Gotowe bibliografie tematyczne / AL ALLOY 6063-T6

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Gotowa bibliografia na temat „AL ALLOY 6063-T6”

Autor: Grafiati

Data publikacji: 11 września 2023

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Artykuły w czasopismach na temat "AL ALLOY 6063-T6"

Leal, Rui M., i Altino Loureiro. "Microstructure and Mechanical Properties of Friction Stir Welds in Aluminium Alloys 2024-T3, 5083-O and 6063-T6". Materials Science Forum 514-516 (maj 2006): 697–701. http://dx.doi.org/10.4028/www.scientific.net/msf.514-516.697.

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The aim of this research is to study the effect of the welding process on the microstructure and mechanical properties of friction stir welded joints in aluminium alloys 2024- T3, 5083-O and 6063-T6. A small loss of hardness and strength was obtained in welds in alloys 2024-T3 and 5083-O as opposed to welds in alloy 6063-T6, where a substantial softening and a drop of strength were observed. In alloy 6063-T6 a strength efficiency of only 45 to 47% was obtained.

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Xu, Anlian. "Properties of High Speed Friction Stir Welded 6063-T6 Aluminum Alloy". Journal of Physics: Conference Series 1676 (listopad 2020): 012107. http://dx.doi.org/10.1088/1742-6596/1676/1/012107.

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GRINSPAN, Alphonse Sahaya, i Rajappa GNANAMOORTHY. "Fatigue Behavior of Oil Jet Peened Aluminum Alloy, AA 6063-T6". Journal of Solid Mechanics and Materials Engineering 1, nr 7 (2007): 875–85. http://dx.doi.org/10.1299/jmmp.1.875.

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Tomaszewski, Tomasz, i Janusz Sempruch. "Analysis of Size Effect in High-Cycle Fatigue for EN AW-6063". Solid State Phenomena 224 (listopad 2014): 75–80. http://dx.doi.org/10.4028/www.scientific.net/ssp.224.75.

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Any changes in specimen size in relation to the reference dimensions involve scaling inaccuracies resulting in the variances in strength testing (monotonic, fatigue) results. It is referred to as a size effect. The size effect is described using a cross-sectional coefficient determined for various specimen sizes and test types. The analysed material is aluminium alloy EN AW-6063 T6 with a cross-sectional area of 28, 7 and 3.5 mm2.

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Hongyang, JING, FENG Qi, XU Lianyong, ZHAO Lei i HAN Yongdian. "Microstructure and Mechanical Properties of Friction Stir Welds on 6063-T6 Aluminum Alloy". Journal of Mechanical Engineering 56, nr 8 (2020): 13. http://dx.doi.org/10.3901/jme.2020.08.013.

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D.S., Balaji. "Effect of garnet abrasive in water jet peening on AL 6063-T6 alloy". International Journal of Emerging Trends in Engineering Research 8, nr 8 (25.08.2020): 4346–49. http://dx.doi.org/10.30534/ijeter/2020/48882020.

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Moreira, P. M. G. P., F. M. F. de Oliveira i P. M. S. T. de Castro. "Fatigue behaviour of notched specimens of friction stir welded aluminium alloy 6063-T6". Journal of Materials Processing Technology 207, nr 1-3 (październik 2008): 283–92. http://dx.doi.org/10.1016/j.jmatprotec.2007.12.113.

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Gnanamoorthy, R., i A. Sahaya Grinspan. "E-11 FATIGUE BEHAVIOUR OF OIL JET PEENED ALUMINIUM ALLOY, AA 6063-T6(Session: Fatique/Contact Strength)". Proceedings of the Asian Symposium on Materials and Processing 2006 (2006): 103. http://dx.doi.org/10.1299/jsmeasmp.2006.103.

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Kumar, Raghuvir, i S. B. L. Garg. "Influence of applied stress ratio on fatigue crack growth in 6063-T6 aluminium alloy". International Journal of Pressure Vessels and Piping 20, nr 1 (styczeń 1985): 65–76. http://dx.doi.org/10.1016/0308-0161(85)90035-3.

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Kumar, Raghuvir, i S. B. L. Garg. "A study of crack closure under constant amplitude loading for 6063-T6 Al-alloy". International Journal of Pressure Vessels and Piping 33, nr 5 (styczeń 1988): 373–84. http://dx.doi.org/10.1016/0308-0161(88)90121-4.

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Rozprawy doktorskie na temat "AL ALLOY 6063-T6"

Angélico, Cristiano [UNESP]. "Soldagem TIG-AC onda retangular: efeitos da velocidade de soldagem sobre as propriedades mecânicas da Liga AA 6063-T6". Universidade Estadual Paulista (UNESP), 2012. http://hdl.handle.net/11449/96488.

