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Aviation materials and technologies №1, 2016

Contents

  • O.G. Ospennikova

    Tendencies of development of heat-resistant nickel alloys of low density with polycrystalline and single-crystal structures (review)

    3-19
  • D.E. Kablov, V.V. Sidorov, S.A. Budinovskiy, P.G. Min

    The influence of sulfur impurity on heat resistance of single crystals of ZhS36-VI alloy with protective coating

    20-23
  • D.E. Kablov, V.V. Sidorov, Y.A. Puchkov

    Diffusion behavior features of impurities and microalloying additives in nickel and single crystal superalloys

    24-31
  • N.I. Kolobnev

    Heat resistance of wrought aluminum alloys

    32-36
  • A.S. Ermolaev, A.M. Ivanov, S.A. Vasilenko, V.S. Babikov, R.M. Mubarakshin, E.V. Kondrashov

    Laser technologies application for manufacture and repair of parts and assemblies of gas turbine engines

    37-43
  • D.P. Farafonov, M.L. Degovets, R.S. Aleshina

    The metal fibers of heat-resistant alloys alloyed by platinum group metals

    44-52
  • E.I. Oreshko, V.S. Erasov, N.Yu. Podzhivotov, A.N. Lucenko

    Strength calculation of hybrid wing panel on the basis of sheets and profiles from high-strength aluminum lithium alloy and laminated aluminum fiberglass

    53-61
  • N.N. Blinova, A.A. Belyaev

    Comparative acoustic characteristics of porous materials on the basis of metal matrix

    62-65
  • Yu.V. Stolyankov, V.M. Aleksashin, N.V. Antyufeeva, T.M. Shcheglova

    Glass-forming ability evaluation of the nickel-based «metall-metalloid» system

    66-71
  • V.A. Kuznetsova, I.S. Deev, L.V. Semenova

    Influence of modification of epoxy film-forming compositions on their phase microstructure and adgesion to aluminium alloy

    72-78
  • V.D. Krylov, N.O. Yakovlev, Yu.A. Kurganova, O.A. Lashov

    Interlayer fracture toughness of structural polymer composites

    79-85
  • E.F. Volkova

    The analysis and results of the International conference «Magnesium-21. Broad horizons» (review)

    86-94
Содержание номера
1.

DOI: 10.18577/2071-9140-2016-0-1-3-19

UDC: 669.018.44:669.245

Pages:: 3-19

O.G. Ospennikova1

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

Tendencies of development of heat-resistant nickel alloys of low density with polycrystalline and single-crystal structures (review)

There is given an analysis of scientific and technical development in the field of development and application of cast heat-resistant nickel alloys of low density with the special properties, the existing world tendencies. The comparative analysis of domestic and foreign experience of creation of heat-resistant nickel alloys for blades of gas turbine engines and progress trends of developments in the field of materials science shows that application of domestic heat-resistant alloys and technologies of new generation will allow to create the Russian competitive engines, which are superior to engines of foreign production in all technical and economic characteristics. The carried out analysis of systems of alloying of heat-resistant nickel alloys with single-crystal and polycrystalline structures for creation of cast heat-resistant nickel alloys with low density, resulted in the opportunity to select general directions in the field of increasing the level of the main characteristics of heat-resistant cast alloys.

Keywords: metallurgy, single-crystal heat-resistant nickel alloys, directional structure, materials science, crystallization, rare-earth elements

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Полнотекстовая версия
">Full version
2.

DOI: 10.18577/2071-9140-2016-0-1-20-23

UDC: 669.018.44

Pages:: 20-23

D.E. Kablov1, V.V. Sidorov1, S.A. Budinovskiy1, P.G. Min1

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

The influence of sulfur impurity on heat resistance of single crystals of ZhS36-VI alloy with protective coating

The harmful influence of high sulfur content on heat resistance of single crystals of ZhS36-VI alloy on SDP-41+VSDP-16 protective coating resistance to gas corrosion during isothermic heat resistance tests at temperature 1150°C and within 500 hours was shown. The mechanism of harmful sulfur influence on heat resistance of alloy is suggested from which follows that sulfur diffuses from alloy into protective coating on sample surface and destroys it so far as low-melt sulfur compounds with base of coating material (nickel) have the melting temperature less than 1150°C.

