ARCHIVE

Aviation materials and technologies №4, 2016

Contents

  • V.I. Gromov, V.N. Krotov, N.A. Kurpyakova, O.V. Sedov, A.V. Doroshenko

    Influence of residual austenite on the structure and properties of diffusion layer of martensitic grade steel after vacuum carburization

    3-8
  • V.S. Denisova, G.A. Solovyeva

    Heat-resistant glass-ceramic coating for protection of gas turbines’ combustion chambers parts

    18-22
  • D.A. Chubarov, S.A. Budinovskiy, A.A. Smirnov

    Magnetron sputtering method for applying ceramic layers for thermal barrier coatings

    23-30
  • R.K. Salakhova, A.B. Tikhoobrazov

    Physical and chemical properties of oxalate-sulfate chromium plating electrolyte, containing metal oxide nanoparticles

    31-39
  • N.V. Buchilin, G.Yu. Lyulyukina

    Characteristics of sintering of highly porous alumina-based ceramic materials

    40-46
  • D.E. Kablov, V.N. Simonov, M.S. Alekseeva

    Research of structure of the filter and features of impurity filtering by porous ceramics from Al2O3 aluminum oxide

    47-53
  • K.I. Donetskiy, R.Yu. Karavaev, A.E. Raskytin, N.N. Panina

    Properties of carbon fiber and fiberglass on the basis of braiding preforms

    54-59
  • I.D. Kraev, E.M. Shuldeshov, M.M. Platonov, G.Yu. Yurkov

    Composite materials combining acoustic and radio shielding properties

    60-67
  • A.S. Boychuk, A.S. Generalov, I.A. Dikov

    Creating acoustic contact between phased array and convex surface of tested object during ultrasonic NDT of FRP

    68-73
  • E.I. Oreshko, V.S. Erasov, A.N. Lutsenko

    Calculation features of cores and plates stability

    74-79
  • A.A. Demidov, A.V. Stepanov, E.M. Turbin, O.A. Krupnina

    The х-ray testing modes providing with radiation imaging with predetermined contrast

    80-85
  • N.V. Antyufeeva, V.M. Aleksashin, M.R. Pavlov, Yu.V. Stolyankov

    Research of possibility of use carbon fiber reinforced polymers in the conditions of the Arctic climate

    86-94
Содержание номера
1.

DOI: 10.18577/2071-9140-2016-0-4-3-8

UDC: 620.1

Pages:: 3-8

V.I. Gromov1, V.N. Krotov2, N.A. Kurpyakova1, O.V. Sedov1, A.V. Doroshenko1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[2] Rostov State Transport University

Influence of residual austenite on the structure and properties of diffusion layer of martensitic grade steel after vacuum carburization

The research of modes of vacuum carburization and subsequent heat treatment influence on phase transformations in the diffusion layer of construction multi-alloyed dispersion-hardened martensitic steel was made by the method of optical microscopy and X-ray diffraction analysis. Influence of carbon percentage in the layer on amount of residual austenite, on dispersion hardening processes during the hardening heat treatment after vacuum carburization, on microstructure and diffusion layer hardness is shown. Photos containing microstructure changing of diffusion layer during the hardening which depend on percentage of carbon in the layer are presented Influence of the temper temperature hardening on the flowing of processes of precipitation carbide hardening is shown. The work is executed within the implementation of the complex scientific direction 8.3. «High-strength nanostructured constructional steels and diffusion coatings composed by methods of chemical and thermal processing» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: diffusion layer, carbide phase, austenite, martensite, hardening, vacuum carburization

Reference List

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    2. Kablov E.N. Sovremennye materialy – osnova innovacionnoj modernizacii Rossii [Modern materials – basis of innovative modernization of Russia] // Metally Evrazii. 2012. №3. S. 10–15.

    3. Kablov E.N. Razrabotki VIAM dlya gazoturbinnyh dvigatelej i ustanovok [Development of VIAM for gas turbine engines and installations] // Krylya Rodiny. 2010. №4. S. 31–33.

    4. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlya vysokonagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for the high-loaded details of gas turbine engines] // Vestnik MGTU im. N.E. Baumana. 2011. Spec. vyp.: Perspektivnye konstrukcionnye materialy i tehnologii. S. 13–19.

    5. Krylov V.S. Razrabotka processov nasyshheniya stali azotom i uglerodom pri ponizhennom davlenii: avtoref. dis. … dokt. tehn. nauk [Development of processes of saturation became nitrogen and carbon with reduced pressure: thesis, Dr. Sc. (Tech.)]. M., 1979. 35 s.

    6. Ryzhov N.M., Smirnov A.E., Fahurtdinov R.S. i dr. Osobennosti vakuumnoj cementacii teplostojkoj stali v acetilene [Features of vacuum cementation of heat-resistant steel in acetylene] // MiTOM. 2004. №6. S. 10–15.

    7. Ryzhov N.M., Smirnov A.E., Fahurtdinov R.S. Upravlenie nasyshhennost\'yu uglerodom diffuzionnogo sloya pri vakuumnoj cementacii teplostojkih stalej [Management of saturation of diffused layer carbon at vacuum cementation heatresistant the staly] //MiTOM. 2004. №8. S. 22–27.

    8. Ryzhov N.M., Smirnov A.E., Fahurtdinov R.S. Vakuumnaya cementaciya hromonikelevoj stali [Vacuum cementation of chrome nickel steel] // MiTOM. 2008. №2. S. 25–29.

    9. Markova E.S., Yakusheva N.A., Pokrovskaja N.G., Shalkevich A.B. Tehnologicheskie osobennosti proizvodstva martensitostareyushhej stali VKS-180 [Technological features of the production of maraging steel VKS-180] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №7. St. 01. Available at: http://www.viam-works.ru (accessed: October 18, 2015).

