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dx.doi.org/ 10.18577/2307-6046-2018-0-5-3-11

УДК 669.018.44:699.245

Shestakova A.A., Karachevtsev F.N., Zhebelev N.M.

THE INVESTIGATION OF THE INFLUENCE OF AGEING TEMPERATURE ON STRUCTURAL AND PHASE TRANSFORMATIONS IN VZh177

The investigation results of the formation of strengthen phases (secondary carbides and γ'-phase) in new Ni-base superalloy VZh177 developed for jet-engine disk application are presented in the article. The structural and phase composition of the material after solution treatment and the further evolution of the microstructure during ageing were esteemed. The main carbide formation elements in bulk primary carbides were determined via the method of energy-dispersion spectroscopy. The nucleation dynamic of the fine dispersion carbides at grain boundaries was investigated via he method of scanning electron microscopy. The investigation of the strengthen γ'-phase morphology in the temperature range from 850 to 1000°C was presented. The dispersion range of the maximum volume of γ'-phase was established. The changing of mean diameter and morphology of the phase depending to ageing regime was also shown. The authors of the article suggest to investigate microhardness after various ageing tim

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1. Kablov E.N. Materialy novogo pokoleniya [Materials of new generation] // Zashchita i bezopasnost. 2014. №4. S. 28–29.
2. Ospennikova O.G. Strategiya razvitiya zharoprochnyh splavov i stalej specialnogo naznacheniya, zashhitnyh i teplozashhitnyh pokrytij [Strategy of development of hot strength alloys and steels special purpose, protective and heat-protective coverings] // Aviacionnye materialy i tehnologii. 2012. №S. S. 19–36.
3. Kablov E.N., Ospennikova O.G., Lomberg B.S. Sozdanie sovremennykh zharoprochnykh materialov i tekhnologij ikh proizvodstva dlya aviatsionnogo dvigatelestroeniya [Creation of modern heat resisting materials and technologies of their production for aviation engine building] // Krylya Rodiny. 2012. №3–4 S. 34–38.
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5. Razuvaev E.I., Bubnov M.V., Bakradze M.M., Sidorov S.A. GIP i deformatsiia granulirovannykh zharoprochnykh nikelevykh splavov [HIP and deformation of the granulated heat resisting nickel alloys] // Aviatsionnye materialy i tekhnologii. 2016. №S1 (43). S. 80–86. DOI: 10.18577/2071-9140-2016-0-S1-80-86.
6. Locq D., Caron (Onera) P. On Some Advanced Nickel-Based Superalloys for Disk Applications // High Temperature Materials AL03-01. 2011. Issue 3. P. 1–9.
7. Lomberg B.S., Bakradze M.M., Chabina E.B., Filonova E.V. Vzaimosvyaz struktury i svojstv vysokozharoprochnykh nikelevykh splavov dlya diskov gazoturbinnykh dvigatelej [Interrelation of structure and properties of high-heat resisting nickel alloys for disks of gas turbine engines] // Aviacionnye materialy i tekhnologii. 2011. №2. S. 25–30.
8. Gabb T.P., Gayda J., Johnson D.F. et al. Comparison of γ-γ′ Phase Coarsening Responses of Three Powder Metal Disk Superalloys // NASA/TM–2016-218936. February, 2016.
9. Ovsepyan S.V., Lomberg B.S., Bakradze M.M., Letnikov M.N. Termicheskaya obrabotka deformiruemykh zharoprochnykh nikelevykh splavov dlya diskov GTD [Thermal processing of deformable heat resisting nickel alloys for disks GTE] // Vestnik Moskovskogo gosudarstvennogo tekhnicheskogo universiteta im. N.E. Baumana. Ser.: Mashinostroenie. 2011. № SP2. S. 122–130.
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11. Zharoprochnyj deformiruemyj splav na osnove nikelya i izdelie, vypolnennoe iz etogo splava: pat. 2280091 Ros. Federatsiya. № 2004137299/02 [Heat resisting deformable alloy on the basis of nickel and the product executed from this alloy: pat. 2280091 Rus. Federation. No. 2004137299/02]; zayavl. 21.12.04; opubl. 20.07.06.
12. Kablov E.N., Ospennikova O.G., Lomberg B.S. Kompleksnaya innovacionnaya tehnologiya izotermicheskoj shtampovki na vozduhe v rezhime sverhplastichnosti diskov iz superzharoprochnyh splavov [Complex innovative technology of isothermal punching on air in mode of superplasticity of disks from superhot strength alloys] // Aviacionnye materialy i tehnologii. 2012. №S. S. 129–141.
13. Buyakina A.A., Letnikov M.N., Bakradze M.M., Shugaev S.A. Vliyanie termomekhanicheskoj i termicheskoj obrabotki na strukturu i svojstva splava VZH177 [The effect of thermomechanical and heat treatment parameters on structure and mechanical properties of superalloy VZH177] // Trudy VIAM: elektron. nauch.-tekhnich. zhurn. 2016. №10. St. 02. Available at: http://www.viam-works.ru (accessed: April 13, 2018). DOI: 10.18577/2307-6046-2016-0-10-2-2.
14. Filonova E.V., Bakradze M.M., Kochubey A.Ya., Vavilin N.L. Issledovanie izmenenij strukturno-fazovogo sostoyaniya splava VZh175 v processe goryachej deformacii i termicheskoj obrabotki [Structural-phase evolution of VZH175-alloy during hot deformation and heat treatment] // Aviacionnye materialy i tehnologii. 2014. №3. S. 10–13. DOI: 10.18577/2071-9140-2014-0-3-10-13.
15. Gaofeng Tian, Jinwen Zou, Yu Wang, Wuxiang Wang. Hot Deformation Behaviors and Microstructure Evolution in a New PM Nickel-Base Superalloy // Advanced Materials Research. 2011. Vol. 278. P. 411–416.
16. Lomberg B.S., Ovsepjan S.V., Bakradze M.M., Letnikov M.N., Mazalov I.S. Primenenie novyh deformiruemyh nikelevyh splavov dlja perspektivnyh gazoturbinnyh dvigatelej [The application of new wrought nickel alloys for advanced gas turbine engines] // Aviacionnye materialy i tehnologii. 2017. №S. S. 116–129. DOI: 10.18577/2071-9140-2017-0-S-116-129.

