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Aviation materials and technologies №3, 2017

Contents

  • O.S. Kashapov, T.V. Pavlova, V.S. Kalashnikov, A.R. Kondratyeva

    The influence of heat treatment conditions on structure and properties of pilot forgings from VT41 alloy with fine grained structure

    3-7
  • A.A. Skupov, M.D. Panteleev, E.N. Ioda, D.A. Movenko

    The efficiency of rare earth metals for filler materials alloying

    14-19
  • E.A. Tikhomirova, S.A. Budinovskiy, A.A. Zhivushkin, E.F. Sidokhin

    Features of thermal fatigue development in details, produced from heat-resistant alloys with coatings

    20-25
  • E.N. Kablov, O.V. Startsev, I.M. Medvedev, I.S. Shelemba

    Fiber optic sensors for monitoring corrosion processes in units of aviation engineering (review)

    26-34
  • A.A. Shavnev, E.I. Kurbatkina, D.V. Kosolapov

    Methods for joining of aluminum composite materials (review)

    35-42
  • A.R. Akmeev, I.N. Gulyaev, A.V. Ilichev, N.V. Ivanov

    Research of mechanical behavior of metal composite (aluminum and carbon fiber-reinforced polymer) with an adaptive reinforcement scheme

    43-49
  • N.S. Perov

    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

    50-55
  • K.I. Donetski, R.Yu. Karavaev, A.I. Tsybin, E.A. Veshkin, E.S. Mikhaldykin

    Constructional fiberglass plastic for manufacturing of enclosing sheeting elements

    56-64
  • A.I. Gulyaev, N.O. Yakovlev, V.D. Krylov, O.A. Lashov

    Application of fractographic analysis in the study of interlayer fracture of PCM

    65-73
  • M.I. Daskovskiy, M.S. Doriomedov, D.V. Sevastyanov, S.Yu. Skripachyov

    Polymer biocomposites - prospects of application (review)

    74-80
  • E.G. Sentyurin, I.V. Mekalina, M.K. Aizatulina, Yu.A. Isaenkova

    The history of aircraft materials of glass and polymer materials with special properties (To the 75th anniversary Laboratory of polymer materials with special properties)

    81-86
  • A.V. Grinevich

    Career of the Professor N.M. Sklyarov

    87-94
Содержание номера
1.

DOI: 10.18577/2071-9140-2017-0-3-3-7

UDC: 669.018.44:669.295

Pages:: 3-7

O.S. Kashapov1, T.V. Pavlova1, V.S. Kalashnikov1, A.R. Kondratyeva1

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

The influence of heat treatment conditions on structure and properties of pilot forgings from VT41 alloy with fine grained structure

The study presents the influence of two-step annealing on mechanical properties - short-term strength, heat-resistance and impact toughness of large-scale experimental-industrial forgings with fine-grained structure made from three melting of pseudo-alpha titanium alloy VT41. The obtained results allow making preliminary conclusions in order to set annealing modes, as well as to carry out a comparative analysis with previous results on the study of bars and blades made of alloy VT41.

Keywords: heat-resistance titanium alloys, mechanical properties, structure, chemical composition.

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. 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.

    4. Kablov E.N. Materialy dlya izdeliya «Buran» – innovacionnye resheniya formirovaniya shestogo tehnologicheskogo uklada [Materials for «Buran» spaceship – innovative solutions of formation of the sixth technological mode] //Aviacionnye materialy i tehnologii. 2013. №S1. S. 3–9.

    5. Orlov M.R. Strategicheskie napravleniya razvitiya Ispytatelnogo centra FGUP «VIAM» [Strategic directions of development of the Test center FSUE «VIAM»] // Aviacionnye materialy i tehnologii. 2012. №S. S. 387–393.

    6. Horev A.I., Belov S.P., Glazunov S.G. Metallovedenie titana i ego splavov [Metallurgical science of titanium and its alloys]. M.: Metallurgiya, 1992. 352 s.

    7. Pavlova T.V., Kashapov O.S., Kondrateva A.R., Kalashnikov V.S.Vozmozhnosti po rasshireniyu oblasti primeneniya splava VT8-1 dlya diskov i rabochih koles kompressora [Opportunities to expand the VT8-1 alloy application for disks and compressor rotor wheels] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №3 (39). St. 05. Available at: http://www.viam-works.ru (accessed: January 10, 2017). DOI: 10.18577/2307-6046-2016-0-3-5-5.

    8. Savushkin A.N., Kashapov O.S., Golynec S.A. Vliyanie skorosti nagruzheniya na mehanicheskie svojstva zharoprochnyh titanovyh splavov [An influence of loading rate on mechanical properties of heat-resistant titanium alloys] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №3. St. 04. Available at: http://www.viam-works.ru (accessed: January 10, 2017). DOI: 10.18577/2307-6046-2015-0-3-4-4.

