Last number

№3 2024

dx.doi.org/ 10.18577/2307-6046-2024-0-3-3-17

УДК 669.018.28

Bazyleva O.A., Rimsha E.G., Chabina E.B., Raevskih A.N.

SOME ASPECTS OF CREATION AND RESEARCH OF STRUCTURAL CASTING INTERMETALLIDE ALLOYS FOR PROMISING HELICOPTER ENGINES

The article presents the calculation of the chemical composition of the intermetallic composition based on the Ni₃Al compound using the doping balance formula, while the average electron concentration is the number of valence electrons per unit atomic mass of the composition; studies of structural and phase transformations in an intermetallic alloy based on Ni3Al depending on high-temperature treatment and during long-term tests at temperatures of 1150, 1200 and 1250 °С. The constructability of the structural alloy was experimentally established when testing the casting of blanks of the nozzle blades of the compressor turbine of a promising helicopter engine.

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Reference list

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32. Bazyleva O.A., Arginbaeva E.G., Chabina E.B., Raevskikh A.N. Study of structural-phase transformations in a cast structural alloy based on the Ni3Al intermetallic compound after high-temperature holding and during the process of operating the alloy as a nozzle blade. Voprosy materialovedeniya, 2023, vol. 114, no. 2, pp. 60–70.
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36. Chabina E.B., Alekseev A.A., Filonova E.V., Lukinа E.A. The use of methods of analytical microscopy and x-ray diffraction analysis for the study of the structural phase state materials. Trudy VIAM, 2013, no. 5, paper no. 06. Available at: http://www.viam-works.ru (accessed: November 27, 2023).
37. Kablov E.N. Innovative developments of FSUE «VIAM» SSC of RF on realization of «Strategic directions of the development of materials and technologies of their processing for the period until 2030». Aviacionnye materialy i tehnologii, 2015, no. 1 (34), pp. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-3.

dx.doi.org/ 10.18577/2307-6046-2024-0-3-18-29

УДК 621.7

Yashin M.S., Bazhenov A.R.

INVESTIGATION OF THERMOMECHANICAL PARAMETERS OF DEFORMATION AND MECHANICAL PROPERTIES DEPENDING ON CONDITIONS OF DEFORMATION OF TITANIUM ALLOY VT30

Technological plasticity, deformation mechanisms and dependence between mechanical properties and the conditions of deformation of titanium alloy VT30 were studied in present work. Samples in cast and forged states were examined. The samples were deformed on a pile driver and press at different temperatures, also forging and stamping were carried out. The results showed that the VT30 alloy has better properties in the forged state. In addition, optimal conditions for pressure treatment of titanium alloy VT30 were obtained.

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Reference list

1. Kablov E.N. Innovative developments of FSUE «VIAM» SSC of RF on realization of «Strategic directions of the development of materials and technologies of their processing for the period until 2030». Aviacionnye materialy i tehnologii, 2015, no. 1 (34), pp. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
2. Kablov E.N., Bakradze M.M., Gromov V.I., Voznesenskaya N.M., Yakusheva N.A. New high strength structural and corrosion-resistant steels for aerospace equipment developed by FSUE «VIAM» (review). Aviacionnye materialy i tehnologii, 2020, no. 1 (58), pp. 3–11. DOI: 10.18577/2071-9140-2020-0-1-3-11.
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14. Dzunovich D.A., Lukina E.A., Yakovlev A.L. Influence of heat treatment parameters on producibility and mechanical properties of sheets made from high-strength titanium alloy VT23. Aviacionnye materialy i tehnologii, 2018, no. 3 (52), pp. 3–10. DOI: 10.18577/2071-9140-2018-0-3-3-10.
15. Duyunova V.A., Oglodkov M.S., Putyrskiy S.V., Kochetkov A.S., Zueva O.V. Modern technologies for melting titanium alloy ingots (review). Aviation materials and technologies, 2022, no. 1 (66), paper no. 03. Available at: http://www.journal.viam.ru (accessed: December 22, 2023). DOI: 10.18577/2713-0193-2022-0-1-30-40.
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17. Krokhina V.A., Arislanov А.A., Putyrskiy S.V., Anisimova A.Yu. Investigation of the regularities of the formation of the structure of rods made of titanium alloy VT6 depending on various technological schemes of manufacture. Aviation materials and technologies, 2023, no. 4 (73), paper no. 04. Available at: http://www.journal.viam.ru (accessed: December 22, 2023). DOI: 10.18577/2713-0193-2023-0-4-36-44.

dx.doi.org/ 10.18577/2307-6046-2024-0-3-30-40

УДК 621.791.14: 621.791.724

Panteleev M.D., Odintsov N.S., Bondarenko S.V., Sviridov A.V.

