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dx.doi.org/ 10.18577/2307-6046-2023-0-11-3-16

УДК 620.165.79

Grigorenko V.B., Lukinа E.A., Terekhin A.M.

STRUCTURAL FEATURES DESTRUCTION OF MONOCRYSTALLINE MATERIALS

The features of the production of single-crystal blades from nickel heat-resistant alloys are considered. Metallographic and fractographic studies of the destroyed blades were performed to identify the causes of destruction. The features of fatigue and static destruction of single-crystal turbine blades have been studied by optical and scanning electron microscopy using X-ray spectral microanalysis. Recommendations are given to prevent the formation of recrystallized polyhedral grains.

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Reference list

1. Vostrikov A.V., Lomberg B.S., Sumynikov M.N., Ovsepyan S.V. Modern heat-resistant deformable nickel alloys of VIAM for GTD details. Modern heat-resistant nickel deformable alloys and technologies for their production: Materials All-Rus. Scientific and Technical Conf. (Moscow, September 24, 2021) Moscow: NIC «Kurchatov Institute» – VIAM, 2021, pp. 5–14.
2. Kablov E.N., Sidorov V.V., Kablov D.E., Min P.G. The metallurgical fundamentals for high quality maintenance of single crystal heat-resistant nickel alloys. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 55–71. DOI: 10.18577/2071-9140-2017-0-S-55-71.
3. Kablov E.N., Echin A.B., Bondarenko Yu.A. History of development of directional crystallization technology and equipment for casting blades of gas turbine engines. Trudy VIAM, 2020, no. 3 (87), paper no. 01. Available at: http://www.viam-works.ru (accessed: May 15, 2023). DOI: 10.18577/2307-6046-2020-0-3-3-12.
4. Kablov E.N. The role of fundamental research in the creation of materials of the new generation. Reports of XXI Mendeleevsky Congress for General and Applied Chemistry: in 6 vols. St. Petersburg, 2019, vol. 4, p. 24.
5. Petrushin N.V., Ospennikova O.G., Svetlov I.L. Single-crystal Ni-based superalloys for turbine blades of advanced gas turbine engines. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 72−103. DOI: 10.18577/2071-9140-2017-0-S-72-103.
6. Toloraya V.N., Kablov E.N., Demonis I.M. The technology for obtaining monocrystalline castings of turbine blades of the GTD of a given crystallographic orientation from renius-containing heat-resistant alloys. Aviacionnye materialy i tehnologii, 2004, no. 1, pp. 107–118.
7. Sims Ch.T., Norman S.S., Wilman S.Kh. Superplanes II: in 2 vols. Moscow: Metallurgiya, 1995, vol. 1: Heat-resistant materials for aerospace and industrial power plants, 384 p.
8. Sidorov V.V., Kablov D.E., Chabina E.B., Ospennikova O.G., Simonov V.N., Puchkov Yu.A. The influence of impurities and microlegy on the structure and operational properties of monocristals of heat-resistant nickel alloys. Moscow: VIAM, 2020, 335 p.
9. Lomberg B.S., Shestakova A.A., Bakradze M.M., Karachevtsev F.N. The investigation of the stability of γʹ-phase with size below 100 nm in Ni-base superalloy VZh175-ID. Aviacionnye materialy i tehnologii, 2018, no. 4 (53), pp. 3–10. DOI: 10.18577/2071-9140-2018-0-4-3-10.
10. Letnikov M.N., Lomberg B.S., Ospennikova O.G., Bakradze M.M. The influence of quench rate on microstructure and mechanical properties of nickel-based wrought superalloy VZh175-ID. Aviacionnye materialy i tehnologii, 2019, no. 2 (55), pp. 21–30. DOI: 10.18577/2071-9140-2019-0-2-21-30.
11. Gerasimov S.A., Kuksenova L.I., Lapteva V.G., Ospennikova O.G., Alekseeva M.S., Gromov V.I. Surface engineering and operational properties of the nitrogenized structural steels. Moscow: VIAM, 2019, 599 p.
12. Kablov E.N., Ospennikova O.G., Kudinov I.I., Golovkov A.N., Generalov A.S., Knyazev A.V. Assessment of the probability of identifying operational defects in the details of aviation equipment from heat-resistant alloys using flaw detective fluids of domestic and foreign production. Defektoskopiya, 2021, no. 1, pp. 64–71.
13. Bytsenko O.A., Grigorenko V.B., Lukina E.A., Morozova L.V. Development of methods for metal-physical research: methodological issues and practical significance. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 498–515. DOI: 10.18577/2071-9140-2017-0-S-498-515.
14. Belyaev M.S., Morozova L.V., Gorbovets M.A. Destruction of the samples of monocrystals of experimental heat-resistant nickel alloy, tested for multicycle fatigue. Materialovedenie, 2020, no. 8, pp. 7–13.
15. Grigorenko V.B., Morozova L.V. Application of the scanning electron microscopy for studying of initial destruction stages. Aviacionnye materialy i tehnologii, 2018, no. 1 (50), pp. 77–87. DOI: 10.18577/2071-9140-2018-0-1-77-87.
16. Naprienko S.A., Orlov M.R. Damage of single-crystal turbine blades of GTP. Trudy VIAM, 2016, no. 2 (38), paper no. 03. Available at: http://www.viam-works.ru (accessed: May 15, 2023). DOI: 10.18577/2307-6046-2016-0-2-3-3.