Keywords: heat resistance, single crystal, sulfur, coating, superalloy, tests

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    3. Kablov E.N., Sidorov V.V., Kablov D.E., Rigin V.E., Goryunov A.V. Sovremennye tehnologii polucheniya prutkovyh zagotovok iz litejnyh zharoprochnyh splavov novogo pokoleniya [Modern technologies of receiving the bar stock preparations from foundry heat resisting alloys of new generation] // Aviacionnye materialy i tehnologii. 2012. №S. S. 97–105.

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    9. Kablov D.E., Chabina E.B., Sidorov V.V., Min P.G. Issledovanie vliyaniya azota na strukturu i svojstva monokristallov iz litejnogo zharoprochnogo splava ZhS30-VI [Research of influence of nitrogen on structure and properties of monocrystals from foundry ZhS30-VI hot strength alloy] // MiTOM. 2013. №8. S. 3–7. 

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    12. Sidorov V.V., Rigin V.E., Min P.G., Folomejkin Yu.I., Timofeeva O.B., Filonova E.V., Isho-dzhanova I.V. Vliyanie primesej na strukturu i svojstva vysokozharoprochnyh litejnyh splavov i razrabotka effektivnyh metodov ustraneniya ih otricatelnogo vliyaniya [Influence of impurity on structure and property of high-heat resisting cast alloys and development of effective methods of elimination of their negative influence] // Novosti materialovedeniya. Nauka i tehnika: elektron. nauch.-tehnich. zhurn. 2014. №2. St. 03. Available at: http://www. materialsnews.ru (accessed: December 23, 2015).

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    14. Min P.G., Sidorov V.V. Rafinirovanie othodov zharoprochnogo nikelevogo splava ZhS32-VI ot primesi kremniya v usloviyah vakuumnoj indukcionnoj plavki [Refining of scraps of Ni-base superalloy ZhS32-VI to eliminate silicon impurity under conditions of vacuum induction melting] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №9. St. 01. Available at: http://www.viam-works.ru (accessed: December 23, 2015). DOI: 10.18577/2307-6046-2014-0-9-1-1.

    15. Kablov D.E., Sidorov V.V., Min P.G., Gerasimov V.V., Bondarenko Yu. A. Vliyanie primesej sery i fosfora na svojstva monokristallov zharoprochnogo splava ZhS36-VI i razrabotka effektivnyh sposobov ego rafinirovaniya [The sulfur and phosphorus influence on properties of single crystals GHS36-VI supperalloy and design of effective methods their refining] // Aviacionnye materialy i tehnologii. 2015. №3 (36). S. 3–9. DOI: 10.18577/2071-9140-2015-0-3-3-9.

    16. Kablov D.E., Sidorov V.V., Min P.G., Puchkov Yu.A. Vliyanie lantana na kachestvo i ekspluatacionnye svojstva monokristallicheskogo zharoprochnogo nikelevogo splava ZhS36-VI [The lanthanum influence on quality and operational properties of single crystal nickel base ZhS36-VI superalloy] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №12. St. 02. Available at: http://www.viam-works.ru (accessed: January 12, 2016). DOI: 10.18577/2307-6046-2015-0-12-2-2.

    17. Kablov D.E., Belyaev M.S., Sidorov V.V., Min P.G. Vliyanie primesej sery i fosfora na malociklovuyu ustalost monokristallov zharoprochnogo splava ZhS36-VI [The influence of sulfur and phosphorus impurities on low cycle fatigue of single crystals of ZhS36-VI alloy] // Aviacionnye materialy i tehnologii. 2015. №4 (37). S. 25–28. DOI: 10.18577/2071-9140-2015-0-4-25-28. 

    18. Kablov D.E., Sidorov V.V., Min P.G., Vadeeev V.E. Vliyanie primesej i lantana na eksplu-atacionnye svojstva splava ZhS36-VI [Influence of impurity and lanthanum on operational properties of alloy ZhS36-VI] // Metallurgiya mashinostroeniya. 2015. №6. S. 19–23. 

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DOI: 10.18577/2071-9140-2016-0-1-24-31

UDC: 669.018.44

Pages:: 24-31

D.E. Kablov1, V.V. Sidorov1, Y.A. Puchkov2

[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

Diffusion behavior features of impurities and microalloying additives in nickel and single crystal superalloys

Data about diffusionmobility, solubilities and distribution coefficients of impurities and microalloying elements in nickel are generalized and analysed to reveal the legitimacy of their influence on technological and operational characteristics of single crystal nickel-base superalloys and to develop the requirements to their chemical composition and the sequence of microalloying.