    9. Kalashnikov V.S., Kashapov O.S., Pavlova T.V., Istrakova A.R. Issledovanie svarnyh soedinenij splava VT41, poluchennyh metodom ELS [Investigation of VT41 alloy welded joints produced by EBW] // Aviacionnye materialy i tehnologii. 2014. №S5. S. 81–88. DOI: 10.18577/2071-9140-2014-0-S5-81-88.

    10. Pavlova T.V., Kashapov O.S., Nochovnaya N.A. Titanovye splavy dlya gazoturbinnyh dvigatelej [Titanium alloys for gas turbine engines] // Vse materialy. Enciklopedicheskij spravochnik. 2012. №5. S. 8–14.

    11. Kashapov O.S., Pavlova T.V., Nochovnaya N.A. Vliyanie rezhimov termicheskoj obrabotki na strukturu i svojstva zharoprochnogo titanovogo splava dlya lopatok KVD [Influence of modes of thermal processing on structure and property of heat resisting titanium alloy for KVD blades] // Aviacionnye materialy i tehnologii. 2010. №2 (15). S. 8–14.

    12. Kashapov O.S. Kinetika izmeneniya mikrostruktury prutkovoj lopatochnoj zagotovki iz splava VT41 v zavisimosti ot temperaturno-vremennyh parametrov termicheskoj obrabotki [Kinetics of change of microstructure of bar scapular preparation from alloy ВТ41 depending on temperature and time parameters of thermal processing] // Perspektivnye materialy. 2008. №5. S. 137.

    13. Kashapov O.S., Pavlova T.V., Nochovnaya N.A. Issledovanie termicheskoj stabil\'nosti splava VT41 posle razlichnoj termicheskoj obrabotki [Research of thermal stability of alloy ВТ41 after different thermal processing] // Metallovedenie i termicheskaya obrabotka metallov. 2010. №8. S. 30–34.

    14. Kashapov O.S., Pavlova T.V. Issledovanie vliyaniya parametrov struktury polufabrikatov iz splava VT41 na mehanicheskie svojstva [Research of influence of parameters of structure of semi-finished products from alloy VT41 on mechanical properties] // Vestnik MGTU im. N.E. Baumana. Ser.: Mashinostroenie. 2015. №2 (101). S. 138–145.

    15. Kablov E.N., Kashapov O.S., Pavlova T.V., Nochovnaya N.A. Razrabotka opytno-promyshlennoj tehnologii izgotovleniya polufabrikatov iz psevdo-α-titanovogo splava VT41 [Development of trial manufacturing techniques of semi-finished products from pseudo-α-titanium alloy VT41] // Titan. 2016. №2 (52). S. 33–42.

    16. Belyaev M.S., Gorbovec M.A., Kashapov O.S., Hodinev I.A. Mehanicheskie svojstva i struktura titanovogo splava VT41 [Mechanical properties and BT41 titanium alloy structure] // Tsvetnye metally. 2014. №8 (860). S. 66–71.

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3.

DOI: 10.18577/2071-9140-2017-0-3-14-19

UDC: 669.046.516

Pages:: 14-19

A.A. Skupov1, M.D. Panteleev1, E.N. Ioda1, D.A. Movenko1

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

The efficiency of rare earth metals for filler materials alloying

Today, the usage of rare earth metals for alloying of aluminum alloys is perspective way. The existing filler materials don’t provide optimal combination of strength, ductility and resistance to the formation of hot cracks of joint welds of high-strength aluminum-lithium alloys. In this article, the influence of filler materials alloying system on crack resistance of high-strength aluminum-lithium alloys was shown and the allocation of rare earth and transition metals in weld seam was discovered. Application of filler material, alloyed by rare earth metals increases mechanical properties of joint welds of high-strength aluminum-lithium alloys as compared with the indices, obtained for a welding variant using a serial filler material. The work is executed within the frames of the complex scientific direction 10.8. «Fusion welding technologies of new structural materials» («The strategic direction of development of materials and technologies of their processing for the period till 2030»)

Keywords: filler materials, welding, aluminum-lithium alloys, rare-earth metals, alloying of aluminum alloys.

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., 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: September 18, 2016).

    3. Lukin V.I., Skupov A.A., Panteleev M.D., Ioda E.N. Vliyanie dobavok skandiya na svarivaemost alyuminievyh splavov sistemy Al–Mg [Influence of additives of scandium on bondability of aluminum alloys of Al–Mg system] // Svarka i diagnostika. 2016. №1. S. 13–15.

    4. Skupov A.A., Ioda E.N., Panteleev M.D. Novye prisadochnye materialy dlya svarki vysokoprochnyh alyuminij-litievyh splavov [New filler materials for welding of high-strength aluminum-lithium alloys] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №9. St. 04. Available at: http://www.viam-works.ru (accessed: October 27, 2016). DOI: 10.18577/2307-6046-2016-0-9-4-4.

