July 23, 2020): 012057. http://dx.doi.org/10.1088/1757-899x/875/1/012057.

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S, Senthil Kumaran, Jayakumar Kaliappan, Kathiravan Srinivasan, Yuh-Chung Hu, Sanjeevikumar Padmanaban, and Srinivasan N. "Realizing a Novel Friction Stir Processing-Enabled FWTPET Process for Strength Enhancement Using Firefly and PSO Methods." Materials 13, no. 3 (February 5, 2020): 728. http://dx.doi.org/10.3390/ma13030728.

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The friction welding of tube to tube plate using an external tool (FWTPET) is widely deployed in several industrial applications, such as aerospace, automotive, and power plants. Moreover, for achieving a better tensile strength and hardness in the weld zone, the friction stir processing (FSP) technique was incorporated into the FWTPET process for joining aluminum alloys (AA6063 tube, AA6061 tube plate). Furthermore, it has to be noted that FWTPET was applied for joining the AA6063 tube to the AA6061 tube plate, and FSP was deployed for reinforcing the weld zone with carbon nanotube (CNT) and silicon nitride (Si3N4) particles, thereby attaining the desirable mechanical properties. Subsequently, the Taguchi L25 orthogonal array was used for identifying the most influential input and output FWTPET + FSP process parameters. Furthermore, particle swarm optimization (PSO) and the firefly algorithm (FFA) were deployed for determining the optimized input and output FWTPET + FSP process parameters. The input process parameters include CNT, Si3N4, rotational tool speed, and depth. Furthermore, the tensile strength of the welded joint was considered as the output process parameter. The process parameters predicted by PSO and FFA were compared with the experimental values. It was witnessed that deviation between the predicted and experimental values was minimal. Moreover, it was found that FFA provided a superior tensile strength prediction than PSO.
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Prasad Reddy, A., P. Vamsi Krishna, and RN Rao. "Two-body abrasive wear behaviour of AA6061-2SiC-2Gr hybrid nanocomposite fabricated through ultrasonically assisted stir casting." Journal of Composite Materials 53, no. 15 (January 6, 2019): 2165–80. http://dx.doi.org/10.1177/0021998318822723.

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Two-body abrasion wear rate of AA6061 aluminium alloy, AA6061-2SiC nanocomposite, and AA6061-2SiC-2Gr hybrid nanocomposites were studied using a pin on disc machine at various applied normal loads 5-20 N and 50-150 µm abrasive grit size by maintaining a constant sliding distance of 120 m. Morphology of fabricated materials, worn surfaces of tested specimens, and abrasive grit papers were analysed under a scanning electron microscope. The wear rate of the AA6061-2SiC-2Gr hybrid nanocomposite was found to be less than that of AA6061 alloy and AA6061-2SiC nanocomposite. The wear rate decreased by 19% for 50 µm, 28.2% for 100 µm, and 22.5% for 150 µm at an applied normal load of 20 N and 120 m sliding distance for Al 6061-2SiC-2Gr hybrid nanocomposite compared to base alloy.
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Suthar, Harish, Anirban Bhattacharya, and Surajit Kumar Paul. "Local deformation response and failure behavior of AA6061-AA6061 and AA6061-AA7075 friction stir welds." CIRP Journal of Manufacturing Science and Technology 30 (August 2020): 12–24. http://dx.doi.org/10.1016/j.cirpj.2020.03.006.

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Bhovi, Prabhakar M., Akash R. Naik, Dattatraya Adarsh, C. G. Ranjitkumar, and K. Venkateswarlu. "Simulation Studies and Evolution of Mechanical Properties of AA6061 Subjected to RCS." Advanced Materials Research 1148 (June 2018): 142–51. http://dx.doi.org/10.4028/www.scientific.net/amr.1148.142.

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AA6061 alloy was selected as starting material, as this alloy play vital role in aerospace, automotive and naval applications. To enhance mechanical properties and study the structural correlation of AA6061 using one of the promising SPD (Severe Plastic Deformation) technique. In RCS (Repetitive Corrugation and Straightening), repetitive bending and shearing stresses act alternatively on the specimen. The die models and work piece were designed using Creo parametric 2.0 and imported to AFDEX-2014 (Adviser metal Forming Design Expert) for simulation studies. AA6061 was subjected to four passes (8 stages) of RCS. Effective strain observed in AA6061 alloy was 2.389 and strain rate increased during corrugation and less during straightening stages. The theoretical effective strain was 2.65.The experimental effective strain was validated and found to be nearly approximately 92% of the theoretical result. Further, mechanical properties like tensile strength and microhardness increased to 1.5 to 2 times in AA6061 alloy after eight passes of RCS. Keywords: AA6061, RCS, SPD, Microhardness, Tensile strength
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Newell, Ryan, Abhishek Mehta, Young Joo Park, Dennis D. Keiser Jr., and Yong Ho Sohn. "Interdiffusion, Reactions, and Phase Transformations Observed during Fabrication of Low Enriched Uranium Monolithic Fuel System for Research and Test Reactors." Defect and Diffusion Forum 383 (February 2018): 10–16. http://dx.doi.org/10.4028/www.scientific.net/ddf.383.10.