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    12. Ryzhov N.M., Smirnov A.E., Fahurtdinov R.S. Ciklicheskaya prochnost\' stali 16H3NVFMB-Sh (VKS-5) posle vakuumnoj cementacii // MiTOM. 2010. №2. S. 23–28.

    13. Grafen W., Edenhofer B. Acetylene low-pressure carburizing – a novel and superior carburizing technology // Heat treatment of metals. 1999. Vol. 26. No. 4. P. 79–85.

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    16. Petrakov A.F., Shalkevich A.B. Vysokoprochnye stali v aviastroenii [High-strength became in aircraft industry] // Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2002: yubilejnyj nauch.-tehnich. sb. M.: VIAM, 2002. S. 180–191.

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3.

DOI: 10.18577/2071-9140-2016-0-4-18-22

UDC: 666.293.52:537.226.2

Pages:: 18-22

V.S. Denisova1, G.A. Solovyeva1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Heat-resistant glass-ceramic coating for protection of gas turbines’ combustion chambers parts

The technology of fabrication of heat-resistant glass-ceramic coating based on glass frit in system BaO-Al2O3-SiO2 and modifying additives for protection of combustion chambers made of high-strength alloy VZH171 was obtained. Main properties of heat resistant glass-ceramic coating were investigated, e.g. bonding strength, thermal stress resistance, heat resistance. The efficiency of coating protection at 1100-1150°C was shown. Heat-resistant glass-ceramic coating is notable by its manufacturability and requires no complex equipment. The work is executed within the implementation of the complex scientific direction 14.2. «New technologies of producing superhigh-temperature ceramic composite materials and coatings» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: thermal stress resistance, heat resistance, coating, nickel alloy, hot corrosion, glass

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., Solntsev S.S., Rozenenkova V.A., Mironova N.A. Sovremennye polifunkcional\'nye vysokotemperaturnye pokrytiya dlya nikelevyh splavov, uplotnitelnyh metallicheskih materialov i berillievyh splavov [Modern multifunctional high temperature coatings for nickel alloys, sealing metal materials and beryllium alloys] // Novosti materialovedeniya. Nauka i tehnika: elektron. nauch.-tehnich. zhurn. 2013. №1. St. 05. Available at: http://www.materialsnews.ru (accessed: January 13, 2016).

    3. Solntsev S.S. Zashhitnye tehnologicheskie pokrytiya i tugoplavkie email [Protective technological coverings and high-melting enamels]. M.: Mashinostroenie, 1984. 256 s. 

    4. Kablov E.N., Grashhenkov D.V., Isaeva N.V., Solncev S.S., Sevastyanov V.G. Vysokotemperaturnye konstrukcionnye kompozicionnye materialy na osnove stekla i keramiki dlya perspektivnyh izdelij aviacionnoj tehniki [High-temperature constructional composite materials on the basis of glass and ceramics for perspective products of aviation engineering] // Steklo i keramika. 2012. №4. S. 7–11.

    5. Lomberg B.S., Ovsepyan S.V., Bakradze M.M., Mazalov I.S. Vysokotemperaturnye zharo-prochnye nikelevye splavy dlya detalej gazoturbinnyh dvigatelej [High-temperature heat resisting nickel alloys for details of gas turbine engines] // Aviacionnye materialy i tehnologii. 2012. №S. S. 52–57.

    6. Ovsepyan S.V., Lukina E.A., Filonova E.V., Mazalov I.S. Formirovanie uprochnyayushhej fazy v processe vysokotemperaturnogo azotirovaniya svarivaemogo zharoprochnogo deformiruemogo splava na osnove sistemy Ni–Co–Cr [Formation of the Strengthening Phase during the High-Temperature Nitriding of Ni–Co–Cr Weldable Wrought Superalloy] //Aviacionnye materialy i tehnologii. 2013. №1. S. 3–8.

    7. Solntsev St.S. Vysokotemperaturnye kompozicionnye materialy i pokrytiya na osnove stekla i keramiki [High-temperature composite materials and coverings on the basis of glass and ceramics] // 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: yubilejnyj nauch.-tehnich. sb. M.: VIAM, 2007. S. 90–99.

    8. Solntsev S.S. Vysokotemperaturnye steklokeramicheskie materialy i pokrytiya – perspektivnoe napravlenie aviacionnogo materialovedeniya [High-temperature steklokeramichesky materials and coverings – the perspective direction of aviation materials science] // Vse materialy. Enciklopedicheskij spravochnik. 2009. №1. S. 26–37.

    9. Solntsev S.S., Denisova V.S., Rozenenkova V.A. Zharostojkie emali dlya zashhity nikelevyh splavov i stalej [Heat resisting enamels for protection of nickel alloys and staly] // Vse materialy. Enciklopedicheskij spravochnik. 2016. №1. S. 22–28.

    10. Denisova V.S., Solntsev S.St., Soloveva G.A. Stekloemalevye pokrytiya dlya zashhity korrozionnostojkih stalej ot vysokotemperaturnoj gazovoj korrozii: svojstva i oblasti primeneniya (obzor) [Glass enamel coatings for stainless steels protection against attacks of hot gas corrosion: properties and application fields (review)] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №5. St. 05. Available at: http://www.viam-works.ru (accessed: January 13, 2016). DOI: 10.18577/23071-6046-2015-0-5-5-5.

    11. Denisova V.S., Solntsev S.S., Soloveva G.A., Malinina G.A. Sovremennoe sostoyanie issledovanij v oblasti zharostojkih resursnyh pokrytij dlya nikelevyh i titanovyh splavov (obzor) [Current state of investigations in the field of heat-resistant coatings for nickel and titanium alloys (review)] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №4. St. 02. Available at: http://www.viam-works.ru (accessed: January 13, 2016). DOI: 10.18577/23071-6046-2015-0-4-2-2.