dx.doi.org/ 10.18577/2307-6046-2023-0-11-17-25

УДК 66.067.124

Deynega G.I., Kuzmina I.G., Bityutskaya O.N., Narskiy A.R.

FOAM CERAMIC FILTERS BASED ON DOMESTIC REFRACTORY MATERIALS. Part 1

In the first part of the study conducted at the National Research Center «Kurchatov Institute» – VIAM, the technology of manufacturing foam ceramic filters designed to purify the melt from non-metallic inclusions is considered. Technological parameters for the manufacture of foam ceramic filters using domestic refractory materials have been developed, several experimental samples of filters based on aluminum oxide (III) and zirconium oxide (IV) have been manufactured, their physical and mechanical properties have been determined. The full compliance of the properties of the manufactured filters with the requirements of the technical specification has been established.

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Reference list

1. Echin A.B., Deynega G.I., Narsky A.R. New developments of NRC «Kurchatov Institute» – VIAM in the field of materials for casting processes of superalloys. Trudy VIAM, 2023, no. 8 (126), paper no. 02. Available at: http://www.viam-works.ru (accessed: September 11, 2023). DOI: 10.18577/2307-6046-2023-0-8-13-24.
2. Kablov E.N., Shompolov E.G., Sidorov V.V., Rigin V.E., Kayumov R.G. Organization of production of cast rod (charge) billets from nickel casting heat-resistant alloys. Elektrometallurgiya, 2007, no. 1, pp. 2–5.
3. Bondarenko Yu.A. Trends in the development of high-temperature metal materials and technologies in the production of modern aircraft gas turbine engines. Aviacionnye materialy i tehnologii, 2019, no. 2 (55), pp. 3–11. DOI: 10.18577/2071-9140-2019-0-2-3-11.
4. Echin A.B., Bondarenko Yu.A., Kolodyazhny M.Yu., Surova V.A. Review of perspective high-temperature superalloys based on refractory non-metallic materials for production of gas turbine engines. Aviation materials and technologies, 2023, no. 3 (72), paper no. 03. Available at: http://www.journal.viam.ru (accessed: September 11, 2023). DOI: 10.18577/2713-0193-2023-0-3-30-41.
5. Kablov E.N., Ospennikova O.G., Sidorov V.V., Rigin V.E., Kablov D.E. Features of the technology of smelting and casting modern foundry high-heat-resistant nickel alloys. Vestnik MGTU im. N.E. Baumana. Ser.: Mechanical engineering, 2011, no. SP2, pp. 68–78.
6. Sidorov V.V., Iskhodzhanova I.V., Rigin V.E., Folomeikin Yu.I. Evaluation of filtration efficiency during casting of complex-alloyed nickel melt. Elektrometallurgiya, 2011, no. 11, pp. 17–21.
7. Kablov E.N., Sidorov V.V., Kablov D.E., Min P.G. The metallurgical fundamentals for high quality maintenance of single crystal heat-resistant nickel alloys. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 55–71. DOI: 10.18577/2071-9140-2017-0-S-55-71.
8. Demchenko A.I., Shevyakov V.F., Korovin V.A., Belyaev S.V., Gushchin V.N. Improving the quality of nickel alloy by filtration through a ceramic foam filter. Liteyshchik Rossii, 2019, no. 6, pp. 29–33.
9. Staroverov Yu.S., Chernov Yu.A. Application of ceramic foam filters in foundries and steelmaking abroad. Ogneupory, 1992, no. 1, pp. 38–40.
10. Ofitserov A.A., Zavolosnov B.S. Foam ceramic filters for filtration of heat-resistant nickel alloys. Liteynoe proizvodstvo, 1993, no. 4, pp. 19–20.
11. Babashov V.G., Varrik N.M., Karaseva T.A. Porous ceramic for filtration of metal melts and hot gases (rеview). Trudy VIAM, 2020, no. 8 (90), paper no. 6. Available at: http://www.viam-works.ru (accessed: August 24, 2023). DOI: 10.18577/2307-6046-2020-0-8-54-63.
12. Ten E.B., Voevodina M.A. Filtration of high-strength cast iron melt. Liteynoe proizvodstvo, 1993, no. 7, pp. 5–8.
13. Dibrov I.A., Kozlov A.V. Developments in the field of melting, pouring, modifying and refining foundry alloys. Liteynoe proizvodstvo, 2000, no. 6, pp. 24–26.
14. Emelyanov V.O., Martynov K.V., Mutilov V.N., Sokolov A.V., Sukhanova V.P. Aqueous solution of silica sol as an alternative to ethyl silicate in LVM. Liteynoe proizvodstvo, 2012, no. 3, pp. 30–31.
15. Min P.G., Vadeev V.E. The development and introduction into serial production of the new superalloy VZhL125 for the advanced aviation engines vanes. Aviation materials and technologies, 2023, no. 1 (70), paper no. 01. Available at: http://www.journal.viam.ru (accessed: August 24, 2023). DOI: 10.18577/2713-0193-2023-0-3-3-14.

