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dx.doi.org/ 10.18577/2307-6046-2019-0-1-3-12

УДК 669.018.44:543.42

Raevskih A.N., Chabina E.B., Petrushin N.V., Filonova E.V.

Boundary between single-crystal substrate and received by selective laser melting alloy ZhS32-VI structural and phase changes after high temperatures and tension influence investigation

By Scanning Electron Microscopy (SEM) and Electrons Back Scattering Diffraction (EBSD) means sample structure in transitional area between single-crystal ZhS32-VI alloy substrate with crystallographic orientation <001> and alloy ZhS32-VI, received on the same substrate by selective laser melting, after traction tests at temperature 1100°С is investigated. Structural changes in local subgrains disorientation sites, caused by microtension raised level are established.

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Reference list

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dx.doi.org/ 10.18577/2307-6046-2019-0-1-13-20

УДК 678.6

Prokopova L.A., Golovina E.Yu.

About the technological properties stability of type I epoxy resins after the warranty period expiration

Test methods for two important quality properties of type I epoxy resins produced by Russian industry are described. The reasons to select the specific research methods are noticed. The epoxy content and the dynamic viscosity of expired type I epoxy resins are determined. It was found that highly purified expired type I epoxy resins preserve their technological properties for a long time subject to the storage conditions.

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Reference list

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dx.doi.org/ 10.18577/2307-6046-2019-0-1-21-30

УДК 678.4

Chaykun A.М., Venediktova M.A., Bryk Ya. А.

Development of the compounding of rubber extremely high heat resistance with temperature range of exploitation from the -60 to +500°С

In some cases, products of special purpose require application of sealing details on the basis of the elastomer, capable to provide working capacity at high temperatures at least short time. The choice for the specified purposes of rubbers is caused by unique highly elastic properties of the elastomer, allowing providing the hard contact of surfaces at small pressing effort. Besides, in this case process of assembly and forming of seal assembly in products of difficult configuration considerably becomes simpler. Application for these purposes of more heat-resistant metals or fluoroplastic is connected with considerable technological difficulties. The solution of the specified problem is impossible without development of compounding of rubber, ability to provide necessary technical characteristics in the expanded temperature range. Besides, features of creation of compounding and property of the specified rubber in many respects define both approaches to development and choice of optimum options of manufacturing techniques of products from it. The declared approaches will allow not only developing rubber with considerably improved complex of properties, but also in the maximum degree to keep them upon transition to manufacturing of specific products.

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Reference list

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dx.doi.org/ 10.18577/2307-6046-2019-0-1-31-39

УДК 678.072, 678.078

Kudryavtseva A.N., Tkachuk A.I., Grigoreva K.N., Gurevich Y.M.

The use of epoxy resin system VSE-30, processed by the infusion technology, for the manufacture of low and medium loaded structural polymer composite materials

In the present work, the main physicochemical and thermomechanical characteristics of a two-component epoxy resin system VSE-30, processed by infusion technology and developed at the FSUE «VIAM», are considered. The DSC method is used to study the kinetic parameters of the curing process and to study the effect of the final curing temperature on the level of mechanical and thermomechanical properties of the cured binder VSE-30. The comparison of obtained data with domestic and foreign analogues are given. It has been established that lowering the curing temperature has little effect on the total thermal effect of the reaction. The optimum curing mode of the epoxy resin system VSE-30 at a low temperature is chosen, which allows to obtain materials with a slight decrease in their glass transition temperature and strength properties.

