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Статті в журналах з теми "AMg6"

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Автор: Grafiati

Опубліковано: 30 травня 2022

Оновлено: 31 травня 2022

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1

Rakhadilov, B., L. Zhurerova, W. Wieleba, Zh Sagdoldina, and A. K. Khassenov. "Features of the structure and properties formation of AMG6 alloy under the equal channel angular pressing." Bulletin of the Karaganda University. "Physics" Series 97, no. 1 (March 30, 2020): 42–49. http://dx.doi.org/10.31489/2020ph1/42-49.

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Анотація:

The results of experimental studies of changes in the structure, microhardness, and wear resistance of the AMG6 aluminum alloy during equal channel angular pressing (ECAP) are presented in this work. The evolution of the fine structure and the formation of secondary phases in the AMG6 alloy during ECAP were studied. The dark-field image of the structure of the AMg6 alloy in the matrix reflex showed the splitting of the material into small disoriented fragments of about 0.5 μm in size with a small-angle disorientation boundary (about 2–5°). Optimal method and modes of ECAP of the AMG6 aluminum alloy were selected of the bases of experimental research, which make it possible to obtain a workpiece with enhanced tribological and mechanical characteristics. It was established that the most intensive grinding of the grain structure in the AMG6 alloy occurs at ECAP-12 at a channel angle intersection of 120°. It is shown that with a decrease in grain size, the microhardness of the alloy AMG6 after ECAP increases by 4 times, compared with the initial state.The results of the test samples for abrasive wear showed a decrease in mass loss after 12 passes of ECAP, which indicates an increase in the wear resistance of the alloy AMG6 by 13–14 %, compared with the initial state.

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2

Коробов, А. И., А. И. Кокшайский, В. М. Прохоров, И. А. Евдокимов, С. А. Перфилов та А. Д. Волков. "Механические и нелинейные упругие характеристики поликристаллического алюминиевого сплава AMg6 и нанокомпозита n-AMg6/C-=SUB=-60-=/SUB=-". Физика твердого тела 58, № 12 (2016): 2384. http://dx.doi.org/10.21883/ftt.2016.12.43861.154.

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Экспериментально исследовано влияние наноструктурования на механические и нелинейные упругие характеристики поликристаллического алюминиевого сплава AMg6 и нанокомпозита n-AMg6/C60. В образцах алюминиевого сплава AMg6 и нанокомпозита n-AMg6/C60 измерены механические характеристики и, ультразвуковым методом, все независимые коэффициенты упругости второго и третьего порядков. Коэффициенты упругости третьего порядка были определены методом Терстона-Браггера по результатам экспериментальных измерений зависимости скорости сдвиговых и продольных объемных акустических волн в исследуемых образцах от величины одноосного сжатия. Спектральным акустическим методом исследованы нелинейные упругие свойства и определены нелинейные акустические параметры этих материалов. Образцы и исследования их механических характеристик выполнены в рамках госзадания Министерства образования и науки РФ на 2016 г. (проект N 3562). Ультразвуковые исследования были выполнены за счет гранта Российского научного фонда (проект N 14-22-00042).

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3

Vladimirov, S. A. "Deformation characteristics of aluminum alloys." Izvestiya MGTU MAMI 9, no. 2-4 (July 20, 2015): 44–50. http://dx.doi.org/10.17816/2074-0530-67119.

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The paper presents the results of tests to failure of aluminum alloys samples AMg6, AMg6M of various forms. Among the samples there were uniaxial samples, tubular samples in torsion, round membranes designed to hidrolipoclasia, thin cut plates, flat samples with holes and round solid samples with an annular undercut with different radius cuts. The impact of volume stress state, calculated by the method of mathematical simulation of each type samples loading processes, on maximum deformation is discussed.

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4

Koryagin, Yu D., S. I. Il'in, and N. A. Shaburova. "Stability of Strength Characteristics of Hardened by Deformation AMg6 Alloy during High-Speed Heating." Materials Science Forum 989 (May 2020): 110–15. http://dx.doi.org/10.4028/www.scientific.net/msf.989.110.