SURVIVABILITY OF WELDED FUSELAGE ELEMENTS MADE OF HEAT-RESISTANT ALUMINUM ALLOYS V-1213 AND 1151

In this work static and fatigue characteristics of welded joints of heat-resistant aluminum alloys V-1213 and 1151 were studied. Mechanical and service-life tests of flat welded structurally similar samples of fuselage elements made of heat-resistant aluminum alloys V-1213 and 1151 welded by laser-beam welding and friction stir welding were carried out. The assessment of the survivability of welded joints was evaluated with introduced stress concentrators. Comparative assessment of cyclic durability to failure was made on structurally similar welded samples.

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Reference list

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dx.doi.org/ 10.18577/2307-6046-2024-0-3-41-51

УДК 621.355

Leonov A.A., Trofimov N.V.

MAGNESIUM ION BATTERIES: PROSPECTS AND CHALLENGES IN THE FIELD OF ENERGY

New type of the energy carrier include magnesium-ion batteries, which represents potentially more effective and ecologically safe alternative to existing storage technologies. The main types of anode, cathode and electrolyte materials for magnesium-ion batteries, ensuring efficient transfer of Mg²⁺ cations and possible cyclic durability, are considered. In the article advantages and disadvantages of this technology, its potential for application in different areas also are analyzed.

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Reference list

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17. Fomina M.A., Volkov I.A., Vdovin A.I., Yamshchikov E.I. Study of protective capacity anodic oxide coating with environmental friendly improved filling technology. Aviation materials and technologies, 2023, no. 4 (73), paper no. 10. Available at: http://www.journal.viam.ru (accessed: January 16, 2024). DOI: 10.18577/2713-0193-2023-0-4-101-110.
18. Shi M., Li T., Shang H. et al. A critical review of inorganic cathode materials for rechargeable magnesium ion batteries. Journal of Energy Storage, 2023, no. 68, pp. 216–228.
19. Deivanayagam R., Ingram B.J., Shahbazian-Yassar R. Progress in development of electrolytes for magnesium batteries. Energy Storage Materials, 2019, no. 21, pp. 136–153.
20. Ma B., Ouyang L., Zheng J. Magnesium-rare earth intermetallic compounds for high performance high power aqueous Magnesium-Air batteries. Journal of Magnesium and Alloys, 2023, no. 4, рр. 76–90. DOI: 10.1016/j.jma.2023.06.010.
21. Lia Q., Xiong W., Yu M. et al. Effect of Ce content on performance of AZ31 magnesium alloy anode in air battery. Journal of Alloys and Compounds, 2021, vol. 891 (4), pp. 132–141. DOI:10.1016/j.jallcom.2021.161914.
22. Kablov E.N., Akinina M.V., Volkova E.F., Mostyaev I.V., Leonov A.A. The research of aspects of phase composition and fine structure of magnesium alloy ML9 in the as-cast and heat-treated conditions. Aviacionnye materialy i tehnologii, 2020, no. 2 (59), pp. 17–24. DOI: 10.18577/2071-9140-2020-0-2-17-24.
23. Miao X., Yang J., Pan W. et al. Graphite fluoride as a cathode material for primary magnesium batteries with high energy density. Electrochimica Acta, 2016, vol. 210, pp. 704–711.
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25. Lee M., Jeong M., Nam Y.S. et al. Nitrogen-doped graphitic mesoporous carbon materials as effective sulfur imbibition hosts for magnesium-sulfur batteries. Journal of Power Sources, 2022, vol. 535, pp. 444–462.
26. Mana Y., Jaumaux P., Xu Y. et al. Research development on electrolytes for magnesium-ion batteries. Science Bulletin, 2023, no. 68, pp. 1819–1842.
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28. Higashi S., Miwa K., Aoki M., Takechi K. A novel inorganic solid-state ion conductor for rechargeable Mg batteries. ChemCommun, 2014, no. 50, pp. 1320–1322. DOI: 10.1039/c3cc47097k.
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33. Kotobuki M., Yan B., Lu L. Recent progress on cathode materials for rechargeable magnesium batteries. Energy Storage Materials, 2023, vol. 54, pp. 227–253.
34. Voronov V.A., Chaynikova A.S., Tkalenko D.M. Aspects of usage of organic or aqueous binders based on III or IV group elements oxides in the production of ceramic molds for chemically active alloys casting (review). Aviation materials and technologies, 2021, no. 2 (63), paper no. 08. Available at: http://www.journal.viam.ru (accessed: January 22, 2024). DOI: 10.18577/2713-0193-2021-0-2-73-84.
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36. Kozlov I.A., Vinogradov S.S., Tarasova K.G., Kulyushina N.V., Manchenko V.A. Plasma electrolytic oxidation of magnesium alloys (review). Aviacionnye materialy i tehnologii, 2019, no. 1 (54), pp. 23–36. DOI: 10.18577/2071-9140-2019-0-1-23-36.
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dx.doi.org/ 10.18577/2307-6046-2024-0-3-52-62

УДК 678.8

Guseva M.A., Ibragimov Z.D.