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Monolithic fuel plates have been developed utilizing low enriched U alloyed with 10 wt.% Mo to replace highly enriched fuels in research and test reactors, in accordance with the goals of the Materials Management and Minimization Reactor Conversion Program. The fuel plates consist of U10Mo fuel, Zr diffusion barrier, and AA6061 cladding. They are fabricated by co-rolling the U10Mo and Zr, which are then encapsulated via hot isostatic pressing of the entire U10Mo/Zr/AA6061 assembly. During fabrication, the metal constituents of the fuel plates undergo phase transformations as well as interdiffusion and reactions at interfaces. The areas of interest are the U10Mo fuel, U10Mo/Zr interface, U10Mo/AA6061 interface, Zr/AA6061 interface, and AA6061-AA6061 bond line. Knowledge of the transformations and growth in the plates is necessary to optimize fabrication parameters and predict behavior as they relate to irradiation performance. Numerous studies have been conducted to analyze these reactions in monolithic fuel plates, and a summary of their observations is provided in this paper.
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Dissertations / Theses on the topic "AA6061"

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Fu, Mian. "Interdiffusion Study of Mg-AA6061 System." Master's thesis, University of Central Florida, 2013. http://digital.library.ucf.edu/cdm/ref/collection/ETD/id/6274.

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Magnesium (Mg) is a light-weight metal that has extraordinary physical and chemical properties for many potential applications in automobile, military, and electronics. Aluminum alloys, because of its light-weight, high strength and corrosion resistance have a wide range of commercial applications. Given these two, sometime competing, alloy systems, there are now many applications where the metallurgical compatibility of Mg- and Al-alloys are required for engineering applications. One such case is the development of diffusion barrier for U-Mo metallic fuel in Al-alloy cladding, where Mg, with its complete immiscibility with U and Mo is being considered as the diffusion barrier. While negligible diffusional interaction between Mg and U-Mo alloys have been reported, diffusional interaction between the Mg and Al-alloy cladding has not been investigated. In this study, solid-to-solid diffusion couples were assembled using discs of pure Mg (99.999 %) and AA6061 Al-alloy. After preparation, Mg was diffusion bonded to AA6061 in sealed quartz capsule at 300°, 350°, and 400°C for 720, 360, and 240 hours, respectively. Scanning electron microscopy was used to inspect the interdiffusion zone, while phase identification was performed using X-ray energy dispersive spectroscopy. One specific phase that exists in the binary Mg-Al system, labeled "?" was observed and characterized by transmission electron microscopy. From the preceding data, the growth rates as well as interdiffusion coefficients of the intermetallic phases were extracted and compared to previous investigations using pure Mg and Al.
M.S.M.S.E.
Masters
Materials Science Engineering
Engineering and Computer Science
Materials Science and Engineering
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Lemnifi, Ahmed. "Influence of excimer laser surface melting on microstructure and corrosion behaviour of AA6061-T6 alloy and SiCp/AA6061-T6 composite." Thesis, University of Manchester, 2017. https://www.research.manchester.ac.uk/portal/en/theses/influence-of-excimer-laser-surface-melting-on-microstructure-and-corrosion-behaviour-of-aa6061t6-alloy-and-sicpaa6061t6-composite(5b945607-0479-411b-bb08-61e3c96a606e).html.

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This thesis presents an investigation of excimer laser surface melting (LSM) on AA6061-T6 alloy and SiCp/AA6061-T6 composite in terms of microstructure and corrosion behaviour. Hardness and wear resistance of the melted layer for both materials were also evaluated and compared with the untreated specimen to understand if the improvement of the corrosion resistance could be achieved without sacrificing the wear resistance. The intermetallic particles within the aluminium matrix are believed to initiate of both galvanic and pitting corrosion for both materials. To effectively dissolve these intermetallic particles, laser fluence from 1 to 8.5 J/cm2 with a number of pulses from 10, 25 to 50 were selected to achieve an optimisation of the LSM condition. It was found that the increase of laser fluence increased the melt depth, but also promoted the formation of defects such as micro-cracks and pores. For AA6061-T6 alloy, under the best laser condition (3 J/cm2 with 50 pulses), the amount of large intermetallic particles (2-10 µm), such as AlFeSi, AlFeMnSi and Mg2Si, were significantly reduced resulting in the formation of a relatively homogeneous and defect-free melt layer with only some small randomly distributed of intermetallic precipitates. For the SiCp/AA6061-T6 composite, under the best laser condition (6 J/cm2 with 25 pulses), decomposition of SiC particles was achieved as well as the dissolution of large AlMgSiCr and AlFeSi intermetallic particles in the melt layer. The melt layer had a relatively complex microstructure consisting of three different regions. MgO was found at the bottom of the melted layer which was discontinuous along the interface between the melted region and bulk material or in some places, at the bottom of the melted layer. The corrosion behaviour of both materials before and after LSM was evaluated using electrochemical measurements and immersion test in deaerated 0.6 M NaCl solution. After LSM the AA6061-T6 with and without SiC showed a better corrosion resistance compared with untreated alloys. The pitting potential of the LSM for both materials was shifted to a more positive value with a significant reduction of the passivation current density. In addition, an intergranular corrosion test based on the standard ASTM G110-92 showed that the LSM had significantly improved the corrosion resistance of both materials due to dissolution of intermetallic particles as well as the removal of the SiC particles in the composite material within the melted regions. In addition, the wear resistance of as-received SiCp/AA6061-T6 composites was found to be much higher than that of the LSM specimen. This is attributed to the decomposition of the majority of the SiCp in the melted region since the contribution to the hardness from the SiC particle in the untreated specimen is much greater that the Si-rich region in the melt layer after LSM.
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Aphane, Abraham Kalaudia. "Effect of thermomechanical processing on the surface roughening of AA6061." Master's thesis, University of Cape Town, 2001. http://hdl.handle.net/11427/5547.