    5. Kablov E.N., Lukin V.I., Ospennikova O.G. Perspektivnye alyuminievye splavy i tehnologii ih soedineniya dlya izdelij aviakosmicheskoj tehniki [Perspective aluminum alloys and technologies of their connection for products of aerospace equipment] // Alyuminij-21. Svarka i pajka: tez. dokl. 2-j Mezhdunar. konf. SPb., 2012. St. 08.

    6. Kablov E.N., Lukin V.I., Zhegina I.P., Ioda E.N., Loskutov V.M. Osobennosti i perspektivy svarki alyuminijlitievyh splavov [Features and welding perspectives aluminumlithium alloys] // Aviacionnye materialy i tehnologii. 2002. №4. S. 3–12.

    7. Lukin V.I., Ioda E.N., Panteleev M.D., Skupov A.A. Vliyanie termicheskoj obrabotki na harakteristiki svarnyh soedinenij vysokoprochnyh alyuminijlitievyh splavov [Heat treatment influence on characteristics of welding joints of high-strength aluminum-lithium alloys] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №4. St. 06. Available at: http://www.viam-works.ru (accessed: September 07, 2016). DOI: 10.18577/2307-6046-2015-0-4-6-6.

    8. Lukin V.I., Ioda E.N., Skupov A.A., Ovchinnikov V.V. Friction stir welding of V-1461 and V-1469 high strength aluminium–lithium alloys // Welding International. 2016. Vol. 30. No.7. P. 552–556.

    9. Lukin V.I., Ioda E.N., Panteleev M.D., Skupov A.A. Osobennosti lazernoj svarki vysokoprochnyh alyuminij-litievyh splavov [Peculiarities of high-strength aluminum-lithium alloys laser welding] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №10. St. 07. Available at: http://www.viam-works.ru (accessed: December 07, 2016). DOI: 10.18577/2307-6046-2016-0-10-7-7.

    10. Lukin V.I., Skupov A.A., Panteleev M.D., Gorelova L.P. Zavisimost svarivaemosti splavov sistemy Al–Mg (serii 5HHH) ot sootnosheniya legiruyushhih elementov (Sc, Zr i Mn) [Dependence of bondability of alloys of Al–Mg system (5HHH series) on ratio of doping elements (Sc, Zr and Mn)] // Svarka i Diagnostika. 2015. №4. S. 9–12.

    11. Kablov E.N., Lukin V.I., Antipov V.V., Ioda E.N., Panteleev M.D., Skupov A.A. Effektivnost primeneniya prisadochnyh materialov pri lazernoj svarke vysokoprochnyh alyuminij-litievyh splavov [Efficiency of application of prisadochny materials at laser bonding high-strength aluminum-lithium alloys] // Svarochnoe proizvodstvo. 2016. №10. S. 17–21.

    12. Ryabov D.K., Kolobnev N.I., Ivanova A.O. Vliyanie dobavok kobalta i skandiya na mehanicheskie harakteristiki i korrozionnuyu stojkost profilej iz sredneprochnogo splava sistemy Al–Zn–Mg s dobavkoj medi [Effect of Co and Sc on mechanical properties and corrosion resistance of middle-strength Al–Zn–Mg alloy with small addition of Cu] // Trudy VIAM. elektron. nauch.-tehnich. zhurn. 2016. №6. St. 01. URL: http://www.viam-works.ru (accessed: October 15, 2016). DOI: 10.18577/2307-6046-2016-0-6-1-1.

    13. Zaharov V.V. Osobennosti kristallizacii alyuminievyh splavov, legirovannyh skandiem [Features of crystallization of the aluminum alloys alloyed by scandium] // Metallovedenie i termicheskaya obrabotka metallov. 2011. №9. S. 12–18.

    14. Filatov Yu.A., Bajdin N.G., Dobrozhinskaya R.I., Hamnagdaeva E.A., Ovsyannikov B.V. Novyj termicheski neuprochnyaemyj svarivaemyj kriogennyj splav 1545K sistemy Al–Mg–Sc [Not strengthened welded cryogenic alloy new thermally 1545К Al-Mg-Sc systems] // Tehnologiya legkih splavov. 2014. №1. S. 32–36.

    15. Shiganov I.N., Holopov A.A., Trushnikov A.V., Ioda E.N., Panteleev M.D., Skupov A.A. Lazernaya svarka vysokoprochnyh alyuminij-litievyh splavov s prisadochnoj provolokoj [Laser bonding high-strength aluminum - lithium alloys with filler wire] // Svarochnoe proizvodstvo. 2016. №6. S. 44–50.