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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. Kablov E.N. Materialy novogo pokoleniya – osnova innovatsiy, tekhnologicheskogo liderstva i natsionalnoy bezopasnosti Rossii [Materials of the new generation - the basis of innovation, technological leadership and national security of Russia] // Intellekt i tekhnologii. 2016. №2. S. 16–22.
3. Kablov E.N., Chursova L.V., Babin A.N., Mukhametov R.R., Panina N.N. Razrabotki FGUP «VIAM» v oblasti rasplavnykh svyazuyushchikh dlya polimernykh kompozitsionnykh materialov [Developments of FSUE «VIAM» in the field of melt binders for polymer composite materials] // Polimernyye materialy i tekhnologii. 2016. T. 2. №2. S. 37–42.
4. Veshkin E.A. Tekhnologii bezavtoklavnogo formovaniya nizkoporistykh polimernykh kompozitsionnykh materialov i krupnogabaritnykh konstruktsiy iz nikh: dis. … kand. tekhn. Nauk [Technologies of non-autoclaving molding of low-porous polymer composite materials and large-sized structures of them: thesis, Cand. Sc. (Tech.)]. M., 2016. 146 s.
5. Grigorev M.M., Hrulkov A.V., Gurevich Ya.M., Panina N.N. Izgotovlenie stekloplastikovyh obshivok metodom vakuumnoj infuzii s ispolzovaniem epoksiangidridnogo svyazuyushhego i polupronicaemoj membrany [Manufacture of fiberglass skins using vacuum infusion using epoxyanhydride resin and a semipermeable membrane] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №2. St. 04. Available at: http://viam-works.ru (accessed: November 20, 2018). DOI: 10.18577/2307-6046-2014-0-2-4-4.
6. Kablov E.N. Kompozity: segodnya i zavtra [Composites: today and tomorrow] // Metally Evrazii. 2015. №1. S. 36–39.
7. Dry fibrous material for subsequent resin infusion: pat. WO 2013096377; filed 20.12.11; publ. 27.06.13.
8. Michelsa J., Widmann R., Czaderski C., Allahvirdizadeh R., Motavalli M. Glass transition evaluation of commercially available epoxy resins used for civil engineering applications // Composites Part B: Engineering 2015. Vol. 77. P. 484–493. DOI: 10.1016/j.compositesb.2015.03.053.
9. Ricciardi M.R., Antonucci V., Durante M. et al. A new cost-saving vacuum infusion process for fiber-reinforced composites: Pulsed infusion // Journal of Composite Materials. 2014. Vol. 48 (11). R. 1365–1373.
10. Kompaniya «KORSIL TREYD» Lamborghini vybirayet Araldite® [Company «KORSIL TRADE» Lamborghini chooses Araldite®] // Kompozitnyy mir. 2013. №4. S. 34–36.
11. Shchepotova A., Raykhlin L., Yatsenko S. Nekotoryye aspekty infuzii krupnogabaritnykh konstruktsiy [Some aspects of the infusion of large structures] // Kompozitnyy mir. 2013. №4. S. 44–51.
12. Arulappan C., Duraisamy A., Adhikari D., Gururaja S. Investigations on pressure and thickness profiles in carbon fiber-reinforced polymers during vacuum assisted resin transfer molding // Journal of Reinforced Plastics and Composites. 2015. Vol. 34. Is. 1. P. 3–18.
13. Savin S.P. Primeneniye sovremennykh polimernykh kompozitsionnykh materialov v konstruktsii planera samoletov semeystva MS-21 [The use of modern polymer composite materials in the construction of a glider of airplanes of the MS-21 family] // Izvestiya Samarskogo nauchnogo tsentra Rossiyskoy akademii nauk. 2012. T. 14. №4 (2). S. 686–693.
14. Chursova L.V., Kim M.A., Panina N.N., Shvetsov E.P. Nanomodificirovannoe epoksidnoe svyazuyushhee dlya stroitelnoj industrii [Nanomodified epoxy binder for the construction industry] // Aviacionnye materialy i tehnologii. 2013. №1. S. 40–47.
15. Chursova L.V., Grebeneva T.A., Panina N.N., Tsybin A.I. Svyazuyushchiye dlya polimernykh kompozitsionnykh materialov stroitelnogo naznacheniya [Binders for polymeric composite materials for construction] // Vse materialy. Entsiklopedicheskiy spravochnik. 2015. №8. S. 13–17.
16. Mishkin S.I., Raskutin A.E., Evdokimov A.A., Gulyaev I.N. Tehnologii i osnovnye etapy stroitelstva pervogo v Rossii arochnogo mosta iz kompozicionnyh materialov [Technologies and the main stages of construction of the arch bridge first in Russia from composite materials] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2017. №6 (54). St. 05. Available at: http://www.viam-works.ru (accessed: November 20, 2018). DOI: 10.18577/2307-6046-2017-0-6-5-5.
17. Doneckij K.I., Karavaev R.Yu., Raskutin A.E., Panina N.N. Svojstva ugle- i stekloplastikov na osnove pletenyh preform [Properties of carbon fiber and fiberglass on the basis of braiding preforms] // Aviacionnye materialy i tehnologii. 2016. №4 (45). S. 54–59. DOI: 10.18577/2071-9140-2016-0-4-54-59.
18. Chursova L.V., Babin A.N., Panina N.N., Tkachuk A.I., Terekhov I.V. Ispolzovaniye aromaticheskikh aminnykh otverditeley dlya sozdaniya epoksidnykh svyazuyushchikh dlya PKM konstruktsionnogo naznacheniya [Usage of aromatic amine curing agents for epoxy resins binders for production of structural PCM] // Trudy VIAM: electron. nauch.-tehnich. zhurn. 2016. №6 (42). St. 04. Available at: http://www.viam-works.ru (accessed: November 20, 2018). DOI: 10.18577/2307-6046-2016-0-6-4-4.
19. Donetskiy K.I., Khrulkov A.V. Printsipy «zelenoy khimii» v perspektivnykh tekhnologiyakh izgotovleniya izdeliy iz PKM [Principles of «green chemistry» in perspective manufacturing technologies of PCM articles] // Aviacionnye materialy i tehnologii. 2014. №S2 (44). S. 24–28. DOI: 10.18577/2071-9140-2014-0-s2-24-28.
20. Antyufeeva N.V., Aleksashin V.M., Stolyankov Yu.V. Opredelenie stepeni otverzhdeniya PKM metodami termicheskogo analiza [Polymer composite curing degree evaluation by thermal analysis test methods] //Aviacionnye materialy i tehnologii. 2015. №3 (36). S. 79–83.