dx.doi.org/ 10.18577/2307-6046-2018-0-5-12-17

УДК 669.018.44:669.245

Lomberg B.S., Moiseev N.V., Letnikov M.N., Korotkiy A.V.

THE INFLUENCE OF ANNEALING TEMPERATURE IN ORIGINAL PRE-DEFORMATION ROUND BARS ON STRUCTURE AND MECHANICAL PROPERTIES OF FORGINGS MADE OF EP742-ID ALLOY

Now to low-dimensional gas turbine engines (GTE) widely apply disks made in FSUE «VIAM» from heat resisting deformable alloy EP742-ID. Initial preparations of punchings of disks for low-dimensional GTE are the press bars with a diameter of 140–150 mm made by method of extrusion from ingots with a diameter of 320 mm of double vacuum smelting (VI+VDP). Recrystallization of original compacted round bars made of EP742-ID alloy, used as a blank to the isothermal forging process of small-sized disks for gas-turbine engine, has been researched. Influence of recrystallization annealing in a single-phase area on mechanical properties of forgings material after finish heat treatment has been determine in the article. The conclusion is in summary drawn that carrying out annealing before deformation at temperature on 15–25°C above Тп.рγʹ allows to increase stability of plastic properties (δ, ψ, KCU) punchings from alloy EP742-ID, and also it is essential to reduce number of re-testing and repeat

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dx.doi.org/ 10.18577/2307-6046-2018-0-5-18-23

УДК 669.85/.86:006

Doriomedov M.S., Sevastyanov D.V., Skripachyov S.Yu., Daskovskiy M.I.

REFERENCE DOCUMENTATION IN THE FIELD OF RARE EARTH ELEMENTS

The major areas of application of rare earth elements in Russian industry are as follows: catalysts for the petrochemical industry (82%), steel industry (11%), materials for the nuclear energy industry (3%), permanent magnets (2%). Thus, the industrial applications of rare earth elements in high technologies give these minerals an immediate critical and strategic importance. the authors have set itself the goal to assess the regulatory framework in the field of rare earth elements. Comprehensive monitoring of the reference documentation in the field of rare earth elements was carried out. Differences in the Russian and foreign reference documentation were revealed. It was found that the Russian reference documentation consisted of state standards (GOST) developed 35–40 years ago, while foreign documentation included segmental documents. The need for actualization of the national reference documentation in the field of rare earth elements was justified.