    16. Shalin R.E., Efremov I.S., Yarovinskij Yu.L., Lukin V.I. Opyt proektirovaniya i izgotovleniya krupnogabaritnyh konstrukcij iz alyuminievo-litievyh splavov izdelij raketno-kosmicheskoj tehniki [Experience of design and manufacturing of large-size designs from aluminum-lithium alloys of products of space-rocket equipment] // Svarochnoe proizvodstvo. 1996. №11. S. 14–18.

    17. Lukin V.I., Ioda E.N., Bazeskin A.V., Lavrenchuk V.P., Kotelnikova L.V., Oglodkov M.S. Povyshenie nadezhnosti svarnyh soedinenij iz vysokoprochnogo alyuminievo-litievogo splava V-1461 [Increase of reliability of welded connections from high-strength aluminum-lithium alloy V-1461] // Svarochnoe proizvodstvo. 2010. №11. S. 14–17.

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    19. Lukin V.I. Effect of alloying elements Sc, Mn, and Zr on weldability of alloys of the Al–Mg–Sc–Mn–Zr system // Welding International. 1996. Vol. 10. No. 12. P. 987–989.

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4.

DOI: 10.18577/2071-9140-2017-0-3-20-25

UDC: 669.018.44

Pages:: 20-25

E.A. Tikhomirova1, S.A. Budinovskiy2, A.A. Zhivushkin1, E.F. Sidokhin3

[1] Join Stock Company «Klimov»
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[3] Limited Liability Company «CB Rentgen devices»

Features of thermal fatigue development in details, produced from heat-resistant alloys with coatings

The details of turbine hot section work under conditions of high temperatures, aggressive environments and multiple thermal changes in modern aviation engines. Multilayer heat-resistant coatings are applied to protect turbine blades surface. The work analyses the results of laboratory thermal cycle tests and metallographic studies of imitation samples of nozzle turbine blades from intermetallic heat-resistant nickel alloys with thermal-protective coatings, produced with the use of ion-plasma and magnetron technologies. The analysis of the features of development of plastic and elastic deformation in the surface of samples under cyclic “heating-cooling” is carried out and a new approach is proposed to estimate results using a graphic card of thermal-cycle tests.

Keywords: thermal fatigue, heat-resistant coatings, thermal-cycle tests, thermal fatigue crack.

Reference List

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5.

DOI: 10.18577/2071-9140-2017-0-3-26-34

UDC: 621.3.084.2:620.193

Pages:: 26-34

E.N. Kablov1, O.V. Startsev1, I.M. Medvedev1, I.S. Shelemba2

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[2] Limited Liability Company «Inversiya-Sensor»

Fiber optic sensors for monitoring corrosion processes in units of aviation engineering (review)

In recent years specialized sensors and devices - corrosion sensors are being developed to monitor corrosion processes in real time. The development of fiber optic sensors is one of the most promising directions in the field of corrosion monitoring and monitoring of microclimate corrosive aggressiveness. The main directions of fiber optic corrosion sensors development are reviewed in this article. It is shown that two types of constructions are the most commonly used, namely: with sputtering of alloy on the ends of optical fiber or optical fiber with Bragg grating, while researches of sensor parameters are performed during accelerated tests.

Keywords: corrosion, corrosive aggressiveness of atmosphere, fiber optic sensors.

Reference List

    1. 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.

    2. Kablov E.N., Karimova S.A., Semenova L.V. Korrozionnaya aktivnost ugleplastikov i zashhita metallicheskih silovyh konstrukcij v kontakte s ugleplastikom [Corrosion activity carbonplastics and protection of metal load bearing structures in contact with the carbonplastics] // Korroziya: materialy, zashhita. 2011. №12. P. 1–7.

    3. Kulyushina N.V., Kozlov I.A., Kutyrev A.E., Vagramyan T.A. Adhesive coatings on the basis of trialkoxysilanes for aluminum and steel // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №8. St. 05. Available at: http://viam-works.ru (accessed: December 09, 2016). DOI: 10.18577/2307-6046-2015-0-8-5-5.

    4. Zakharova L.V. Anodno-oksidnoe pokrytie – zashhita titanovyh splavov ot goryachesolevoj korrozii [Anodic oxide coating – protection of titanium alloys against hot salt corrosion] //Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №10. St. 02. Available at: http://www.viam-works.ru (accessed: December 09, 2016). DOI: 10.18577/2307-6046-2015-0-10-2-2.

    5. Karpov V.A., Kovalchuk Yu.L., Kuznecov Yu.I. i dr. Zashhita ot morskoj korrozii stalej v zamknutyh obemah [Protection against sea corrosion staly in the closed volumes] // Korroziya: materialy, zashhita. 2013. №5. S. 35–40.

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    9. Kablov E.N., Starcev O.V., Medvedev I.M., Panin S.V. Korrozionnaya agressivnost primorskoj atmosfery. 1. Faktory vliyaniya (obzor) [Corrosion aggression of the seaside atmosphere. 1. Factors of influence (overview)] // Korroziya: materialy, zashhita. 2013. №12. S. 6–18.