    12. Solntsev S.S. Nekotorye osobennosti pokrytij dlya plitok mnogorazovoj teplozashhity orbitalnyh kosmicheskih korablej [Some features of coatings for tiles reusable heat-protection orbiting spacecraft] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №2. St. 01. Available at: http://www.viam-works.ru (accessed: January 13, 2016). DOI: 10.18577/2307-6046-2014-0-2-1-1.

    13. Solntsev S.S., Rozenenkova V.A., Mironova N.A., Soloveva G.A. Vysokotemperaturnye pokrytiya na osnove zol-gel tehnologii [High-temperature coatings on basis of sol-gel technology] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №1. St. 03. Available at: http://www.viam-works.ru (accessed: January 13, 2016). DOI: 10.18577/2307-6046-2014-0-1-3-3.

    14. Solntsev S.S., Shvagireva V.V., Isaeva N.V., Soloveva G.A. Armirovannye zharostojkie stekloemali dlya kamer sgoraniya gazoturbinnyh dvigatelej [Reinforced heat resisting glass enamel for combustion tubes of gas turbine engines] // Aviacionnye materialy i tehnologii. 2010. №1. S. 26–29.

    15. Solntsev St.S., Rozenenkova V.A., Mironova N.A. Vysokotemperaturnye steklokeramicheskie pokrytiya i kompozicionnye materialy [The high-temperature glass ceramic coatings and composite materials] // Aviacionnye materialy i tehnologii. 2012. №S. S. 359–368.

    16. Solntsev S.S., Shvagireva V.V., Isaeva N.V., Soloveva G.A. Zharostojkoe pokrytie dlya zashhity vysokoprochnyh slozhnolegirovannyh nikelevyh splavov ot vysokotemperaturnoj gazovoj korrozii [High temperature coating for protection of high-strength complex alloyed of nickel alloys of high-temperature gas corrosion] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №6. St. 04. Available at: http://www.viam-works.ru (accessed: January 13, 2016). DOI: 10.18577/2307-6046-2014-0-6-4-4.

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DOI: 10.18577/2071-9140-2016-0-4-23-30

UDC: 621.385.64:629.7.023.226

Pages:: 23-30

D.A. Chubarov1, S.A. Budinovskiy1, A.A. Smirnov1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Magnetron sputtering method for applying ceramic layers for thermal barrier coatings

The article describes the magnetron sputtering deposition of ceramic layers of thermal barrier coatings developed by VIAM for applying to turbine blades of new GTE in military and civil aviation. The description of the method, its advantages and disadvantages, the description of the experimental magnetron sputtering unit designed and installed by VIAM are also discussed. The comparison between the microstructure of the ceramic layer produced by this method and the microstructure obtained by electron-beam vapor deposition (EB-PVD) is investigated. The article also describes a phase analysis and thermal conductivity of the ceramic layer produced by magnetron sputtering. The work is executed within the implementation of the complex scientific direction 17.3. «Multilayer heat resistant and heat-protective coatings, nanostructural strengthening erosion and corrosion resistant, antiwear, antifretting coatings for protection of hot path and the GTЕ parts and GTU compressor» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: thermal barrier coating, TBC, YSZ, gas turbine engine, magnetron sputtering

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. Budinovskij S.A., Muboyadzhyan S.A., Gayamov A.M. Sovremennoe sostoyanie i osnovnye tendencii razvitiya vysokotemperaturnyh teplozashhitnyh pokrytij dlya rabochih lopatok turbin aviacionnyh GTD [Current state and the main tendencies of development of high-temperature heat-protective coverings for working blades of turbines of aviation GTE] // Aviacionnaya promyshlennost. 2008. №4. S. 33–37. 

    3. Gayamov A.M., Budinovskij S.A., Muboyadzhyan S.A., Kosmin A.A. Vybor zharostojkogo pokrytija dlya zharoprochnogo nikelevogo renij-rutenijsoderzhashhego splava marki VZhM4 [Selection of heat-resistant coating with metalloceramic barrier layer for protection of Re-Ru nickel-based superalloy] // Trudy VIAM : elektron. nauch.-tehnich. zhurn. 2014. №1. St. 01. Available at: http://viam-works.ru (accessed: August 02, 2015). DOI: 10.18577/2307-6046-2014-0-1-1-1.

    4. Smirnov A.A., Budinovskij S.A., Matveev P.V. Issledovanie vliyaniya velichiny otricatelnogo elektricheskogo potenciala podlozhki na skorost osazhdeniya mnogokomponentnyh nikelevyh pokrytij na poverhnost zharoprochnyh litejnyh splavov [Investigation of an impact of a negative electric potential of the substrate on deposition rate of multicomponent nickel coatings on the surface of cast heat -resistant nickel alloys] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №2. St. 05. Available at: http://www.viam-works.ru (accessed: August 02, 2015). DOI: 10.18577/2307-6046-2015-0-2-5-5.

    5. Kablov E.N., Muboyadzhyan S.A., Budinovskij S.A., Lutsenko A.N. Ionno-plazmennye zashhitnye pokrytiya dlya lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] // Metally. 2007. №5. S. 23–34.

    6. Kablov E.N., Ospennikova O.G., Vershkov A.V. Redkie metally i redkozemelnye elementy – materialy sovremennyh i budushhih vysokih tehnologij [Rare metals and rare earth elements – materials of modern and future high technologies] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №2. St. 01. Available at: http://www.viam-works.ru (accessed: August 02, 2015).