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The results were shown in influence of fast heating parameters on the structure and properties of cold-worked alloy AMg6 with original hot-forged structure. Based on the measured data, the change of mechanical properties of cold-worked alloy AMg6 during the process of short duration heating was evaluated. There was reviewed the role of the temperature and the time of heat on the processes of softening the samples of cold-worked alloy AMg6. The stability of mechanical characteristics of hammer-hardened alloy AMg6 under elevated test temperatures was evaluated. It is shown that the return processes in cold-deformed AMg6 alloy during heating in the temperature range studied receive the most intensive development in the first 5–10 minutes, reducing the hardening effect from cold deformation, determined by tensile strength, respectively: by 8–9% with 100 °C; 26–27% at 150 °C; 37–38% at 200 °C; 42–44% at 250 °C and 50% at 300 °C. A decrease in the yield strength during high-speed heating in the temperature range studied is much faster ,compared with the change in the tensile strength. Hour exposure at 200 °C reduces the hardening effect on the yield strength from 340 MPa to 258 MPa, while the tensile strength decreases from 430 MPa to 385 MPa.

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5

Прохоров, В. М., та Е. Л. Громницкая. "Зависимость от давления коэффициентов упругости алюминий-магниевого сплава AMg6 и нанокомпозитного сплава n-Mg6/C-=SUB=-60-=/SUB=-". Физика твердого тела 60, № 4 (2018): 765. http://dx.doi.org/10.21883/ftt.2018.04.45690.300.

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AbstractThe ultrasonic study results for dependence of the elastic wave velocities and second-order elasticity coefficients of the polycrystalline aluminum alloy AMg6 and its nanocomposite n -AMg6/C_60 on hydrostatic pressure up to 1.6 GPa have been described. The ultrasonic research has been carried out using a highpressure ultrasonic piezometer based on the piston-cylinder device. The pressure derivatives of the secondorder elastic constants of these materials established in the present study have been compared with the results of the third-order elastic constants measurements of the test alloys using the Thurston–Brugger method. Involving available literature data, we determined the relationships between the pressure derivatives of the second-order elastic constants of the AMg6 alloy and the Mg-content and nanostructuring.

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6

Yasnii, P. V., M. P. Halushchak, S. I. Fedak, and V. Yu Pidkol'zin. "Cyclic creep of AMg6 alloy." Materials Science 36, no. 1 (January 2000): 48–53. http://dx.doi.org/10.1007/bf02805116.

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7

Korobov, A. I., A. I. Kokshaiskii, V. M. Prokhorov, I. A. Evdokimov, S. A. Perfilov, and A. D. Volkov. "Mechanical and nonlinear elastic characteristics of polycrystalline AMg6 aluminum alloy and n-AMg6/C60 nanocomposite." Physics of the Solid State 58, no. 12 (December 2016): 2472–80. http://dx.doi.org/10.1134/s106378341612012x.

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8

Uazyrkhanova, Gulzhaz, Bauyrzhan K. Rakhadilov, Alexandr Myakinin, and Zhuldyz Uazyrkhanova. "The Change in the Thin Structure and Mechanical Properties of Aluminum Alloys at Intensive Plastic Deformation." Materials Science Forum 906 (September 2017): 114–20. http://dx.doi.org/10.4028/www.scientific.net/msf.906.114.

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Electron microscopy and x-ray analysis and mechanical testing have been investigated the influence of severe plastic deformation on structure and mechanical properties of aluminum alloys. It is established that in the initial state in the alloy AMC has a high density of chaotically distributed dislocations with a density of 5-10*109 сm-2. It is shown that microdiffraction paintings in alloy AMC in the bulk of grains are observed uniformly distributed particles of the second phase. It is established that in the initial state in the alloy AMG6 there is a high density of chaotically distributed dislocations with a density of 2-6 *1010 сm-2. Determined that after ECAP the dislocation structure of alloys AMG6, AMC and changes: formed dislocation networks inside the fragments of the dislocation is practically not observed. Determined that after ECAP-12 increase the tensile strength and yield strength of alloys AMG6 and AMC.

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9

Trusova, G. I. "Structural changes in type AMg6 alloys." Metal Science and Heat Treatment 34, no. 5 (May 1992): 341–45. http://dx.doi.org/10.1007/bf00776661.

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10

Novikov, S. A., and A. I. Ruzanov. "Fracture failure in the alloy AMg6." Journal of Applied Mechanics and Technical Physics 32, no. 2 (1991): 288–91. http://dx.doi.org/10.1007/bf00858052.

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11

Prokhorov, V. M., та E. L. Gromnitskaya. "Pressure Dependences of Elastic Constants of AMg6 Aluminum–Magnesium Alloy and n-AMg6/С60 Nanocomposite Alloy". Physics of the Solid State 60, № 4 (квітень 2018): 769–73. http://dx.doi.org/10.1134/s106378341804025x.