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Полнотекстовая версия
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DOI: 10.18577/2071-9140-2017-0-3-35-42

UDC: 669.018.95

Pages:: 35-42

A.A. Shavnev1, E.I. Kurbatkina1, D.V. Kosolapov1

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

Methods for joining of aluminum composite materials (review)

In high-technology industries such as aerospace industry, traditional materials and alloys have nowadays been replaced by composite materials due to their high operational properties - strength, wear resistance, low density, etc. Aluminum-based composite materials are the most dynamically developing and significant direction- both in terms of the number of conducted researches and issued patents and in terms of volume of industrial production. Along with the developments in the field of structure, properties and technologies the results in secondary processing are becoming extremely important, in particular, in the field of joining of metal composite materials between themselves and with other materials. The main joining methods of aluminum composite materials such as: welding, soldering, bonding and mechanical fastening are considered. The advantages and disadvantages of each method are analyzed, and recommendations on the choice of technological modes to obtain quality joints with high mechanical properties are given.

Keywords: рowder metallurgy, mechanical alloying, composite materials, solid-phase interaction.

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DOI: 10.18577/2071-9140-2017-0-3-43-49

UDC: 620.1:669.018.95

Pages:: 43-49

A.R. Akmeev1, I.N. Gulyaev1, A.V. Ilichev1, N.V. Ivanov1

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

Research of mechanical behavior of metal composite (aluminum and carbon fiber-reinforced polymer) with an adaptive reinforcement scheme

Researches of mechanical characteristics of «self-adapting» metal composite based on aluminum and carbon fiber-reinforced polymer are given in this work . Different reinforcement schemes (orientation of laying of reinforcing filler - carbon fiber-reinforced polymer) and their influence on elastic and strength properties of metal composite are considered. Tests simulating the complex stress state of samples with different order and structure of reinforcement of metal composite material are also carried out. Work is executed within the implementation of the complex scientific directions: 4. «Smart, adaptive materials and coatings» and 6. «Multilayer metal polymer, bimetallic and hybrid materials» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: metal composite, carbon fiber-reinforced polymer, aluminum, polymer composite material, mechanical tests.

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DOI: 10.18577/2071-9140-2017-0-3-50-55

UDC: 66.017

Pages:: 50-55

N.S. Perov1

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

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

Based on the analysis of scientific and technical data, the connection of molecular mobility in polymer materials at low temperatures with the parameters of fracture toughness and impact strength is shown in the article. The performed calculations by the method of molecular dynamic modeling demonstrated the possibility to develop polymer systems with additional mechanisms of dissipation of mechanical energy at low temperatures. The analysis of molecular mobility in the polystyrene matrix with the use of modifiers based on dendrimers and hyperbranched polymers is performed to check the theoretical approaches .

Keywords: dynamic mechanical properties, glass transition, secondary relaxation transitions, molecular dynamic modeling.

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. 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.

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    5. Sokolov I.I., Raskutin A.E. Ugleplastiki i stekloplastiki novogo pokoleniya [Coalplastics and fibreglasses of new generation] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №4. St. 09. Available at: http://www.viam-works.ru (accessed: January 16.2017).

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DOI: 10.18577/2071-9140-2017-0-3-56-64

UDC: 678.8

Pages:: 56-64

K.I. Donetski1, R.Yu. Karavaev1, A.I. Tsybin1, E.A. Veshkin1, E.S. Mikhaldykin2

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

Constructional fiberglass plastic for manufacturing of enclosing sheeting elements

The possibility of using polymer composite materials (PCM) on the basis of braided preforms for constructional elements of enclosing sheeting, first of all sheet piles of circular section and «trough-shaped» type are considered. Advantages of polymer composite materials in comparison with traditionally applied materials are considered. Epoxy vinyl ester binding, fiberglass plastic for designs of enclosing sheeting are developed and their properties are studied. The manufacturing technology by the method of vacuum infusion of two types of enclosing sheeting designs, namely, circular section on the basis of braided sleeve and «trough-shaped» type on the basis of full-strength glass-fiber fabric are developed. The complex of physicomechanical tests and assessment of stress-strain behavior of samples of enclosing sheeting elements at different values of loads and loading conditions is carried out. A batch of enclosing sheeting elements of «trough-shaped» type (Larssen sheet piles) has been produced by the method of vacuum infusion using full-strength glass-fiber fabric. With their use, the underground protective wall is established, excluding soil motions and providing grout cutoff curtain.

Keywords: polymer composite materials, fiberglass, binder, braided preforms, glass-fiber fabrics, autoclave-free molding, composite enclosing sheeting.