dx.doi.org/ 10.18577/2307-6046-2023-0-11-26-36

УДК 678.8

Kulagina G.S., Zhelezina G.F., Levakova N.M., Safonov P.E.

POLYMER FIBERS IN THE COMPOSITION OF FABRICS FOR SELF-LUBRICATING ANTIFRICTION MATERIALS

The article discusses synthetic heatresistant polymer fibers that for the manufacture of antifriction composite materials. The properties of fibre of various chemical nature (para- and metaаramid, polyimide, fluorinecontaining, etc.) are given. Doublesided fabrics based on heat-resistant polymer fibers containing two types of fibers with antifriction and reinforcing properties for use as part of selflubricating antifriction materials are considered.

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Reference list

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2. Mikhailin Yu.A. Fibrous polymer composite materials in technology. St. Petersburg: Scientific principles and technologies, 2013, 720 p.
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19. Kan A.Ch., Kulagina G.S., Ayupov T.R., Zhelezina G.F. The influence of environmental factors on the characteristics of antifriction organoplasty Orgalon AF-1M. Trudy VIAM, 2018, no. 3 (109), paper no. 09. Available at: http://www.viam-works.ru (accessed: September 01, 2023). DOI: 10.18577/2307-6046-2022-0-3-91-101.
20. Kablov E.N. Materials for aerospace technology. Vse materialy. Entsiklopedicheskiy spravochnik, 2007, no. 5, рр. 7–27.
21. Kablov E.N. Main directions of development of materials for aerospace technology of the XXI century. Perspektivnye materialy, 2000, no. 3, pp. 27–36.
22. Kulagina G.S., Zhelezina G.F., Levakova N.M. Antifriction organoplastics for high-loaded friction knots. Trudy VIAM, 2019, no. 2 (74), paper no. 09. Available at: http://www.viam-works.ru (accessed: September 01, 2023). DOI: 10.18577/2307-6046-2019-0-2-89-96
23. Sorokin A.E., Ivanov M.S., Sagomonova V.A. Thermoplastic polymer composite materials based on polyetheretherketones of various manufacturers. Aviation materials and technologies, 2022, no. 1 (66), paper no. 04. Available at: http://www.journal.viam.ru (accessed: September 01, 2023). DOI: 10.18577/2071-9140-2022-0-1-41-50.

dx.doi.org/ 10.18577/2307-6046-2023-0-11-37-46

УДК 678.8

Kulagina G.S., Zhelezina G.F., Kan A.Ch., Kurshev E.V.

EXPLOITATION PROPERTIES OF ANTIFRICTION SELFLUBRICATING ORGANOPLASTIC BASED ON FABRIC MADE OF POLYTETRAFLUOROETHYLENE AND ARCELON FIBERS

The article studied the exploitation properties of antifriction organoplastics based on a new reinforcing fabric consisting of two types of fibers: polytetrafluoroethylene and polyoxadiazole fiber Arcelon. The nature of destruction during delamination of organoplastic from a metal substrate and the influence of various factors (temperature, humidity, salt fog, tropical chamber conditions, etc.) on adhesive strength were studied. It has been shown that, under the influence of operational factors, organoplastic has high adhesive strength values – above the allowable minimum level.