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12

Goncharova, O. A., D. S. Kuznetsov, N. N. Andreev, N. P. Andreeva, and Yu I. Kuznetsov. "Chamber corrosion inhibitors of aluminum alloy AMG6." Corrosion: Materials, Protection, no. 8 (August 21, 2019): 23–28. http://dx.doi.org/10.31044/1813-7016-2019-0-8-23-28.

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13

Lukonina, Natalya, E. Nosova, and Fedor V. Grechnikov. "The Effect of Annealing on Mechanical Properties, the Number of Fluidity, and the Size of Coherent Scattering Regions in AMg1, AMg5, and AMg6 Alloys." Solid State Phenomena 284 (October 2018): 470–75. http://dx.doi.org/10.4028/www.scientific.net/ssp.284.470.

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The paper presents the results of research of the structural blocking influence in Al-Mg sheet aluminum alloys on the change in mechanical properties and the stamp ability after cold working and annealing. The study was provided on sheet billets of AlMg1, AlMg5 and AlMg6 alloys containing respectively 1, 5 and 6 mass.% Mg. The initial thickness of the blanks is 2.5 mm. The blanks were cold rolled with a reduction rate of 30%. To eliminate the cold working hardening alloys were subjected to annealing at temperatures of 380 and 420°C for 1 hour. The charts of tensile strength, yield stress, and elongation change are plotted, depending on the state of the samples. Stamping was evaluated by the stamping ratio σ0.2/σb. To analyze the alloys’ grain structure blocking, the change in the size of the coherent scattering areas was estimated on the basis of X-ray diffraction studies. It is established that annealing leads to a significant decrease in the tensile strength, yield stress and elongation growth of alloys AlMg1, AlMg5 and AlMg6 sheet samples in the annealing temperature interval 380...420 ̊С. Despite the high plasticity of the AlMg1 alloy, it has lower stamping characteristics than alloys with higher magnesium content (AlMg5 and AlMg6). The yield stress of alloys decreases with increasing of annealing temperature, which indicates an increase in their stamping ability after annealing. The change in the coherent scattering areas sizes in alloys depends on the magnesium content. With an increase in the magnesium content, the coherent scattering area size increase with the annealing temperature. For an AlMg1 alloy, annealing after cold rolling does not lead to a change in the coherent scattering area size.

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14

Sokovikov, Mikhail A. "A study of plastic strain localization under static and dynamic loading using the StrainMaster non-invasive strain measurement system." ВЕСТНИК ПЕРМСКОГО УНИВЕРСИТЕТА. ФИЗИКА, no. 2 (2021): 59–63. http://dx.doi.org/10.17072/1994-3598-2021-2-59-63.

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Static and dynamic testing of specimens specially designed for studying the localization of plastic deformation in AMg6 and D16 alloys were performed on then electromechanical Testometric machine and split Hopkinson pressure bar using the StrainMaster system for noninvasive measurement of shape and deformation. Displacement and strain fields are plotted for special-shaped specimens of AMg6 and D16 alloys subjected to static deformation and dynamic loading. Comparison between the experimentally obtained strain fields and the results of numerical simulation made with account of the kinetics of microdefect accumulation in the examined material demonstrates good agreement to the accuracy of ~20%. The performed tests and their numerical simulation with consideration for the evolution of the defect material structure confirm the concept of the strain localization mechanism associated with the processes in the system of microdefects.

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15

Lobanov, L. M., M. O. Pashchyn, O. M. Tymoshenko, P. V. Goncharov, O. L. Mikhodui, and K. V. Shiyan. "Increase in the life of welded joints of AMg6 aluminum alloy." Paton Welding Journal 2020, no. 4 (April 28, 2020): 2–8. http://dx.doi.org/10.37434/tpwj2020.04.01.

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16

Loginov, Yu N., and A. G. Illarionov. "DISCONTINUITY OF AMG6 ALUMINUM ALLOY EXTRUDED TUBE STRUCTURE." Izvestiya Vuzov. Tsvetnaya Metallurgiya (Proceedings of Higher Schools. Nonferrous Metallurgy), no. 6 (March 1, 2015): 35. http://dx.doi.org/10.17073/0021-3438-2013-6-35-40.