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    13. Chursova L.V., Raskutin A.E., Gurevich Ya.M., Panina N.N. Svyazuyushhee holodnogo otverzhdeniya dlya stroitelnoj industrii [Binding cold curing for the construction industry] // Klei. Germetiki. Tehnologii. 2012. №5. S. 40–44.

    14. Postnova M.V., Postnov V.I. Opyt razvitiya bezavtoklavnyh metodov formovaniya PKM [Development experience out-of-autoclave methods of formation PCM] // Trudy VIAM: ehlektron. nauch.-tekhnich. zhurn. 2014. №4. St. 06. Available at: http://www.viam-works.ru (accessed: November, 21 2016). DOI 10.18577/2307-6046-2014-0-4-6-6.

    15. 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.

    16. Donetskij K.I., Kogan D.I., Hrulkov A.V. Ispolzovanie tehnologij pleteniya pri proizvodstve elementov konstrukcij iz PKM [The use of thecnology of braiding in production of structural elements of polymer composites materials] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №10. St. 04. Available at: http://www.viam-works.ru (accessed: November, 22 2016).

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    22. Muhametov R.R., Ahmadieva K.R., Kim M.A., Babin A.N. Rasplavnye svyazujushhie dlya perspektivnyh metodov izgotovleniya PKM novogo pokoleniya [Melt binding for perspective methods of production of PCM of new generation] // Aviacionnye materialy i tehnologii. 2012. №S. S. 260–265.

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DOI: 10.18577/9140-2071-2017-0-3-65-73

UDC: 539.422:691.175.3

Pages:: 65-73

A.I. Gulyaev1, N.O. Yakovlev1, V.D. Krylov1, O.A. Lashov1

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

Application of fractographic analysis in the study of interlayer fracture of PCM

The fractographic analysis has been carried out and static interlayer fracture toughness characteristics of layered glass and carbon fiber polymer composites, perspective for application in aviation products have been defined. Using scanning electron microscopy the microrelief characteristics of the fracture surfaces formed under mode I and mode II fracture resistance tests have been revealed. The influence of the matrix phase morphology, the reinforcing structure, and also the temperature and climatic factors on the deformation and fracture micromechanisms under the composites delamination has been studied.

Keywords: fracture mechanics, interlayer fracture toughness, mode I, mode II, fractography, phase morphology, scanning electron microscopy.

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. Sokolov I.I., Raskutin A.E. Ugleplastiki i stekloplastiki novogo pokoleniya [Coalplastics and fibreglasses of new generation] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №4. St. 09. Available at: http://www.viam-works.ru (accessed: April, 15 2017).

    3. Kablov E.N. Kompozity: segodnya i zavtra [Composites: today and tomorrow] // Metally Evrazii. 2015. №1. S. 36–39.

    4. Kablov E.N., Chursova L.V., Lukina N.F., Kucevich K.E., Rubcova E.V., Petrova A.P. Issledovanie epoksidno-polisulfonovyh polimernyh sistem kak osnovy vysokoprochnyh kleev aviacionnogo naznacheniya [Research of epoxy and polysulfonic polymeric systems as bases of high-strength adhesives of aviation assignment] // Klei. Germetiki. Tehnologii. 2017. №3. S. 7–12.

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    8. Kablov E.N., Kirillov V.N., Zhirnov A.D., Starcev 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. Yakovlev N.O., Gulyaev A.I., Lashov O.A. Treshchinostoikost sloistykh polimernykh kompozitsionnykh materialov (obzor) [Crack firmness of layered polymeric composite materials (review)] // Trudy VIAM: elektron. nauch.-tekhnich. zhurn. 2016. №4 (40). St. 12. Available at:  http://www.viam-works.ru (accessed: April 15, 2017) DOI: 10.185772307-6046-2016-0-4-12-12.

    13. Krylov V.D., Yakovlev N.O., Kurganova Yu.A., Lashov O.A. Mezhsloevaya treshchinostoikost konstruktsionnykh polimernykh kompozitsionnykh materialov [Mezhsloyevy crack firmness of constructional polymeric composite materials] // Aviacionnye materialy i tehnologii. 2016. №1 (40). S. 79–85. DOI: 10.18577/2071-9140-2016-0-1-79-85.

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    15. Yakovlev N.O., Gulyaev A.I., Krylov V.D., Shurtakov S.V. Mikrostruktura i svojstva konstrukcionnyh kompozicionnyh materialov pri ispytanii na staticheskuyu mezhsloevuyu treshhinostojkost [Microstructure and Properties of the Structural Composite Material at Static Interlaminar Fracture Toughness Test] // Novosti materialovedeniya. Nauka i tehnika: elektron. nauch.-tehnich. zhurn. 2016. №1 (19). St. 09. Available at: http://www.materialsnews.ru (accessed: April 15, 2017).