    7. Kablov E.N., Muboyadzhyan S.A. Teplozashhitnye pokrytiya dlya lopatok turbin vysokogo davleniya perspektivnyh GTD [Heat-protective coverings for blades of high-pressure turbines of perspective GTE] // Metally. 2012. №1. S. 5–13. 

    8. 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.

    9. Chubarov D.A., Budinovskij S.A. Vybor keramicheskogo materiala dlya teplozashhitnyh pokrytij lopatok aviacionnyh turbin na rabochie temperatury do 1400°C [Choosing ceramic materials for thermal barrier coating of GTE turbine blades on working temperatures up to 1400°С] // Trudy VIAM : elektron. nauch.-tehnich. zhurn. 2015. №4. St. 07. Available at: http://viam-works.ru (accessed: August 02, 2015). DOI: 10.18577/2307-6046-2015-0-4-7-7.

    10. Chubarov D.A., Matveev P.V. Novye keramicheskie materialy dlya teplozashhitnyh pokrytij rabochih lopatok GTD [New ceramic materials for thermal barrier coating using in GTE turbine blades] // Aviacionnye materialy i tehnologii. 2013. №4. S. 43–46.

    11. Clarke D.R., Phillpot S.R. Thermal barrier coating materials // Materialstoday. 2005. Vol. 8. Issue 6. P. 22–29.

    12. Levi C.G. Emerging materials and processes for thermal barrier system // Current Opinion in Solid State and Materials Science. 2004. №8. P. 77–91.

    13. Budinovskij S.A., Chubarov D.A., Matveev P.V. . Sovremennye sposoby naneseniya teplozashhitnyh pokrytij na lopatki gazoturbinnyh dvigatelej (obzor) [Modern methods for deposition of thermal barrier coatings on GTE turbine blades] // Aviacionnye materialy i tehnologii. 2014. №S5. S. 38–44.

    14. Muboyadzhyan S.A., Budinovskij S.A., Gayamov A.M., Smirnov A.A. Poluchenie keramicheskih teplozashhitnyh pokrytij dlya rabochih lopatok turbin aviacionnyh GTD magnetronnym metodom [Receiving ceramic heat-protective coatings for working blades of turbines of aviation GTD magnetronny method] // Aviacionnye materialy i tehnologii. 2012. №4. S. 3–8.

    15. Budinovskij S.A., Smirnov A.A., Matveev P.V., Chubarov D.A. Razrabotka teplozashhitnyh pokrytij dlja rabochih i soplovyh lopatok turbiny iz zharoprochnyh i intermetallidnyh splavov [Development of thermal barrier coatings for rotor and nozzle turbine blades made of nickel-base super- and intermetallic alloys] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №4. St. 05. Available at: http://www.viam-works.ru (accessed: August 02, 2015). DOI: 10.18577/2307-6046-2015-0-4-5-5.

    16. Budinovskij S.A., Muboyadzhyan S.A., Gayamov A.M., Matveev P.V. Razrabotka ionno-plazmennyh zharostojkih metallicheskih sloev teplozashhitnyh pokrytij dlya ohlazhdaemyh rabochih lopatok turbin [Development of ion-plasma heat resisting metal layers of heat-protective coverings for cooled working blades of turbines] // MiTOM. 2013. №11. S. 16–21.

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5.

DOI: 10.18577/2071-9140-2016-0-4-31-39

UDC: 621.357.7

Pages:: 31-39

R.K. Salakhova1, A.B. Tikhoobrazov1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Physical and chemical properties of oxalate-sulfate chromium plating electrolyte, containing metal oxide nanoparticles

This work is devoted to research of physical & chemical properties of oxalate-sulphate chromium plating electrolyte as the most stable and efficient among the known electrolytes based on trivalent chromium compounds. By the method of absorption spectroscopy the ionic composition of colored solutions chromium sulfate & modification conversion of Cr(III) complex compounds is investigated. We present the results of sedimentation analysis of electrolyte containing nanoparticles of metal oxides. Specific electrical conductivity (SEC) of electrolyte & effect of Al2O3 nanoparticles in electrolyte on the value of SEC is investigated by conductivity meter KRAB-D №0647.

Keywords: oxalate-sulfate electrolyte, chromium plating, nanoparticles, light transmission, sedimentation stability, specific electrical conductivity

Reference List

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DOI: 10.18577/2071-9140-2016-0-4-40-46

UDC: 666.77

Pages:: 40-46

N.V. Buchilin1, G.Yu. Lyulyukina1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Characteristics of sintering of highly porous alumina-based ceramic materials

The investigations results of sintering conditions and optimization of the firing modes of alumina-based materials with cellular pore structure are presented. It is shown that addition of finely milled glass powder to ceramic mass consisting of corundum with particle sizes 10-40 mm leads to implementation of material sintering according to liquid-phase mechanism. The optimum concentration of the glass additive in the ceramic mass allowing to obtain materials with 85% interconnected porosity and compressive strength up to 0,7 MPa at firing temperatures not exceeding 1670°C is determined. The work is executed within the implementation of the complex scientific direction14.2. «New technologies of receiving superhigh-temperature ceramic and metal composite materials» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: oxide ceramics, alumina, ceramic filters, sintgering, firing

Reference List

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7.

DOI: 10.18577/2071-9140-2016-0-4-47-53

UDC: 669.018.44: 669.245

Pages:: 47-53

D.E. Kablov1, V.N. Simonov2, M.S. Alekseeva1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[2] Bauman Moscow State Technical University

Research of structure of the filter and features of impurity filtering by porous ceramics from Al2O3 aluminum oxide

Specialty of the melt filtering from impurities for obtaining ultrapure nickel-based alloys is studied. The structure of the foam-ceramic filter from aluminum oxides (Al2O3) in initial condition and after the ZhS36-VI melt passing through with the raised sulfur content and phosphorus is investigated. Calculations of phase state of the filter after vacuum annealing are carried out. Geometrical parameters of the foam-ceramic filter are determined: diameter of pores and web thickness between the pores in initial condition. Sequence of appearance and place where adhesion of the particles containing sulfur is observed on internal channels during refinement by lanthanum are determined by methods of electron microscopy and micro x-ray spectral analysis. It is established that lanthanum phosphides are not adsorbed on the filter walls.