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dx.doi.org/ 10.18577/2307-6046-2018-0-5-24-33

УДК 669.018.44:669.721.5

Volkova E.F., Mostyaev I.V., Akinina M.V.

COMPARATIVE ANALYSIS OF MECHANICAL PROPERTIES ANISOTROPY AND MICROSTRUCTURE OF SEMI-FINISHED PRODUCTS FROM HIGH-STRENGTH MAGNESIUM ALLOYS WITH REE

In recent years the problem of flight vehicles weight reduction becomes the most actual. At replacement of details from aluminum alloys on detail from high-strength magnesium alloys the weight economy about 20–25% can be reached. One of shortcomings of the deformed semi-finished products of high-strength magnesium alloys is anisotropy of their mechanical properties. It is conditionally possible to consider two types of anisotropy, in view of structural sign: – crystal (homogeneous) anisotropy; – heterogeneous (fibrous) anisotropy. For magnesium alloys both types of anisotropy are inherent. Anisotropy of mechanical properties can be reduced by applying the complicated scheme of deformation of material for receiving better structure and due to alloying magnesium, in particular, by rare earth metals (RE). The comparative analysis of results of microstructure research, phase structure research, mechanical properties and their anisotropy, investigation on example of high strength MA1

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dx.doi.org/ 10.18577/2307-6046-2018-0-5-34-43

УДК 678.073

Kirin B.S., Kuznetsova K.R., Petrova G.N., Sorokin A.E.

COMPARATIVE ANALYSIS OF PROPERTIES OF POLYETHERETHERKETONES OF DOMESTIC AND FOREIGN PRODUCTION

More than 40 years as polymeric matrix of PKM thermosetting materials were used. However complexity thermosetting binding, their limited viability, duration of process of curing and some other shortcomings stimulated use searches alternatively thermoflexible binding in the form of thermoflexible matrixes. Thermoplastics on level of strength and elastic characteristics do not concede to cured polymers, and on chemical resistance, warm and to electric insulation characteristics, tightness in some cases exceed the last. In the last years abroad tendency in development of KTM is use of high-heat-resistant constructional thermoplastics: poliarilsulfony, polyetherimide, polyetherketones, polyimide, etc. In Russia such materials commercially are not issued. Article is devoted to problem of import substitution of high-temperature constructional thermoplastics. The comparative assessment of strength and heatphysical properties of polyetheretherketones (PEEK) domestic (Institute of Plastics

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dx.doi.org/ 10.18577/2307-6046-2018-0-5-44-54

УДК 669.018.95

Antipov V.V., Kotova E.V., Serebrennikova N.Yu., Petrova A.P.

GLUE BINDERS AND GLUE PREPREGS FOR ALUMOPOLYMERIC COMPOSITE MATERIALS

Multilayer composite materials of GLARE type with metallic and polymeric layers of GLARE type regarding to sheet constructions for additional weight reduce and resource characteristics increase of aviation parts are shown in this paper. GLARE is a constructive aluminum glassfiber, where a combination of thin aluminum sheets and glue prepregs based on glassfiber provides a unique combination of properties: high strength and crack resistance with low density. It is shown that strength increase in GLARE type materials is provided by new filler material usage. A melt-type VSK-14-2mR glue compound based on a mix of defined structural epoxide olygomers and polyacrylsulfones has a low dynamic viscosity and good viscosity properties and was developed as a glass filler for RVMPN-10-400 roving with increased filament packing density and helps to reach maximum strength of polymeric composite material. Properties of fiberglass with KMKS-1.80.T60.37, KMKS-2.120.T60.37 and KMKS-2mR.120.RVMPN.30 g