dx.doi.org/ 10.18577/2307-6046-2019-0-1-40-46

УДК 669.715

Antipov V.V., Konovalov A.N., Serebrennikova N.Yu., Somov A.V., Nefedova Yu.N.

Influence of structure on fire resistance and fireproof FMLs SIAL-type and possibility of application of data of materials in aircraft industry

A method of fire resistance testing subject to foreign and national regulations of materials made for fire dangerous areas in aircraft engineering was developed. Different compositions of aluminum fiber-glass materials based on 1441 Al–Li alloy sheets were tested to determine a fire-resistance value. Recommendations of forming an aluminum fiber-glass material to enhance a fire resistance level are stated. Technological process of manufacturing of aviation details with requirements of fire resistance is described through the example aircraft engine cowling prototype manufacture.

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Reference list

1. Fridlyander I.N. Vospominaniya o sozdanii aviakosmicheskoy i atomnoy tekhniki iz alyuminiyevykh splavov [Memories of the creation of aerospace and nuclear technology from aluminum alloys]. M.: Nauka, 2005. 275 s.
2. Kablov E.N. Materialy novogo pokoleniya – osnova innovatsiy, tekhnologicheskogo liderstva i natsionalnoy bezopasnosti Rossii [Materials of the new generation - the basis of innovation, technological leadership and national security of Russia] // Intellekt & Tekhnologii. 2016. №2. S. 41–46.
3. Kablov E.N. Kompozity: segodnya i zavtra [Composites: today and tomorrow] // Metally Yevrazii. 2015. №1. S. 36–39.
4. Kablov E.N. O nastoyashchem i budushchem VIAM i otechestvennogo materialovedeniya: interv'yu [About the present and the future of the Institute of Scientific and Technical Information and Russian Materials Science: an interview] // Rossiyskaya akademiya nauk. 2015. 19 yanvarya. S. 10–15.
5. Raskutin A.E. Strategiia razvitiia polimernykh kompozitsionnykh materialov [Development strategy of polymer composite materials] // Aviatsionnye materialy i tekhnologii. 2017. №S. S. 344–348. DOI: 10.18577/2071-9140-2017-0-S-344-348.
6. 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.
7. Roebroeks G.H.J.J. GLARE: a structural material for fire resistant fuselages // AGARD Conference Proceedings. October, 1996. R. 26–1; 26–13.
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9. Fridlyander I.N., Senatorova O.G., Anikhovskaya L.I. Struktura i svoystva konstruktsionnykh alyumostekloplastikov marki SIAL [Structure and properties of structural aluminum-glass plastics of the SIAL brand] // Sloistyye kompozitsionnyye materialy – 98: sb. tr. Mezhdunar. konf. Volgograd, 1998. S. 131–133.
10. Shavnev A.A., Kurbatkina E.I., Kosolapov D.V. Metody sozdaniya alyuminiyevykh kompozitsionnykh materialov [Methods for joining of aluminum composite materials (review)] // Aviacionnye materialy i tehnologii. 2017. №3 (38). S. 35–42. DOI: 10.18577/2071-9140-2017-0-3-35-42.