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Surface roughening is an undesirable feature in materials. This work investigates the cause of surface roughening in four plates of AA6061 with different thicknesses (Le. 6 mm, 9 mm and two 12 mm). Production of these plates requires thermomechanical processing of the cast slab via a two stage process, namely the initial rolling stage on a hot roughing mill (HRM) and final rolling on the hot finishing mill (HFM). After rolling. the plates are levelled by a tensile stretching process and it is during this process that surface roughening of the plates can arise. Three of these plates exhibited severe roughening and the other 12 mm thick plate exhibited mild surface roughening during the stretch levelling process. Investigations looked closely at how the cause of surface roughening is related to the thermomechanical processing. The four products studied exhibited different degrees of surface roughening during uniaxial tensile deformation. Detailed investigation of the microstructure of these four products was carried out. It was found that the plates that exhibited severe roughening had large flat and elongated grains at the surface. It is the rotation of these surface grains during tensile deformation that was thought to be inducing the roughness in the material. The microstructure evolution was explained relative to the thermomechanical history of the plates. Plane strain compression (PSC) tests were used to simulate the thermomechanical processing cycles on the HFM. Large strain rates used in the industry were compensated with an adjustment in temperature so that an equivalent Zener-Holloman parameter (Z) could be achieved. The microstructure of the PSC specimen was characterised using the electron back scattered technique. It was found that the grain size increases with a decrease in the value of Z.
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Hapazari, Innocent. "Effects of thermomechanical processing on microstructure and hardness profiles in AA6061 plates." Master's thesis, University of Cape Town, 2003. http://hdl.handle.net/11427/10615.

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Effects of rolling variables - strain (?), strain rate (?) and temperature (T) - on grain structure and hardness evolution in AA6061 plates were investigated by simulating the rolling process using plane strain compression (PSG). Particular emphasis was exerted on understanding the impact of the variables on the overall mean grain size and hardness, as well as how they influence the grain size and hardness profiles through the thickness of the rolled plates. Prior to PSG investigations, the grain size and hardness profiles of the supplied material (transfer and finished plates) were determined using a Reichert MeF3A optical microscope and Vickers hardness tester. No significant grain size variations were observed through the thickness of transfer plate. On the contrary, finished plates exhibited grain size gradients, with grain size progressively decreasing from the surface to the centre of the plate thickness.
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Gilbert, François. "Influence des conditions d'anodisation dure de l'aluminium (AA6061-T6) sur la couche d'oxyde formée." Thesis, Université Laval, 2011. http://www.theses.ulaval.ca/2011/28580/28580.pdf.

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Silva, Ana Márcia Barbosa da. "Estudo do comportamento em fadiga de alto ciclo das ligas de alumínio AA6005 T6, AA6063 T6 e AA6351 T6." Universidade de São Paulo, 2012. http://www.teses.usp.br/teses/disponiveis/97/97134/tde-07102013-092520/.

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A indústria automotiva tem mostrado um crescente interesse pelas ligas de alumínio, em especial as ligas de alumínio da série 6xxx. Esta classe é amplamente empregada nas áreas de construção e de transporte, devido a sua boa resistência mecânica e excelente resistência à corrosão. No setor automobilístico sempre houve a necessidade de aprimoramento dos estudos do comportamento em fadiga, pois os componentes estruturais são submetidos a carregamentos vibratórios, esforços e tensões cíclicas e, como consequência, podem trincar e finalmente fraturar. A presença de um entalhe geralmente diminui a vida em fadiga, criando regiões de altas tensões triaxiais localizadas que restringem a deformação plástica, fragilizando o material. A resposta mecânica depende das solicitações, microestrutura, componentes da liga e propriedades do material. Neste trabalho foi realizado o estudo do comportamento em fadiga de alto ciclo e da sensibilidade ao entalhe de três ligas de alumínio da série 6xxx destinadas à fabricação de componentes de carroçarias para caminhões e ônibus: AA 6005, AA 6063 e AA 6351, todas na condição T6. As curvas S/N foram obtidas por meio de ensaios de fadiga em flexão rotativa (R = -1). Ensaios com peças entalhadas (Kt ? 3,0) permitiram determinar e comparar o fator de concentração de tensão em fadiga e a sensibilidade ao entalhe das ligas estudadas. Também foi estudada a influência da microestrutura e das partículas intermetálicas sobre as propriedades de fadiga. As superfícies das peças fraturadas foram observadas ao MEV e verificou-se que a maioria dos sítios de nucleação de trincas por fadiga ocorreram próximos a partículas de segunda fase que atuam como concentradores de tensão.
The automotive industry has shown a growing interest in aluminum alloys, particularly the AA 6xxx series. This class of alloys is widely used in construction and transportation because of their good mechanical strength, easy fabrication and excellent corrosion resistance. In the automotive sector there was always a need for improved studies of the fatigue behavior, because the structural components are subjected to vibratory loads and cyclic stresses and, as a consequence, may eventually crack and fracture. The presence of a notch generally decreases the fatigue life, creating regions of high triaxial stresses which restrain plastic deformation, weakening the material. The response depends on the mechanical solicitations, microstructure, the alloy components and the material properties. In this work it was conducted a study of the high cycle fatigue behavior and the notch sensitivity of three aluminum alloys used in components of truck and bus bodies: AA 6005, AA 6063 and AA 6351, all provided in T6 condition. The S/N curves were obtained by tests in rotating bending fatigue (R = -1). Tests with notched samples (Kt?3.0) allowed to determine and compare the fatigue concentration factor and the notch sensitivity of the studied alloys. It was also studied the influence of microstructure and the intermetallic particles on the fatigue properties. The surfaces of the fractured samples were observed via SEM and showed that most of the nucleation sites of fatigue cracking occurred near the second phase particles, which act as stress concentrators.
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FERNANDES, Camila Albuquerque. "Estudo do desempenho mecânico e microestrutural de uniões da liga de alumínio, AA6061-T6, por solda a ponto por fricção (FSpW)." Universidade Federal de Pernambuco, 2016. https://repositorio.ufpe.br/handle/123456789/18599.