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Reference list

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16. Serebrennikova N.Yu., Antipov V.V., Senatorova O.G., Erasov V.S., Kashirin V.V. Gibridnye sloistye materialy na baze alyuminij-litievyh splavov primenitelno k panelyam kryla samoleta [Hybrid multilayer materials based on aluminum-lithium alloys applied to panels of plane wing] // Aviacionnye materialy i tehnologii. 2016. №3 (42). S. 3–8. DOI: 10.18577/2071-9140-2016-0-3-3-8.
17. Oreshko E.I., Erasov V.S., Podjivotov N.Yu. Vybor shemy raspolozheniya vysokomodulnyh sloev v mnogoslojnoj gibridnoj plastine dlya ee naibolshego soprotivleniya potere ustojchivosti [Arrangement of high-modular layers in a multilayer hybrid plate for its greatest resistance to stability loss] // Aviacionnye materialy i tehnologii. 2014. №S4. S. 109–117. DOI: 10.18577/2071-9140-2014-0-S4-109-117.
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19. Oreshko E.I., Erasov V.S., Podzhivotov N.Yu., Lutsenko A.N. Raschet na prochnost gibridnoj paneli kryla na baze listov i profilej iz vysokoprochnogo alyuminijlitievogo splava i sloistogo alyumostekloplastika [Strength calculation of hybrid wing panel on the basis of sheets and profiles from high-strength aluminum lithium alloy and laminated aluminum fiberglass] // Aviacionnye materialy i tehnologii. 2016. №1 (40). S. 53–61. DOI: 10.18577/2071-9140-2016-0-1-53-61.

dx.doi.org/ 10.18577/2307-6046-2018-0-5-55-63

УДК 669.018.95:677.53

Grishina O.I., Serpova V.M.

INFLUENCE OF DIAMETER OF FIBERS OF SILICON CARBIDE ON MECHANICAL PROPERTIES OF THE METAL-MATRIX COMPOSITE (review)

The article is a review of foreign studies in the field of the influence of the diameter of reinforcing fibers of silicon carbide in metal matrix composite based on titanium alloys on mechanical behavior. The article consists of four parts. The introduction refers to the need to create composite materials based on high-temperature titanium alloys reinforced with carbide fibers for the creation of new generation aircraft. Within the framework of the implementation of the complex direction 12 Metal-matrix and poly-matrix composite materials reviewed foreign scientific and technical literature in the field of research, materials for the development of metal composite materials based on titanium alloys, fiber-reinforced refractory compounds of various diameters. At the beginning of the article, a detailed description of two types of silicon carbide fibers and methods for their production is given. The features of the structure and composition of the coating of core fibers considered in

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Reference list

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dx.doi.org/ 10.18577/2307-6046-2018-0-5-64-75

УДК 629.7.023.224

Kashin D.S., Dergacheva P.E., Stekhov P.A.

HEAT RESISTANT SLURRY COATINGS (review)

The slurry method is one of the most simple and economical methods of coating application. Thanks to it it is possible to apply coatings on large-sized products of complex shape. Slurry coatings are used to improve the heat resistance of various metallic, and also non-metallic materials. Slurry-resistant heat-resistant coatings applied to various groups of steels are based on Al, Al–Si, Cr–Al–Si, and also some other metals. It is shown that the aluminide coating at 650°C is operable for more than 40,000 h. Al–Si slurry coatings provide high protective properties at temperatures up to 450°C, as well as in contact with the Pb-Bi melt at 600°C. The Cr–Al–Si system protects steel from corrosion at elevated temperatures in corrosive environments. Coatings of SiO2–Al2O3–BaO and SiO2–Al2O3–B2O3 are used for deposition on iron-nickel alloys, reducing the oxidizability by 25–30 times at temperatures of 700°C. The system SiC–Si3N4–SiO2, is applied to sealing abradable materials of composition