11. Fridlyander I.N., Anikhovskaya L.I., Senatorova O.G. Kleyenyye metallicheskiye i sloistyye kompozity. Tsvetnyye metally i splavy. Kompozitsionnyye metallicheskiye materialy [Glued metal and laminated composites. Non-ferrous metals and alloys. Composite metallic materials]. M.: Mashinostrienie, 2001. T.: II–3. S. 814–832.
12. Podzhivotov N.YU., Kablov E.N., Antipov V.V., Yerasov V.S. Sloistyye metallopolimernyye materialy v elementakh konstruktsii vozdushnykh sudov [Laminated metal-polymer materials in the structural elements of aircraft] // Perspektivnyye materialy. 2016. №10. S. 5–19.
13. Shestov V.V., Antipov V.V., Senatorova O.G., Sidelnikov V.V. Konstruktsionnyye sloistyye alyumostekloplastiki 1441-SIAL [Structural layered alumino-glass plastics 1441-SIAL] // Metallovedeniye i termicheskaya obrabotka metallov. 2013. №9. S. 28–32.
14. Leshchiner L.N., Latushkina L.V., Fedorenko T.P. Splav 1441 sistemy Al–Cu–Mg–Li [Alloy 1441 of the Al – Cu – Mg – Li system] // Tez. dokl. Vsesoyuz. nauch. konf. Metallovedeniye splavov alyuminiya s litiyem. M.: VILS, 1991. S. 76–77.
15. Antipov V.V., Senatorova O.G., Lukina N.F. i dr. Sloistye metallopolimernye kompozicionnye materialy [Layered metalpolymeric composite materials] // Aviacionnye materialy i tehnologii. 2012. №S. S. 226–230.
16. Antipov V.V., Senatorova O.G., Sidelnikov V.V. Issledovanie pozharostojkosti sloistyh gibridnyh alyumostekloplastikov klassa SIAL [Research of fire firmness layered hybrid aluminum fibreglasses of SIAL’s class] // Aviacionnye materialy i tehnologii. 2011. №3. S. 36–41.
17. Barbotko S.L., Kirillov V.N., Shurkova E.N. Ocenka pozharnoj bezopasnosti polimernyh kompozicionnyh materialov aviacionnogo naznacheniya [Fire safety evolution for polymer composites of aeronautical application] // Aviacionnye materialy i tehnologii. 2012. №3. S. 56–63.
18. Kutsevich K.E., Tyumeneva T.Yu., Petrova A.P. Vliyaniye napolniteley na svoystva kleyevykh prepregov i PKM na ikh osnove [Influence of fillers on properties of adhesive prepregs and PCM on their basis] // Aviacionnye materialy i tehnologii. 2017. №4 (49). S. 51–55. DOI: 10.18577/2071-9140-2017-0-4-51-55.
19. Barbotko S.L. Razvitie metodov ocenki pozharobezopasnosti materialov aviacionnogo naznacheniya [Development of the fire safety test methods for aviation materials] // Aviacionnye materialy i tehnologii. 2017. №S. S. 516–526. DOI: 10.18577/2071-9140-2017-0-S-516-526.

dx.doi.org/ 10.18577/2307-6046-2019-0-1-47-54

УДК 678.8

Kolobkov A.S., Malakhovskiy S.S.

Self-healing composite materials (review)

Examined methods of modification polymer matrix for increasing their impact and crack resistance with domination modification via encapsulated agents and compounds, that able to react in Diels–Alder reaction. Described approaches for increasing service life and efficiency thermoset composite materials, containing healing agents and releasing through growth the crack or another damages in cured polymer matrix and reversible self-regulation chemical bonds in Diels–Alder reaction.