Keywords: heat resistant nickel alloy, sulfur, phosphorus, aluminum oxide, foam ceramic filter, impurity, filtering, electron microscopy

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DOI: 10.18577/2071-9140-2016-0-4-54-59

UDC: 678.747.2:678.067.5

Pages:: 54-59

K.I. Donetskiy1, R.Yu. Karavaev1, A.E. Raskytin1, N.N. Panina1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Properties of carbon fiber and fiberglass on the basis of braiding preforms

Carbon fiber and fiberglass executed on the basis of braided preforms are widely applied in manufacturing new items of modern equipment. The leading foreign companies such as Boeing, Airbus, General Electric Aircraft Engines, Snecma and some other have implemented such polymer composite materials in aerospace and civil products. Now these technologies are used for manufacturing of stringer, frames, load-carrying structures of aviation engineering, propeller blades, elements of fuselage, the chassis, transmissions, drafts of management and many others. The main advantage of these technologies is possibility of obtaining workpieces from any type of fibers of almost unlimited form and size, obtaining materials which are characterized by considerable resistance to delaminating and blow, high fatigue rates. The work is executed within the implementation of the complex scientific direction 13.2. «Constructional PСM» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: braided preforms, carbon fiber, fiberglass, epoxy binders, non-autoclave molding methods, angle reinforcement, physical and mechanical properties

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    18. Kompozitnaya lopatka ventilyatora s mnogoslojnym armiruyushhim materialom: pat. 2384749 Ros. Federaciya [Composite blade of the fan with multi-layer reinforcing material: pat. 2384749 Rus. Federation]; opubl. 20.03.10. Byul. №8.

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DOI: 10.18577/2071-9140-2016-0-4-60-67

UDC: 678.8:628.517.2.699.844

Pages:: 60-67

I.D. Kraev1, E.M. Shuldeshov1, M.M. Platonov2, G.Yu. Yurkov3

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[2] Limited Liability Company «Himprodukt»
[3] Institute of Metallurgy and Materials Science A.A. Baykova of Russian academy of sciences

Composite materials combining acoustic and radio shielding properties

This article is devoted to matters of creation of radio and acoustic shielding materials and describes the basic principles of their application. The basic principles of radio and acoustic materials, their classification are provided. The global level of the existing radio sound dampening materials is evaluated, the necessity of comprehensive approach to development of hybrid materials which ensure improvement of the acoustic and radio shielding properties and allow reducing construction dimensions and weight. Conclusions on the future of new hybrid functional materials development are done. The work is executed within the implementation of the complex scientific direction 15.3. «Materials and coatings for protection against EMЕ, shock, vibrating, acoustic and electric influences» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: еlectromagnetic radiation, noise pollution, radio engineering characteristics, acoustic properties, radio and acoustic shielding materials

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    33. Zhelezina G.F., Bejder E.Ya., Raskutin A.E., Migunov V.P., Stolyankov Yu.V. Materialy dlya zvukopogloshhayushhih konstrukcij samoletov [Materials for sound-proof designs of airplanes] // Vse materialy. Enciklopedicheskij spravochnik. 2012. №4. S. 12–16.

    34. Gorelik G.S. Kolebaniya i volny. Vvedenie v akustiku, radiofiziku i optiku. 2-e izd. [Fluctuations and waves. Introduction in acoustics, radiophysics and optics. 2nd ed.] M., 1959. 572 s.

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    37. Radio wave absorbing sound shielding panel: pat. 2002261489 Japan; publ. 13.09.02.

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DOI: 10.18577/2071-9140-2016-0-4-68-73

UDC: 620.179:678.8

Pages:: 68-73

A.S. Boychuk1, A.S. Generalov1, I.A. Dikov1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Creating acoustic contact between phased array and convex surface of tested object during ultrasonic NDT of FRP

Integral monolith structures of polymer composite materials such as CFRP panels with small radius convex surfaces with molded stiffeners (stringers) are merely hard to test using traditional NDT techniques. Special tools to create the acoustic contact between the phased array and the test object have been designed in order to test the parts and structures of FRP with curvilinear surfaces. The research was carried out and the possibility of forming a stable acoustic contact between the phased array and the convex surface of the object under testing with the curvilinear surfaces radius of not less than 250 mm using the designed tools was experimentally demonstrated. The work is executed within the implementation of the complex scientific direction 2.3. «Methods of nondestructive research and control» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: ultrasonic testing, phased array, fiber reinforced plastic (FRP), carbon fiber reinforced plastic (CFRP), acoustic contact

Reference List

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    2. Dementeva L.A., Serezhenkov A.A., Lukina N.F., Kucevich K.E. Kleevye prepregi i sloistye materialy na ih osnove [Adhesive prepregs and layered materials on their basis] // Aviacionnye materialy i tehnologii. 2013. №2. S. 19–21.

    3. Poliimidnoe svyazuyushhee dlya armirovannyh plastikov, prepreg na ego osnove i izdelie, vypolnennoe iz nego: pat. 2394857 Ros. Federaciya [Polyimide binding for the reinforced plastics, prepreg on its basis and the product which has been executed of it: pat. 2394857 Rus. Federation]; opubl. 07.05.09.