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Reference list

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8. Sposob vosstanovleniya vysokotemperaturnogo kremnijsoderzhashchego zashchitnogo pokrytiya na zharoprochnykh konstruktsionnykh materialakh: pat. 2437961 Ros. Federatsiya [Way of recovery of high-temperature siliceous protecting cover on heat resisting constructional materials: pat. 2437961 Rus. Federation]; zayavl. 29.07.10; opubl. 27.12.11.
9. Kolovertnov D.V. Protsessy okisleniya steklokeramicheskikh kompozitsij na osnove borida tsirkoniya i kremnijsoderzhashchikh soedinenij: dis. ... kand. khim. nauk [Processes of oxidation of glassceramic compositions on the basis of boride of zirconium and siliceous connections: thesis, PhD (Chem.)]. SPb., 2012. 215 s.
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11. Plotnikova A.S. Zakonomernosti geterogennykh vzaimodejstvij pri sinteze reaktsionno-svyazannykh zashchitnykh pokrytij dlya uglerodnykh materialov [Patterns of heterogeneous interactions at synthesis of the reactionary and connected protecting covers for carbon materials] // I Mezhdistsiplinarnaya shkola-seminar «Khimiya neorganicheskikh materialov i nanomaterialov»: sb. tez. dokl. M., 2006. S. 28–31.
12. Astapov A.N. Razrabotka vysokotemperaturnykh zashchitnykh pokrytij na uglerodsoderzhashchie kompozitsionnye materialy primenitelno k osoboteplonagruzhennym elementam konstruktsij aviakosmicheskoj i raketnoj tekhniki: dis. ...kand. tekhn. nauk [Development of high-temperature protecting covers on carbon-containing composite materials with reference to especially heat loaded elements of designs aerospace and rocketry: thesis, PhD (Tech.)]. M., 2011. 207 s.
13. Terenteva V.S., Zhestkov B.E. Mnogofunktsionalnye vysokotemperaturnye pokrytiya D5 MAI i M1 MAI [Multifunction high temperature coatings Д5 of MAI and М1 MAI] // Khimicheskaya fizika. 2009. T. 28. №5. S. 64–70.
14. Gildebrandt E.M., Vershinina E.P., Frizorger V.K. Zashchita poverkhnosti anoda alyuminievogo elektrolizera ot okisleniya [Surface protection of the anode of aluminum reduction cell from oxidation] // Journal of Siberian Federal University. Engineering & Technologies. 2010. №3. S. 272–283.
15. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitiya materialov i tehnologij ih pererabotki na period do 2030 goda» [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. №1 (34). S. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
16. Golubeva O.V., Markov V.G., Yakovlev V.A., Chikiryaka A.V. Metod povysheniya soprotivleniya okisleniyu v teplonositele svinets–vismut [Method of increase of resistance to oxidation in the heat-carrier lead-bismuth] // Voprosy materialovedeniya. 2008. №4 (56). S. 106–115.
17. Galoyan A.G., Muboyadzhyan S.A., Egorova L.P., Bulavinceva E.E. Korrozionnostojkoe pokrytie dlya zashhity detalej GTD iz vysokoprochnyh konstrukcionnyh martensitostareyushhih stalej na rabochie temperatury do 450°C [Corrosion-resistant coating for protection of GTE details made of high-strength maraging constructional steel with operating temperature up to 450°C] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №6. St. 03. Available at: http://www.viam-works.ru (accessed: May 11, 2018). DOI: 10.18577/2307-6046-2014-0-6-3-3.
18. Agüero A., Muelas R., Pastor A., Osgerby S. Long exposure steam oxidation testing and mechanical properties of slurry aluminide coatings for steam turbine components // Surface & Coatings Technology. 2005. No. 200. P. 1219–1224.
19. Agüero A., Muelas R., Gutierrez M., Van Vulpen R., Osgerby S., Banks J.P. Cyclic oxidation and mechanical behaviour of slurry aluminide coatings for steam turbine components // Surface & Coatings Technology. 2007. No. 201. P. 6253–6260.
20. Protective system for high temperature metalalloy products: pat. US 6682780 B2; publ. 27.01.04.
21. Solntsev S.St., Shvagireva V.V., Isaeva N.V., Soloveva G.A. Mnogocelevoe stekloemalevoe pokrytie dlya zashhity lityh fasonnyh detalej gazoturbinnyh dvigatelej [Multipurpose glass-enamel coating for protection of cast parts of gas turbine engines] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №3. St. 04. Available at: http://www.viam-works.ru (accessed: May 11, 2018). DOI: 10.18577/2307-6046-2014-0-3-4-4.
22. Rozenenkova V.A., Solntsev St.S., Mironova N.A. Tonkoplenochnye pokrytiya dlya uplotnitelnykh istiraemykh materialov na osnove diskretnykh volokon dlya protochnogo trakta GTD [Thin-film coatings for discrete fibers based sealing abraded materials of the wheel space gas turbine engine path] // Trudy VIAM: elektron. nauch.-tekhnich. zhurn. 2013. №5. St. 03. Available at: http://www.viam-works.ru (accessed: May 11, 2018).
23. Denisova V. S., Solov'eva G. A., Orlova L.A. Sintez resursnykh zharostojkikh emalevykh pokrytij na osnove stekol barijalyumosilikatnoj sistemy dlya nikelevykh splavov [Synthesis of resource heat resisting enamel coatings on the basis of glasses of barium silica-alumina system for nickel alloys] // Uspekhi v khimii i khimicheskoj tekhnologii. 2014. T. XXVIII. №8. S 39–42.
24. Pugacheva N.B. Sovremennye tendentsii razvitiya zharostojkikh pokrytij na osnove alyuminidov zheleza [Current trends of development of heat resisting coverings on the basis of iron aluminides] // Diagnostics, Resource and Mechanics of materials and structures. 2015. №3. S 51–82.
25. Slurry compositions for diffusion coatings: pat. 6110262 US; publ. 29.08.00.
26. Denisova V.S., Soloveva G.A. Zharostojkoe steklokeramicheskoe pokrytie zhdya zashchity detalej kamer sgoraniya gazoturbinnykh dvigatelej [Heat-resistant glass-ceramic coating for protection of gas turbines’ combustion chambers parts] // Aviacionnye materialy i tehnologii. 2016. №4 (45). S. 18–22. DOI: 10.18577/2071-9140-2016-0-4-18-22.
27. Solntsev S.S. Vysokotemperaturnye kompozitsionnye materialy i pokrytiya na osnove stekla i keramiki dlya aviakosmicheskoj tekhniki [High-temperature composite materials and coverings on the basis of glass and ceramics for aerospace equipment] // Rossijskij khimicheskij zhurnal. 2010. №1. S. 25–33.
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29. Sposob naneseniya pokrytiya: pat. 2214475 Ros. Federatsiya [Coating application method: pat. 2214475 Rus. Federation]; zayavl. 27. 11.01; opubl. 20.10.03.
30. Karasik T.L. Vliyanie oksidov shchelochnozemelnykh metallov na svojstva zharostojkikh pokrytij [Influence of oxides of alkaline earth metals on properties of heat resisting coverings] // Zbіrnik naukovikh prats PAT «Ukrndі vognetrivіv іm. A. S. Berezhnogo». 2013. №113. S. 240–245.