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Made available in DSpace on 2014-06-11T19:28:21Z (GMT). No. of bitstreams: 0 Previous issue date: 2012-10-26Bitstream added on 2014-06-13T20:37:08Z : No. of bitstreams: 1 angelico_c_me_bauru.pdf: 3319014 bytes, checksum: 6e80b1957b5cf72eb5800b57aafd8569 (MD5)
Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)
Neste trabalho foram investigados os efeitos da velocidade de soldagem no comportamento mecânico em juntas da liga AA 6063-T6, soldadas pelo processo TIG-CA com onda retangular desbalanceada. Foram analisadas as características macroestruturais (diluição do metal de base e coeficiente de forma). O planejamento experimental contemplou a utilização de metal de adição (AWS ER 4043), chanfro em v (60º), e variações nos parâmetros de ajuste de onda retangular nominalmente: amplitude de corrente negativa e tempo de polaridade negativa do eletrodo. A análise microestrutural utilizou microscopia ótica e microscopia eletrônica de varredura em observações no metais de solda obtidos e correspondentes ZTA. A avaliação mecânica foi realizada por meio de ensaios de tração nas juntas soldadas e medidas de microdureza Vickers. Adicionalmente, foram medidas as temperaturas máximas alcançadas nas juntas durante a soldagem. Os resultados mostram alterações nos valores das diluições do metal de base e na configuração geométrica dos cordões, em função da variação na velocidade de soldagem. As microestruturas desenvolvidas nos meios de solda e ZTA não se diferenciaram significativamente e, por consequencia, o comportamento mecânico detectado foi similar em todas as condições de soldagem aplicadas
In this study were investigated the welding speed effects in the mechanical behavior in welded joints of AA 6063-T6 alloy, welded by TIG-CA process with retangular wave. Were analyzed characteristics macrostructural (base material dillution, width and depth) of the weld bead. The experimental planning used and addition metal (AA 4043 alloy), bevel type v (60º) and variations in the setting parameter of retangular wave called negative current amplitude and duration of negative electrode polarity. The microstructural analysis used optical microscopy and scanning electron microcopy observation in the weld metals and HAZ obtained. The mechanical evaluation was performed by a tensile test on welded joints and Vickers microhardness measurements. In addition, it was measure the maximum temperature reached in during welding. The results show market changes in the values of the dillutions tested and the geometric configuration of the weld beads, mainly due to the variation in the welding speed. The microstuctures developed in the weld meal and HAZ did not differ significantly and, consequently, the mechanical behavior detected was similar in all welding conditions applied

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Angélico, Cristiano. "Soldagem TIG-AC onda retangular : efeitos da velocidade de soldagem sobre as propriedades mecânicas da Liga AA 6063-T6 /". Bauru : [s.n.], 2012. http://hdl.handle.net/11449/96488.

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Orientador: Gilberto de Magalhães Bento Gonçalves
Banca: Sérgio Rodrigues Barra
Banca: Yukio Kobayashi
Resumo: Neste trabalho foram investigados os efeitos da velocidade de soldagem no comportamento mecânico em juntas da liga AA 6063-T6, soldadas pelo processo TIG-CA com onda retangular desbalanceada. Foram analisadas as características macroestruturais (diluição do metal de base e coeficiente de forma). O planejamento experimental contemplou a utilização de metal de adição (AWS ER 4043), chanfro em "v" (60º), e variações nos parâmetros de ajuste de onda retangular nominalmente: amplitude de corrente negativa e tempo de polaridade negativa do eletrodo. A análise microestrutural utilizou microscopia ótica e microscopia eletrônica de varredura em observações no metais de solda obtidos e correspondentes ZTA. A avaliação mecânica foi realizada por meio de ensaios de tração nas juntas soldadas e medidas de microdureza Vickers. Adicionalmente, foram medidas as temperaturas máximas alcançadas nas juntas durante a soldagem. Os resultados mostram alterações nos valores das diluições do metal de base e na configuração geométrica dos cordões, em função da variação na velocidade de soldagem. As microestruturas desenvolvidas nos meios de solda e ZTA não se diferenciaram significativamente e, por consequencia, o comportamento mecânico detectado foi similar em todas as condições de soldagem aplicadas
Abstract: In this study were investigated the welding speed effects in the mechanical behavior in welded joints of AA 6063-T6 alloy, welded by TIG-CA process with retangular wave. Were analyzed characteristics macrostructural (base material dillution, width and depth) of the weld bead. The experimental planning used and addition metal (AA 4043 alloy), bevel type "v" (60º) and variations in the setting parameter of retangular wave called "negative current amplitude and duration of negative electrode polarity". The microstructural analysis used optical microscopy and scanning electron microcopy observation in the weld metals and HAZ obtained. The mechanical evaluation was performed by a tensile test on welded joints and Vickers microhardness measurements. In addition, it was measure the maximum temperature reached in during welding. The results show market changes in the values of the dillutions tested and the geometric configuration of the weld beads, mainly due to the variation in the welding speed. The microstuctures developed in the weld meal and HAZ did not differ significantly and, consequently, the mechanical behavior detected was similar in all welding conditions applied
Mestre