SELECTION OF CURING SYSTEM WHEN DEVELOPING EPOXY COMPOSITIONS WITH ENERGY-EFFICIENT CURING MODE

Polymer binders with an energy-efficient curing mode are compositions containing hardeners and curing accelerators that are capable of curing the polymer system at low temperatures (120–150 °C), with minimal time, while maintaining the increased strength and thermomechanical characteristics of PCM, derived from it. This paper presents a technology for the development of a polymer binder with selection of a curing system to obtain an epoxy composition with an energy-efficient curing mode as part of import substitution issues.

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Reference list

1. Panina N.N., Kim M.A., Gurevich Ya.M., Grigoriev M.M., Chursova L.V., Babin A.N. Binders for non-autoclave molding of products from polymer composite materials. Klei. Germetiki. Tekhnologii, 2013, no. 10, pp. 18–27.
2. Veshkin E.A., Postnov V.I., Abramov P.A. Ways to improve the quality of PCM parts during vacuum forming. Izvestiya Samarskogo nauchnogo tsentra Rossiyskoy akademii nauk, 2012, vol. 14, no. 4 (3), pp. 831–838.
3. Postnova M.V., Postnov V.I. Development experience out-of-autoclave methods of formation PCM. Trudy VIAM, 2014, no. 4, paper no. 06. Available at: http://viam-works.ru (accessed: January 10, 2024). DOI: 10.18577/2307-6046-2014-0-4-6-6.
4. Khrulkov A.V., Grigoriev M.M. Prospects for the market for non-autoclave technologies in the aircraft industry. Reports conf. «Non-autoclave technologies for processing new generation polymer composite materials». Moscow: VIAM, 2015, paper no. 09.
5. Veshkin E.A. Technologies for non-autoclave molding of low-porosity polymer composite materials and large-sized structures made from them: thesis, Cand. Sc. (Tech.). Moscow, 2016, 146 p.
6 Trostyanskaya E.B., Mikhailin Yu.A., Kulik S.G., Stepanova M.A. Binders based on epoxy resins: textbook. Moscow, 1990, p. 27.
7. Kogan D.I., Chursova L.V., Panina N.N. et al. Promising polymer materials for structural composite products with energy-efficient molding mode. Plasticheskie massy, 2020, no. 3–4, pp. 52–54.
8. Ivanov N.V., Gurevich Ya.M., Khaskov M.A., Akmeev A.R. Studying of cure mode of VSE-34 binding and its influences on mechanical properties. Aviacionnye materialy i tehnologii, 2017, no. 2 (47), pp. 50–55. DOI: 10.18577/2071-9140-2017-0-2-50-55.
9. Mukhametov R.R., Petrova A.P. Thermosetting binders for polymer composite materials: textbook. Ed. E.N. Kablov. Moscow: NRC «Kurchatov Institute» – VIAM, 2021, p. 363.
10. Kablov E.N. Strategical Areas of Developing Materials and Their Processing Technologies for the Period up to 2030. Aviacionnye materialy i tehnologii, 2012, no. S, pp. 7–17.
11. Kablov E.N., Kondrashov S.V., Melnikov A.A., Schur P.A. Application of functional and adaptive materials obtained by 3D printing (review). Trudy VIAM, 2022, no. 2 (108), paper no. 03. Available at: http://www.viam-works.ru (accessed: November 20, 2023). DOI: 10.18577/2307-6046-2022-0-2-3-3.
12. Mishkin S.I., Malakhovskiy S.S. Fast curing resins and prepregs: receiving, properties and areas of application (review). Trudy VIAM, 2019, no. 5 (77), paper no. 04. Available at: http://viam-works.ru (accessed: November 10, 2023). DOI: 10.18577/2307-6046-2019-0-5-32-40.
13. Donetskiy K.I., Khrulkov A.V. Principles of «green chemistry» in perspective manufacturing technologies of PCM articles. Aviacionnye materialy i tehnologii, 2014, no. S2, pp. 24–28. DOI: 10.18577/2071-9140-2014-0-S2-24-28.
14. Bolshakov V.A., Antyufeeva N.V. Evaluation of the curing process model of the adhesive binder in prepreg. Aviation materials and technologies, 2023, no. 4 (73), paper no. 07. Available at: http://www.journal.viam.ru (accessed: November 25, 2023). DOI: 10.18577/2713-0193-2023-0-4-66-77.
15. Startsev V.O., Antipov V.V., Slavin A.V., Gorbovets M.A. Modern domestic polymer composite materials for aviation industry (review). Aviation materials and technologies, 2023, no. 2 (71), paper no. 10. Available at: http://www.journal.viam.ru (accessed: November 15, 2023). DOI: 10.18577/2713-0193-2023-0-2-122-144.

dx.doi.org/ 10.18577/2307-6046-2024-0-3-63-75

УДК 669.018.95

Nyafkin A.N., Zhabin A.N., Avtaev V.V.

