Bibliografías temáticas / AA2024-T4

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Literatura académica sobre el tema "AA2024-T4"

Autor: Grafiati
Publicado: 4 de septiembre de 2021
Última modificación: 29 de julio de 2025

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Artículos de revistas sobre el tema "AA2024-T4"

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Urrego, Luis Fabian, Olimpo García-Beltrán, Nelson Arzola, and Oscar Araque. "Mechanical Fracture of Aluminium Alloy (AA 2024-T4), Used in the Manufacture of a Bioproducts Plant." Metals 13, no. 6 (2023): 1134. http://dx.doi.org/10.3390/met13061134.

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Aluminium alloy (AA2024-T4) is a material commonly used in the aerospace industry, where it forms part of the fuselage of aircraft and spacecraft thanks to its good machinability and strength/weight ratio. These characteristics allowed it to be applied in the construction of the structure of a pilot plant to produce biological extracts and nano-encapsulated bioproducts for the phytosanitary control of diseases associated with microorganisms in crops of Theobroma Cacao L. (Cacao). The mechanical design of the bolted support joints for this structure implies knowing the performance under fatigue
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Ahmed, Mohamed M. Z., Mohamed M. El-Sayed Seleman, Zeinab A. Zidan, Rashad M. Ramadan, Sabbah Ataya, and Naser A. Alsaleh. "Microstructure and Mechanical Properties of Dissimilar Friction Stir Welded AA2024-T4/AA7075-T6 T-Butt Joints." Metals 11, no. 1 (2021): 128. http://dx.doi.org/10.3390/met11010128.

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Aircraft skin and stringer elements are typically fabricated from 2xxx and 7xxx series high strength aluminum alloys. A single friction stir welding (FSW) pass using a specially designed tool with shoulder/pin diameter ratio (D/d) of 3.20 is used to produce dissimilar T-butt welds between AA2024-T4 and AA7075-T6 aluminum alloys at a constant travel speed of 50 mm/min and different rotational speeds of 400, 600 and 800 rpm. The AA2024-T4 is the skin and the AA7075-T6 is the stringer. Sound joints are produced without macro defects in both the weld top surfaces and the joint corners at all rotat
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Ahmed, Mohamed M. Z., Mohamed M. El-Sayed Seleman, Zeinab A. Zidan, Rashad M. Ramadan, Sabbah Ataya, and Naser A. Alsaleh. "Microstructure and Mechanical Properties of Dissimilar Friction Stir Welded AA2024-T4/AA7075-T6 T-Butt Joints." Metals 11, no. 1 (2021): 128. http://dx.doi.org/10.3390/met11010128.

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Aircraft skin and stringer elements are typically fabricated from 2xxx and 7xxx series high strength aluminum alloys. A single friction stir welding (FSW) pass using a specially designed tool with shoulder/pin diameter ratio (D/d) of 3.20 is used to produce dissimilar T-butt welds between AA2024-T4 and AA7075-T6 aluminum alloys at a constant travel speed of 50 mm/min and different rotational speeds of 400, 600 and 800 rpm. The AA2024-T4 is the skin and the AA7075-T6 is the stringer. Sound joints are produced without macro defects in both the weld top surfaces and the joint corners at all rotat
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4

Алвин, А. Х., Х. Ксиби, З. Дрисс, and Х. Алалкави. "Mechanical properties and fatigue performance of AA2024-T361 alloy under elevated temperatures." Металловедение и термическая обработка металлов, no. 4 (May 2, 2025): 16–21. https://doi.org/10.30906/mitom.2025.4.16-21.

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Экспериментально исследованы механические свойства при статическом растяжении и усталостные характеристики при постоянной амплитуде нагружения алюминиевого сплава 2024-T361 (аналог AA2024-T4) при повышенных температурах. Показано, что повышение температуры до 200 – 250 °C приводит к значительному снижению механических свойств, долговечности и прочности сплава при циклическом нагружении по схеме изгиб с кручением. Относительное снижение механических свойств сплава при повышении температуры до 200 – 250 °C, наблюдаемое в настоящем исследовании, согласуется с данными других авторов. Однако сопрот
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5

Alwin, Allawi H., Hatem Ksibi, Zied Driss, and Hussain J. M. Alalkawi. "Fatigue Variable Loading Under Combined High Temperature and Shot Peening Treatment for AA2024-T4 and AA2024-T361." Strojnícky časopis - Journal of Mechanical Engineering 73, no. 1 (2023): 1–12. http://dx.doi.org/10.2478/scjme-2023-0001.

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Abstract The variable fatigue loading (VL) is an important issue for aircraft safety. Indeed, aluminium alloy parts are always the subject of this type of thermo-mechanical alterations. This study examined the effect (VL) under normal operating conditions. We investigated the effect of fatigue variable loading (VL) under combined high temperature (HT) and shot peening (SP) treatment for (AA2024-T4 and AA2024-T361). Fatigue under loading from 250 to 350MPa with various combinations of loading cycles is presented. The experimental fatigue life results were compared to Miner’s rule. The compariso
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6

Yusoff, N. I., and L. H. Sulaiman. "Influence of Clad Layer Thickness of Aluminium Alloy by Friction Surface Cladding Process." Journal of Modern Manufacturing Systems and Technology 7, no. 2 (2023): 17–22. http://dx.doi.org/10.15282/jmmst.v7i2.9935.