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Reference list

1. Kablov E.N., Chursova L.V., Babin A.N., Mukhametov R.R., Panina N.N. Razrabotki FGUP «VIAM» v oblasti rasplavnykh svyazuyushchikh dlya polimernykh kompozitsionnykh materialov [Developments of FSUE «VIAM» in the field of melt binders for polymer composite materials] // Polimernyye materialy i tekhnologii. 2016. T. 2. №2. S. 37–42.
2. Zheleznyak V.G., Chursova L.V., Grigoryev M.M., Kosarina E.I. Issledovaniye povysheniya soprotivlyayemosti udarnym nagruzkam politsianurata s modifikatorom na osnove lineynykh termostoykikh polimerov [Study of an increase in shock resistance of polycyanurate with modifier based on linear heat-resistant polymers] // Aviacionnye materialy i tehnologii. 2013. №2. S. 26–28.
3. Kablov E.N., Kondrashov S.V., Yurkov G.Yu. Perspektivy ispolzovaniya uglerodsoderzhashchikh nanochastits v svyazuyushchikh dlya polimernykh kompozitsionnykh materialov [Prospects for the use of carbon-containing nanoparticles in binders for polymer composite materials] // Rossiyskiye nanotekhnologii. 2013. T. 8. №3–4. S. 24–42.
4. Akatenkov R.V., Kondrashov S.V., Fokin A.S., Marahovskij P.S. Osobennosti formirovaniya polimernyh setok pri otverzhdenii jepoksidnyh oligomerov s funkcializovannymi nanotrubkami [Features of forming of polymeric grids when curing epoxy oligomers with functionalizing nanotubes] // Aviacionnye materialy i tehnologii. 2011. №2. S. 31–37.
5. Perov N.S. Konstruirovanie polimernykh materialov na molekulyarnykh printsipakh. I. Sozdanie polimernykh materialov s dopolnitelnymi mekhanizmami dissipatsii mekhanicheskoy energii pri nizkikh temperaturakh [Design of polymer materials on the molecular principles. I. The development of polymer materials with additional mechanisms of dissipation of mechanical energy at low temperatures] // Aviacionnye materialy i tehnologii. 2017. №3 (48). S. 50–55. DOI: 10.18577/2071-9140-2017-0-3-50-55.
6. Das R., Melchior C., Karumbaiah K.M. Self-healing composites for aerospace applications // Advanced Composite Materials for Aerospace Engineering. Elsevier, 2016. P. 333–364.
7. 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.
8. Benight S.J., Wang C., Tok J., Bao Z. Stretchable and self-healing polymers and devices for electronic skin // Progress in Polymer Science. 2013. Vol. 38. P. 1961–1977.
9. Doan T.Q., Leslie S., Kim S.Y. et al. Characterization of core-shell microstructure and self-healing performance of electrospun fiber coatings // Polymer. 2016. Vol. 107. P. 1–42.
10. Thakur V.K., Kessler M.R. Self-healing polymer nanocomposite materials: a review // Polymer. 2015. Vol. 69. P. 369–383.
11. Jones A.R., Watkins C.A., White S.R., Sottos N.R. Self-healing thermoplastic-toughened epoxy // Polymer. 2015. Vol. 74. P. 254–260.
12. Uprochneniye epoksidnykh smol kauchukom [Hardening of epoxy resins with rubbe]. Available at: http://stilin.ru/polimernye-smesi/449-uprochnenie-epoksidnyh-smol-kauchukom.html (accessed: October 28, 2018).
13. Neisianya R.E., Leeb J.K.Y., Khorasania S.N. et al. Facile strategy toward fabrication of highly responsive self-healing carbon/epoxy composites via incorporation of healing agents encapsulated in poly(methylmethacrylate) nanofiber shell // Journal of Industrial and Engineering Chemistry. 2018. Vol. 59. 456–466.
14. Rehman H.U., Chen Y., Guo Y. et al. Stretchable, strong and self-healing hydrogel by oxidized CNT-polymer composite, Self-healing polymer nanocomposite materials: a review // Composites: Part A. 2016. Vol. 90. P. 250–260.
15. Guadagno L., Naddeo C., Raimondo M. et al. Development of Self-Healing Multifunctional Materials // Composites: Part B. 2017. Vol. 128. P. 30–38.
16. Champagne J., Su-Seng Pang, Guoqiang Li. Effect of Confinement Level and Local Heating on Healing Efficiency of Self-healing Particulate Composites // Composites: Part B. 2016. Vol. 97. P. 344–352.
17. Lee J., Bhattacharyya D., Zhang M.Q., Yuan Y.C. Mechanical properties of mendable composites containing self-healing thermoplastic agents // Composites: Part B. 2014. Vol. 62. P. 10–18.
18. Turkenburg D.H., Fischer H.R. Diels-Alder based, thermo-reversible cross-linked epoxies for use in self-healing composites // Polymer. 2015. Vol. 79. P. 187–194.
19. Heo Y., Sodano H.A. Thermally Responsive Self-Healing Composites with Continuous Carbon Fiber Reinforcement // Composites Science and Technology. 2015. Vol. 118. P. 244–250.
20. Scheiner M., Dickens T.J., Okoli O. Progress towards self-healing polymers for composite structural applications // Polymer. 2015. Vol. 83. P. 260–282.