Keywords: single crystal nickel-base superalloy, impurities, refining additions, alloying elements, diffusion coefficient, solubility, distribution coefficient

Reference List

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    12. Kablov D.E., Belyaev M.S., Sidorov V.V., Min P.G. Vliyanie primesej sery i fosfora na malociklovuyu ustalost monokristallov zharoprochnogo splava ZhS36-VI [The influence of sulfur and phosphorus impurities on low cycle fatigue of single crystals of ZhS36-VI alloy] // Aviacionnye materialy i tehnologii. 2015. №4 (37). S. 25–28. DOI: 10.18577/2071-9140-2015-0-4-25-28.

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DOI: 10.18577/2071-9140-2016-0-1-32-36

UDC: 669.018.44:669.715:669.018.26

Pages:: 32-36

N.I. Kolobnev1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute», admin@viam.ru

Heat resistance of wrought aluminum alloys

The paper is presenting a review of certain matters relating to the theory of heat resistant aluminum alloys as well as the major factors affecting the heat resistance including physical, chemical and structural properties of the alloys. Results of investigations of chemical and phase composition, grain structure and mechanical properties of alloys most widely used for operation at elevated temperatures are given; an influence of heat treatment conditions on heat resistance is described as well. A comparative estimation of ultimate values of rupture strength and creep characteristics is given for Al-Cu-Mg (D19, АK4-1, VD17, В-1213), Al-Cu-Mn (D20, 1201) and Al-Cu-Li (1230, V-1461) alloys additionally alloyed with transition metals and rare-earth elements. In the temperature range 150-200°C at 100-1000 hours exposure the alloys can be arranged in the following order based on increasing levels of heat resistance: D19, АK4-1, VD17, D20, V-1213. The Al-Li alloy В-1461 has the advantage of heat resistance up to a temperature of 175°C at 100-1000 hours exposure due to higher strength properties at room temperature.

Keywords: heat resistance, wrought aluminum alloys, creep, diffusion, grain structure, crystal lattice

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    19. Fridlyander I.N., Grushko O.E., Antipov V.V., Kolobnev N.I., Hohlatova L.B. Alyuminijlitievye splavy [Aluminum lithium alloys] / V kn. 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: yubilejnyj nauch.-tehnich. sb. M.: VIAM. 2007. S. 163–171.

    20. Antipov V.V., Kolobnev N.I., Hohlatova L.B. Razvitie alyuminijlitievyh splavov i mnogostupenchatyh rezhimov termicheskoj obrabotki [Development aluminum lithium alloys and multistage modes of thermal processing] // Aviacionnye materialy i tehnologii. 2012. №S. S. 183–195.

    21. Hohlatova L.B., Kolobnev N.I., Antipov V.V., Karimova S.A., Rudakov A.G., Oglodkov M.S. Vliyanie korrozionnoj sredy na skorost rosta treshhiny ustalosti v alyuminievyh splavah [Influence of the corrosion environment on the growth rate of crack of fatigue in aluminum alloys] // Aviacionnye materialy i tehnologija. 2011. №1. S. 16–20.

    22. Loshhinin Yu.V., Pahomkin S.I., Fokin A.S. Vliyanie skorosti nagrevanii pri issledovanii fazovyh prevrashhenij v alyuminievyh splavah metodom DSK [Speed influence heating at research of phase transformations in aluminum alloys DSC method] // Aviacionnye materialy i tehnologii. 2011. №2. S. 3–6.

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DOI: 10.18577/2071-9140-2016-0-1-37-43

UDC: 669-1

Pages:: 37-43

A.S. Ermolaev1, A.M. Ivanov1, S.A. Vasilenko1, V.S. Babikov1, R.M. Mubarakshin2, E.V. Kondrashov1

[1] AVIADVIGATEL OPEN JOINT STOCK COMPANY
[2] Ural Engineering Consulting Ltd. Center for Advanced Technologies

Laser technologies application for manufacture and repair of parts and assemblies of gas turbine engines

Keywords: laser adaptive cladding, repair, blisk, blade, high pressure compressor, laser welding, punching of an aperture, technology

Reference List

    1. Mubarakshin R.M., Bencinger M. Gibkij lazernyj modul [Flexible laser module] // Svarochnoe proizvodstvo. 1996. №3. S. 25–29.

