Last number
№6 2026
In this work, using the method of transmission electron microscopy, the mechanisms of grain structure formation during hot deformation and microstructure formation during subsequent full heat treatment in the two-phase (γ + γ′)-region of an experimental nickel-based superalloy with zero γ/γ'-misfit for gas turbine engine disks have been identified. The chemical composition of this alloy was developed based on a granular nickel-based superalloy VZh178P using the method of computer design. Creep mechanisms at temperatures of 750 and 850 °C for an experimental deformed alloy in a heat-treated state were analyzed.
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This review analyzes the influence of alloying elements on the mechanical properties of granulated high-temperature nickel alloys. It is shown that the introduction of alloying elements such as Al, Ti, W, Mo, Nb, Ta, and Hf into the alloys contributes to material strengthening. Alloying with γ-forming elements such as Co and Cr leads to an increased creep resistance at temperatures up to 750 °C and heat resistance. A small content of microalloying elements such as B and Zr also has a positive effect on ductility.
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The article discusses the production of large-diameter «ring» capsules with a diameter-to-height ratio of more than 8 and massive large-diameter capsules with a diameter of up to 1000 mm for subsequent production of disk blanks by hot isostatic pressing. The features of filling the capsules with granules in a horizontal position are considered. The shape change of compact blanks after hot isostatic pressing is analyzed and shrinkage coefficients are calculated. The factors that affect the shape change of compact disk blanks and the shrinkage coefficients are examined.
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This paper presents a comprehensive analysis of the deformation hardening of a NiCoCrWReNbAlTiC system heat-resistant alloy, made by casting, hot plastic deformation and selective laser sintering. It is established that materials produced by selective laser sintering method with further heat treatment demonstrate the highest deformation hardening characteristics with a relative contribution of up to 70 %. The material after hot plastic deformation with subsequent heat treatment shows maximum values of the hardening modulus (460.4 MPa at ε = 0.1).
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This article describes studies of the microstructure of high-carbon complex-alloyed steel blanks after various hot plastic deformation (forging) modes and subsequent preliminary heat treatment (annealing). The dependence of the steel microstructure during final heat treatment on the choice of temperature-time characteristics for hot plastic deformation and subsequent preliminary heat treatment is demonstrated. The influence of steel microstructure on the machinability of blanks during mechanical processing is described.
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The widespread use of titanium alloys in the aviation sector requires the development of standard samples necessary for precise determination and control of hydrogen content levels in these materials. The study investigates the influence of hydrogenation factors such as holding time, electrolyte composition, and the concentration of active salts and acids in it, as well as direct current voltage on the process of hydrogen saturation of the VT14 type titanium alloy. An analysis has been conducted of hydrogen content and distribution in samples obtained under various hydrogenation conditions.
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The article describes the results of a research on polycondensation «in situ» in the processes of partial hydrolysis of C2H5O(CH3)2SiOSi(CH3)2OC2H5. The influence of the molar ratio of reagents on the oligomeric composition of the partial hydrolysis products and the dependence of the monomer conversion degree on conversion of functional groups are presented. A comparison of the patterns of macromolecules formation in the processes of partial hydrolysis of 1,1,3,3-tetramethyl-1,3-diethoxydisiloxane and homofunctional condensation of 1,1,3,3-tetramethyldisiloxane-1,3-diol is carried out.
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An assessment was made of the impact of operational factors on the physical and mechanical properties of carbon fiber reinforced plastics (CFRPs) based on adhesive prepregs developed by the Kurchatov Institute – VIAM. The changes in tensile strength, compressive strength and flexural strength after exposure to elevated temperatures were demonstrated for CFRPs with various forms of carbon fillers. The properties of carbon fiber reinforcements and their potential impact on changes in CFRP performance after climatic exposure were examined.
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In the study the technological and operational characteristics of the epoxy resin system VSE-81, developed at the NRC «Kurchatov Institute» – VIAM, are considered. The results of gelation and rheological tests are presented. Mechanical properties are obtained by stretching VSE-81 samples cured according to the selected mode, and the conversion rate is determined by the DSC method. We compared the mechanical characteristics of microplastics based on UMT49S-12K-EP carbon fiber with VSE-81 binder and its imported analogue. The results of microstructural research interpreted using a model of the microcomposite structure of thermosetting polymers are presented.
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32. Kotomin S.V., Obidin I.M., Pavlyuchkova E.A. Calculation of the strength of the adhesive bond of reinforcing fibers with polymers using the «loop» method. Mekhanika kompozitnykh materialov, 2022, vol. 58, no. 1, pp. 197–212.
33. Kotomin S.V., Obidin I.M., Pavlyuchkova E.A. Scale factor in testing adhesive-glue joints of heteroaramid yarns using the «loop» method. Klei. Germetiki. Tekhnologii, 2023, no. 11, pp. 35–40.
34. 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.