CRACK PROPAGATION IN COMPOSITE MATERIALS OF THE Al‒SiC SYSTEM UNDER CYCLIC LOADS

The review presents the features of fatigue crack propagation in composite materials (CM) based on aluminum alloys reinforced with silicon carbide (SiC) particles with different volume content under cyclic loading conditions. The influence of the volume content and size of SiC particles on the growth rate of a fatigue crack in CM under the action of cyclic loads is considered. The results of studying the influence of the CM structure on the growth rate and development of cracks during cyclic tests are presented.

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Reference list

1. Kablov E.N. Marketing of materials science, aircraft engineering and industry: present and future. Direktor po marketingu i sbytu, 2017, no. 5–6, pp. 40–44.
2. Kablov E.N. Composites: today and tomorrow. Metally Evrazii, 2015, no. 1, pp. 36–39.
3. Kablov E.N. The key problem is materials. Trends and guidelines for innovative development of Russia. Moscow: VIAM, 2015, pp. 458–464.
4. Grashchenkov D.V. Strategy of development of non-metallic materials, metal composite materials and heat-shielding. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 264–271. DOI: 10.18577/2071-9140-2017-0-S-264-271.
5. Antipov V.V. Prospects for development of aluminium, magnesium and titanium alloys for aerospace engineering. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 186–194. DOI: 10.18577/2071-9140-2017-0-S-186-194.
6. Kosolapov D.V., Shavnev A.A., Kurbatkina E.I., Nyafkin A.N., Gololobov A.V. Study on structure and properties of dispersion hardened mmc based on aluminium alloy of Al–Mg–Si system. Trudy VIAM, 2020, no. 1 (85), paper no. 06. Available at: http://www.viam-works.ru (accessed: December 12, 2022). DOI: 10.18577/2307-6046-2020-0-1-58-67.
7. Shavnev A.A., Kurbatkina E.I., Nyafkin A.N., Kosolapov D.V. Technologies for manufacturing dispersion-strengthened metal composite material based on aluminum alloy (review). Materialovedenie, 2022, no. 4, pp. 42–48. DOI: 10.31044/1684-579X-2022-0-4-42-48.
8. Певчев Д.И., Горбовец М.А., Рыжков П.В., Курбаткина Е.И. Исследование характеристик прочности дисперсноупрочненного металлического композиционного материала марки ВКМ22. Trudy VIAM, 2021, no. 2 (96), paper no. 04. Available at: http://www.viam-works.ru (accessed: December 12, 2022). DOI: 10.18577/2307-6046-2021-0-2-30-38.
9. Milan M.T., Bowen P. Fatigue сrack growth resistance of SiCp reinforced Al alloys: effects of particle size, particle volume fraction, and matrix strength. Journal of Materials Engineering and Performance, 2004, vol. 13, pp. 612–618. DOI: 10.1361/10599490420638.
10. Mason J.J., Ritchie R.O. Fatigue crack growth resistance in SiC particulate and whisker reinforced P/M 2124 aluminum matrix composites. Materials Science and Engineering A, 1997, vol. 231, pp. 170–182. DOI: 10.1016/S0921-5093(97)00086-5.
11. Lia W., Liang H., Chen J. et al. Effect of SiC particles on fatigue crack growth behavior of SiC particulate-reinforced Al‒Si alloy composites produced by spray forming. Procedia Materials Science, 2014, vol. 3, pp. 1694–1699. DOI: 10.1016/j.mspro.2014.06.273.
12. Xu F.M., Zhu S.J., Zhao J.L. et al. Fatigue crack growth in SiC particulates reinforced Al matrix graded composite. Materials Science and Engineering A, 2003, vol. 360, pp. 191–196. DOI: 10.1016/S0921-5093(03)00397-6.
13. Uzun H., Lindley T.C., McShane H.B., Rawlings R.D. Fatigue crack growth behavior of 2124/SiC/10p functionally graded materials. Metallurgical and Materials Transactions A, 2001, vol. 32A, pp. 1831–1839. DOI: 10.1007/s11661-001-0159-x.
14. Chena Z.Z., Tokaji K. Effects of particle size on fatigue crack initiation and small crack growth in SiC particulate-reinforced aluminium alloy composites. Materials Letters, 2004, vol. 58, pp. 2314–2321. DOI: 10.1016/j.matlet.2004.02.034.
15. Li K., Jin X.D., Yan B.D., Li P.X. Effect of SiC particles on fatigue crack propagation in SiC/Al composites. Composites, 1992, vol. 23, no. 1, pp. 54–58. DOI: 10.1016/0010-4361(92)90286-4.
16. Bruzzi M.S., McHugh P.E. Micromechanical investigation of the fatigue crack growth behaviour of Al–SiC MMCs. International Journal of Fatigue, 2004, vol. 26, pp. 795–804. DOI: 10.1016/j.ijfatigue.2004.01.007.
17. Nyafkin A.N., Loshinin U.V., Kurbatkina E.I., Kosolapov D.V. Investigation of influence of silicon carbide fractional composition on thermal conductivity of composite material based on aluminium alloy. Trudy VIAM, 2019, no. 11 (83), paper no. 06. Available at: http://www.viam-works.ru (accessed: December 20, 2022). DOI: 10.18577/2307-6046-2019-0-11-53-59.
18. Erasov V.S., Oreshko E.I. Fatigue tests of metal materials (review). Part 1. Main definitions, loading parameters, representation of results of tests. Aviacionnye materialy i tehnologii, 2020, no. 4 (61), pp. 59–70. DOI: 10.18577/2071-9140-2020-0-4-59-70.
19. Andrew O.N., Joel O.O., Murray A.O., Eruke U.J. Effect of Compaction on Thermal Conductivity of Aluminium Powder. International Journal of Emerging Engineering Research and Technology, 2018, vol. 6, is. 2, pp. 1–5.
20. Verma R.K., Mahesh N.S., Anwar M.I. Numerical Analysis of Powder Compaction to Obtain High Relative Density in ‘601AB' Aluminum Powder. SasTech Journal, 2012, vol. 11, is. 1, pp. 79–84.
21. Sevostianov I., Kachanov M. Nanoparticle reinforced materials: Effect of interphase layers on the overall properties. International Journal of Solids and Structures, 2007, vol. 44, is. 3–4, pp. 1304–1315. DOI: 10.1016/j.ijsolstr.2006.06.020.