    2. Kelbassa I., Gasser A., Vissenbah K. Lazernoe napylenie kak metod remonta diskovyh lopatok iz titanovyh i nikelevyh splavov, ispolyzuemyh v aviacionnyh dvigatelyah [Laser dusting as method of repair of disk blades from the titanium and nickel alloys used in aircraft engines] / V sb. Trudov I Tihookeanskoj Mezhdunar. konf. po primeneniyu lazerov i optiki. 2004.

    3. Shmotin Yu.N., Starkov R.Yu., Danilov D.V., Ospennikova O.G., Lomberg B.S. Novye materialy dlya perspektivnogo dvigatelya OAO «NPO „Saturn”» [New materials for the perspective engine of JSC «NPO „Saturn”»] // Aviacionnye materialy i tehnologii. 2012. №2. S. 6–8.

    4. 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.

    5. Grigoryants A.G., Shiganov I.N., Misyurov A.I. Tehnologicheskie processy lazernoj obrabotki [Technological processes of laser processing]. M.: Izd-vo MGTU im. N.E. Baumana, 2008. 664 s.

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DOI: 10.185.77/2071-9140-2016-0-1-44-52

UDC: 621.775.8

Pages:: 44-52

D.P. Farafonov1, M.L. Degovets2, R.S. Aleshina2

[1] ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS, admin@viam.ru
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

The metal fibers of heat-resistant alloys alloyed by platinum group metals

The properties of porous materials from metal fibers allow their applying as effective abradable seals and elements of sound-proof structures of aviation GTE. However, high-temperature corrosion and oxidation resistance of these materials has to be improved to apply them in modern and advanced GTE. The metal fibers from heat-resistant alloys alloyed by platinum group metals which can have high oxidation resistance and plasticity are researched and developed at VIAM. First results of researches of such fibers obtained from heat-resistant alloys alloyed by platinum group metals by method of hanging liquid-alloy droplet extraction are given in the article.

Keywords: metal fibers, porous and fibrous metal material, high-temperature oxidation resistance, gas-turbine engine

Reference List

    1. Migunov V.P., Lomberg B.S. Poristovoloknistye metallicheskie materialy dlya zvukopogloshhayushhih i uplotnitelnyh konstrukcij [Porous and fibrous metal materials for sound-proof and sealing designs] / V kn.: 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: yubilejnyj nauch.-tehnich. sb. M. : VIAM, 2007. S. 270–275.

    2. Sun F.G., Chen H.L., Wu J.H., Feng K. Sound absorbing characteristics of fibrous metal materials at high temperatures // Appl. Acoust. 2010. V. 711. P. 221–235.

    3. Serov M.M., Borisov B.V. Poluchenie metallicheskih volokon i poristyh materialov iz nih metodom jekstrakcii visjashhej kapli rasplava [Receiving metal fibers and porous materials from them method of extraction of hanging drop rasplava] // Tehnologija legkih splavov. 2007. №3. S. 62–65.

    4. Migunov V.P., Farafonov D.P. Issledovanie osnovnyh ekspluatacionnyh svojstv novogo klassa uplotnitelnyh materialov dlya protochnogo trakta GTD [Research of the main operational properties of new class of sealing materials for flowing path of GTE] // Aviacionnye materialy i tehnologii. 2011. №3. S. 15–20.

    5. Migunov V.P., Farafonov D.P., Degovets M.L., Stupina T.I. Uplotnitelnye materialy dlya protochnogo trakta GTD [Sealing materials for flowing path of GTE] // Aviacionnye materialy i tehnologii. 2012. №S. S. 94–97.

    6. Migunov V.P., Farafonov D.P., Degovec M.L. Istiraemyj uplotnitelnyj material na osnove volokon iz mednyh splavov [Abradable sealing material made of fibers from copper alloys] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №9. St. 04. Available at: http://viam-works.ru (accessed: February 12, 2015). DOI: 10.18577/2307-6046-2014-0-9-4-4.

    7. Farafonov D.P., Degovets M.L., Serov M.M. Issledovanie svojstv i tehnologicheskih parametrov polucheniya metallicheskih volokon dlya istiraemyh uplotnitelnyh materialov aviacionnyh GTD [The investigation of the properties and technological parameters producing metallic fibers for abradable sealing materials of aircraft GTE] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №7. St. 02 Available at: http://viam-works.ru (accessed: February 12, 2015). DOI: 10.18577/2307-6046-2014-0-7-2-2.

    8. 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.