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17

Goncharova, O. A., D. S. Kuznetsov, N. N. Andreev, Yu I. Kuznetsov, and N. P. Andreeva. "Chamber Inhibitors of Corrosion of AMg6 Aluminum Alloy." Protection of Metals and Physical Chemistry of Surfaces 56, no. 7 (December 2020): 1293–98. http://dx.doi.org/10.1134/s2070205120070060.

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18

Yasnii, P. V., S. I. Fedak, V. B. Glad'o, and M. P. Galushchak. "Jumplike Deformation in AMg6 Aluminum Alloy in Tension." Strength of Materials 36, no. 2 (March 2004): 113–18. http://dx.doi.org/10.1023/b:stom.0000028300.06024.59.

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19

Ovchinnikov, Viktor, Viktorya Berezina, and Tat'yana Skakova. "A normalized method for determining the influence on the fixed joints tightness using the technology of the sealing surface job." Science intensive technologies in mechanical engineering 2021, no. 11 (November 30, 2021): 20–29. http://dx.doi.org/10.30987/2223-4608-2021-11-20-29.

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On the basis of metallographic analysis and test results of samples of welded junctions of aluminum alloys AMg6 and D16T, made by friction stir welding, for static stretching, it is shown that destruction occurs in the zone of thermo-mechanical action for the AMg6 alloy and in the zone of thermal influence for the D16T alloy. At the same time, the dependence of the temporary resistance value of the welded junction on the state of the seam weld face has not been revealed. Tests for low-cycle fatigue have shown that the endurance limit is clearly dependent on the amount of seam weld face roughness. The value of the roughness of the seam weld face for the studied alloys has been determined, in which the nature of the fracture during the low-cycle fatigue test changes from multi-stage to single-stage.

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20

Neshpor, G. S., A. A. Armyagov, and G. I. Berezhnaya. "Optimization of the magnesium content in AMg6 alloy sheet." Soviet Materials Science 21, no. 4 (1986): 388–89. http://dx.doi.org/10.1007/bf00726571.

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21

Bakulin, I. A., S. I. Kuznetsov, A. S. Panin, and E. Yu Tarasova. "Laser shock processing of AMg6 Al alloy without coating." Physics and Chemistry of Materials Treatment 1 (2021): 31–39. http://dx.doi.org/10.30791/0015-3214-2021-1-31-39.

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A microstructure and distribution of residual stresses after the laser shock peening of the AMg6 Al alloy without a protective coating were studied. The X-ray diffraction analysis showed the correlation between the parameters of the crystal structure and the profile of residual stresses of the treated samples. It was found that domain size decreased up to 50 nm, microstrains increased up to 0,0019 and average dislocation density increased up to 4,7·1014 м–2. Laser shock processing generates residual compressive stresses in depth up to 2 mm with a maximum of –120 MPa on the surface of the material. The profile and depth of the residual compressive stresses depend on the power density, overlap coefficient and the number of processing.

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22

Abramova, M. G., A. A. Goncharov, and Ya Yu Nikitin. "Study of the corrosion resistance of aluminum alloy AMg6 and steel 12Kh18N10T in conditions of loading under the impact of environmental factors." Industrial laboratory. Diagnostics of materials 87, no. 6 (June 18, 2021): 33–40. http://dx.doi.org/10.26896/1028-6861-2021-87-6-33-40.

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Stress corrosion cracking is one of the most dangerous types of corrosion damage in metallic materials. We present the results of studying the impact of environmental factors on the susceptibility of AMg6 aluminum alloy and 12Kh18N10T stainless steel to stress corrosion cracking under four-point bending. Tests of loaded samples were carried out in laboratory and field conditions of the moderately warm climate of the coastal zone over a period of six months. The samples were examined daily with fixation of the time to their destruction and upon completion of the tests the appearance of the samples and the depth of intergranular corrosion on microsections were assessed. A 3D relief was constructed using macro photography of the surface with the determination of the depth of corrosion foci. We also carried out a comparative analysis of the frequency of stress-induced destruction of steel samples of various grades both in atmospheric and laboratory conditions. It is shown that in atmospheric conditions characterized by the presence of dust particles acting as concentrators for the formation of corrosion foci, the aggressiveness of the corrosive effect of the environment increases, whereas the general corrosion resistance of materials decreases. The most pronounced effect of the environment was recorded in AMg6 alloy samples when exposed under a ventilated canopy in conditions of periodic spraying of seawater aerosols. The depth of surface corrosion damage was up to 0.1 mm. When the test samples were exposed under other conditions (salt fog chamber and louvered storage) the corrosion damage was absent. The results obtained can be used to predict the corrosion resistance of the products made of AMG6 alloy and 12Kh18N10T steel when operated in conditions of loading under the impact of environmental factors.