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Reference list

1. Kablov E.N. The main directions of the development of materials for the Authoric technique of the XXI century. Perspektivnye materialy, 2000, no. 3, pp. 27–36.
2. Kulagina G.S., Zhelezina G.F., Levakova N.M. Antifriction organoplastics for high-loaded friction knots. Trudy VIAM, 2019, no. 2 (74), paper no. 09. Available at: http://www.viam-works.ru (accessed: September 22, 2023). DOI: 10.18577/2307-6046-2019-0-2-89-96.
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6. Kulagina G.S., Kan A.Ch., Zhelezina G.F., Levakova N.M. Antifriction materials based on polymer fibers. Trudy VIAM, 2022, no. 11 (117), paper no. 05. Available at: http://www.viam-works.ru (accessed: September 22, 2023). DOI: 10.18577/2307-6046-2022-0-11-48-59.
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10. Kuzharov A.S., Rygchenko V.G. Compositional antifriction coatings based on the fibers of political radiatorethnicity. Consistency: interuniversity collection scientific works. Rostov-on-Don: RISHM, 1992, is. 2, pp. 140–147.
11. Voinstein V.E., Troyanovskaya G.I. Dry lubricants and selflubricating materials. Moscow: Mechanical Engineering, 1968, p. 179.
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14. Dresvyanina E.N., Makarova R.A., Trusov Yu.D. Highterm-resistant polyoxadiazol fibers, threads and textiles based on them. Tekhnicheskiy tekstil, 2007, no. 16, pp. 15–20.
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17. Tkachuk A.I., Donetsky K.I., Terekhov I.V., Karavaev R.Yu. The use of thermosetting matrices for the manufacture of polymer composite materials by the non-autoclave molding methods. Aviation materials and technology, 2021, no. 1 (62), paper no. 03. Available at: https://journal.viam.ru (accessed: September 22, 2023). DOI: 10.18577/2713-0193-2021-0-1-22-33.
18. Deev I.S., Kobets L.P. Study of microstructure and micropolis of deformations in polymer composites by the method of raster electron microscopy. Zavodskaya laboratoriya. Diagnostika materialov, 1999, vol. 65, no. 4, pp. 27–34.
19. Deev I.S., Kablov E.N., Kobets L.P., Chursova L.V. Research of the scanning electron microscopy method deformation of microphase structure of polymeric matrix at mechanical loading. Trudy VIAM, 2014, no. 7, paper no. 06. Available at: http://www.viam-works.ru (accessed: September 22, 2023). DOI: 10.18577/2307-6046-2014-0-7-6-6.
20. Grigorenko V.B., Morozova L.V. Application of the scanning electron microscopy for studying of initial destruction stages. Aviacionnye materialy i tehnologii, 2018, no. 1 (50), pp. 77–87. DOI: 10.18577/2071-9140-2018-0-1-77-87.

dx.doi.org/ 10.18577/2307-6046-2023-0-11-47-55

УДК 678.067.5; 678.747.2

Kolokoltseva T.V., Popov J.O., Usacheva M.N., Gromova A.A.

PREPREGS OF FIBERGLASS AND PREPREG OF CARBON FIBER ON THE BASIS OF THE RESIN VSE-67 FOR THE USE IN THE STRUCTURES OF HELICOPTER BLADES

This article presents the main results on the development of prepregs and polymer composite materials (fiberglass and carbon fiber) based on the melting epoxy resin union and reinforcing fillers-glass-circuits of the T-64(VMP)-78, glass-winding RVMPN10-1200-14 and carbon fiber UMT49S-12K-EP. The process of developing prepregs, technologies for their manufacture on the impregnation, the choice of the main parameters of impregnation is described. The results of a study of the properties of the prepregs obtained under selected technological regimes and made from them PCM are also given.

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Reference list

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dx.doi.org/ 10.18577/2307-6046-2023-0-11-56-65

УДК 678.747.2

Kolokoltseva T.V., Popov J.O., Lantsov I.A., Gusev Y.A.

PREPREGS AND FIBERGLASS BASED ON VSR-3М RESIN AND FIBERGLASS FABRICS FOR USE IN HELICOPTER BLADES

This article presents the main results on the development of prepreg and carbon fiber based on the VSR-3M resin and carbon fabric grade VTkU-2.200. The process of studying prepreg, the technology of its production in an impregnation installation, and the selection of the main parameters of impregnation are described. Correct selection of impregnation parameters guarantees the production of materials with the required properties. The results of a study of the properties of prepreg obtained using the selected technological mode and carbon fiber reinforced plastic made from it are also presented.

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dx.doi.org/ 10.18577/2307-6046-2023-0-11-66-76

УДК 669.018.95:621.791.724

Shoshev F.L., Bogachev I.A., Sukhov D.I.

THE FEATURES OF PROCESSING AN ALUMINUM MATRIX COMPOSITE MATERIAL BY SELECTIVE LASER MELTING

The structure of aluminum matrix composite powder reinforced by silicon carbide particles and then spheroidized is investigated. The structure of selective laser melting material made of this powder is investigated as well. The main principles of forming of such structure are determined. In addiction an effect of gasostatic and heat treatment on selective laser melting material structure is considered.