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Submitted by Rafael Santana (rafael.silvasantana@ufpe.br) on 2017-04-19T18:29:57Z No. of bitstreams: 2 license_rdf: 1232 bytes, checksum: 66e71c371cc565284e70f40736c94386 (MD5) Dissertação CAMILA ALBUQUERQUE FERNANDES 2016.pdf: 2707069 bytes, checksum: 1af5a8e892dd9aa2682c79f98c6cde09 (MD5)
Made available in DSpace on 2017-04-19T18:29:57Z (GMT). No. of bitstreams: 2 license_rdf: 1232 bytes, checksum: 66e71c371cc565284e70f40736c94386 (MD5) Dissertação CAMILA ALBUQUERQUE FERNANDES 2016.pdf: 2707069 bytes, checksum: 1af5a8e892dd9aa2682c79f98c6cde09 (MD5) Previous issue date: 2016-07-29
Solda a Ponto por Fricção (Friction Spot Welding – FSpW) é um processo relativamente novo de soldagem desenvolvido e patenteado pelo GKSS na Alemanha, que visa complementar e/ou substituir tecnologias de uniões de soldagem convencionais. Essa nova tecnologia de soldagem se dá pela união no estado sólido, onde duas ou mais chapas são unidas através da transferência de energia térmica e mecânica que é gerada pela rotação da ferramenta. O presente trabalho visou avaliar a aplicabilidade da união da liga de alumínio 6061-T6 pela técnica de Solda a Ponto por Fricção. Essas soldas foram produzidas em configuração de sobreposição utilizando condições de soldagens variadas, por meio de diferentes combinações de velocidade de rotação, profundidade de penetração e velocidade de penetração; os quais foram estabelecidos através de uma análise estatística, utilizando como ferramenta o Box-Behnken. A integridade da junta soldada foi avaliada através dos efeitos dos parâmetros de processo, na geometria e na microestrutura da junta, e também no desempenho mecânico. Realizou-se também a otimização do processo de soldagem e um estudo sobre o comportamento de fratura das soldas submetidas a um esforço de cisalhamento. Os resultados mostraram que a melhor combinação de parâmetros foi encontrada na condição de soldagem: 130 rpm, 4,0 mm/s e 1,4 mm, com um valor médio de resistência ao cisalhamento de 6243,29 N, com boa reprodutibilidade. O botão da solda é constituído por três elementos geométricos que se mostraram inerentes ao processo: cunha, união principal e união secundária. Estes elementos mostraram possuir forte influência sobre o desempenho mecânico.
Friction Spot Welding (FSpW) is a relatively new welding process patented by GKSS in Germany. This new welding technology is given by the joining in a solid state, in which two or more plates are joined by thermal and mechanical energy transfer that is generated by the rotation of the welding tool. The aim of this work is to study the integrity of the welds of AA6061-T6, by the FSpW process. These welds were produced in an overlapping configuration using different welding conditions, through different combinations of rotational speed, depth of penetration and penetration speed, which were set through a statistical approach using the Box-Behnken. The integrity of the welded joint was evaluated by the effects of process parameters on geometry and microstructure of the joint, and also in the mechanical performance. It was also performed the optimization of the welding process and a brief study on the fracture behavior of the welds subjected to a shear stress. The results showed that the best combination of parameters was found in the welding condition: 130 rpm 4.0 mm / s and 1.4 mm with an average value of the shear strength of 6243.29 N, with good reproducibility. The metallurgical investigation revealed three geometric elements that are inherent to the process: primary union and secondary union and hook. These elements were shown to have strong influence on the mechanical performance.
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Nascimento, Denise Ferreira Laurito. "Estudo do comportamento em fadiga de baixo ciclo e fadiga sob cargas multiaxiais das ligas de alumínio AA6005, AA6063 e AA6351." Universidade de São Paulo, 2015. http://www.teses.usp.br/teses/disponiveis/97/97134/tde-21052015-153422/.