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23

Jakovlev, S. S., and A. A. Pasynkov. "Theoretical and experimental research of forging operation in split dies." Izvestiya MGTU MAMI 7, no. 2-2 (March 20, 2013): 92–96. http://dx.doi.org/10.17816/2074-0530-68071.

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This article describes a new mathematical model of stamping products in split die on the universal hydro-pressure equipment from high-strength materials. It describes the calculations of materials pressure in split die stamping of cross billet that is made from aluminium Amg6 (АМг6) and titanium ВТ6С alloys. The work contains the comparison of the experimental research results with theoretical data.

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24

Yasnii, P. V., Yu I. Pyndus, V. B. Hlad’o, and I. V. Shul’han. "Computer modeling of the jump-like deformation of AMg6 alloy." Materials Science 44, no. 1 (January 2008): 43–48. http://dx.doi.org/10.1007/s11003-008-9041-y.

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25

Tomilin, A. K., F. Yu Kuznetsov, I. S. Konovalenko, N. V. Druzhinin, V. A. Krasnoveikin, and I. Yu Smolin. "Frequency Dependence of the Internal Friction of the AMg6 Alloy." Journal of Machinery Manufacture and Reliability 50, no. 3 (May 2021): 243–50. http://dx.doi.org/10.3103/s1052618821030158.

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26

Rushchits, S. V., E. V. Aryshensky, S. M. Sosedkov, and A. M. Akhmed'yanov. "Modeling the Hot Deformation Behavior of 1565ch Aluminum Alloy." Key Engineering Materials 684 (February 2016): 35–41. http://dx.doi.org/10.4028/www.scientific.net/kem.684.35.

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The deformation behavior of 1565ch alloy under the plane-strain conditions in the temperature range of 350–490 оС and strain rates range of 0,1–10 s-1 is studied. The expression for steady flow stress as the functions of temperature of deformation and strain rate is obtained. It is established that 1565ch alloy with zirconium addition shows higher strain resistance and less tendency to dynamic and static recrystallization than AMg6.

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27

Gololobov, A. V., A. N. Nyafkin, and A. N. Zhabin. "ASPECTS OF STRUCTURE FORMATION DISPERSION-STRENGTHENED METAL COMPOSITE MATERIAL OBTAINED ON THE BASIS OF SHAVINGS AND POWDER OF ALUMINUM CORROSION-RESISTANT ALLOY." Proceedings of VIAM, no. 12 (2021): 39–46. http://dx.doi.org/10.18577/2307-6046-2021-0-12-39-46.

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A metal composite material (MCM) based on an aluminum corrosion-resistant alloy of the AMg6 brand, containing 22.5 % (vol.) Silicon carbide, obtained by mechanical alloying, has been investigated. Aspects of the formation of the MCM structure based on chips and powder from this alloy are considered. The influence of the initial components on the structure of the dispersion-strengthened MCM was investigated, and samples were made from this composite material.

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28

Chernykh, I. K., E. V. Vasil’ev, E. N. Matuzko, and E. V. Krivonos. "UPGRADING WELD QUALITY OF A FRICTION STIR WELDED ALUMINUM ALLOYS AMG6." Dynamics of Systems, Mechanisms and Machines 5, no. 1 (2017): 113–20. http://dx.doi.org/10.25206/2310-9793-2017-5-1-113-120.

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29

Lobanov, L. M., M. O. Pashchyn, O. M. Tymoshenko, P. V. Goncharov, O. L. Mikhoduj, and K. V. Shiyan. "Increase in the life of welded joints of AMG6 aluminum alloy." Avtomatičeskaâ svarka (Kiev) 2020, no. 4 (April 28, 2020): 3–10. http://dx.doi.org/10.37434/as2020.04.01.

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30

Zhdanov, I. M., V. N. Nifantov, B. V. Medko, and S. L. Dykhno. "Relaxation of the stresses in welded joints in AMg6 alloy sheet." Welding International 1, no. 2 (January 1987): 125–27. http://dx.doi.org/10.1080/09507118709452097.

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31

Velichko, O. A. "Welding T joints in AMg6 aluminium-magnesium alloy with a CO2laser." Welding International 2, no. 5 (January 1988): 406–9. http://dx.doi.org/10.1080/09507118809447487.