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SINGH, VIBHU. "INVESTIGATIONS FOR ENHANCEMENT OF MECHANICAL PROPERTIES WITH REINFORCEMENT SIZE VARIATION IN METAL MATRIX COMPOSITES". Thesis, 2019. http://dspace.dtu.ac.in:8080/jspui/handle/repository/16726.

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Metal matrix composites are emanating as advance engineering and structural materials and their demands are continuously growing in various sectors with higher pace. Among all the metals matrix composite, aluminum matrix composite are coming out as a tough potential competitor for the conventional materials for having large number of applications in aerospace, manufacturing, transportation, defence, sports and count goes on. The driving force for the usage of AMC over other is due to its ductility, toughness, strength and being less expensive. In this investigation, AMC has been fabricated using aluminum alloy Al 6063 T6 as base matrix material as aluminum characterizes the property of being light weight, durable, corrosion resistance and good strength and strengthening it by adding hard ceramic particle Boron Carbide (B4C) as reinforcement which the third hardest material known. Three different micro sizes of B4C have been incorporated viz.104µm, 74µm, 53µm. Stir casting technique has been used to synthesize aluminum metal matrix composite. Though several other techniques are available for the composite preparation, stir casting is preferred because of being simple, cost-effective, convenient to use, suitable for mass production and one of the proven processes. Micro-structure and mechanical behaviour of the Al alloy and prepared composites has been analyzed. Through optical microscopy, uniform and proper distribution of B4C particle is observed in the developed composites. It was observed that hardness of reinforced composite has been more than that of base alloy, in which composite with particle size 104µm has maximum hardness. Ultimate tensile strength of the prepared composite has found to be less as compared to base alloy which further shows a decreasing trend in tensile strength as the particle size decreases from to 104µm to 53µm.

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Części książek na temat "AL ALLOY 6063-T6"

Erzi, Eray, Cem Kahruman i Suat Yilmaz. "Creep Behavior of Plasma Sprayed Y-PSZ Coated 6063-T6 Aluminum Alloy". W Supplemental Proceedings, 35–39. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118356074.ch5.

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Erzi, Eray, Selim Yildirim i Suat Yilmaz. "Abrasive Wear Properties of Plasma Sprayed Y-PSZ Coated 6063-T6 Aluminum Alloy". W Supplemental Proceedings, 73–77. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118356074.ch10.

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Ismail, Azman, Mokhtar Awang i Shaiful Hisham Samsudin. "The Influence of Process Parameters on the Temperature Profile of Friction Stir Welded Aluminium Alloy 6063-T6 Pipe Butt Joint". W Mechanical and Materials Engineering of Modern Structure and Component Design, 243–49. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-19443-1_19.

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Mrówka-Nowotnik, Grażyna. "6XXX Alloys: Chemical Composition and Heat Treatment". W Encyclopedia of Aluminum and Its Alloys. Boca Raton: CRC Press, 2019. http://dx.doi.org/10.1201/9781351045636-140000212.