    4. Epoksidnoe svyazuyushhee, prepreg na ego osnove i izdelie, vypolnennoe iz nego: pat. 2424259 Ros. Federaciya [Epoxy binding, prepreg on its basis and the product which has been executed of it: stalemate. 2424259 Rus. Federation]; opubl. 22.10.2009.

    5. Chursova L.V., Dushin M.I., Hrulkov A.V., Muhametov R.R., Kogan D.I., Popov Yu.O. Osobennosti tehnologii izgotovleniya detalej iz kompozicionnyh materialov metodom propitki pod davleniem [Features of manufacturing techniques of details from composite materials impregnation method under pressure] // Kompozicionnye materialy v aviakosmicheskom materialovedenii: sb. tez. dokl. Mezhotraslevoj nauch.-tehnich. konf., posvyashhennoj 100-letiyu so dnya rozhdeniya chl.-korr. A.T. Tumanova. M.: VIAM, 2009. S. 17.

    6. Dushin M.I., Hrulkov A.V., Muhametov R.R. Vybor tehnologicheskih parametrov avtoklavnogo formovaniya detalej iz polimernyh kompozicionnyh materialov [A choice of technological parameters of autoclave formation of details from polymeric composite materials] // Aviacionnye materialy i tehnologii. 2011. №3. S. 20–26.

    7. Hrulkov A.V., Dushin M.I., Popov Yu.O., Kogan D.I. Issledovaniya i razrabotka avtoklavnyh i bezavtoklavnyh tehnologij formovaniya PKM [Researches and development autoclave and out-of-autoclave technologies of formation of PCM] //Aviacionnye materialy i tehnologii. 2012. №S. S. 292–301.

    8. Kogan D.I., Chursova L.V., Petrova A.P. Tehnologiya izgotovleniya PKM sposobom propitki plenochnym svyazuyushhim [PCM manufacturing techniques in the way of impregnation by the film binding] // Klei. Germetiki. Tehnologii. 2011. №5. S. 25–29. 

    9. Kablov E.N., Kondrashov S.V., Yurkov G.Yu. Perspektivy ispolzovaniya uglerodsoderzhashhih nanochastic v svyazuyushhih dlya polimernyh kompozicionnyh materialov [Perspectives of use of carbon-containing nanoparticles in binding for polymeric composite materials] // Rossijskie nanotehnologii. 2013. T. 8. №3–4. S. 24–42. 

    10. Kablov E.N., Kirillov V.N., Zhirnov A.D., Startsev O.V., Vapirov Yu.M. Centry dlya klimaticheskih ispytanij aviacionnyh PKM [The centers for climatic tests of aviation PCM] // Aviacionnaya promyshlennost. 2009. №4. S. 36–46. 

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    12. Dalin M.A., Generalov A.S., Bojchuk A.S., Lozhkova D.S. Osnovnye tendencii razvitiya akusticheskih metodov nerazrushayushhego kontrolya [Basic development tendencies of acoustic non-destructive control methods] // Aviacionnye materialy i tehnologii. 2013. №1. S. 64–69.

    13. Boychuk A.S., Generalov A.S., Stepanov A.V., Yuhackova O.V. Nerazrushayushhij kontrol PKM s ispolzovaniem ultrazvukovyh fazirovannyh reshetok [Non-destructive testing of PKM with use of the ultrasonic phased grids] // Promyshlennye ASU i kontrollery. 2013. №2. S. 39–43. 

    14. Boychuk A.S., Stepanov A.V, Kosarina E.I., Generalov A.S. Primenenie tehnologii ultrazvukovyh fazirovannyh reshetok v nerazrushayushhem kontrole detalej i konstrukcij aviacionnoj tehniki, izgotavlivaemyh iz PKM [Application of ultrasonic phased lattice technique for nondestructive testing of aviation FRP parts structures] // Aviacionnye materialy i tehnologii. 2013. №2. S. 41–46. 

    15. Boychuk A.S., Stepanov A.V., Generalov A.S. Ultrazvukovoj kontrol krivolinejnyh poverhnostej konstrukcij sovremennyh samoletov iz polimernyh kompozicionnyh materialov s pomoshh\'yu preobrazovatelya na fazirovannoj reshetke i special\'nyh prisposoblenij [Ultrasonic control of curvilinear surfaces of designs of modern airplanes from polymeric composite materials by means of the converter on the phased grid and special adaptations] // Sb. tez. dokl. XIX Mezhdunar. konf. «Sovremennye metody i sredstva nerazrushayushhego kontrolya i tehnicheskoj diagnostiki». Gurzuf, 2011. S. 129–130. 

    16. Boychuk A.S., Stepanov A.V., Generalov A.S. Ultrazvukovoj kontrol integralnyh konstrukcij iz polimernyh kompozicionnyh materialov s pomoshhyu preobrazovatelya na fazirovannoj reshetke i specialnyh prisposoblenij [Ultrasonic control of integral designs from polymeric composite materials by means of the converter on the phased grid and special adaptations] // Novye materialy i tehnologii glubokoj pererabotki syrya – osnova innovacionnogo razvitiya ekonomiki Rossii: sb. tez. dokl. Mezhdunar. nauch.-tehnich. konf. M.: VIAM, 2012.

    17. Lozhkova D.S., Boychuk A.S., Trifonova S.I., Generalov A.S., Stepanov A.V. Issledovanie vliyaniya krivizny poverhnosti integralnoj konstrukcii iz ugleplastika na ee kontroleprigodnost s ispolzovaniem preobrazovatelya na fazirovannyh reshetkah [Research of influence of curvature of surface of integral design from ugleplastika on its kontroleprigodnost with converter use on the phased grids] // Radioelektronika, elektrotehnika i energetika: sb. tez. dokl. XVIII Mezhdunar. nauch.-tehnich. konf. studentov i aspirantov. M., 2012. T. 2. S. 143. 