dx.doi.org/ 10.18577/2307-6046-2024-0-3-76-90

УДК 661.177

Sedova L.S., Shestakov A.M.

FOREIGN HYDROLIQUIDS, APPLIED IN CIVIL AVIATION OF THE RUSSIAN FEDERATION

Information on the foreign hydroliquids applied in the territory of the Russian Federation in civil aviation is provided. Properties of foreign hydroliquids are given: Skydrol LD-4, Skydrol 500B-4, Nyjet-IV-A^plus, AeroShell Fluid 41, Mobil Aero HF, Hydraunycoil FH 51, ROYCO 756, Nycolube 934. Data on the Russian analogs are provided: working fluids 7-50C-3 and NGZh-5U, oils AMG-10 and MGE-10A. Characteristics of domestic hydroliquids in comparison with import analogs are provided. Information on available foreign patent researches is specified.

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Reference list

1. Kablov E.N. All-Russian Institute of Aviation Materials is 80 years old. Deformatsiya i razrushenie materialov, 2012, no. 6, pp. 17–19.
2. Kablov E.N. Strategical areas of developing materials and their processing technologies for the period up to 2030. Aviacionnye materialy i tehnologii, 2012, no. S, pp. 7–17.
3. Kablov E.N. Modern materials – the basis of innovative modernization of Russia. Metally Evrazii, 2012, no. 3, pp. 10–15.
4. Buznik V.M., Kablov E.N. State and prospects of Arctic materials science. Vestnik RAN, 2017, vol. 87, no. 9, pp. 827–839.
5. Kablov E.N. The role of chemistry in the creation of new generation materials for complex technical systems. Reports of XX Mendeleev Congress on General and Applied Chemistry. Ekaterinburg: UB of the RAS, 2016, pp. 25–26.
6. Buznik V.M., Kablov E.N. Technologies for obtaining and adapting materials for use in the Arctic. Reports of satellite conference «V International Conference-School on Chemical Technology» of the XX Mendeleev Congress on General and Applied Chemistry. Volgograd: VolgSTU, 2016, pp. 9–10.
7. Sukhotin A.M., Zotikov V.S., Kazankina A.F. et al. Non-flammable coolants and hydraulic fluids: guide. Leningrad: Khimiya, 1979, 235 p.
8. Konyaev E.A., Nemchikov M.L. Aviation fuels and lubricants: textbook. Moscow: MSTU GA, 2013, pp. 75–79.
9. Kablov E.N., Kutyrev A.E., Vdovin A.I., Kozlov I.A., Afanasyev-Khodykin A.N. The research of possibility of galvanic corrosion in brazed connections used in aviation engine construction. Aviation materials and technologies, 2021, no. 4 (65), paper no. 01. Available at: http://www.journal.viam.ru (accessed: September 25, 2023). DOI: 10.18577/2713-0193-2021-0-4-3-13.
10. Tarasova P.N., Sleptsova S.A., Laukkanen S., Dyakonov A.A. Sealing materials based on polytetrafluoroethylene for aviation products. Aviation materials and technologies, 2022, no. 1 (66), paper no. 05. Available at: http://www.journal.viam.ru (accessed: September 27, 2023). DOI: 10.18577/2713-0193-2022-0-1-51-64.
11. Kablov E.N., Bakradze M.M., Gromov V.I., Voznesenskaya N.M., Yakusheva N.A. New high strength structural and corrosion-resistant steels for aerospace equipment developed by FSUE «VIAM» (review). Aviacionnye materialy i tehnologii, 2020, no. (58), pp. 3–11. DOI: 10.18577/2071-9140-2020-0-1-3-11.
12. Vetrova E.Yu., Shchekin V.K., Kurs M.G. Comparative evaluation of methods for the determination of corrosion aggressivity of the atmosphere. Aviacionnye materialy i tehnologii, 2019, no. 1 (54), pp. 74–81. DOI: 10.18577/2071-9140-2019-0-1-74-81.