    9. Fei W., Kuiry S.C., Seal S. Inhibition of Metastable Alumina Formation on Fe–Cr–Al–Y Alloy Fibers at High Temperature Using Titania Coating // Oxidation of Metals. 2004. V. 62. №1–2. P. 29–44.

    10. Solntsev S.S., Rozenenkova V.A., Mironova N.A., Gavrilov S.V. SiC–Si3N4–SiO2 high temperature coatings for metal fibers sealing materials // Glass and ceramics. 2011. V. 68. №5–6. P. 194–196.

    11. Kablov E.N., Solntsev S.S., Rozenenkova V.A., Mironova N.A. Sovremennye polifunkcionalnye vysokotemperaturnye pokrytiya dlya nikelevyh splavov, uplotnitelnyh metallicheskih voloknistyh materialov i berillievyh splavov [Modern multifunctional high temperature coatings for nickel alloys, sealing metal fibrous materials and beryllium alloys] // Novosti materialovedeniya. Nauka i tehnika: elektron. nauch.-tehnich. zhurn. 2013. №1. St. 05. Available at: http://materialsnews.ru (accessed: February 12, 2015).

    12. Solntsev S.S., Rozenenkova V.A., Mironova N.A., Gavrilov S.V. Vysokotemperaturnye tonkoplenochnye pokrytiya dlya uplotnitelnyh materialov iz metallicheskih volokon [High-temperature thin-film coverings for sealing materials from metal fibers] // Aviacionnye materialy i tehnologii. 2012. №1. S. 30–36.

    13. Smarsly W., Zheng N., Buchheim C.S. et al. Advanced High Temperature Turbine Seals Materials and Designs // Material Science Forum. 2005. V. 492–493. P. 21–26.

    14. Simms N.J., Norton J.F., McColvin G. Performance of candidate gas turbine abradeable seal materials in high temperature combustion atmospheres // Materials and Corrosion. 2005. V. 56. P. 765–777.

    15. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Litejnye konstrukcionnye splavy na osnove alyuminida nikelya [Cast structural alloys on the basis of nickel aluminide] // Dvigatel. 2010. №4. S. 24–25.

    16. Kablov E.N., Buntushkin V.P., Povarova K.B., Bazyleva O.A., Morozova G.I., Kazanskaya N.K. Malolegirovannye legkie zharoprochnye vysokotemperaturnye materialy na osnove intermetallida Ni3Al [The low-alloyed easy heat resisting high-temperature materials on the basis of Ni3Al intermetallic compound] // Metally. 1999. №1. S. 58–65.

    17. Buntushkin V.P., Kablov E.N., Bazyleva O.A., Morozova G.I. Splavy na osnove alyuminidov nikelya [Alloys on the basis of nickel aluminides] // MiTOM. 1999. №1. S. 32–34.

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    19. Mahaptara R.N., Varma S.K., Lei C.S. Thermal Stability and Oxidation Resistance of Pt–10Al–4Cr Alloy at Super-High Temperatures // Oxidation of Metals. 2006. V. 66. №3–4. P. 127–135.

    20. Odusote J.K., Cornish L.A., Chown L.H., Erasmus R.M. Isothermal Oxidation Behaviour of a Two-Phase g/gʹ Precipitation-Hardened Quaternary Pt-Based Alloys in Air at 1,35°С // Oxidation of Metals. 2012. V. 78. P. 123–143.

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    24. Ballard D.L., Plichak А.L. The use of Precious-metal-modified Nickel-based Superalloys for Thin Gage Apllications // JOM. 2010. V. 62. P. 45–47.

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DOI: 10.185.77/2071-9140-2016-0-1-53-61

UDC: 669.715:669.018.95

Pages:: 53-61

E.I. Oreshko1, V.S. Erasov1, N.Yu. Podzhivotov1, A.N. Lucenko1

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

Strength calculation of hybrid wing panel on the basis of sheets and profiles from high-strength aluminum lithium alloy and laminated aluminum fiberglass

A necessary step in designing a hybrid wing panel is to develop methods for calculating the strength and determination of the equivalent load for testing. In this regard, the aim of this work was to develop methods for strength calculation of a hybrid wing panel on the basis of sheets and profiles made of high-strength aluminum-lithium alloy and laminated aluminum fiberglass and subsequent strength calculation of the hybrid wing panel fragment by the developed methodology. The calculation of the bearing capacity in compression of the hybrid wing panel sample was also performed using finite element software. The calculation was performed in the linear and nonlinear formulation. The critical load, at which a general loss of stability of the panel occurred, was determined.