dx.doi.org/ 10.18577/2307-6046-2018-0-5-76-89

УДК 669.3

Artemenko N.I.

RESEARCH OF THE OPERATION MODES OF THE METCO F4 SERIAL PLASMA-GUN USING PLASMA-FORMING GASES ARGON AND NITROGEN

In this paper was obtained the analytical dependence of the total and voltage power of the plasma arc on the arc current and the flow rates of argon and nitrogen of the serial plasma-gun Metco F4. It is established that an increase in nitrogen consumption has the greatest effect on the increase in arc voltage. A computational and graphical technique for estimating the average temperature and the velocity of the plasma flow at the cutoff of the nozzle of the serial plasma-gun Metco F4 is proposed.

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10.

dx.doi.org/ 10.18577/2307-6046-2018-0-5-90-100

УДК 629.7.023.224

Pavlova T.V., Dobrynin D.A., Avanesyan T.G., Muboyadzhyan S.A.

ELECTROLYTIC-PLASMA METHOD OF REMOVING THE HEAT-RESISTANT COATING FROM THE SURFACE OF NICKEL ALLOY PRODUCTS

To increase the reliability and the service life of gas turbine engine (GTE) blades, heat-resistant coatings are used. The repeated use of the GTE blades after their operation or in violation of the technology of applying protective coatings is possible only in case of removing the defective coating and subsequent preparation of the blade surface for its repeated application. The currently used surface preparation methods for re-applying protective coatings are based on the preliminary cleaning of the GTE blades from the combustion products of the fuel, removal of protective coatings and surface finishing. A comparative analysis of traditional methods of removing spent coatings has shown that the electrolytic-plasma treatment method is distinguished by high productivity, high quality of the treated surface, no need for intermediate preparation stages, and its environmental friendliness. The disadvantages of this method include the inability to process the internal cavities of parts, a