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    18. Gulyaev A.I., Yakovlev N.O., Krylov V.D., Shurtakov S.V. Mikromehanika razrusheniya stekloplastikov pri rassloenii po modam I i II [Microfracture mechanics of fibreglasses at stratification on modes of I and II] // Materialovedenie. 2016. №2. S. 13–22.

    19. Gulyaev A.I., Yakovlev N.O., Shurtakov S.V., Krylov V.D. Fraktograficheskij analiz epoksidnogo i bismaleimidnogo ugleplastikov posle ispytanij na mezhsloevuyu treshhinostojkost [Interlaminar fracture toughness and fractography of epoxy and bismaleimide carbon composites] // Novosti materialovedeniya. Nauka i tehnika: elektron. nauch.-tehnich. zhurn. 2017. №2 (26). St. 07. Available at: http://www.materialsnews.ru (accessed: May 10, 2017).

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DOI: 10.18577/2071-9140-2017-0-3-74-80

UDC: 678.8

Pages:: 74-80

M.I. Daskovskiy1, M.S. Doriomedov1, D.V. Sevastyanov1, S.Yu. Skripachyov1

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

Polymer biocomposites - prospects of application (review)

Biocomposite materials are modern industrial products, where reinforcing filler made from renewable agricultural and forestry feedstocks, which can include wood, grasses, and crops, as well as wastes and residues. The results of various natural reinforcing filler influence on physical and mechanical properties of biocomposites. According to analysis of science and research publications, the status of current biocomposite materials technologies and their use is presented in different branches of industry. Considerable growth has been seen in the use of biocomposites in the domestic sector, building materials, and automotive applications over the past decade. This article focuses specifically on the adoption of biocomposite materials in the manufacture of automotive components.

Keywords: polymer biocomposites, biodegradable matrixes, natural fibers.

Reference List

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    2. Doriomedov M.S., Daskovskij M.I., Skripachev S.Yu., Shein E.A. Polimernye kompozicionnye materialy v zheleznodorozhnom transporte Rossii (obzor) [Polymer composite materials in the Russian railways (review)] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №7. St. 12. Available at: http://www.viam-works.ru (September 25, 2016). DOI: 10.18577/2307-6046-2016-0-7-12-12.

    3. Doriomedov M.S., Petrov A.V., Daskovskiy M.I., Skripachev S.Yu. Pererabotka  armiruyushchikh napolniteley pri utilizatsii izdeliy iz PKM [Processing of reinforcing fillers at utilization of products from PCM] // Trudy VIAM: elektron. nauch.-tekhnich. zhurn. 2016. №8. St. 12. Available at: http://www.viam-works.ru (accessed: September 27, 2016). DOI: 10.18577/2307-6046-2016-0-8-12-12.

    4. Kablov E.N. Kompozity: segodnya i zavtra [Composites: today and tomorrow] // Metally Evrazii. 2015. №1. S. 36–39.

    5. Pandey J.K., Nagarajan V., Mohanty A.K., Misra M. Commercial potential and competitiveness of natural fiber composites // Biocomposites: Design and Mechanical Performance. Elsevier, 2015. Р. 1–15.

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    19. 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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DOI: 10.18577/2071-9140-2017-0-3-81-86

UDC: 629.7:666.001.5(091)

Pages:: 81-86

E.G. Sentyurin1, I.V. Mekalina1, M.K. Aizatulina1, Yu.A. Isaenkova1

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

The history of aircraft materials of glass and polymer materials with special properties (To the 75th anniversary Laboratory of polymer materials with special properties)

The results of work have been described since the establishment of the «Laboratory of aircraft glazing» in May 1942 up to the present time. These results include the following information: from the beginning of production and application of transparent armor; development of structural heat-resistant organic glasses of the linear structure up to modern partially cross-linked organic glasses mastered by industry, future heat-resistant glasses, weather-resistant polycarbonate and laminated glazing materials. The results of work on production and application of nontransparent thermoplastics as follows: molding, thermoplastic elastomers, glass, coal and organic plastics, vibration-absorbing materials, foamed polyimides, fluorine plastics in the aerospace industry have been described since 1964 to our days.

Keywords: armor, poly methyl methacrylate, orientation, annealing, thermal stability, thermoplastics.

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. 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. Shestoj tehnologicheskij uklad [Sixth technological way] // Nauka i zhizn. 2010. №4. S. 2–7. 

    4. Kablov E.N. Aviacionnoe materialovedenie v XXI veke. Perspektivy i zadachi [Aviation materials science in the XXI century. Perspectives and tasks] // Aviacionnye materialy. Izbrannye trudy VIAM 1932–2002. M.: MISIS–VIAM. 2002. S. 23–47.

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

    6. Kablov E.N. Rol himii v sozdanii materialov novogo pokoleniya dlya slozhnyh tehnicheskih system [Chemistry role in creation of materials of new generation for complex technical systems] // HH Mendeleevskij sezd po obshhej i prikladnoj himii: dokl. v 5 t. UrO RAN. 2016. T. 1. S. 25–26.