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O uso das ligas de alumínio em aplicações estruturais tem crescido consideravelmente nas últimas décadas. Nos transportes, a baixa massa específica do alumínio resulta em uma alta razão resistência/ peso, favorecendo a fabricação de aviões, trens e automóveis. Com a crescente preocupação em reduzir a emissão de gases poluentes, vem tornando-se promissora a alternativa de reduzir o peso dos veículos substituindo peças convencionalmente produzidas com outros materiais por peças de alumínio. As ligas tratáveis termicamente da série 6xxx são frequentemente escolhidas para estas aplicações. Assim, para que o emprego dessas ligas seja otimizado, é importante um estudo mais detalhado de suas propriedades mecânicas, principalmente sob solicitações cíclicas. Neste trabalho foram estudadas ligas de Al-Si-Mg que são amplamente utilizadas nas indústrias automotivas, em especial na fabricação de componentes de carroçarias para caminhões e ônibus. Foi realizado o estudo do comportamento em fadiga de baixo ciclo e fadiga multiaxial das ligas AA6005 T6, AA6063 T6 e AA6351 T6, fornecidas pela CBA (Companhia Brasileira de Alumínio) visando caracterizar e comparar essas ligas em sua microestrutura, propriedades de tração e fadiga. As propriedades básicas de fadiga foram determinadas por meio do método ε-N (fadiga de baixo ciclo) e os ensaios foram realizados com controle de deformação total, onda triangular e taxa de deformação 0,005 seg-1. As análises dos laços de histerese elasto-plástica permitiram inferir sobre aspectos microestruturais relacionados às propriedades mecânicas das ligas estudadas. O comportamento em fadiga multiaxial foi avaliado por meio de carregamentos combinados axial-torcional em fase e fora de fase. Para ajustar os dados experimentais obtidos, foram testados alguns dos modelos encontrados na literatura. Os cálculos baseados no modelo de plano crítico, proposto por Fatemi e Socie, apresentaram resultados satisfatórios. Também foram realizadas análises microestruturais e fractográficas para as três ligas. As superfícies de fratura dos ensaios de fadiga multiaxial mostraram resultados diferentes de acordo com o carregamento adotado. A avaliação comparativa das três ligas estudadas fornece subsídios para fundamentar a seleção de materiais para a fabricação de componentes estruturais para o setor automotivo.
The use of aluminum alloys in structural applications has grown considerably in recent decades. In transportation, the low density of aluminum results in a high strength-to weight ratio, proving attractive for production of aircrafts, trains and automobiles. With a growing concern for the reduction of pollutant gas emissions, aluminum alloys are becoming a promising alternative to diminish vehicle weight through the replacement of conventionally produced parts made from other heavier materials for aluminum parts. The heat treatable alloys from the 6xxx series are often chosen for these applications. Therefore, to optimize the employment of these alloys, a detailed study of their mechanical properties, primary under cyclic solicitations is necessary For the present study Al-Mg-Si alloys were chosen, which are widely used in automotive industries, particularly in the manufacturing of components for trucks and bus bodies. The low-cycle fatigue behavior and multiaxial fatigue of the three following aluminum alloys: AA6005 T6, AA6063 T6 and AA6351 T6, provided by CBA (Brazilian Aluminum Company), were assessed, with the aim of characterizing and comparing these alloys in their microstructure, tensile properties and fatigue. The basic properties of fatigue were studied by ε-N method (low cycle fatigue) and the experiments were performed with total strain control, triangular waveform and with a constant deformation rate of 5.0x10-3 s-1. The analyses of hysteresis loops elasto-plastic provided insight about microstructural aspects, related to mechanical properties of the studied alloys. Multiaxial fatigue behavior was assessed in combined axial-torsion loading in phase and out of phase. To adjust the experimental data, some models found in the literature were tested. Calculations based on critical plane model, proposed by Fatemi Socie, presented satisfactory results. Furthermore, microstructure analyses and fractography were performed for these three alloys. The fracture surface of multiaxial fatigue assays demonstrated different results according to the adopted loading. Comparative evaluation of the three studied alloys provides support for the selection of materials for manufacturing structural components of the automotive sector.
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Bravo, Salazar Jaime Alejandro. "Estudo do processo de fabricação de compósitos AA6061 + TiCN por sinterização com fase líquida e caracterização do produto." [s.n.], 2007. http://repositorio.unicamp.br/jspui/handle/REPOSIP/263635.