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1. Kanth U.R., Rao P.S., Krishna M.G. Mechanical behaviour of fly ash/SiC particles reinforced Al–Zn alloy-based metal matrix composites fabricated by stir casting method. Journal of Materials Research and Technology, 2019, vol. 8, no. 1, pp. 737–744. DOI: 10.1016/J.JMRT.2018.06.003.
2. Kablov E.N., Evgenov A.G., Petrushin N.V., Shurtakov S.V., Zaitsev D.V. To the question of the mechanism of the formation of the thin structure of the track in the process of selective laser rafting. Metallovedenie i termicheskaya obrabotka metallov, 2023, no. 2 (812), pp. 44–55. DOI: 10.30906/Mitom.2023.2.44-55.
3. Aslanian G.G., Sukhov D.I., Mazalov P.B., Sulyanova E.A. Fractographic study of Co–Cr–Ni–W–Ta alloy samples obtained by selective laser melting. Trudy VIAM, 2019, no. 4 (76), paper no. 01. Available at: http://www.viam-works.ru (accessed: August 16, 2023). DOI: 10.18577/2307-6046-2019-0-4-3-10.
4. Ospennikova O.G., Naprienko S.A., Medvedev P.N., Zaitsev D.V., Rogalev A.M. Features of the formation of the structural-phase state of the EP648 alloy during selective lase manufacture. Trudy VIAM, 2021, no. 8 (102), paper no. 01. Available at: http://www.viam-works.ru (accessed: August 16, 2023). DOI: 10.18577/2307-6046-2021-0-8-3-11.
5. Nerush S.V., Kaplanskii Yu.Yu., Dynin N.V., Benarieb I., Savichev I.D. Development of laser powder bed fusion parameters, structure and mechanical properties of a high-strength aluminum alloy Al–Ce–Cu. Trudy VIAM, 2023, no. 1 (119), paper no. 05. Available at: http://www.viam-works.ru (accessed: August 16, 2023). DOI: 10.18557/2307-6046-2023-0-1-50-68.
6. Sukhov D.I., Kaplansky Yu.Yu., Rogalev A.M., Kurkin S.E. The features of processing Cr-rich nickel based alloy by selective laser melting. Trudy VIAM, 2023, no. 1 (119), paper no. 02. Available at: http://www.viam-works.ru (accessed: August 16, 2023). DOI: 10.18557/2307-6046-2023-0-1-15-27.
7. Stoyakina E.A., Kurbatkina E.I., Simonov V.N., Kosolapov D.V., Gololobov A.V. Mechanical properties of aluminium-matrix composite materials reinforсed with SiC particles, depending on the matrix alloy (review). Trudy VIAM, 2018, no. 2, paper no. 08. Available at: http://www.viam-works.ru (accessed: August 16, 2023). DOI: 10.18577 / 2307-6046-2018-0-2-8-8.
8. Nyafkin A.N., Shavnev A.A., Kurbatkina E.I., Kosolapov D.V. Studying the effect of silicon carbide particle size on the linear thermal expansion coefficient of the composite material based on aluminum alloy. Trudy VIAM, 2020, no. 2 (86), paper no. 05. Available at: http://www.viam-works.ru (accessed: August 16, 2023). DOI: 10.18577/2307-6046-2020-0-2-41-49.
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15. Canali R. Study, development and characterization of aluminum based materials by additive manufacturing: PhD thesis. Turin: Politecnico di Torino, 2015, 116 p. DOI: 10.6092/polito/porto/2598770.
16. Zhitnyuk S.V., Medvedev P.N. Investigation of microstructure and phase composition of the metallic composite material Al–Si–Mg system modified by silicon carbide particles by mechanical alloying. Part 1. Trudy VIAM, 2023, no. 1 (119), paper no. 08. Available at: http://www.viam-works.ru (accessed: August 16, 2023). DOI: 10.18577/2307-6046-2023-0-1-97-106.
17. Zhitnyuk S.V., Medvedev P.N. Investigation of microstructure and phase composition of the metallic composite material Al–Si–Mg system modified by silicon carbide particles by mechanical alloying. Part 2. Trudy VIAM, 2023, no. 1 (119), paper no. 09. Available at: http://www.viam-works.ru (accessed: August 16, 2023). DOI: 10.18577/2307-6046-2023-0-1-107-118.

dx.doi.org/ 10.18577/2307-6046-2023-0-11-77-89

УДК 621.318.2

Cherednichenko I.V., Bavina M.A., Bondarenko Yu.A., Shurygin V.D., Ovchinnikov A.D., Galimullin S.A.

INFLUENCE OF DIRECTED CRYSTALLIZATION PARAMETERS ON STRUCTURE AND PROPERTIES OF ALNICO 5-7 ALLOY PERMANENT MAGNETS

In this paper has been investigated influence of direct crystallizations parameters on permanent magnets alloy UNDKBA (Alnico 5-7) for non-defective percent. For this paper were produced permanent magnets by using different types of seeds and technological parameter. It established that the main parameters for manufacturing castings permanent magnets are temperature, broaching speed, composition and type of the seed. Revealed that slow broaching speed, monocrystalline seed with the crystallographic orientation allows to obtain permanent magnets with non-defective percent higher than 80.

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Reference list

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dx.doi.org/ 10.18577/2307-6046-2023-0-11-90-98

УДК 620.179

Kozlov I.A., Volkov I.A., Fomina M.A., Zakharov К.Е.