dx.doi.org/ 10.18577/2307-6046-2019-0-1-55-63

УДК 678.8

Donetskiy K.I., Karavaev R.Y., Raskutin A.E., Dun V.A.

Carbon fibers composite material on the basis of volume reinforcing triax braiding preformes

In work it is considered carbon fibers composite on the basis of volume reinforcing triax braiding preformes, made in the way of vacuum infusion with use of the molten epoxy binding. Possible scopes of such material and its physicomechanical properties are given. It is shown that when manufacturing the designs working at influence of outside hydrostatic pressure, important task is decrease in their weight and dimensional characteristics. Application carbon fibers composite on the basis of volume reinforcing braiding preformes will allow to improve weight characteristics that will lead in turn to increase of technical characteristics of made designs.

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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. Kablov E.N. Kompozity: segodnya i zavtra [Composites: today and tomorrow] // Metally Evrazii. 2015. №1. S. 36–39.
3. Borshchev A.V., Gusev Yu.A. Polimernye kompozicionnye materialy v avtomobilnoj promyshlennosti [Polymer composite materials in automotive industry] // Aviacionnye materialy i tehnologii. 2014. №S2. S. 34–38.
4. Raskutin A.E. Rossiiskie polimernye kompozitsionnye materialy novogo pokoleniia, ikh osvoenie i vnedrenie v perspektivnykh razrabatyvaemykh konstruktsiiakh [Russian polymer composite materials of new generation, their exploitation and implementation in advanced developed constructions] // Aviacionnye materialy i tehnologii. 2017. №S. S. 349–367. DOI: 10.18577/2071-9140-2017-0-S-349-367.
5. Kablov E.N., Startsev V.O., Inozemtsev A.A. Vlagonasyshhenie konstruktivno-podobnyh elementov iz polimernyh kompozicionnyh materialov v otkrytyh klimaticheskih usloviyah s nalozheniem termociklov [The moisture absorption of structurally similar samples from polymer composite materials in open climatic conditions with application of thermal spikes] // Aviacionnye materialy i tehnologii. 2017. №2 (47). S. 56–68. DOI: 10.18577/2071-9140-2017-0-2-56-68.
6. Braided reinforcement for aircraft fuselage frames and method of producing the same: pat. 8210086B2 US; publ. 03.07.12.
7. Dushin M.I., Doneckij K.I., Karavaev R.Yu. Ustanovlenie prichin obrazovaniya poristosti pri izgotovlenii PKM [Identification of the reasons of porosity formation when manufacturing composites] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №6 (42). St. 08. Available at: http://www.viam-works.ru (accessed: December 14, 2018). DOI: 10.18577/2307-6046-2016-0-6-8-8.
8. Donetskij K.I., Hrulkov A.V., Kogan D.I., Belinis P.G., Lukyanenko Yu.V. Primenenie obemno-armiruyushhih preform pri izgotovlenii izdelij iz PKM [Use of three-dimensional reinforcing preforms during the production of polymer composite products] // Aviacionnye materialy i tehnologii. 2013. №1. S. 35–39.
9. Vlasenko F.S., Raskutin A.E., Doneckij K.I. Primenenie pletenyh preform dlya polimernyh kompozicionnyh materialov v grazhdanskih otraslyah promyshlennosti (obzor) [Application of braided preforms for polymer composite materials in civil industries (review)] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №1. St. 05. Available at: http://www.viam-works.ru (accessed: December 14, 2018). DOI: 10.18577/2307-6046-2015-0-1-5-5.
10. Erber A., Birkefeld K., Drechsler K. The influence of braiding configuration on damage tolerance of drive shafts // SAMPE EUROPE: 30th International Jubilee Conference and Forum. 2010. P. 364–371.
11. Branscomb D., Beale D., Broughton R. New directions in braiding // Journal of Engineered Fibers and Fabrics. 2013. No. 8 (2). R. 11–24.
12. Donetskij K.I., Kogan D.I., Hrulkov A.V. Svojstva polimernyh kompozicionnyh materialov, izgotovlennyh na osnove pletenyh preform [Properties of the polymeric composite materials made on the basis of braided preforms] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №3. St. 05. Available at: http://www.viam-works.ru (accessed: December 14, 2018). DOI: 10.18577/2307-6046-2014-0-3-5-5.
13. Lebel L.L., Nakai A. Design and manufacturing of an L-shaped thermoplastic composite beam by braid-trusion // Composites. Part A: Applied Science and Manufacturing. 2012. No. 43 (10). P. 1717–1729.
14. Kohlman L.W., Bail J.L., Roberts G.D. et al. A notched coupon approach for tensile testing of braided composites // NASA Publications. 2012. No. 65. P. 1–9.
15. Dun V.A., Petrovskiy O.L., Rumyantsev A.F., Ushakov P.G. Rezultaty primeneniya ugleplastika dlya izgotovleniya malogabaritnykh korpusov [The results of carbon fiber for the manufacture of small buildings] // Sudostroitelnaya promyshlennost, seriya PVMO. 1986. Vyp. 2. S. 70–75.
16. Kompozitnyy korpus glubokovodnogo tekhnicheskogo sredstva: pat. 2453464 Ros. Federatsiya [Composite hull deep-sea technical means: pat. 2453464 Rus. Federation]; zayavl. 17.08.10; opubl. 20.06.12.
17. Carey J.P. Handbook of Advances in Braided Composite Materials. Woodhead Publishing is an Imprint of Elsevier, 2017. No. 72. R. 3–6.
18. Chursova L.V., Babin A.N., Panina N.N., Tkachuk A.I., Terekhov I.V. Ispolzovaniye aromaticheskikh aminnykh otverditeley dlya sozdaniya epoksidnykh svyazuyushchikh dlya PKM konstruktsionnogo naznacheniya [Usage of aromatic amine curing agents for epoxy resins binders for production of structural PCM] // Trudy VIAM: electron. nauch.-tehnich. zhurn. 2016. №6 (42). St. 04. Available at: http://www.viam-works.ru (accessed: December 14, 2018). DOI: 10.18577/2307-6046-2016-0-6-4-4.