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Orientadores: Maria Helena Robert, Elisa Maria Ruiz Navas
Tese (doutorado) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecânica
Made available in DSpace on 2018-08-19T00:27:43Z (GMT). No. of bitstreams: 1 BravoSalazar_JaimeAlejandro_D.pdf: 9695376 bytes, checksum: d35ebfbcaf1dac8c6665392b7d784d23 (MD5) Previous issue date: 2007
Resumo: Este trabalho estuda o processo de fabricação de compósitos de matriz de alumínio AA6061 reforçado com TiCN por metalurgia do pó, envolvendo as etapas de mistura de pós, compactação uniaxial e sinterização com fase líquida. Para efeitos de comparação foram produzidos e caracterizados compactados da liga AA6061 sem adição de reforços. Foram investigados os parâmetros de processo: teores de reforço (5% e 10% massa), teor de aditivos Pb e Sn (0,1, 0,15, 0,2 e 0,4% massa), pressão de compactação (400, 600 e 800 MPa), tempos (15, 30, 45 e 60 min) e temperatura de sinterização (590, 600, 610 e 620 ºC). Em cada etapa do processo foram caracterizados os produtos (mistura de pós e compactados); o produto final obtido, após sinterização, foi caracterizado com relação à sua microestrutura, propriedades físicas (densificação e variação dimensional) e mecânicas (resistência à flexão e dureza). Os resultados obtidos mostraram uma grande eficiência do processo na obtenção de compósitos; a adição do teor de reforço de 5%TiCN foi eficiente na promoção de rupturas das camadas de óxidos do pó da liga de alumínio compactado à pressão de 400 MPa, auxiliando a sinterização por difusão da fase líquida formada a partir da fusão de Al+Mg2Si, melhorando a densificação e diminuindo a variação dimensional dos produtos sinterizados. Do ponto de vista metalúrgico, os materiais compósitos obtidos apresentaram microestruturas homogêneas, com uma boa distribuição dos reforços na matriz e relativa diminuição de poros. A adição de Pb e Sn promovem maior eficiência de ativação de mecanismos de sinterização; para compactados produzidos à pressão de 800 MPa, a adição de 0,1% desses elementos já apresentou significativa influência na sinterização. Com relação às propriedades mecânicas e físicas observou-se que a adição de TiCN aumentou quase no dobro de seus valores obtidos quando são comparados com a liga AA6061
Abstract: This work investigates the process of production of composites of the alloy AA6061 reinforced with TiCN particles, by powder metallurgy involving the steps: conventional mixture of powders, compaction by uniaxial cold pressing and sintering with formation of a liquid phase. For comparative analysis it was also produced sintered AA6061 without addition of reinforcements. The following processing parameters were studied: reinforcing particles content (5 and 10 wt%); content of trace elements Pb and Sn (0.1, 0.15, 0.2 0.4 wt%); compaction pressure (from 400, 600 and 800 MPa); time and temperature of sintering (15, 30, 45, 60 min and 590, 600, 610, 620 oC). In each step products were characterized (powder mixture and green compacts); the final sintered product was characterized related to microstructure, physical (densification and dimensional changes) and mechanical (hardness and bending strength) properties. Obtained results showed high efficiency of the applied process to produce reliable composite products; the addition of 5 wt% TiCN was efficient to promote fracture of the oxide layer in the aluminum particles surface during pressing. At sintering temperatures liquid phase is formed by Al+Mg2Si melting and is distributed among particles through the fractures of the oxide layer, improving the material densification and its mechanical properties. Microstructures obtained showed homogeneous distribution of TiCN and reduced porosity, whereas AA6061 alloy microstructure showed higher porosity. Addition of Pb and Sn promoted higher efficiency of sintering mechanisms in compacts submitted to high pressures, leading to enhanced physical and mechanical properties in those materials.
Doutorado
Materiais e Processos de Fabricação
Doutor em Engenharia Mecânica
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Campana, Rodrigo Camargo. "Parâmetros de processo, microestrutura e textura das ligas de aluminio AA6063 e AA6082 extrudadas." Universidade de São Paulo, 2007. http://www.teses.usp.br/teses/disponiveis/3/3133/tde-01042008-175024/.

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O desenvolvimento de ligas de alumínio de propriedades mecânicas intermediárias possibilitou a extrusão de alumínio a participar de grandes mercados como a construção civil, transportes, automobilística, estruturas, entre outras. O conhecimento do processo de extrusão propicia o aumento de produtividade com melhor desempenho e precisão dimensional do produto acabado. Neste trabalho, procurou-se analisar as características de conformação de perfis sólidos das ligas de alumínio AA6063 e AA6082 com razão de extrusão (RE) variando de 2,0 a 27,8 e tubular com RE de 8,7. A partir da extrusão realizada em uma prensa industrial de 3300 toneladas de força, compararam-se os resultados obtidos da tensão média de escoamento (\"sigma\") em função da temperatura de deformação e do parâmetro de Zener-Hollomon (Z) e este último em função do tamanho de subgrão observado no produto extrudado. Foram obtidos, em condições industriais, para estas ligas os valores da constante \"alpha\" que relaciona a RE com a pressão de fim de extrusão. Foram realizadas observações metalográficas e constatadas regiões de recristalização e de não recristalização diferentes para as ligas estudadas, bem como as relações do parâmetro Z e o tamanho do subgrão do produto sólido e tubular na liga AA6082. Em termos de textura foi possível obter as figuras de pólo e do tipo FDO no perfil extrudado ilustrando a presença de fibras do tipo \"beta\" (característica de produto conformado) e cubo (característica de produto recristalizado/recuperado). Os resultados confirmam valores próximos àqueles encontrados na literatura.
The development of medium strength aluminum alloys enabled aluminum extrusions to take part of the large world markets, associated with the building, transport and automotive industries, amongst several applications. The knowledge of the extrusion process details enables the productivity increase with better performance and higher dimensional accuracy of the finished extrusion product. In the present study the deformation characteristics of solid extrusion profiles in the AA6063 and AA6082 alloys with extrusion ratios (ER) in the range of 2.0 to 27.8 and for solid and tubular of 8.7 sections were studied. Extrusions were carried out in an industrial 3300 ton press. Results are compared in terms of average flow stress as a function of extrusion temperature and of the Zener-Hollomon (Z) parameter; the latter one also as a function of the observed subgrain size in the final product. Under industrial conditions, for the studies alloys, the values of the \"alpha\"-constant (which relates the end pressure to the extrusion ratio), has been evaluated. Metallographic observations have been conducted to study the recrystallised and unrecrystallised regions in the studied alloys, as well as the relationship between the Z parameter and the subgrain size of the end extrusion, both for the solid and tubular products, mainly for the AA6082 alloy. In terms of texture components it has been observed that the pole figures and the ODF´s of the extruded product presented the \"beta\" (characteristic of rolled/worked products) and cube (characteristic of recrystallised/recovered products). The results obtained confirmed those reported in the literature.
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Books on the topic "AA6061"

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SURI, Gurvir. Optimization of Process Parameters of Friction Stir Welding of Aa6061-T6 and Aa6082-t6. Independently Published, 2018.