Keywords: hybrid material, the panel covered, strength calculation, bearing capacity, finite element method

Reference List

    1. Panin V.E., Kablov E.N., Pochivalov Yu.I., Panin S.V., Kolobnev N.I. Vliyanie nanostrukturirovaniya poverhnostnogo sloya alyuminiy-litievogo splava 1424 na mehanizmy deformacii, tehnologicheskie harakteristiki i ustalostnuyu dolgovechnost. Povyshenie plastichnosti i tehnologicheskih harakteristik [Influence of nanostructuring surface layer aluminum-lithium alloy 1424 on deformation mechanisms, technical characteristics and fatigue life. Increase of plasticity and technical characteristics] // Fizicheskaja mezomehanika. 2012. T. 15. №6. S. 107–111.

    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. 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.

    4. Zotov A.A. Raschet samoleta na prochnost. Vneshnie nagruzki. Konstrukcionno-silovye shemy. Konstrukcionnye materialy: ucheb. posobie [Airplane calculation on durability. External loadings. Constructional and power schemes. Constructional materials: studies. grant.]. M.: Vuzovskaya kniga. 2014. S. 52–58.

    5. Kablov E.N., Antipov V.V., Senatorova O.G., Lukina N.F. Novyj klass sloistyh alyumostekloplastikov na osnove alyuminij-litievogo splava 1441 s ponizhennoj plotnostyu [New class layered alyumostekloplastikov on basis aluminum-lithium alloy 1441 with lowered density] // Vestnik MGTU im. N.E. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 174–183.

    6. Efimov V.A., Shvedkova A.K., Korenkova T.G., Kirillov V.N. Issledovanie polimernyh konstrukcionnyh materialov pri vozdejstvii klimaticheskih faktorov i nagruzok v laboratornyh i naturnyh usloviyah [Research of polymeric constructional materials at influence of climatic factors and loadings in laboratory and natural conditions] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №1. St. 05. Available at: http://www.viam-works.ru (accessed: September 14, 2015).

    7. Muhametov R.R., Ahmadieva K.R., Chursova L.V., Kogan D.I. Novye polimernye svyazujushhie dlya perspektivnyh metodov izgotovleniya konstrukcionnyh voloknistyh PKM [New polymeric binding for perspective methods of manufacturing of constructional fibrous PCM] // Aviacionnye materialy i tehnologii. 2011. №2. S. 38–42.

    8. Kablov E.N., Startsev O.V., Krotov A.S., Kirillov V.N. Klimaticheskoe starenie kompozicionnyh materialov aviacionnogo naznacheniya. III. Znachimye faktory stareniya [Climatic aging of composite materials of aviation assignment. III. Significant factors of aging] // Deformaciya i razrushenie materialov. 2011. №1. S. 34–40.

    9. Kablov E.N., Shhetanov B.V., Ivahnenko Yu.A., Balinova Yu.A. Perspektivnye armiruyushhie vysokotemperaturnye volokna dlya metallicheskih i keramicheskih kompozicionnyh materialov [Perspective reinforcing high-temperature fibers for metal and ceramic composite materials] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №2. St. 05. Available at: http://www.viam-works.ru (accessed: September 14, 2015).

    10. Kirillov V.N., Startsev O.V., Efimov V.A. Klimaticheskaya stojkost i povrezhdaemost polimernyh kompozicionnyh materialov, problemy i puti resheniya [Climatic firmness and damageability of polymeric composite materials, problems and solutions] //Aviacionnye materialy i tehnologii. 2012. №S. S. 412–423.

    11. Tarasov Yu.M., Antipov V.V. Novye materialy VIAM – dlya perspektivnoj aviacionnoj tehkniki proizvodstva OAO «OAK» [The VIAM new materials – for perspective aviation engineering of production of JSC «OAK»] // Aviacionnye materialy i tehnologii. 2012. №2. S. 5–6.

    12. Kirillov V.N., Efimov V.A., Shvedkova A.K., Nikolaev E.V. Issledovanie vliyaniya klimaticheskih faktorov i mehanicheskogo nagruzheniya na strukturu i mehanicheskie svojstva PKM [Research of influence of climatic factors and mechanical loading on structure and the PCM mechanical properties] // Aviacionnye materialy i tehnologii. 2011. №4. S. 41–45.