This study examined the effect of filler spatial orientation in polymer composite materials on fire hazard characteristics – heat release during combustion. The materials studied were carbon fiber reinforced plastics (CFRPs) based on carbon tow and unidirectional carbon fabric. It was found that depending on the orientation of the specimen in the test holder (vertical filler fiber direction – [0°] or horizontal – [90°]), the heat release characteristics change, with the maximum heat release rate changing.
2. Slavin A.V., Donetskiy K.I., Khrulkov A.V. Prospects for the use of polymer composite materials in aircraft structures in 2025–2035 (review). Trudy VIAM, 2022, no. 11 (117), pp. 81–92. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2022-0-11-81-92.
3. Erasov V.S., Sibayev I.G. Scheme for the development and evaluation of properties of structural aviation composite materials. Aviation materials and technologies, 2023, no. 1 (70), pp. 61–81. Available at: http://www.journal.viam.ru (accessed: January 12, 2026). DOI: 10.18577/2713-0193-2023-0-1-61-81.
4. Kan A.Ch., Zhelezina G.F., Kulagina G.S., Ayupov T.R. Fire safety of structural organic plastics reinforced with aramid fabrics. Aviation materials and technologies, 2022, no. 4 (69), pp. 51–60. Available at: http://www.journal.viam.ru (accessed: January 12, 2026). DOI: 10.18577/2713-0193-2022-0-4-51-60.
5. Veshkin E.A., Slavin A.V., Postnova M.V., Apalkova A.V. The role of temperature-time curing conditions in the formation of unidirectional and equally strong carbon fiber plastics properties. Aviation materials and technologies, 2025, no. 2 (79), pp. 59–71. Available at: http://www.journal.viam.ru (accessed: January 12, 2026). DOI: 10.18577/2713-0193-2025-0-2-59-71.
6. Marakhovskij P.S., Barinov D.Ya., Shorstov S.Yu., Vorobev N.N. On creation of physical and mathematical models of heat and mass transfer during manufacturing by additive technologies (review). Aviation materials and technologies, 2022, no. 2 (67), pp. 111–119. Available at: http://www.journal.viam.ru (accessed: January 12, 2026). DOI: 10.18577/2713-0193-2022-0-2-111-119.
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8. Barbotko S.L., Volny O.S., Kiriyenko O.A., Shurkova E.N. Fire safety assessment of polymeric materials for aviation purposes. Ed. E.N. Kablov. Moscow: VIAM, 2018, 408 p.
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10. Sidorina A.I., Safronov A.M. Study of the resistance of carbon fibers to oxidation. Trudy VIAM, 2022, no. 7 (113), pp. 63–73. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2022-0-7-63-73.
11. Barbotko S.L., Dementyeva L.A., Serezhenkov A.A. Combustibility of fiberglass and carbon fiber reinforced plastics based on adhesive prepregs. Klei. Germetiki. Tekhnologii, 2008, no. 7, pp. 29–31.
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13. Shurkova E.N., Volny O.S., Izotova T.F., Barbotko S.L. Research of possibility of decrease in heat release when burning composite material by change of its structure. Aviacionnye materialy i tehnologii, 2012, no. 1, pp. 27–30.
14. Garashchenko A.N., Vinogradov A.V., Kobylkov N.V., Nikolchenkin A.A., Antipov E.A. Experimental and computational modeling of fire and thermal protection composite materials under high-temperature exposure. Aviation materials and technologies, 2022, no. 3 (68), pp. 84–97. Available at: http://www.journal.viam.ru (accessed: January 12, 2026). DOI: 10.18577/2713-0193-2022-0-3-84-97.
15. Airworthiness standards for transport category aircraft NLG 25: approved by Order of the Federal Air Transport Agency dated December 27, 2022 No. 961-P. Available at: https://old.favt.gov.ru/
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19. Rehn S. Vertical Bunsen Burner Testing of 3-D Printed Material. International Aircraft Materials Fire Test Forum. Cologne, 2019, 12 p. Available at: http: www.fire.tc.faa.gov/ppt/
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23. Barbotko S.L., Volnyj O.S., Postnov V.I., Shurkova E.N. Investigation of the effect of reinforcement structures on fire hazard characteristics of the fiberglass. Trudy VIAM, 2019, no. 4 (76), pp. 108–120. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2019-0-4-108-120.
24. Barbotko S.L., Volnyj O.S., Marakhovskii P.S. Investigation of the influence of the rein-forcement scheme on the combustibility characteristics of carbon fiber reinforced polymer material. Trudy VIAM, 2019, no. 10 (82), pp. 103–110. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2019-0-10-103-110.
25. Gulyaev I.N., Pavlovskiy K.A. High modulus carbon plastics for civil aviation equipment (review). Trudy VIAM, 2023, no. 3 (121), pp. 95–106. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2023-0-3-95-106.
26. Barannikov A.A., Veshkin E.A., Savitsky R.S., Slavin A.V. On the question of manufacturing fire-resistant and fireproof hoods of helicopter power plant engine nacholds from polymer composite materials. Part 1. Trudy VIAM, 2025, no. 8 (150), pp. 123–133. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2025-0-8-123-133.