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Reference list

1. Kablov E.N., Ospennikova O.G., Petrushin N.V., Visik E.M. Monokristallicheskij zharoprochnyj nikelevyj splav novogo pokoleniya s nizkoj plotnostyu [Single-crystal nickel-based superalloy of a new generation with low-density] // Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 14–25. DOI: 10.18577/2071-9140-2015-0-2-14-25.
2. Kablov E.N. Strategicheskie napravleniya razvitiya materialov i tehnologij ih pererabotki na period do 2030 goda [The strategic directions of development of materials and technologies of their processing for the period to 2030] // Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.
3. Kablov E.N., Muboyadzhyan S.A. Zharostojkie i teplozashhitnye pokrytiya dlya lopatok turbiny vysokogo davleniya perspektivnyh GTD [Heat resisting and heat-protective coverings for turbine blades of high pressure of perspective GTE] // Aviacionnye materialy i tehnologii. 2012. №S. S. 60–70.
4. Kablov E.N., Startsev O.V., Medvedev I.M. Obzor zarubezhnogo opyta issledovanij korrozii i sredstv zashhity ot korrozii [Review of international experience on corrosion and corrosion protection] // Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 76–87. DOI: 10.18577/2071-9140-2015-0-2-76-87.
5. Kablov E.N., Muboyadzhyan S.A., Budinovskij S.A., Pomelov YA.A. Ionno-plazmennye zashchitnye pokrytiya dlya lopatok gazoturbinnykh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] // Konversiya v mashinostroenii. 1999. №2. S.42–47.
6. Muboyadzhyan S.A., Aleksandrov D.A., Gorlov D.S., Egorova L.P., Bulavinceva E.E. Zashhitnye i uprochnyayushhie ionno-plazmennye pokrytiya dlya lopatok i drugih otvetstvennyh detalej kompressora GTD [Protective and strengthening ion-plasma coverings for blades and other responsible details of the GTE compressor] // Aviacionnye materialy i tehnologii. 2012. №S. S. 71–81.
7. Kablov D.E., Belyaev M.S., Sidorov V.V., Min P.G. Vliyanie primesej sery i fosfora na malociklovuyu ustalost monokristallov zharoprochnogo splava ZhS36-VI [The influence of sulfur and phosphorus impurities on low cycle fatigue of single crystals of ZhS36-VI alloy] // Aviacionnye materialy i tehnologii. 2015. №4 (37). S. 25–28. DOI: 10.18577/2071-9140-2015-0-4-25-28.
8. Kablov D.E., Sidorov V.V., Budinovskij S.A., Min P.G. Vliyanie primesi sery na zharostojkost monokristallov zharoprochnogo splava ZhS36-VI s zashhitnym pokrytiem [The influence of sulfur impurity on heat resistance of single crystals of ZhS36-VI alloy with protective coating] // Aviacionnye materialy i tehnologii. 2016. №1 (40). S. 20–23. DOI: 10.18577/2071-9140-2016-0-1-20-23.
9. Kablov E.N., Muboyadzhyan S.A., Budinovskij S.A., YAgodkin YU.D. Perspektivy primeneniya ionno-plazmennoj tekhnologii vysokikh energij dlya mezhresursnogo remonta lopatok turbin [Perspectives of application of ion-plasma technology of high energy for interresource repair of blades of turbines] // Aviacionnye materialy i tehnologii. 2002. №1. S. 6–13.
10. Method for cleaning metal parts with elemental fluorine: pat. US4188237A; publ. 02.02.78.
11. Method of removing a thermal barrier coating: pat. US6238743B1; publ. 20.01.00.
12. Shoe form: pat. US1784661A; publ. 24.10.29.
13. Sposob remonta lopatok turbiny gazoturbinnogo dvigatelya: pat. 2367554 Ros. Federatsiya [Way of repair of turbine blades of the gas turbine engine: pat. 2367554 Rus. Federation]; opubl. 08.08.07.
14. Rastvor dlya udaleniya alyuminijsoderzhashchikh mnogokomponentnykh zharostojkikh pokrytij s nikelevykh splavov: pat. 1324344 Ros. Federatsiya [Solution for removal of aluminum containing multicomponent heat resisting coverings from nickel alloys: pat. 1324344 Rus. Federation]; opubl. 07.09.85.
15. Sposob udaleniya pokrytiya s metallicheskoj podlozhki: pat. 2094546 Ros. Federatsiya [Way of removal of covering from metal substrate: pat. 2094546 Rus. Federation]; opubl. 04.03.95.
16. Process for removing chromide coatings from metal substrates, and related compositions: pat. US6953533B2; publ. 16.06.03.
17. Method for removing aluminide coating from metal substrate and turbine engine part so treated: pat. US7008553B2; publ. 09.01. 03.
18. Method for chemically stripping a cobalt-base substrate: pat. US5944909A; publ. 02.02.98
19. Process of selectively removing layers of a thermal barrier coating system: pat. US6955308B2; publ. 23.06.03.
20. Method of removing a coating from a substrate: pat. US6905396B1; publ. 20.11.03.
21. Chemical stripping composition and method: pat. US8859479B2; publ. 26.09.11.
22. Method of decoating a turbine blade: United States paten US6660102B2; publ. 27.12.00.
23. Process for applying a protective layer: pat. US7736704B2; publ. 15.09.04.
24. Method for removal of surface layers of metallic coatings: pat. US6036995A; publ. 31.01.97.
25. Kulikov I.S., Vashchenko S.V., Kamenev A.YA. Elektrolitno-plazmennaya obrabotka materialov [Electrolit plasma processing of materials]. Minsk: Belоruskaya nauka, 2010. 232 s.