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32

Chernykh, I. K., E. V. Vasil’ev, E. N. Matuzko, and E. V. Krivonos. "Upgrading weld quality of a friction stir welded aluminum alloys AMG6." Journal of Physics: Conference Series 944 (January 2018): 012025. http://dx.doi.org/10.1088/1742-6596/944/1/012025.

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33

Volkov, A. D., A. I. Kokshaiskii, A. I. Korobov, and V. M. Prokhorov. "Second- and third-order elastic coefficients in polycrystalline aluminum alloy AMg6." Acoustical Physics 61, no. 6 (November 2015): 651–56. http://dx.doi.org/10.1134/s1063771015060147.

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34

Krushenko, G. G., and A. S. Mishin. "Welding sheets of AMg6 alloy with a rod containing ultrafine powders." Welding International 9, no. 8 (January 1995): 649–50. http://dx.doi.org/10.1080/09507119509548869.

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35

Zubchaninov, V. G., and Dzh Al'-Delemi Saadi. "Experimental investigation of the processes of complex loading of alloy AMg6." Strength of Materials 25, no. 5 (May 1993): 342–47. http://dx.doi.org/10.1007/bf00772953.

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36

Golubev, V. K., A. I. Korshunov, S. A. Novikov, Yu S. Sobolev, and N. A. Yukina. "Strength and failure of aluminum alloy AMg6 with shock-wave loading." Journal of Applied Mechanics and Technical Physics 29, no. 2 (1988): 274–80. http://dx.doi.org/10.1007/bf00908594.

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37

Shtrikman, M. M., V. A. Polovtsev, G. V. Shillo, N. V. Makarov, and A. N. Sabantsev. "Friction welding sheet structures made of 1201 and AMg6 aluminium alloys." Welding International 18, no. 9 (September 2004): 742–47. http://dx.doi.org/10.1533/wint.2004.3359.

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38

Belov, D. V., S. N. Belyaev, M. V. Maksimov, and G. A. Gevorgyan. "On mechanism of biocorrosion of aluminum alloys D16T and AMg6 (Review)." Corrosion: Materials, Protection, no. 10 (October 21, 2021): 1–22. http://dx.doi.org/10.31044/1813-7016-2021-0-10-1-22.

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39

Lobanov, L. M., N. A. Pashchin, A. N. Timoshenko, O. L. Mikhoduj, P. V. Goncharov, and A. V. Cherkashin. "Influence of parameters of electrodynamic treatment on residual stresses of welded joints of alloy AMg6." Paton Welding Journal 2019, no. 4 (April 28, 2019): 2–4. http://dx.doi.org/10.15407/tpwj2019.04.01.

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40

Савельева, Н. В., Ю. В. Баяндин, А. С. Савиных, Г. В. Гаркушин, С. В. Разоренов та О. Б. Наймарк. "Формирование упругопластических фронтов и откольное разрушение в сплаве АМг6 при ударных воздействиях". Письма в журнал технической физики 44, № 18 (2018): 39. http://dx.doi.org/10.21883/pjtf.2018.18.46610.17411.

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Анотація:

AbstractFull wave profiles were monitored by the laser interferometry method by means of a VISAR laser Doppler velocimeter under shock-wave loading of samples of AMg6 aluminum alloy. Analysis of these profiles was used to study the laws of elastic precursor formation and its amplitude variation during elastic–plastic transition front propagation in samples loaded by a shock wave of variable intensity. Critical stresses leading to the spall fracture of samples were determined as dependent on the strain rate under unloading.

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41

Kaisheva, D., V. Angelov, and P. Petrov. "Simulation of heat transfer at welding with oscillating electron beam." Canadian Journal of Physics 97, no. 10 (October 2019): 1140–46. http://dx.doi.org/10.1139/cjp-2018-0495.

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This work presents a numerical model of the temperature distribution during electron beam welding, performed by circular and elliptical beam oscillation. The numerical calculations have been done using Green’s functions. A method of finding the dependence between the source power and the weld’s depth is proposed. We present the calculated temperature distribution in electron beam welded aluminium alloy AMg6 with circular and elliptical oscillating beam for different technological parameters. The experimental shape of the weld and the calculated one show a good correspondence.

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42

Potapov, V. V., V. P. Kolmakov, and L. M. Chebotnyagin. "The algorithm of constructor and technological." E3S Web of Conferences 114 (2019): 03007. http://dx.doi.org/10.1051/e3sconf/201911403007.