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Effect of Welding Processes of Mechanical and Metallurgical Properties of AA6061. Karur, India: ASDF International, 2017.

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Book chapters on the topic "AA6061"

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Pogatscher, Stefan, Helmut Antrekowitsch, Thomas Ebner, and Peter J. Uggowitzer. "The Role of Co-Clusters in the Artificial Aging of AA6061 and AA6060." In Light Metals 2012, 415–20. Cham: Springer International Publishing, 2012. http://dx.doi.org/10.1007/978-3-319-48179-1_70.

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Pogatscher, Stefan, Helmut Antrekowitsch, Thomas Ebner, and Peter J. Uggowitzer. "The Role of Co-Clusters in the Artificial Aging of AA6061 and AA6060." In Light Metals 2012, 413–20. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118359259.ch70.

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Tiwari, Nilesh, and Megha Nagrale. "Analysis of Aluminum AA6061 in Electromagnetic Forming." In Lecture Notes on Multidisciplinary Industrial Engineering, 497–509. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-4619-8_36.

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Krishna, P. Vamsi, and A. Prasad Reddy. "Mechanical and Tribological Properties of AA6061-2SiCp-xGr." In Handbook of Polymer and Ceramic Nanotechnology, 1–35. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-10614-0_66-1.

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Krishna, P. Vamsi, and A. Prasad Reddy. "Mechanical and Tribological Properties of AA6061-2SiCp-xGr." In Handbook of Polymer and Ceramic Nanotechnology, 487–521. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-40513-7_66.

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Moreira, P. M. G. P., V. Richter-Trummer, and P. M. S. T. de Castro. "Fatigue Behaviour of FS, LB and MIG Welds of AA6061-T6 and AA6082-T6." In Multiscale Fatigue Crack Initiation and Propagation of Engineering Materials: Structural Integrity and Microstructural Worthiness, 85–111. Dordrecht: Springer Netherlands, 2008. http://dx.doi.org/10.1007/978-1-4020-8520-8_5.

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Das, Nandan Kanan, Arun Kumar Kadian, Avinish Tiwari, Pardeep Pankaj, and Pankaj Biswas. "Transient Thermal Analysis on Friction Stir Welding of AA6061." In Lecture Notes on Multidisciplinary Industrial Engineering, 67–82. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6287-3_5.

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Nashrudin, MN, and AB Abdullah. "Investigation of Twist Springback Pattern of the AA6061 Strip." In Springback Assessment and Compensation of Tailor Welded Blanks, 141–58. Boca Raton: CRC Press, 2022. http://dx.doi.org/10.1201/9781003164241-6.

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de Haas, Marc, S. M. van Scherpenzeel, and Jeff Th M. de Hosson. "Grain Boundary Segregation and Precipitation in Aluminium Alloy AA6061." In Materials Science Forum, 467–72. Stafa: Trans Tech Publications Ltd., 2006. http://dx.doi.org/10.4028/0-87849-408-1.467.

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Maheshwaran, K. J., and R. Padmanaban. "Study of Friction Stir Processing of AA6061 Using CFD." In Lecture Notes in Mechanical Engineering, 169–81. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-3895-5_13.

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Conference papers on the topic "AA6061"

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Mayer, Robert R., Brian Peterson, Raj Mishra, and Anil Sachdev. "The Effect of Tempering (Artificial Aging) on the Crashworthiness Performance of Mass-Efficient Extruded Aluminum Structures." In ASME 2003 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/detc2003/dac-48754.

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The effect of tempering (artificial aging) on the axial crush strength of four cell extruded rectangular aluminum alloy (AA) 6061 and 6063 tubes is developed in this report. Increasing the aging time from the press quenched condition increases the flow strength of the material and also increases the axial energy absorbed up to a point when the material showed fracture. Good predictions were made between experimental, theoretical, and numerical mean crush loads for various tempers of AA6061 and AA6063, except in the cases where a large amount of fracture was present. A recommended temper time of three hours was obtained for AA6063, with an increase in mean crush load of 60%. A recommended temper time of six hours was obtained for AA6061 with an increase in mean crush load of 40%. These results will be useful in future aluminum automotive body projects, both for their predictive capability, and for the temper recommendations.
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Arsyad, Hairul, Lukmanul Hakim Arma, and Indar Jaya. "Influence of extrusion speed and lubrication on extrusion behavior of AA6061 as-cast, AA6061-O and AA6061-T6." In THE PROCEEDINGS OF THE 4TH EPI INTERNATIONAL CONFERENCE ON SCIENCE AND ENGINEERING (EICSE) 2020. AIP Publishing, 2022. http://dx.doi.org/10.1063/5.0095502.