13. Laptev A.B., Barbotko S.L., Nikolaev E.V. The main research areas of the persistence properties of materials under the influence of climatic and operational factors. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 547–561. DOI: 10.18577/2071-9140-2017-0-S-547-561.
14. Vinogradov S.S., Nikiforov A.A., Dyomin S.A., Chesnokov D.V. Protection against corrosion of carbon steel. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 242–263. DOI: 10.18577/2071-9140-2017-0-S-242-263.
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18. Hydraulic fluid X/C 5606J Aviation. Available at: https://us-packaging.ru/phillips66-aviation/catalog/gidravlicheskie-masla/gidravlicheskaya-zhidkost-x-c-5606j-aviation/?ysclid=lpay
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21. Sedova L.S., Dolgova E.V. Production of hydroliquids for aviation engineering in Russia (review) // Trudy VIAM, 2022, no. 8 (114), paper no. 05. Available at: http://www.journal.viam.ru (accessed: September 04, 2023). DOI: 10.18577/2307-6046-2022-0-8-65-76.
22. State Standard 20734–75. Working fluid 7-50С-3. Technical conditions. Moscow: Standards Publishing House, 1975, 4 p.
23. MOP-1313500-01–2021. Interindustry restrictive list of fuels, oils, lubricants, special liquids, conservation materials and additives permitted for use in weapons, military and special equipment. Moscow: 25 GosNII Khimmotologii of the Ministry of Defense of Russia, 2021, pp. 46–50. Available at: https://ens.mil.ru/files/MOP-2021.pdf (accessed: September 25, 2023).
24. State Standard 6794–2017. AMG-10 oil. Technical conditions. Moscow: Standartinform, 2019, 14 p.
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26. Mobil Aero HF aviation hydraulic fluid: properties and characteristics. Available at: https://www.mobil.com/en-us/aviation/pds/gl-xx-mobil-aero-hf-series?ad=semD&an=msn_s&am=modifiedbroad&q=mil+h+5606+hydraulic+fluid&o=29593&qsrc=999&l=sem&askid=22e4232a-71aa-4021-bc7d-7a040b240feb-0-ab_msm (accessed: November 21, 2023).
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30. Hydraulic fluid composition: pat. US 11053448B2; appl. 21.12.17; publ. 06.07.21.
31. Hydraulic fluids from renewable isoparaffins: pat. WO 2015/192072 A1; appl. 12.06.15; publ. 17.12.15.
32. Hydraulic fluid and fuel resistant sealants: pat. US 20190010370 A1; appl. 07.07.17; publ. 10.01.19.
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dx.doi.org/ 10.18577/2307-6046-2024-0-3-91-100

УДК 678.747.2

Starkov A.I., Isaev A.Yu., Kutsevich K.E.

COMPREHENSIVE ASSESSMENT OF THE IMPACT OF OPERATIONAL AND CLIMATIC TESTS ON THE CHANGE OF STRENGTH PROPERTIES OF POLYMER COMPOSITE MATERIALS BASED ON ADHESIVE PREPREGS Part 1. Carbon fiber-reinforced plastic VKU-59

A comprehensive assessment of the retention of strength properties of carbon fiber plastic of the VKU-59 brand under tension, compression, bending, interlayer shear at test temperatures of –60, +20, +80 and +105 °C was carried out in the initial state and after climatic influences in a tropical climate chamber for 1 and 3 months, heat and humidity aging for 1 and 3 months, thermal aging for 500 and 1000 hours. The influence of the mycological environment and process fluids on the tensile strength of carbon fiber reinforced plastic in bending and compression was studied. To confirm the viability, samples of VKU-59 carbon fiber plastic were tested in tension and compression after 3 months of storage.