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Analysis of the influence of chemical composition, crystallization process and heat treatment on the phase constituents’ morphology, and mechanical properties and crack resistance of 6xxx Al alloys were conducted. The alloys with low Mg and Si content (6063) in the as-cast state are characterized by presence of Si particles and primary intermetallic phases: α-Al8Fe2Si, β-Al5FeSi, β-Mg2Si, and α-Al(FeMn)Si. Higher Mg, Si, and Mn content (6005 and 6082) leads to separation of additional phase particles: Al6Fe, Al6Mn, and Al12(FeMn)Mg3Si6, whereas high Cu content (6061—0.35% and 6066—0.95%, respectively) is responsible for precipitation of additional phase particles: Q-Al5Cu2Mg8Si6 and θ-Al2Cu. It has been established that homogenization results in total dissolution of the θ-Al2Cu and Q-Al5Cu2Mg8Si6 primary phases and partial dissolution of β-Mg2Si. Needle-like and Chinese-script α-Al8Fe2Si and β-Al5FeSi were transformed into spheroidal α-Al(FeMn)Si particles. The maximal consolidation of the 6xxx alloys is a result of precipitation of metastable particles, the transient βʺ, βʹ, and Qʹ/θʹ phases (6061 alloy) with high dispersion. The highest mechanical properties were achieved after holding in the temperature of 565°C/6 h, supersaturated in water, and aging at 175°C/10–20 h (T6). The decohesion process in the presence of tensile stresses in the room temperature proceeds through nucleation, the growth and joining of the voids, as well as the cracking of the primary and secondary large-sized intermetallic phase particles. The increase of deformation temperature up to 300°C causes the changes of the nucleation source and joining of voids—it occurs mainly along the matrix–particle interface.

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L. Avila Ambriz, Jorge, Erasmo Correa Gómez, Julio C. Verduzco Juárez, Gonzalo M. Dominguez Almaraz i Aymeric E. Dominguez. "Fatigue Endurance under Torsion Testing: 6061-T6 and 6063-T5 Aluminum Alloys". W Encyclopedia of Aluminum and Its Alloys. Boca Raton: CRC Press, 2019. http://dx.doi.org/10.1201/9781351045636-140000217.

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This article deals with torsion fatigue tests carried out on the aluminum alloys: AISI 6061-T6 and 6063-T5, under two load ratios: R = −1 and R = 0, both of them at 10 Hz of frequency. The tests were obtained at room temperature (23°C) and with environmental humidity comprised between 35% and 45%. Results reveal a noticeable fatigue endurance reduction on tests with R = 0 against tests at R = −1 for both aluminum alloys. The load ratio was fixed by imposing the initial angle before the testing starting. A new torsion fatigue machine has been developed by two of the authors (under patent consideration before the Mexican Institute of Industrial Property), which has the versatility of torsion tests at different frequencies and load ratios; a general description of this machine is presented in the article. The torsion fatigue life and the fracture surfaces were analyzed for the two aluminum alloys and both torsion fatigue load ratios, leading to drawing up the conclusions related to this research article.

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Streszczenia konferencji na temat "AL ALLOY 6063-T6"

Koganti, Ramakrishna, Armando Joaquin, Matthew Zaluzec i Chris Karas. "Gas Metal Arc Welded (GMAW) Joint Strength Comparison of Aluminum Sheet (5754) and Exturded (6063) Alloys". W ASME 2007 International Mechanical Engineering Congress and Exposition. ASMEDC, 2007. http://dx.doi.org/10.1115/imece2007-43423.

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The development of lightweight vehicles, in particular aluminum intensive vehicles, require significant manufacturing process development for joining and assembling aluminum structures. Currently, 5xxx and 6xxx aluminum alloys are being used in various structural applications in a number of lightweight vehicles worldwide. Various joining methods, such as GMAW (it is also referred as Metal Inert Gas Welding), Laser and adhesive bonding have been investigated as technology enablers for high volume joining of 5xxx, and 6xxx series alloys. In this study, GMA welding was used to join 5754 non-heat-treatable alloy sheet and 6063-T6 heat treatable extrusion products. The objective of this study was to develop optimum weld process parameters for non-heat-treatable 5754 aluminum and heat treatble 6063-T6 alloys. For both the alloys, the lap joint configuration was used. The GMA welding equipment used in this study was an OTC/Daihen CPD-350 welding systems and DR-4000 pulse power supply. In the first phase of the experiments for 5754 aluminum alloy, the factors selected for the experiment were power input (torch speed, voltage, current, wire feed), pulse frequency, gas flow rate and surface condition. A full factorial design of experiment (DOE) was conducted (DOE #1) to understand the main and interaction effects on lap joint failure and weld penetration. Based on the results from phase 1 results, surface condition was eliminated in the phase 2 experiments. In phase 2 experiments for heat treatable alloys 6063 T6, the factors selected were power input (torch speed, voltage, current, wire feed), pulse frequency, gas flow rate, torch angle, and arc intensity. A partial factorial DOE was conducted (DOE # 2) primarily to understand the main effects and some two level interaction effects. For both phase 1 (non-heat treatable alloy 5754) and phase 2 (heat treatable alloy 6063-T6) experiments, the factors influence on the mechanical properties of the lap joint, metallurgy (weld penetration) and micro hardness were evaluated. Post weld analysis indicates for non heat treatable alloy 5754, power input and gas flow rate are the two signficant factors (statistically) based on lap shear load to failure and weld penentration data. For heat treatable alloy 6063, power input was the significant factor on joint load to failure, however, for weld penetration, power input, pulse frequency and gas flow rate were the significant factors. Based on the joint strength and weld penetration, optimum weld process factors were determined for both non-heat treatable alloy 5754 and heat treatble alloy 6063 T6.

