The mechanical properties of pressings from alloy 1960 in state T1 are determined at 20, 55, 60 and 65°C. Samples of pressings from alloy 1960 in state T1 are tested for creep resistance for up to 5000 h at 55, 60 and 65°C at a stress of 295, 390 and 440 MPa. The creep rate and the deformation of the samples are determined. It is shown that increase of the temperature to 65°C in the tensile tests lowers the strength characteristics of the pressings by 20 – 40 MPa. Increase of the temperature and of the stress in the creep tests elevates the creep rate of the pressings.
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The work has been performed using the equipment of the “Clima- tic Tests” common access center of the Kurchatov Institute – VIAM Research Center.
References
I. N. Fridlyander, O. G. Senatorova, E. A. Tkachenko, and I. I. Molostova, “Development an application of high strength alloys of the Al – Zn – Mg – Cu system for aerospace engineering,” in: 75 Years. Aviation Materials [in Russian], VIAM, Moscow (2007), pp. 155 – 163.
V. V. Antipov, “Prospects of development of aluminum, magnesium and titanium alloys for articles of aerospace engineering,” Aviats. Mater. Tekhnol., No. S, 186 – 194 (2017); DOI: https://doi.org/10.18577/2071-9140-2017-0-S-186-194.
E. N. Kablov, “New-generation materials and digital technologies of their processing,” Vest. Ross. Akad. Nauk, 90(4), 331 – 334 (2020).
I. N. Fridlyander, O. G. Senatorova, and E. A. Tkachenko, “High-strength alloys of the Al – Zn – Mg – Cu system,” in: Machine Building: Encyclopedia in 40 Vols., V. II-3. Nonferrous Metals and Alloys. Composite Metallic Materials [in Russian], Mashinostroenie, Moscow (2001), pp. 94 – 128.
I. N. Fridlyander, Creation, Investigation and Application of Aluminum Alloys, Selected Works on the 100th Anniversary [in Russian], Nauka, Moscow (2013), 291 p.
I. N. Fridlyander, Reminiscences on Creation of Aerospace and Nuclear Machinery from Aluminum Alloys [in Russian], Nauka, Moscow (2005), 276 p.
O. G. Senatorova, V. V. Antipov, A. V. Bronz, et al., “High-strength and super-high-strength alloys of the traditional Al – Zn – Mg – Cu system, their role in engineering and possibilities of development,” Tekhnol. Legk. Splavov, No. 2, 43 – 49 (2016).
V. V. Antipov, O. G. Senatorova, E. A. Tkachenko, and R. O. Vakhromov, “Aluminum deformable alloys,” Aviats. Mater. Tekhnol., No. S, 167 – 182 (2012).
E. N. Kablov, “Principal directions of development of materials for aerospace engineering in century XXI,” Perspekt. Mater., No. 3, 27 – 36 (2000).
E. N. Kablov (ed.), “History of the science of aviation materials: VIAM – 75 years of search, creativity and discoveries,” in: Deformable Aluminum Alloys [in Russian], Nauka, Moscow (2007), pp. 77 – 86.
T. A. Nechaikina, N. E. Blinova, A. L. Ivanov, et al., “A study of the effect of homogenization and quenching modes on the structure and mechanical properties of forging rolls from alloy V95o.ch.-T2,” Trudy VIAM, Electron. Nauch.-Tekh. Zh., No. 10, 04 (2018); URL: http://www.viam-works.ru.
A. I. Astashkin, V. V. Babanov, A. A. Selivanov, and E. A. Tkachenko, “Structure and properties of massive pressings with reduced level of residual stresses from aluminum alloy 1933sb with balanced composition,” Trudy VIAM, Electron. Nauch.-Tekh. Zh., No. 7, 02 (2021); URL: http://www.viam-works.ru.
T. A. Nechaikina, M. S. Oglodkov, A. L. Ivanov, et al., “Special features of quenching of wide clad cover plates from aluminum alloy V95p.ch. in the line for continuous heat treatment,” Trudy VIAM, Electron. Nauch.-Tekh. Zh., No. 11, 03 (2021); URL: http://www.viam-works.ru.
A. N. Astashkin, V. V. Babanov, A. A. Selivanov, et al., “Improvement of the hardenability of massive forgings from alloys of the Al – Zn – Mg – Cu system by balanced alloying with zinc and magnesium,” Aviats. Mater. Tekhnol., Electron. Nauch.-Tekh. Zh., No. 2, 04 (2021).
E. I. Abbakumov, V. A. Bazhenov, and Yu. V. Verbin, “Development and commercial application of gas centrifuges for enrichment of uranium in the USSR,” Atom. Energ., 67(4), 255 – 257 (1998), UDC 621.039.031.
A. P. Gergert, I. I. Molostova, and D. K. Ryabov, “Advancement of alloy 1960 for gas centrifuges,” Tsvetn. Met., No. 9, 33 – 36 (2013).
L. I. Kaigorodova, E. I. Sel’nikhina, E. A. Tkachenko, and O. G. Senatorova,” “Effect of low additions of scandium and zirconium on the structure and mechanical properties of alloy Al – Zn – Mg – Cu,” Fiz. Met. Metalloved., 81(5), 75 – 86 (1996).
A. E. Semenov, N. S. Korzina, and V. V. Solov’eva, “Intermetallic compounds in articles from alloy V96ts,” in: Structural Alloys [in Russian], Metallurgiya, Moscow (1968), No. 5, pp. 21 – 25.
Z. N. Archakova, G. A. Balakhontsev, and I. G. Basova, Structure and Properties of Semiproducts from Aluminum Alloys [in Russian], Metallurgiya, Moscow (1984), 408 p.
V. M. Rozenberg, Creep of Metals [in Russian], Metallurgiya, Moscow (1967), 276 p.
OST 1 90048–90. Aluminum Deformable Alloys. Grades [in Russian].
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Translated from Metallovedenie i Termicheskaya Obrabotka Metallov, No. 4, pp. 46 – 50, April, 2023.
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Shlyapnikova, T.A., Oglodkov, M.S., Blinova, N.E. et al. Creep Rate of Pressings from High-Strength Aluminum Alloy 1960 (V96ts). Met Sci Heat Treat 65, 233–237 (2023). https://doi.org/10.1007/s11041-023-00919-w
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DOI: https://doi.org/10.1007/s11041-023-00919-w