FEATURES OF CHEMICAL OXIDATION OF SEMI-FINISHED PRODUCTS OBTAINED BY SELECTIVE LASER MELTING FROM A METAL POWDER COMPOSITION OF THE ALLOY VAS1

The work is devoted to the adaptation of the traditional technology of chemical oxidation of parts and workpieces made of aluminum alloys obtained by traditional methods for surface treatment of parts manufactured by selective laser fusion and metal powder composition of the VAC1 alloy. The work investigated the compatibility and influence of the main chemical components of electrolytes on the stability of solutions and the quality of the formed coating. The performance of electrolytes for oxidation and various options for chemical preparation of the surface of samples from the alloy VAC1 are considered.

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Reference list

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2. Kablov E.N., Startsev O.V. The basic and applied research in the field of corrosion and ageing of materials in natural environments (review). Aviacionnye materialy i tehnologii, 2015, no. 4 (37), pp. 38–52. DOI: 10.18577/2071-9140-2015-0-4-38-52.
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14. Kravchenko D.V., Kozlov I.A., Nikiforov A.A. Methods for preparing the surface of aluminum alloys for electroplating (review). Trudy VIAM, 2021, no. 6 (100), paper no. 09. Available at: http://www.viam-works.ru (accessed: September 04, 2023). DOI: 10.18577/2307-6046-2021-0-6-82-99.
15. Zhelonkina S.I. Review of modern methods of preparing the surface of aluminum alloys for the application of metal coatings (part 1). Uprochnyayushchie tekhnologii i pokrytiya, 2021, vol. 17, no. 5 (197), pp. 227–231.
16. 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: 10.18577/2107-9140-2017-0-S-186-194.

10.

dx.doi.org/ 10.18577/2307-6046-2023-0-11-99-110

УДК 666.3

Kuznetsov B.Yu., Vlasov I.I., Grinevich D.V., Sorokin O.Ju.

MODELING THE DESTRUCTION OF A METAL-CERAMIC COMPOSITE MATERIAL WITH A MULTILAYER STRUCTURE BY THE FINITE ELEMENT METHOD

The purpose of this work is to determine the effect of the transitional diffusion zone at the interfacial boundary of the layers of the ceramic composite material of the Mo–Si–B system on the nature of destruction and physical and mechanical properties. Qualitative models have been created that make it possible to predict the most critical fracture zones of a composite material, and the effect of microstructure on the fracture mechanisms has been studied. Field tests of a ceramic-metal composite material with a multilayer structure were carried out, as a result of which a high convergence with the calculated models was established.

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Reference list

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9. Kablov E.N., Antipov V.V., Girsh R.I. Constructed layered materials based on sheets of aluminum-lithium alloys and fiberglass in the structures of new generation aircraft. Vestnik mashinostroyeniya, 2020, no. 12, pp. 46–52.
10. Sevalnev G.S., Dulnev K.V., Bannykh I.O., Krasulya A.A., Tsikh S.G., Lukin E.I. Investigation of the structure and properties of diffusion layers after boriding high nitrogen steels. Aviation materials and technologies, 2023, no. 1 (70), paper no. 02. Available at: http://www.journal.viam.ru (accessed: April 27, 2023). DOI: 10.18577/2307-6046-2023-0-1-17-29.
11. Shuwei Z., Rabczuk T., Zhuang X. Phase field modeling of quasi-static and dynamic crack propagation: COMSOL implementation and case studies. Advances in Engineering Software, 2018, no. 122, pp. 31–49.
12. Kablov E.N. New generation materials and digital technologies for their processing. Vestnik Rossiyskoy akademii nauk, 2020, vol. 90, no. 4, pp. 331–334.
13. Voronov V.A., Chainikova A.S., Lebedeva Yu.E., Zhitnyuk S.V. Production, physico-mechanical and tribotechnical properties of hot-pressed carbon-ceramic composite material on the basis of silicon carbide. Aviation materials and technologies, 2022, no. 2 (67), paper no. 07. Available at: http://www.journal.viam.ru (accessed: April 14, 2023). DOI: 10.18577/2713-0193-2022-0-2-74-84.
14. Kiiko V., Prokhorov D., Stroganova T. Investigation of heat resistance and structure of layered refractory composites reinforced by chemical compound with silicon, carbon, and boron. Scientific proceedings XIV International congress «Machines. Technologies. Materials», 2017, vol. VII, pp. 544–547.
15. Goncharov B.E., Sipatov A.M., Cherkashneva N.N., Pleskan A.Yu., Samokhvalov N.Yu., Vaganova M.L., Sorokin O.Yu., Solntsev St.S., Evdokimov S.A. Studies of thermal shock resistance of an anti-oxidation coating for a multi-layered ceramic composite. Aviation materials and technologies, 2021, no. 4 (65), paper no. 06. Available at: http://www.journal.viam.ru (accessed: April 23, 2023). DOI: 10.18577/2713-0193-2021-0-51-58.
16. Kiyko V.M., Korzhov V.P. Structure of layered composites Mo–Si–B and Nb–Si–B. Izvestiya RAN, ser.: Physical, 2017, vol. 81, no. 11, pp. 1513–1521.
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18. Korzhov V.P., Kiyko V.M. Phase structure of multilayer Nb/(Si–B) and Mo/(Si–B) composites after heat treatment under pressure. VI All-Rus. Conference on Nanomaterials. Moscow, 2016, pp. 386–387.