dx.doi.org/ 10.18577/2307-6046-2019-0-1-64-73

УДК 66.017

Zagora A.G., Kondrashov S.V., Antyufeeva N.V., Pykhtin A.A.

Research of influence of technological modes of production of epoxy nanocomposites with carbon nanotubes on their heat resistance

In work the temperature and time mode of hardening of the studied epoxy compositions which provided its almost full course was chosen. Therefore, temperature change of vitrification as a result of the conducted researches is explained by exclusively modifying action of carbon nanotubes. It is shown that the three-roll mixer plays a key role in the technological modes of production of epoxynanocomposites. Non-functional multiwall carbon nanotubes (MWCNTs) with its help considerably increase heat resistance of epoxy compositions.

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Reference list

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17. Allaoui A., Bounia N.El. How carbon nanotubes affect the cure kinetics and glass transition temperature of their epoxy composites?: a review // Express Polymer Letters. 2009. Vol. 3. No. 9. Р. 588–594.
18. Marakhovskiy P.S., Kondrashov S.V., Akatenkov R.V., Aleksashin V.M., Anoshkin I.V., Mansurova I.A. O modifikatsii teplostoykikh epoksidnykh svyazuyushchikh uglerodnymi nanotrubkami // Vestnik MGTU im. N.E. Baumana. Ser.: Mashinostroyeniye. 2015. №2. S. 118–127.
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22. Thostenson E.T., Chou T.W. Processing-structure-multi-functional property relationship in carbon nanotube/epoxy composites // Carbon. 2006. Vol. 44. No. 14. P. 3022–3029.
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24. Puglia D., Valentini L., Kenny J.M. Analysis of the Cure Reaction of Carbon Nanotubes/Epoxy Resin Composites Through Thermal Analysis and Raman Spectroscopy // Journal of Applied Polymer Science. 2003. Vol. 88. P. 452–458.
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26. Bae J., Jang J., Yoon S.-H. Cure Behavior of the Liquid-Crystalline Epoxy/Carbon Nanotube System and the Effect of Surface Treatment of Carbon Fillers on Cure Reaction // Macromolecular Chemistry Physics. 2002. Vol. 203. P. 2196–2204.
27. Pykhtin A.A. Vysokotekhnologichnyye epoksidnyye nanodispersii i nanokompozity s reguliruyemoy strukturoy i kompleksom svoystv: dis. … kand. tekhn. nauk [High-tech epoxy nanodispersions and nanocomposites with adjustable structure and complex properties: thesis Dr. Sc. (Tech.)]. M., 2017. 125 c.