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Berkeley, D. W., H. E. M. Sallam, and H. Nayeb-Hashemi. "The Effect of pH on the Mechanism of Corrosion and Stress Corrosion, and Degradation of Mechanical Properties of AA6061 and Nextel 440 Fiber Reinforced AA6061 Composite." In ASME 1996 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/imece1996-0497.

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Abstract The breaking load method was used to determine the degradation rate of mechanical properties of wrought T6 aluminum 6061, and Nextel 440 fiber reinforced AA6061 composite, as a function of pH, by measuring their post-exposure residual strength. The materials were exposed to acidic NaCl at two initial pH of 1.5 and 2. Two different exposure techniques were employed; one in which the pH of the solution was kept constant by refreshing the corrosive medium, and a second method in which the solution was not refreshed. The change in pH with exposure time was also investigated to provide a more comprehensive understanding of the role of H+ ions in the corrosion process. At an initial pH of 1.5 the matrix showed a significant strengthening response, after an initial decrease in residual strength with time, if the solution was unrefreshed. However, if the solution was refreshed, the residual strength for both the corrosion and stress corrosion specimens continued to decline at an approximately constant rate. The specimens at an initial pH of 2 show a much more gradual strengthening because of the slower initial reaction rates between the solution and the alloy. The Nextel 440 fiber reinforced AA6061 composite was found to be considerably more susceptible to corrosion than the AA6061 matrix. From the results attained, it was concluded that the pH of the solution played a crucial role in the degradation rate of mechanical properties in the AA6061 matrix, and the Nextel 440 fiber reinforced AA6061 composite.
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Raman Goud, R., and Aryan Rachala. "The Effect of Temperature on Formability of AA6061-T6 Alloy Material Under Stretching Operation." In ASME 2019 Gas Turbine India Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gtindia2019-2710.

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Abstract Forming process is one of the most promising techniques in sheet metal forming process in which flat sheet is converted into desired component. Formability analysis has to be carried out in order to obtain successful forming components. In this paper the effect of temperature on formability of AA6061-T6 alloy material was estimated by conducting stretch forming operations on one mm AA6061-T6 alloy material sheets at different temperatures. The range of specimen sizes wastaken from 110 mm × 20 mm to 110 mm × 110mm of AA6061-T6 alloy material for experimentation. The experiments were conducted on the sheet metal forming setupat temperatures RT (250C), 1000C and 2000C.The obtained results were compared with the finite element analysis. The data extracted by the simulation results was well matched with the experimentation results.
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Udoye, N. E., O. S. I. Fayomi, A. O. Inegbenebor, S. T. A. Okolie, ,. J. O. Dirisu, and T. C. Jen. "Corrosion impact of AA6061/clay composite for industrial application." In TECHNOLOGIES AND MATERIALS FOR RENEWABLE ENERGY, ENVIRONMENT AND SUSTAINABILITY: TMREES21Gr. AIP Publishing, 2022. http://dx.doi.org/10.1063/5.0092584.

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Liang, J., D. Guines, and L. Léotoing. "Thermo-viscoplastic behavior of AA6061 under dynamic biaxial loadings." In PROCEEDINGS OF THE 22ND INTERNATIONAL ESAFORM CONFERENCE ON MATERIAL FORMING: ESAFORM 2019. AIP Publishing, 2019. http://dx.doi.org/10.1063/1.5112752.

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Surya, Indra, Nukman, Irsyadi Yani, Amir Arifin, Kaprawi Sahim, and Saloma. "TGA/DTA analysis for AA6061 with fine coal blend." In TOWARD ADAPTIVE RESEARCH AND TECHNOLOGY DEVELOPMENT FOR FUTURE LIFE. AIP Publishing, 2023. http://dx.doi.org/10.1063/5.0114727.

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Man, H. C., C. T. Kwok, and T. M. Yue. "Laser surface cladding of SiC / Si3N4 on AA6061 aluminum alloy." In ICALEO® ‘97: Proceedings of the Laser Applications in the Medical Devices Industry Conference. Laser Institute of America, 1999. http://dx.doi.org/10.2351/1.5059276.

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Karakoc, Halil, Henifi Cinici, Sener Karabulut, and Ramazan Citak. "Fabrication of AA6061/B4C composites and investigation of ballistic performances." In 2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE, 2017. http://dx.doi.org/10.1109/icmae.2017.8038757.

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Arnold, Bryan, and William Altenhof. "Finite Element Modeling of the Axial Crushing of AA6061 T4 and T6 and AA6063 T5 Structural Square Tubes with Circular Discontinuities." In SAE 2005 World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2005. http://dx.doi.org/10.4271/2005-01-0703.

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Reports on the topic "AA6061"

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Miller, Richard. Manufacturing Systems Demonstration: Bimetallic Friction STIR Joining of AA6061 and High Hardness Steel. Fort Belvoir, VA: Defense Technical Information Center, May 2013. http://dx.doi.org/10.21236/ada589399.

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Miller, Richard. A Preliminary Report on the Strength and Metallography of a Bimetallic Friction Stir Weld Joint Between AA6061 and MIL-DTL-46100E High Hardness Steel Armor. Fort Belvoir, VA: Defense Technical Information Center, November 2012. http://dx.doi.org/10.21236/ada580292.

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