    7. Sklyarov N.M. Put dlinoyu v 70 let – ot drevesiny do supermaterialov [Way of 70 years – from wood to supermaterials]. M.: MISIS–VIAM, 2002. S. 370–373.

    8. Levadnyj N.D. 80 let dlya VVS: ot I-5 do MiG-31. K 80-letiyu voennogo predstavitelstva na Nizhegorodskom aviastroitel\'nom zavode «Sokol» [To the 80 anniversary of military representation at Nizhny Novgorod aircraft building plant «Sokol»] / Nizhegorodskij aviastroitelnyj zavod «Sokol». Nizhnij Novgorod, 2012. S. 30–49.

    9. Sentyurin E.G., Bogatov V.A., Petrova A.P., Mekalina I.V. Gudimov M.M. 100 let so dnya rozhdeniya vydayushhegosya uchenogo i organizatora nauki [Gudimov M. M. 100 years since the birth of the outstanding scientist and the organizer of science]. M.: VIAM, 2013. 25 s.

    10. Kargin V.A., Slonimskij G.L. Kratkie ocherki po fiziko-himii polimerov [Short sketches in physic chemistry of polymers]. M.: Himiya, 1967. 228 s.

    11. Gudimov M.M., Perov B.V. Organicheskoe steklo [Organic glass]. M.: Himiya, 1981. 216 s.

    12. Mekalina I.V., Sentyurin E.G., Klimova S.F., Bogatov V.A. Novye «serebrostojkie» organicheskie stekla [New «silver resistant» organic glasses] // Aviacionnye materialy i tehnologii. 2012. №4. S. 45–48.

    13. Bogatov V.A., Trigub T.S., Mekalina I.V., Ayzatulina M.K. Otsenka ekspluatatsionnykh kharakteristik novykh teplostoykikh organicheskikh stekol VOS-1 i VOS-2 [Assessment of utilization properties of new heatresistant organic glasses VOS-1 and VOS-2] // Aviacionnye materialy i tehnologii. 2010. №1. S. 21–26.

    14. Petrov A.A., Mekalina I.V., Sentyurin E.G., Bogatov V.A. Issledovanie osobennostej izgotovleniya detalej ostekleniya iz chastichno sshityh organicheskih stekol [Features of manufacture of glazing parts from partially cross-linked organic glasses] // Aviacionnye materialy i tehnologii. 2013. №2. S. 32–34.

    15. Mekalina I.V., Trigub T.S., Bogatov V.A., Sentyurin E.G. Novoe vysokoteplostojkoe orientirovannoe orgsteklo marki VOS-2AO [The new high-heatresistant oriented organic glass of the VOS-2AO brand] // Aviacionnye materialy i tehnologii. 2010. №3. S. 14–19.

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DOI: 10.18577/2071-9140-2017-0-3-87-94

UDC: 929

Pages:: 87-94

A.V. Grinevich1

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

Career of the Professor N.M. Sklyarov

It is told about scientific achievements of the Professor, Doctor of Sciences (Tech.) Nikolay M. Sklyarov who was the outstanding scientist in the field of aviation materials science, the creator of the unique armour for the attack aircraft Il-2, the developer of the theory of burning of titanium alloys, the researcher in the field of durability and reliability of materials in extreme conditions.

Keywords: aviation armour, high-strength materials, burning of titanium alloys.

Reference List

    1. Sklyarov N.M. Put dlinojyu v 70 let – ot drevesiny do supermaterialov / pod onshch. red. E.N. Kablova [Way of 70 years – from wood to supermaterials / gen. ed. by E.N. Kablov]. M.: MISIS–VIAM, 2002. S. 24–31.

    2. Sklyarov N.M. Rabotosposobnost aviatsionnykh materiaalov, ee kriterii I otsenka [Operability of aviation materials, its criteria and assessment] // Aviatsionnaya promyshlennost. 1997. №5–6. S. 31–38.

    3. Borisova E.A., Sklyarov N.M. Aviatsionnye materialy i tehnologii [Aviation materials and technologies]. M.: VIAM, 2000. Vyp.: Gorenie i pozharobezopasnost titanovykh splavov. 86 s.

    4. Sklyarov N.M. Put dlinojyu v 70 let – ot drevesiny do supermaterialov / pod onshch. red. E.N. Kablova. [Way of 70 years – from wood to supermaterials / gen. ed. by E.N. Kablov]. M.: MISIS–VIAM, 2002. S. С. 260–276.

    5. Sklyarov N.M. Upravlenie kachestvom aviatsionnykh materialov [Quality management of aviation materials] // Aviatsionnye materialy na rubezhe XX–XXI vekov. M.: VIAM, 1994. S. 572–576.

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