dx.doi.org/ 10.18577/2307-6046-2019-0-1-74-91

УДК 677.523

Shestakov A.M., Khaskov M.A., Sorokin O.Ju.

Organosilicon polymer compounds based inorganic fibers for high-temperature composite materials (review)

This article discusses the main types of organosilicon polymer compounds based inorganic fibers, produced abroad, for high-temperature composite materials of various nature. The methods for producing organosilicon polymer compounds and fibers are briefly described. Also, the effect of the nature of the organosilicon polymer and the method of producing fibers on their physical and mechanical properties, phase composition and thermal-oxidative stability is shown. The prospects for the use of fibers as reinforcing filler for high-temperature composites are shown.

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Reference list

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10.

dx.doi.org/ 10.18577/2307-6046-2019-0-1-92-104

УДК 678.067.5

Melnikov D.A., Petrova A.P., Gromova A.A., Sokolov I.I., Raskutin A.E.

The calculation of the ratio of the components of the prepreg stamps VPS-53/120, determination of physico-mechanical and operational characteristics of GRP

Process of selection of ratio of components of prepreg is described. The data on electrochemical corrosion in the contact zone of «metal–carbon» fiber and describes a method of protection against contact corrosion by isolating the carbon-plastic metal layer prepreg GRP. The initial components of prepreg GRP VPS-53/120, designed to prevent contact corrosion between metal and carbon fiber, were selected. Two methods for calculating the surface density of the binder and prepreg are described. The ranges of permissible dispersion of the surface densities of the binder and prepreg film are calculated taking into account the dispersion of the surface density of GRP and the selected range of the binder content in the prepreg. The actual values of the prepreg characteristics of the VPS-53/120 brand are determined and their statistical analysis is carried out, the high convergence of the actual values with the calculated ones is shown. Physical-mechanical and operational characteristics of GRP of the VPS-53/120 brand are defined.

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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.
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11.

dx.doi.org/ 10.18577/2307-6046-2019-0-1-105-114

УДК 678.8

Minibaev M.I., Raskutin A.E., Goncharov V.A.

Peculiarities of technology production specimens of PCM on CNC machines (review)

The polymer composite materials industry is in constant development, however, PCM processing technologies must be developed, and the effects of mechanical processing on the properties of the material after processing should be investigated. Manufacturers of tools offer special cutters, differing in the materials from which they are made, geometry, grinding angles, etc. It is necessary to conduct research for each brand of material in order to designate the optimal cutting mode. The design of the equipment should provide reliable protection of personnel and take into account the properties formed during the processing of chips.

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Reference list

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12.

dx.doi.org/ 10.18577/2307-6046-2019-0-1-115-124

УДК 620.1:669.295

Ospennikova O.G., Naprienko S.A., Avtaev V.V.

Influence of sea water on fatigue limit of alloy VT3-1 at different load ratio

On specially developed samples of VT3-1 alloy, it was experimentally established that the sea water leads to an increase of fatigue limit under symmetrical loading cycle, under conditions of cyclic stretching and cyclic compression.

By the method of scanning electron microscopy it was found that under the conditions of cyclic compression the development of fatigue cracks is accompanied by the formation of a faceted relief of the forming trickle with longitudinal folds. When tested in sea water facets have a fragile appearance, while in the air on their surface there are signs of plastic deformation. With a symmetrical loading cycle and cyclic stretching, fatigue grooves are formed in sea water, as in the air atmosphere.

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Reference list

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