    13. Doneckij K.I., Kogan D.I., Khrulkov A.V. Svojstva polimernyh kompozicionnyh materialov, izgotovlennyh na osnove pletenyh preform [Properties of the polymeric composite materials made on the basis of braided preforms] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №3. St. 05. Available at: http://www.viam-works.ru (accessed: September 14, 2015). DOI: 10.18577/2307-6046-2014-0-3-5-5.

    14. 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.

    15. Oreshko E.I., Erasov V.S., Lucenko A.N. Matematicheskoe modelirovanie deformirovanija konstrukcionnogo ugleplastika pri izgibe [Mathematical modeling of deformation constructional plastic coal at bend] // Aviacionnye materialy i tehnologii. 2016 (v pechati).

    16. Oreshko E.I., Erasov V.S., Lucenko A.N., Terentev V.F., Slizov A.K. Postroenie diagramm deformirovanija v trehmernom prostranstve σ–ε–t [Creation of charts of deformation in three-dimensional space of σ–ε–t] // Aviacionnye materialy i tehnologii. 2016 (v pechati).

    17. Oreshko E.I., Erasov V.S., Lucenko A.N. Osobennosti raschetov ustojchivosti sterzhnej i plastin [Features of calculations of stability of rods and plates] // Aviacionnye materialy i tehnologii. 2016 (v pechati).

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

    19. Dimitrienko Ju.I., Lucenko A.N., Gubareva E.A., Oreshko E.I., Bazyleva O.A., Sborshhikov S.V. Raschet mehanicheskih harakteristik zharoprochnyh intermetallidnyh splavov na osnove nikelja metodom mnogomasshtabnogo modelirovanija struktury [Calculation of mechanical characteristics of heat resisting intermetallidny alloys on the basis of nickel method of multilarge-scale modeling of structure ] //Aviacionnye materialy i tehnologii. 2016 (v pechati).

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8.

DOI: 10.18577/2071-9140-2016-0-1-62-65

UDC: 669.018.95

Pages:: 62-65

N.N. Blinova1, A.A. Belyaev1

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

Comparative acoustic characteristics of porous materials on the basis of metal matrix

The article is devoted to the questions of analysis and study of acoustic characteristics (e.g. sound absorption factor) of rather rarely used for the acoustic purposes metal materials. Two kinds of porous metals - a foamy-metal and a porous-fibers-metal material with identical porosity and thickness are taken for the study. Some possibilities of application of the materials are considered. Basic operation principles of the device for acoustic characteristics evaluation of the materials are described. The possibility to increase the material specific rigidity, thermal stability and fire safety of different structures on the basis of porous metals is investigated.

Keywords: sound absorption, foamy-metal, porous-fibrous metal material, specific rigidity, thermal stability

Reference List

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    7. Farafonov D.P., Migunov V.P. Izgotovlenie poristovoloknistogo materiala sverhnizkoj plotnosti dlya zvukopogloshhajushhih konstrukcij aviacionnyh dvigatelej [Manufacturing of porous fibrous material of ultralow density for sound-proof designs of aircraft engines] // Aviacionnye materialy i tehnologii. 2013. №4. S. 26–30.

    8. Migunov V.P., Lomberg B.S. Poristovoloknistye metallicheskie materialy dlya zvukopogloshhayushhih i uplotnitelnyh konstrukcij [Porous fibrous metal materials for sound-proof and sealing designs] / V sb.: 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: Yubilejnyj nauch.-tehnich. sb. M.: VIAM. 2007. S. 270–275.

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    12. Plity iz metallicheskogo volokna [Plates from metal fiber]: pat. 3469297 SShA; opubl. 16.09.93.

    13. Sposob polucheniya poristovoloknistogo metallicheskogo materiala [Way of receiving poristovoloknisty metal material] : pat. 2311262 Ros. Federaciya; opubl. 27.11.07.

    14. Serov M.M., Borisov B.V. Poluchenie metallicheskih volokon i poristyh materialov iz nih metodom ekstrakcii visyashhej kapli rasplava [Receiving metal fibers and porous materials from them method of extraction of hanging drop rasplava] // Tehnologiya legkih splavov. 2007. №3. S. 62–65.

    15. Borisov B.V., Serov M.M. Formirovanie poristyh voloknovyh materialov metodom ekstrakcii visyashhej kapli rasplava [Forming of porous voloknovy materials by method of extraction of hanging drop rasplava] // Izvestiya vuzov. Poroshkovaya metallurgiya i funkcionalnye pokrytiya. 2013. №1. S. 55–58.