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Mayer, Robert R., Weigang Chen i Anil Sachdev. "Crashworthiness Performance of Mass-Efficient Extruded Structures". W ASME 2002 International Mechanical Engineering Congress and Exposition. ASMEDC, 2002. http://dx.doi.org/10.1115/imece2002-39077.

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Theoretical, numerical and experimental studies were conducted on the axial crushing behavior of traditional single-cell and innovative four-cell extrusions. Two commercial aluminum alloys, 6061 and 6063, both with two tempers (T4 and T6), were considered in the study. Testing coupons taken from the extrusions assessed the nonlinear material properties. A theoretical solution was available for the one-cell design, and was developed for the mean crushing force of the four-cell section. Numerical simulations were carried out using the explicit finite element code LS-DYNA. The aluminum alloy 6063T4 was found to absorb less energy than 6061T4, for both the one-cell and four-cell configurations. Both 6061 and 6063 in the T6 temper were found to have significant fracture in the experimental testing. Theoretical analysis and numerical simulations predicted a greater number of folds for the four-cell design, as compared to the one-cell design, and this was confirmed in the experiments. The theoretical improvement in energy absorption of 57% for the four-cell in comparison with the one-cell design was confirmed by experiment. The good agreement between the theoretical, numerical and experimental results allows confidence in the application of the theoretical and numerical tools for both single-cell and innovative four-cell extrusions. It was also demonstrated that these materials have very little dynamic strain rate effect.

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Koganti, Ramakrishna, Adrian Elliott, Matthew Zaluzec, Ari Caliskan i Armando Joaquin. "Influence of Heat Treatment on Gas Metal Arc Welded Aluminum 6063 Alloy for Automotive Aluminum Spaceframe Architectures". W ASME 2008 International Mechanical Engineering Congress and Exposition. ASMEDC, 2008. http://dx.doi.org/10.1115/imece2008-68495.

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An aluminum structure has many advantages over steel for automotive application, but the combination of lower weight, with high torsional stiffness and good energy management performance in crash is perhaps the most beneficial. Hybrid architectures, consisting of a combination of aluminum products including stampings, extrusions (straight and hydroformed) and castings, are becoming more common. The Ford GT represents the first Ford Motor Company hybrid aluminum spaceframe. The frame is comprised of castings, extrusions and stamped, flat and roll-bonded, panels. All structural connections between the extrusions and the castings are fusion welded with the exception of the front and rear crush structures. Ford R&AE supported the Ford GT program in the joining and assembly of the hybrid aluminum body architecture, with responsibility for the development of the Gas Metal Arc Welding (GMAW) process. Recognizing that the heat input from the GMA welding process is significant, it is necessary to understand the aluminum material properties after temperature exposure during welding. The frame is subject to further temperature exposure during manufacture during the painting operations. Additionally, those areas of the frame around the engine will be exposed to high temperatures in service. The objective of this study, in support of the Ford GT, was to evaluate the mechanical properties of GMA welded 6063-T6 extruded coupons after different heat treatments simulating the paint ovens during vehicle build and extreme engine temperatures when in service. This information was critical for use in the program Finite Element Models (FEM) developed for Noise, Vibration, and Harshness (NVH), Crash and Durability. The study was successful in showing that the tensile strength of the welded aluminum was not affected by thermal exposure for the range of different temperatures and times, chosen to represent vehicle build and in service temperature conditions. The most consistent results were obtained for tests simulating the paint bake (180 °C for 30 minutes). The ‘as welded’ and engine bay temperature exposures (24 hour at 150 °C and 200 °C) showed higher variability. The failure mode for the 24 hour exposures was in the weld, as compared to the HAZ for the other samples.

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Espezua, Sandro Victor Polanco, Carlos Antonio Reis Pereira Baptista, Denise Ferreira Laurito i Ana Marcia Barbosa da Silva. "Influence of Intermetallics and Precipitates on the Fatigue Crack: Nucleation And Propagation in Aluminum Alloys 6005-T6, 6063-T6 and 6351-T6". W 21st SAE Brasil International Congress and Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2012. http://dx.doi.org/10.4271/2012-36-0520.

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