11.

dx.doi.org/ 10.18577/2307-6046-2018-0-5-101-109

УДК 620.193.21

Kurs M.G.

FORECASTING THE STRENGTH PROPERTIES OF THE SKIN COVER OF A DEFORMABLE ALUMINUM ALLOY В95о.ч.-Т2 WITH THE USE OF THE INTEGRATED CORROSION REDUCTION COEFFICIENT

At present, the issue of developing methods for predicting the change in the strength properties of structural aluminum alloys used in the composition of structural elements in conditions of environmental factors for long periods of operation is topical. In this case, the key is to search for the principal approaches to predicting the corrosive behavior of aluminum alloys as materials for which uneven corrosion damage is characteristic, and assessing the complex effect of the most dangerous types of local corrosion on the change in the mechanical properties of aluminum alloys. The calculation of the integral coefficient of corrosion failure based on the predicted values of the main corrosion characteristics of aluminum alloys-loss of weight, depth of pitting and intercrystalline corrosion, as well as the tendency to delaminating corrosion, has been performed. It is shown that the application of the method of calculating the integral corrosion coefficient can be used to obtain the pred

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Reference list

1. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitiya materialov i tehnologij ih pererabotki na period do 2030 goda» [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. №1 (34). S. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
2. Antipov V.V. Strategiya razvitiya titanovyh, magnievyh, berillievyh i alyuminievyh splavov [Strategy of development of titanium, magnesium, beryllium and aluminum alloys] // Aviacionnye materialy i tehnologii. 2012. №S. S. 157–167.
3. Kablov E.N., Startsev O.V., Medvedev I.M. Obzor zarubezhnogo opyta issledovanij korrozii i sredstv zashhity ot korrozii [Review of international experience on corrosion and corrosion protection] // Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 76–87. DOI: 10.18577/2071-9140-2015-0-2-76-87.
4. Samojlov I.A., Stradomskij O.Yu., Shapkin V.S. Sostoyanie grazhdanskoj aviatsionnoj tekhniki Rossii i prognoz ee obnovleniya do 2030 goda [Condition of civil aviation engineering of Russia and the forecast of its updating till 2030] // Nauchnyj vestnik MGTUGA. 2013. Vyp. 187. S. 7–18.
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12. Mikhajlov A.A., Panchenko Yu.M., Igonin T.N. i dr. Atmosfernaya korroziya uglerodistoj stali: modelirovanie i kartografirovanie territorii Rossijskoj Federatsii [Atmospheric corrosion of carbon steel: modeling and mapping of the territory of the Russian Federation] // Korroziya: materialy, zashchita. 2010. №11. S. 1–10.
13. Lutsenko A.N., Kurs M.G., Laptev A.B. Obosnovanie srokov naturnykh klimaticheskikh ispytanij metallicheskikh materialov v atmosfere chernomorskogo poberezhya. Analiticheskij obzor [Justification of terms of natural climatic tests of metal materials in the atmosphere of the Black Sea coast. Analytical review] // Voprosy materialovedeniya. 2016. №3 (87). S. 126–137.
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12.

dx.doi.org/ 10.18577/2307-6046-2018-0-5-110-118

УДК 539.24

Startsev V.O., Plotnikov V.I., Antipov Yu.V.

REVERSIBLE INFLUENCE OF MOISTURE ON THE MECHANICAL PROPERTIES OF PCM AFTER WEATHERING

Mechanical properties of glass and carbon reinforced plastics were investigated after natural weathering in mild warm climate. The seasonal changes in mechanical properties of PCMs were found to be in agreement with moisture content in the samples. The difference in compressive and bending strength of VKU-49 carbon fiber reinforced plastic, measured in winter and summer month reached 10%. It was shown that for evaluation of reversible influence of moisture during the natural weathering measurements of the mechanical properties of PCM should be measured in three states: without conditioning, after drying and after moisture absorption till the steady state.

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