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Reference list

1. Kablov E.N. Innovative developments of FSUE «VIAM» SSC of RF on realization of «Strategic directions of the development of materials and technologies of their processing for the period until 2030». Aviacionnye materialy i tehnologii, 2015, no. 1 (34), pp. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
2. Kablov E.N. New generation materials and digital technologies for their processing. Vestnik Rossiyskoy akademii nauk, 2020, vol. 90, no. 4, pp. 331–334.
3. Aviation materials: reference book in 13 vols. Ed. E.N. Kablov. 7th ed., proc. and add. Moscow: VIAM, 2019, vol. 10: Adhesives, sealants, rubbers, hydraulic fluids, part 1: Adhesives, adhesive prepregs. 276 p.
4. Kablov E.N., Startsev V.O. Systematical analysis of the climatics influence on mechanical properties of the polymer composite materials based on domestic and foreign sources (review). Aviacionnye materialy i tehnologii, 2018, no. 2 (51), pp. 47–58. DOI: 10.18577/2071-9140-2018-0-2-47-58.
5. Satdinov R.A., Veshkin E.A, Postnov V.I. Assessment of the impact of climatic factors on the performance properties of fiberglass VPS-42P/T-64. Trudy VIAM, 2020, no. 10 (92), paper no. 03. Available at: http://www.viam-works.ru (accessed: October 20, 2023). DOI: 10.18577/2307-6046-2020-0-10-21-29.
6. Gulyaev I.N., Zelenina I.V., Valevin E.O., Khaskov M.A. Influence of climatic ageing on the properties of high-temperature carbon fiber reinforced plastics. Trudy VIAM, 2021, no. 2 (96), paper no. 05. Available at: http://www.viam-works.ru (accessed: August 20, 2023). DOI: 10.18577/2307-6046-2021-0-2-39-51.
7. Borshchev A.V., Gusev Yu.A. Polymer composite materials in automotive industry. Aviacionnye materialy i tehnologii, 2014, no. S2, pp. 34–38. DOI: 10.18577/2071-9140-2014-0-s2-34-38.
8. Dementeva L.A., Serezhenkov A.A., Lukina N.F., Kutsevich K.E. Adhesive prepregs and layered materials on their basis. Aviacionnye materialy i tehnologii, 2013, no. 2, pp. 19–21.
9. Mishkin S.I. Application of carbon fiber plastics in constructions of pilotless devices (review). Trudy VIAM, 2022, no. 5 (111), paper no. 08. Available at: http://www.viam-works.ru (accessed: October 20, 2023). DOI: 10.18577/2307-6046-2022-0-5-87-95.
10. Mishkin S.I., Zhakova L.S., Klimenko O.N., Vasilchuk E.A. Research of influence of the contents resin in CFRP on their mechanical properties. Trudy VIAM, 2023, no. 2 (120), paper no. 07. Available at: http://www.viam-works.ru (accessed: October 20, 2023). DOI: 10.18577/2307-6046-2023-0-2-77-86.
11. Malakhovsky S.S., Panafidnikova A.N., Kostromina N.V., Osipchik V.S. Carbon plastics in the modern world: their properties and applications. Uspekhi v khimii i khimicheskoy tekhnologii, vol. XXXIII, 2019, no. 6, pp. 62–64.
12. Gulyaev A.I., Medvedev P.N., Sbitneva S.V., Petrov A.A. Experimental research of «fiber–matrix» adhesion strength in carbon fiber epoxy/polysulphone composite. Aviacionnye materialy i tehnologii, 2019, no. 4 (57), pp. 80–86. DOI: 10.18577/2071-9140-2019-0-4-80-86.
13. Veshkin E.A., Startsev V.O., Postnov V.I., Barannikov A.A. The climate impacts as the assessment of maintainability of products from carbon fiber. Trudy VIAM, 2019, no. 8 (80), paper no. 11. Available at: http://www.viam-works.ru (accessed: October 20, 2023). DOI: 10.18577/2307-6046-2019-0-8-98-108.
14. Starkov A.I., Kutsevich K.E., Petrova A.P., Antyufeeva N.V. Development of temperature and time curing regime for prepregs based on adhesive binder with reduced flammability. Trudy VIAM, 2023, no. 3 (121), paper no. 03. Available at: http://www.viam-works.ru (accessed: October 20, 2023). DOI: 10.18577/2307-6046-2023-0-3-29-38.
15. Dementyeva L.A., Lukina N.F., Serezhenkov A.A., Kutsevich K.E. Basic properties and purpose of PCM based on adhesive prepregs. Reports XIX Int. sci.-tech. conf. «Designs and technology for producing products from non-metallic materials». Obninsk: ONPP «Technology», 2010, pp. 11–12.
16. Petrova A.P., Malysheva G.V. Adhesives, adhesive binders and adhesive prepregs: textbook. Ed. E.N. Kablov. Moscow: VIAM, 2017, 472 p.
17. Perov N.S. Design of polymeric materials on the molecular principles. II. The molecular mobility in the cross-linked complex systems. Aviacionnye materialy i tehnologii, 2017, no. 4 (49), pp. 30–36. DOI: 10.18577/2071-9140-2017-0-4-30-36.
18. Laptev A.B., Barbotko S.L., Nikolaev E.V. The main research areas of the persistence properties of materials under the influence of climatic and operational factors. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 547–561. DOI: 10.18577/2071-9140-2017-0-S-547-561.
19. Kutsevich K.E., Tyumeneva T.Yu., Petrova A.P. Influence of fillers on properties of adhesive prepregs and PCM on their basis. Aviacionnye materialy i tehnologii, 2017, no. 4 (49), pp. 51–55. DOI: 10.18577/2071-9140-2017-0-4-51-55.
20. Isaev A.Yu., Rubtsova E.V., Kotova E.V., Sutyagin M.N. Research of properties of glues and glue binding, made with use of modern domestic component base. Trudy VIAM, 2021, no. 3 (97), paper no. 05. Available at: http://www.viam-works.ru (accessed: October 18, 2023). DOI: 10.18577/2307-6046-2021-0-3-58-67.
21. Lukina N.F., Petrova A.P., Muhametov R.R., Kogtyonkov A.S. New developments in the field of adhesive aviation materials. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 452–459. DOI: 10.18577/2071-9140-2017-0-s-452-459.
22. Malysheva G.V., Grashchenkov D.V., Guzeva T.A. Evaluation of technological use efficiency of adhesives and glue prepregs in the manufacture of three-layer panels. Aviacionnye materialy i tehnologii, 2018, no. 4 (53), pp. 26–30. DOI: 10.18577/2071-9140-2018-0-4-26-30.