27. Erasov V.S., Sibayev I.G., Sutubalov A.I. Testing of samples from three-layer structures with honeycomb filler. Trudy VIAM, 2025, no. 10 (152), pp. 133–155. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2025-0-10-133-155.
28. 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.
29. Gamazina A.V., Kurnosov A.O., Vavilova M.I., Kochetov N.R. Investigation of fiberglass properties based on the melt binder VSE-1212 for radio engineering purposes. Trudy VIAM, 2024, no. 12 (142), pp. 56–65. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2024-0-12-56-65.
30. Platonov A.A., Dushin M.I. Carbon composites VKU-25 based on unidirectional prepregs. Trudy VIAM, 2015, no. 11, pp. 50–54. Available at: http://www.viam-works.ru (accessed: January 12, 2026). DOI: 10.18577/2307-6046-2015-0-11-6-6.
The taxonomic identification of mycelial fungal strains from the NRC «Kurchatov Institute» – VIAM collection was carried out using the methods of genome-wide taxonomy in the Kurchatov Genome Center. The article presents data on the molecular identification of strains of the following taxa: family Chaetomiaceae; order Pleosporales, genera Nothophoma, Didymella, Epicoccum; orders Hypocreales and Erysiphales, genera Purpureocillium, Beauveria; class Leotiomycetes, genus Botrytis, family Phacidiaceae; class Dothideomycetes, genera Delphinella, Aureobasidium; family Trichocomaceae, genus Talaromyces et al.
2. Zakirova L.I., Afanasyev-Khodykin A.N., Movenko D.A., Laptev A.B. Features of the formation of the Sn–Zn–Fe diffusion layer at the boundary of galvanothermal coating of systems zinc–tin and 30HGSA steel with high protec-tive capability. Aviation materials and technologies, 2022, no. 4 (69), pp. 61–71. Available at: http://www.journal.viam.ru (accessed: July 29, 2025). DOI: 10.18577/2713-0193-2022-0-4-61-71.
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Heat-resistant alloys and steels
Karashaev M.M., Petrushin N.V., Zaitsev D.V., Svetlov I.L. Structure formation during hot plastic deformation of a nickel high-temperature alloy with zero γ/γ′-misfit
Yashin M.S., Shpagin A.S., Vostrikov A.V. Improvement of the mechanical properties of granulated heat-resistant nicke-based alloys by their complex alloying
Knyazev A.E., Min P.G., Logunov A.V. Features of manufacturing and filling large-sized and ring-shaped capsules in granule metallurgy. Analysis of shape change after hot isostatic pressing
Vlasov I.I., Sevalnev G.S., Valyuhova I.V., Dyachenko O.A. Analysis of the parameters of deformation hardening of a multicomponent high-entropy alloy of the NiCoCrWReNbAlTiC system according to the Johnson–Cook model
Korobova E.N., Kurpyakova N.A., Doroshenko A.V., Gromov V.I. Microstructure study of heat-resistant high-carbon complex-alloyed steel after hot plastic deformation
Light-metal alloys
Shvetsova A.N. Research of the process of hydrogen saturation of standard samples of titanium alloy type VT14
Polymer materials
Butuzov A.V. The study of chemical assembly of macromolecules in hydrolytic polycondensation of 1,1,3,3-tetrametyl-1,3-diethoxydisiloxane
Composite materials
Isaev A.Yu., Putilina P.M., Starkov A.I. Strength of carbon fiber reinforced plastics after exposure to operational factors
Vakhrusheva Ya.A., Tkachuk A.I., Afanaseva E.A., Kurshev E.V., Lonskii S.L. Perspective epoxy resin system VSE-81 for incoming quality inspection of carbon fiber
Bespalov A.S. Aluminum oxide-based catalyst carriers
Platonova Ya.B., Leonov A.A., Kirillova V.A., Savilov S.V. Palladium complex compounds as catalysts for cross-coupling reactions for obtaining functional materials. Part 1. Sonogashira reaction
Protective and functional
coatings
Laptev A.B., Matishov G.G., Bulysheva N.I., Krivushina A.A., Startsev V.O. Toxicity of microparticles of paint coatings. Part 2. Degradation processes and mechanisms of toxic effects
Timoshina E.A., Kuznetsova V.A., Marchenko S.A., Zheleznyak V.G. Fillers used to create wear-resistant paint and varnish coatings (review)
Material tests
Ivankov R.R., Sidorina A.I., Kotomin S.V. The relationship between fiber wettability and adhesion value in the «fiber–polymer matrix» system
Barbotko S.L., Bochenkov M.M., Klimenko O.N. The influence of spatial orientation of the filler in unidirectional carbon fiber reinforced plastics on the heat release characteristics during combustion
Krivushina A.A., Startsev V.O. Identification of the mycelial fungi collection of NRC «Kurchatov Institute» – VIAM by molecular genetic methods. Part 3