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Friction Surface Cladding (FSC) is a process that enables the deposition of clad material on a substrate through a hollow rotating tool to create thin clad layers at sufficiently high temperatures. Heat is produced during the cladding process by friction at the tool-clad layer and the substrate. This study focus on the influence of clad layer thickness of aluminium alloy AA2024 at the control process temperature around 300℃ to 350℃. The material used is AA2024-T4 for the clad layer and AA2024-T351 for the substrate. A thermal model is built using COMSOL Multiphysics 6.0 and Heat Transfer in So
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Zhang, Yanxin, Yongxian Huang, Xiangchen Meng, Junchen Li, Yuming Xie, and Qiang Fan. "Friction stir lap welding of AA2024-T4 with drastically different thickness." International Journal of Advanced Manufacturing Technology 106, no. 9-10 (2020): 3683–91. http://dx.doi.org/10.1007/s00170-019-04865-x.

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8

Delaunois, Fabienne, Edwin Denil, Yves Marchal, and Véronique Vitry. "Accelerated Aging and Portevin-Le Chatelier Effect in AA 2024." Materials Science Forum 879 (November 2016): 524–29. http://dx.doi.org/10.4028/www.scientific.net/msf.879.524.

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AA2024 aluminium alloy is used in aeronautics for various applications. However, the aging treatment (“T4 temper”) at ambient temperature used to bring it to optimal mechanical properties causes several problems. The main one is its duration (5 days) which brings the need for storage of the parts. Moreover temperature control during such a long period is difficult.The aim of this work was to develop an alternative treatment leading to optimized mechanical properties in a shorter time. For this, we investigated the kinetics of the aging process and observed the apparition and disappearance of “
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9

Wang, Lei, and Jian Jun Zhu. "Experiment and Simulation of Influence of Welding Parameters on Temperature in Friction Stir Welding." Applied Mechanics and Materials 44-47 (December 2010): 76–80. http://dx.doi.org/10.4028/www.scientific.net/amm.44-47.76.

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Temperature distribution is the foundation to study friction stir welding technique, influence of welding parameters on temperature was studied through experiment measurement on AA2024-T4 aluminum alloy plates. An instantaneous relative linear velocity based heat source was utilized to build the FEM model of friction stir welding process, good agreement was observed between the measured and simulated thermal profiles. FEM model was also utilized to study effect of welding parameters on temperature distribution.
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10

Sun, Shuangqing, Shenghui Chen, Yunfei Ma, Qifei Zheng, and Songqing Hu. "Exfoliation Corrosion of Extruded AA2024-T4 in the Industrial and Coastal-Industrial Environments." CORROSION 70, no. 10 (2014): 1064–73. http://dx.doi.org/10.5006/1276.

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Tesis sobre el tema "AA2024-T4"

1

Melo, Joao Carlos Simões. "Comportamento à fadiga de ligações T em ligas de alumínio dissimilares, soldadas por laser." Master's thesis, 2017. http://hdl.handle.net/10316/83422.

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Dissertação de Mestrado Integrado em Engenharia Mecânica apresentada à Faculdade de Ciências e Tecnologia<br>Este trabalho foi feito com o objetivo de estudar a influência dos parâmetros de soldadura na morfologia e no comportamento à fadiga de juntas T de ligas de alumínio dissimilares soldadas a laser, com o fim da sua aplicação na indústria aeronáutica.Utilizando a soldadura laser, foram fabricadas juntas T em chapas com 2 mm de espessura das ligas AA2024-T4 (Skin) e AA7075-T6 (Stringer) e elétrodo da liga AA4047 como material de adição. Foi feita a variação de parâmetros de soldadura como
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Capítulos de libros sobre el tema "AA2024-T4"

1

Kumar, Deepak, Md Parwez Alam, and A. N. Sinha. "Numerical and Experimental Analysis of Friction Stir Welding of Aluminum Alloy AA2024-T4." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-7709-1_4.

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Actas de conferencias sobre el tema "AA2024-T4"

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Shivaraj, Manoj Kumar, Vijay Dinakaran, and Venkatesh Mahadevan. "Notice of Retraction: Frictional stir welding on aluminum alloys AA2024-T4 and AA7075-T6." In 2010 2nd International Conference on Computer Engineering and Technology (ICCET). IEEE, 2010. http://dx.doi.org/10.1109/iccet.2010.5485331.

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Alwin, Allawi H., Hatem Ksibi, Zied Driss, and Hussain J. M. Alalkawi. "Optimization of the shot peening time (SPT) in terms of mechanical properties and fatigue life of AA2024-T4." In ELECTROMECHANICAL ENGINEERING AND ITS APPLICATIONS. AIP Publishing, 2024. http://dx.doi.org/10.1063/5.0206464.

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