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On the basis of the pulse-pressure model of the velocity-induced de-formation of metal pipes proposed by the authors [1] the expanding plas-ma channel of an electric spark, the influence of the collision angle and the contact point speed on the quality of welding of pipes with a tube grid of a heat exchanger were investigated. An algorithm for estimating welding zones is proposed. The applicability of the algorithm is tested on pairs of pipe made of alloy AD1 + tube made of alloy AMg6.

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43

Anikin, К. A., A. V. Apelfeld, and I. O. Kondratskiy. "Study of influence of micro-arc oxidation process duration on the characteristics of thermal control coatings for space applications." Journal of Physics: Conference Series 2144, no. 1 (December 1, 2021): 012006. http://dx.doi.org/10.1088/1742-6596/2144/1/012006.

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Анотація:

Abstract Thermal control coatings were obtained on the AMg6 aluminum alloy with the aid of micro-arc oxidation (MAO) process. The dependences of the thickness, roughness, porosity and thermal control properties of the coating on MAO process duration were studied. The thermal control properties (solar absorbance αs and emissivity ε) were investigated by ultraviolet–visible-near infrared spectrophotometer instrument and solar absorption reflectometer. The analysis of thickness, roughness and MAO process duration influence on the thermal control properties of the coating was carried out.

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44

Efremov, Denis, Sergei Uvarov, Lev Spivak, and Oleg Naimark. "Statistical patterns of deformation localization during plastic flow in the AMg6 alloy." Letters on Materials 10, no. 1 (2020): 38–42. http://dx.doi.org/10.22226/2410-3535-2020-1-38-42.

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45

Shibkov, A. A., A. E. Zolotov, and M. A. Zheltov. "Acoustic precursor of unstable plastic deformation in the aluminum-magnesium alloy AMg6." Physics of the Solid State 52, no. 11 (November 2010): 2376–84. http://dx.doi.org/10.1134/s1063783410110259.

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46

Zubchaninov, V. G., and V. V. Garanikov. "Effect of material unloading on the creep of alloys 01570 and AMg6." Strength of Materials 22, no. 9 (September 1990): 1286–88. http://dx.doi.org/10.1007/bf00770968.

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47

Polovtsev, V. A., M. M. Shtrikman, G. V. Shillo, N. V. Makarov, N. S. Barabokhin, V. E. Silis, and P. V. Zagreev. "Service characteristics of friction welded joints in 1201 and AMg6 aluminium alloys." Welding International 20, no. 5 (May 2006): 390–94. http://dx.doi.org/10.1533/wint.2006.3637.

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48

Bakulin, I. A., N. G. Kakovkina, S. I. Kuznetsov, A. S. Panin, and E. Yu Tarasova. "Structure and Residual Stresses in the AMg6 Alloy after Laser Shock Processing." Inorganic Materials: Applied Research 12, no. 1 (January 2021): 55–60. http://dx.doi.org/10.1134/s2075113321010032.

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49

Polunin, A. V., A. G. Denisova, A. O. Cheretaeva, M. R. Shafeev, E. D. Borgardt, I. A. Rastegaev, and A. V. Katsman. "The effect of process current parameters on the properties of oxide layers under plasma electrolytic oxidation of AMg6 alloy." Journal of Physics: Conference Series 2144, no. 1 (December 1, 2021): 012018. http://dx.doi.org/10.1088/1742-6596/2144/1/012018.

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Abstract The effect of current density and current ratio in the cathodic and anodic half-cycles during prolonged (180 minutes) plasma electrolytic oxidation (PEO) of AMg6 wrought alloy on the oxide layer wear and corrosion resistance were studied. It was established that the best wear resistance is achieved in the oxide layers obtained in the “soft sparking” mode (negative-to-positive pulse ratios of 1.15–1.30) at current densities of 9–15 A dm−2, and the best set of wear resistance and corrosion resistance – in the oxide layers obtained in “symmetrical” mode (negative-to-positive pulse ratio of 1.00).

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50

Yasniy, Oleh, Iryna Didych, Sergiy Fedak, and Yuri Lapusta. "Modeling of AMg6 aluminum alloy jump-like deformation properties by machine learning methods." Procedia Structural Integrity 28 (2020): 1392–98. http://dx.doi.org/10.1016/j.prostr.2020.10.110.

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