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DOI: 10.18577/2071-9140-2016-0-4-74-79

UDC: 517.25

Pages:: 74-79

E.I. Oreshko1, V.S. Erasov1, A.N. Lutsenko1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Calculation features of cores and plates stability

Questions of stability of cores and plates depending on their geometrical parameters are considered. The finite element method is applied for calculating the stability of the cores and plates. Analysis of the results of these calculations allowed us to determine the factors affecting the stability of the cores and plates. Limits of formulas applicability for the critical force calculation of the cores and plates stability loss are defined.

Keywords: stability calculation, plate, core, finite element method, critical force for buckling

Reference List

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    3. Kablov E.N. Aviakosmicheskoe materialovedenie [Aerospace materials science] // Vse materialy. Yenciklopedicheskij spravochnik. 2008. №3. S. 2–14.

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    5. Astahov M.F., Karavaev A.V., Makarov S.Ya., Suzdaltsev Ya.Ya. Spravochnaya kniga po raschetu samoleta na prochnost [The reference book by airplane calculation on durability]. M.: Gos. izd-vo oboronnoj prom-sti, 1954. S. 411–412.

    6. Prochnost. Ustojchivost. Kolebaniya: spravochnik v 3-h t. / pod obshh. red. I.A. Birgera, Ya.G. Panovko [Fluctuations: the directory in 3 t. / gen. ed. by I.A. Birger, Ya.G. Panovko]. M.: Mashinostroenie, 1968. T. 3. S. 94.

    7. Oreshko E.I., Erasov V.S., Lutsenko A.N., Terentev V.F., Slizov A.K. Postroenie diagramm deformirovaniya v trehmernom prostranstve σ–ε–t [Creation of charts of deformation in three-dimensional space σ–ε–t] // Aviacionnye materialy i tehnologii. 2017 (v pechati).

    8. Dimitrienko Yu.I., Gubareva E.A., Sborshhikov S.V., Bazyleva O.A., Lutsenko A.N., Oreshko E.I. Modelirovanie uprugoplasticheskih harakteristik monokristallicheskih intermetallidnyh splavov na osnove mikrostrukturnogo chislennogo analiza [Modeling of elasto-plastic characteristics of single-crystal intermetallic alloys on the basis of the microstructural numerical analysis] // Matematicheskoe modelirovanie i chislennye metody. 2015. №2. S. 3–22.

    9. Dimitrienko Yu.I., Lucenko A.N., Gubareva E.A., Oreshko E.I., Bazyleva O.A., Sborshhikov S.V. Raschet mekhanicheskikh kharakteristik zharoprochnykh intermetallidnykh splavov na osnove nikelya metodom mnogomasshtabnogo modelirovaniya struktury [Calculating of mechanical characteristics of heat resistant intermetallic alloys on the basis of nickel by method of multi-scale modeling of structure] // Aviacionnye materialy i tehnologii. 2016. №3 (42). S. 33–48. DOI: 10.18577/2071-9140-2016-0-3-33-48.

    10. Oreshko E.I., Erasov V.S., Lutsenko A.N. Matematicheskoe modelirovanie deformirovaniya konstrukcionnogo ugleplastika pri izgibe [Mathematical modeling of deformation constructional carbon fiber at a bend] // Aviacionnye materialy i tehnologii. 2016. №2 (41). S. 50–59. DOI: 10.18577/2071-9140-2016-2-50-59.

    11. 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 alyuminij-litievogo 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.

    12. Gusev D.E., Kollerov M.Yu., Rudakov S.S., Korolev P.A., Oreshko E.I. Ocenka biomehanicheskoj sovmestimosti implantiruemyh opornyh plastin iz splavov na osnove titana i nikelida titana metodom komp\'yuternogo modelirovaniya [Assessment of biomechanical compatibility of implanted bed plates from titanium-based alloys and nickelid titanium method of computer modeling] // Titan. 2011. №3 (33). S. 39–44. 

    13. Kollerov M.Yu., Gusev D.E., Oreshko E.I. Yeksperimentalno-teoreticheskoe obosnovanie vybora metoda i implantatov dlya ustraneniya voronkoobraznoj deformacii grudnoj kletki [Experimental and theoretical justification of choice of method and implants for elimination of funneled deformation of thorax] // Nauchnye trudy (Vestnik MATI). 2012. №19 (91). S. 331–336.

    14. Kollerov M.Yu., Usikov V.D., Kuftov V.S., Gusev D.E., Oreshko E.I. Mediko-tehnicheskoe obosnovanie ispolzovaniya titanovyh splavov v implantiruemyh konstrukciyah dlya stabilizacii pozvonochnika [Medico-technical justification of use of titanium alloys in implanted designs for backbone stabilization] // Titan. 2013. №1 (39). S. 39–45.

    15. 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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12.

DOI: 10.18577/2071-9140-2016-0-4-80-85

UDC: 620.179.1

Pages:: 80-85

A.A. Demidov1, A.V. Stepanov2, E.M. Turbin2, O.A. Krupnina1

[1] Federal State Unitary Enterprise «All-Russian Scientific Research Institute of Aviation Materials»
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

The х-ray testing modes providing with radiation imaging with predetermined contrast

The process of analytical formation of radiation image of х-ray inspection objects is presented and approximate contrast expression of the radiation image as a measure of useful information is obtained. Radiation contrast is a monotonic function that has no extreme points, so a certain level of sensitivity and necessary energy of the radiation should be given for the optimum x-ray inspection. The calculation of the minimum value of the radiation contrast based on requirements of the optical contrast is performed. The minimum value of anode voltage of х-ray inspection of steel objects up to 80 mm thickness is determined. The experimental verification of the calculated data and the analysis of the results are performed. The obtained data on the radiation energy selection is much lower than those in standard documents. The work is executed within the implementation of the complex scientific direction 2.3. «Methods of nondestructive researches and control» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: х-ray inspection, radiation contrast, radiation energy, optical contrast, optimum exposure mode

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. Aviakosmicheskoe materialovedenie [Aerospace materials science] // Vse materialy. Enciklopedicheskij spravochnik. 2008. №3. S. 2–14.