dx.doi.org/ 10.18577/2307-6046-2024-0-3-101-116

УДК 666.7

Sidorov D.V., Grunin А.А., Shavnev A.A.

IMPLEMENTATION OF TECHNOLOGY FOR CHEMICAL VAPOR DEPOSITION OF SILICON CARBIDE IN ELECTRONICS. Part 1

The comparative characteristics of modern semiconductor materials, the basic electrophysical properties of the applied silicon carbide polytypes, and the possibilities of using silicon carbide semiconductors in microelectronic devices are presented. The most common methods for producing silicon carbide crystals are considered, which are growing crystals from a melt, sublimation and chemical vapor deposition.

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Reference list

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40. Sidorov D.V., Shavnev A.A., Melentev A.A. Formation of silicon carbide coatings by chemical vapor deposition (review). Part 2. Trudy VIAM, 2022, no. 2 (108), paper no. 07. Available at: http://www.viam-works.ru (accessed: December 18, 2023). DOI: 10.18577/2307-6046-2022-0-2-88-89.

10.

dx.doi.org/ 10.18577/2307-6046-2024-0-3-117-124

УДК 667.6

Kondrashov E.K., Kozlova A.A.

EFFICIENCY OF ANTICORROSIVE PROTECTION BY ORGANIC SILICON ENAMELS OF WELDED CONNECTIONS OF VNS-2 AND VNS-5 STEELS

The effectiveness of using organic silicon enamels of various grades for anticorrosive protection of welded connections steels VNS-2 and VNS-5 working at high temperatures has been studied. The assessment of properties of coatings on the basis of organic silicon enamels after exposure to salt spraying, humidity, sign-variable temperatures is carried out. By results of the study the most effective enamels providing reliable protection of steels in difficult operating conditions are chosen.

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Reference list

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11.

CONTENТS

Heat-resistant alloys and steels

Bazyleva O.A., Rimsha E.G., Chabina E.B., Raevskikh A.N.Some aspects of creation and research of structural casting intermetallide alloys for promising helicopter engines

Light-metal alloys

Yashin M.S., Bazhenov A.R.Investigation of thermomechanical parameters of deformation and mechanical properties depending on conditions of deformation of titanium alloy VT30

Panteleev M.D., Sviridov A.V., Odintsov N.S., Bondarenko S.V.Survivability of welded fuselage elements made of heat-resistant aluminum alloys V-1213 and 1151

Leonov A.A., Trofimov N.V.Magnesium ion batteries: prospects and challenges in the field of energy

Polymer materials

Guseva M.A., Ibragimov Z.D.Selection of curing system when developing epoxy compositions with energy-efficient curing mode

Composite materials

Nyafkin A.N., Zhabin A.N., Avtaev V.V.Сracks рropagation in composite materials of the Al–SiC system under cyclic loads

Sedova L.S., Shestakov A.M.Foreign hydroliquids, applied in civil aviation of the Russian Federation

Starkov A.I., Isaev A.Yu., Kutsevich K.E.Comprehensive assessment of the impact of operational and climatic tests on the change of strength properties of polymer composite materials based on adhesive prepregs. Рart 1. Сarbon fiber-reinforced plastic VKU-59

Protective and functional

coatings

Sidorov D.V., Grunin A.A., Schavnev A.A.Implementation of technology for chemical vapor deposition of silicon carbide in electronics. Part 1

Kondrashov E.K., Kozlova A.A. Efficiency of anticorrosive protection by organic silicon enamels of welded connections of VNS-2 and VNS-5 steels

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