11.

dx.doi.org/ 10.18577/2307-6046-2023-0-11-111-122

УДК 620.178.35:669.245

Ryzhkov P.V., Gorbovets M.A., Khodinev I.A.

ENERGY CRITERIA FOR FATIGUE FRACTURE OF A HEAT-RESISTANT NICKEL ALLOY

Tests for low-cycle fatigue of a heat-resistant nickel alloy were carried out at operating temperature, deformation of tensile cycle and a frequency of 1 Hz. On the example of the obtained data of elastic-plastic deformation, the material constants of the Manson–Coffin and Ramberg–Osgood equations are determined. The main relationships that use the energy of destruction, necessary for predicting fatigue life, are considered. It is shown that the application of the energy criterion in terms of the accumulated strain energy density parameter more accurately describes the fatigue behavior in the low-cycle fatigue regime. The data obtained will make it possible in the second part of the article to use the energy criterion to predict the durability of the alloy under study under conditions of stress concentration.

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Reference list

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2. Socie D., Marquis G. Multiaxial Fatigue. SAE International, 1999, 502 p.
3. 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.
4. Erasov V.S., Oreshko E.I. Tests for fatigue of metal materials (review). Part 2. Analysis of the Basquin–Manson–Coffin equation. Methods of testing and processing of results. Aviation materials and technology, 2021, no. 1 (62), paper no. 08. Available at: http://www.journal.viam.ru (accessed: March 10, 2023). DOI: 10.18577/2071-9140-2021-0-1-80-94.
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7. Benedetti M., Berto F., Le Bone L., Santus C. A novel Strain-Energy-Density based fatigue criterion accounting for mean stress and plasticity effects on the medium-to-high-cycle uniaxial fatigue strength of plain and notched components. International Journal of Fatigue, 2020, vol. 133, p. 105397. DOI: 10.1016/j.ijfatigue.2019.105397.
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16. 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.
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18. Kablov E.N., Letnikov M.N., Ospennikova O.G., Bakradze M.M., Shestakova A.A. Particulars of the precipitation strengthening γʹ-phase during aging of heat-resistant wrought nickel superalloy VZh175-ID. Trudy VIAM, 2019, no. 9 (81), paper no. 01. Available at: http://www.viam-works.ru (accessed: August 15, 2023). DOI: 10.18577/2307-6046-2019-0-9-3-14.
19. Lomberg B.S., Shestakova A.A., Letnikov M.N., Bakradze M.M. The influence of temperature and stresses on nature of nanosize γʹ-phase in Ni-base superalloy VZh175-ID. Trudy VIAM, 2019, no. 12 (84), paper no. 01. Available at: http://www.viam-works.ru (accessed: August 13, 2023). DOI: 10.18577/2307-6046-2019-0-12-3-10.
20. Gorbovets M.A., Khodinev I.A., Ryzhkov P.V. Equipment for testing carrying out the strain-controlled low-cycle fatigue. Trudy VIAM, 2018, no. 9 (69), paper no. 06. Available at: http://www.viam-works.ru (accessed: August 03, 2023). DOI: 10.18577/2307-6046-2018-0-9-51-60.
21. Shun‐Peng Z., Lei Q., Huang H. et al. Mean stress effect correction in strain energy-based fatigue life prediction of metals. International Journal of Damage Mechanics, 2017, vol. 26, pp. 1219–1241.
22. Łagoda T. Energy models for fatigue life estimation under uniaxial random loading. Part I: The model elaboration. International Journal of Fatigue, 2001, vol. 23, is. 6, pp. 467–480.

12.

dx.doi.org/ 10.18577/2307-6046-2023-0-11-123-136

УДК 929

Grinevich A.V.

THE LEGACY OF PROFESSOR N.M. SKLYAROV(to the 115th anniversary of the birth)

The article, along with the achievements of N.M. Sklyarov, which have received universal recognition, examines the provisions developed by him, which determine the activities of the institute at the present time. The defining role of N.M. Sklyarov in the formation of the ideology of aviation armor, the creation of high-strength steel and in the development of a quality system of aviation materials is presented. The algorithm for the development of aviation materials formed by N.M. Sklyarov is the basis for meeting the requirements of the Airworthiness Standards of aircraft in terms of ensuring their safety and durability.