    3. Kablov E.N., Morozov G.A., Krutikov V.N., Muravskaya N.P. Attestaciya standartnyh obrazcov sostava slozhnolegirovannyh splavov s primeneniem etalona [Certification of standard samples of structure of complex-alloyed alloys using standard] // Aviacionnye materialy i tehnologii. 2012. №2. S. 9–11.

    4. Kablov E.N. K 80-letiyu VIAM [To VIAM 80 anniversary] // Zavodskaya laboratoriya. Diagnostika materialov. 2012. T. 78. №5. S. 79–82.

    5. Kablov E.N. Sovremennye materialy – osnova innovacionnoj modernizacii Rossii [Modern materials – basis of innovative modernization of Russia] // Metally Evrazii. 2012. № 3. S. 10–15.

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    7. Standart EN444: 1994. Nerazrushayushhij kontrol. Principy radiograficheskogo metoda kontrolya metallov rentgenovskim i gamma-izlucheniem. Autentichnyj perevod. Evropejskij institut standartizacii. Stassart 36, V 1050 [EN444 standard: 1994. Non-destructive testing. Principles of radiographic control method of metals x-ray and gamma radiation. Authentic transfer. European institute of standardization. Stassart 36, In 1050. Brussels. 1994. 8 pages.]. Bryussel. 1994. 8 s.

    8. Dobromyslov V.A. Radiacionnye metody nerazrushayushhego kontrolya [Radiation methods of non-destructive testing]. M.: Mashinostroenie, 1999. 101 s. 

    9. Rumyancev S.V., Shtan A.S., Goltsev V.A. Spravochnik po radiacionnym metodam nerazrushayushhego kontrolya [Directory on radiation methods of non-destructive testing]. M.: Energoizdat, 1982. 240 s.

    10. Shpagin A.P., Vystropov V.I. K raschetu kontrasta rentgenovskogo izobrazheniya [To calculation of contrast of the x-ray image] // Defektoskopiya. 1972. №3. S. 118–122. 

    11. Dobromyslov V.A., Zharkova L.V. Integralnye (effektivnye) i differencialnye linejnye koefficienty oslableniya tormoznogo rentgenovskogo izlucheniya i effektivnye faktory nakopleniya rasseyannogo izlucheniya [Integral (effective) and differential linear factors of weakening of braking x-ray emission and effective factors of accumulation of stray radiation] // Defektoskopiya. 1985. №1. S. 1–3.

    12. Sosnin F.R. Ocenka parametrov radiacionnyh izobrazhenij defektov [Assessment of parameters of radiation images of defects] // Defektoskopiya. 1988. №4. S. 40–44.

    13. Okunade A.A. Parameters and computer software for the evaluation of mass attenuation and mass energy-absorption coefficients for body tissues and substitutes // Jour. Medical Physics. 2007. Vol. 32. P. 124–132.

    14. Sasanpur M.T., Kosarina E.I. Rekomendacii po vyboru anodnyh napryazhenij pri rentgenovskom kontrole stal\'nyh obektov [Recommendations about choice of anode voltages at x-ray control of steel objects] // Defektoskopiya. 2011. №5. S 48–53.

    15. Sasanpur M.T., Savvina N.A. Rentgenovskij kontrol izdelij iz stali pri zadannom urovne chuvstvitelnosti [X-ray control of products from steel at the set level of sensitivity] // Vestnik MEI. 2009. №1. S. 158–162.

    16. Stepanov A.V., Kosarina E.I., Savvina N.A. Radiograficheskie tehnicheskie plenki RT-K i RT-7T. Rezultaty ih ispytaniya [Radiographic technical films of RT-K and RT-7T. Results of their testing] // Aviacionnye materialy i tehnologii. 2012. №1. S. 37–42.

    17. Kosarina E.I., Mihajlova N.A., Demidov A.A., Turbin E.M. Rentgenovskij kontrol krupnogabaritnyh otlivok slozhnoj formy iz splavov gruppy «silumin» [X-ray testing of large-sized intricate castings made from aluminum alloys] // Aviacionnye materialy i tehnologii. 2013. №2. S. 55–58.

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DOI: 10.18577/2071-9140-2016-0-4-86-94

UDC: 678.747.2

Pages:: 86-94

N.V. Antyufeeva1, V.M. Aleksashin1, M.R. Pavlov1, Yu.V. Stolyankov1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Research of possibility of use carbon fiber reinforced polymers in the conditions of the Arctic climate

Carbon fiber reinforced polymers (CFRP) have taken important place among constructional materials that became possible thanks to unique high level of strength and elastic characteristics, high values of long and fatigue resistance, small creep and low density of this class of materials. In the article methodical approaches are given to research curing kinetics of prepregs and to model curing process of carbon fiber reinforced polymers. Influence of external factors on operation properties of carbon fiber reinforced polymers has been studied using laboratory and environmental methods of exposure at high (+100°C) and extremely low temperatures (-60°C). Researches have shown that carbon fiber reinforced polymers keep their mechanical properties at low temperatures (-60°C) and can be recommended as building structures in the conditions of the Arctic climate.

Keywords: carbon fiber reinforced polymers, Arctic region, curing kinetics, climatic and mechanical tests

Reference List

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