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Reference list

1. Grinevich A.V. Career of the Professor N.M. Sklyarov. Aviacionnye materialy i tehnologii, 2017, no. 3 (48), pp. 87–94. DOI: 10.18577/2071-9140-2017-0-3-87-94.
2. Dulnev R.A., Kotov P.I. Thermal fatigue of metals. Moscow: Mashinostroyenie, 1980, 200 p.
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13. VIAM 90 years: proud of the past, create the future. Ed. E.N. Kablov. Moscow: NRC «Kurchatov Institute» – VIAM, 2022, 168 p.
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15. Grinevich A.V., Slavin A.V., Yakovlev N.O., Gulina I.V. The phenomenon of breakdown destruction during stretching. Deformatsiya i razrusheniye materialov, 2020, no. 4, pp. 43–48. DOI: 10.31044/1814-4632-2020-4-43-48.
16. Sklyarov N.M. Aviation materials quality management. Aviation materials at the turn of the XX–XXI centuries. Moscow: VIAM, 1994, pp. 572–576.
17. Kapitsa P.L. The future of science: a stenigram of speech on the International Symposium in Prague on science planning. Moscow, 1962, 8 p.
18. Kablov E.N. Quality control of materials – a guarantee of the safety of the operation of aviation equipment. Aviation materials and technologies, 2001, no. 1, pp. 3–8.
19. Antipov V.V., Panteleev M.D., Sviridov A.V., Skupov A.A., Odintsov N.S. Heat-resistant aluminum alloys 1151 and B-1213 welded fuselage panels fabrication and testing. Trudy VIAM, 2023, no. 5 (123), paper no. 03. Available at: http://www.viam-works.ru (accessed: May 22, 2023). DOI: 10.18577/2307-6046-2023-0-4-27-39.
20. Mitrakov O.V., Yakovlev N.O., Yakusheva N.A., Grinevich A.V. Destruction features of steel 20ХГСН2МФА-ВД during the fracture toughness test. Aviacionnye materialy i tehnologii, 2019, no. 1 (54), pp. 49–56. DOI: 10.18577/2071-9140-2019-0-1-49-56.
21. Iakovlev N.O., Selivanov A.A., Gulina I.V., Grinevich A.V. Revisiting the durability of hinged-bolt connections. Aviacionnye materialy i tehnologii, 2020, no. 4 (61), pp. 79–85. DOI: 10.18577/2071-9140-2020-0-4-79-85.
22. 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.
23. Oreshko E.I., Erasov V.S., Yakovlev N.O., Utkin D.A. Methods for determining the mechanical characteristics of materials using indentation (review). Aviation materials and technology, 2021. no. 1 (62), paper no. 10. Available at: http://www.journal.viam.ru (accessed: July 08, 2023). DOI: 10.18577/2071-9140-2021-0-1-104-118.

13.

CONTENТS

Heat-resistant alloys and steels

Grigorenko V.B., Lukina Е.А., Terekhin А.М. Structural features destruction of monocrystalline materials

Deynega G.I., Kuzmina I.G., Bityutskaya O.N., Narsky A.R. Foam ceramic filters based on domestic refractory materials. Part 1

Polymer materials

Kulagina G.S., Zhelezina G.F., Levakova N.M., Safonov P.E. Polymer fibers in the composition of fabrics for self-lubricating antifriction materials

Kulagina G.S., Zhelezina G.F., Kan A.Ch., Kurshev E.V. Exploitation properties of antifriction selflubricating organoplastic based on fabric made of polytetrafluoroethylene and Аrcelon fibers

Composite materials

Kolokoltseva T.V., Popov Yu.O., Usacheva M.N., Gromova A.A. Prepregs of fiberglass and prepreg of carbon fiber on the basis of the resin VSE-67 for the use in the structures of helicopter blades

Kolokoltseva T.V., Popov Yu.O., Lantsov I.A., Gusev Yu.A. Prepregs and fiberglass based on VSR-3М resin and fiberglass fabrics for use in helicopter blades

Shoshev F.L., Bogachev I.A., Suhov D.I. The features of processing an aluminum matrix composite material by selective laser melting

Cherednichenko I.V., Bavina M.A., Bondarenko Yu.A., Shurygin V.D., Ovchinnikov A.D., Galimullin S.A. Influence of directed crystallization parameters on structure and properties of Alnico 5-7 alloy permanent magnets

Protective and functional

coatings

Kozlov I.A., Volkov I.A., Fomina M.A., Zakharov K.E. Features of chemical oxidation of semi-finished products obtained by selective laser melting from a metal powder composition of the alloy VAS1

Material tests

Kuznetsov B.Yu., Vlasov I.I., Grinevich D.V., Sorokin O.Yu. Modeling the destruction of a metal-ceramic сomposite material with a multilayer structure by the finite element method

Ryzhkov P.V., Gorbovets M.A., Hodinev I.A. Energy criteria for fatigue fracture of a heat-resistant nickel alloy

Outstanding scientists of VIAM

Grinevich A.V. The legacy of professor N.M. Sklyarov (to the 115th anniversary of the birth)

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