    16. Migunov V.P., Farafonov D.P., Degovets M.L. Poristovoloknistyj material sverhnizkoj plotnosti na osnove metallicheskih volokon [Porous fibrous material of ultralow density on the basis of metal fibers] // Aviacionnye materialy i tehnologii. 2012. №4. S. 38–41.

    17. Migunov V.P., Farafonov D.P. Issledovanie osnovnyh ekspluatacionnyh svojstv novogo klassa uplotnitelnyh materialov dlya protochnogo trakta GTD [Research of the main operational properties of new class of sealing materials for flowing path of GTE] // Aviacionnye materialy i tehnologii. 2011. №3. S. 15–20.

    18. Grishina O.I., Kochetov V.N., Shavnev A.A., Serpova V.M. Aspekty primenenija vysokoprochnyh i vysokomodul\'nyh voloknistyh metallicheskih kompozicionnyh materialov aviacionnogo naznachenija (obzor) // Trudy VIAM: elektron. nauch-tehnih. zhurn. 2014. №10. St. 05. Available at: http://www.viam-works.ru (accessed: November 20, 2014).

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DOI: 10.185.77/2071-9140-2016-0-1-66-71

UDC: 669.055

Pages:: 66-71

Yu.V. Stolyankov1, V.M. Aleksashin1, N.V. Antyufeeva1, T.M. Shcheglova1

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

Glass-forming ability evaluation of the nickel-based «metall-metalloid» system

«Metal-metalloid» amorphous metal system is one of the representatives of the amorphous metal materials class. Flat stream melt spinning method on the fast rotating surface of the iron chill provides rather high melt cooling rate and represents a quite efficient technique of amorphous metal materials production. The key point here is the evaluation method of the system glass ability providing a proper level of the rapid-quenched materials characteristics. The system glass ability characterizes not only the possibility of production of the alloy in amorphous state itself, but it determines the production method output and the quality of the quenched materials.

Keywords: amorphous metal material, amorphization, system glass forming ability, amorphism factor, surface flaw

Reference List

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    7. Stolyankov Yu.V., Aleksashin V.M., Antyufeeva N.V. K voprosu ob ocenke sklonnosti metallicheskih sistem k stekloobrazovaniyu [On the question of glass-forming ability tendency evaluation (review)] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №7. St. 08 Available at: http://www.viam-works.ru (accessed: July 22, 2015). DOI: 10.18577/2307-6046-2015-7-8-8.

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    13. Lukin V.I., Stoljankov Yu.V., Rylnikov V.S., Shherbakov A.I. Pajka amorfnymi pripoyami [Soldering amorphous solders] // Aviacionnye materialy i tehnologii. 2002. №4. S. 96–102.

    14. Kablov E.N., Evgenov A.G., Rylnikov V.S., Afanasev-Hodykin A.N. Issledovanie melkodispersnyh poroshkov pripoev dlja diffuzionnoj vakuumnoj pajki, poluchennyh metodom atomizacii rasplava [Research of finely divided powders of solders for the diffusion vacuum soldering, received by atomizatsiya method melt] // Vestnik MGTU im. N.E. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 79–87.

    15. Rylnikov V.S., Lukin V.I. Pripoi, primenyaemye dlya pajki materialov aviacionnogo naznacheniya [Solders used for soldering materials aviation applications] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №8. St. 02. Available at: http://viam-works.ru (accessed: April 15, 2015).

    16. Afanasev-Hodykin A.N., Lukin V.I., Rylnikov V.S. Vysokotehnologichnye polufabrikaty zharoprochnyh pripoev (lenty i pasty na organicheskom svyazuyushhem) [High-tech semi-finished high-temperature solders (tape and paste on an organic binder] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №9. St. 02. Available at: http://viam-works.ru (accessed: April 15, 2015).

    17. Stolyankov Yu.V., Antyufeeva N.V., Raskutin A.E., Karimova S.A. Issledovanie vozmozhnosti sozdaniya sloistyh metallopolimernyh kompozicionnyh materialov s ispolzovaniem tonkolistovyh amorfnyh splavov [Research of possibility of creation of layered metalpolymeric composite materials with use is thin sheet amorphous alloys] // Kompozity i nanostruktury. 2014. T. 6. №1. S. 25–31. 

    18. Stolyankov Yu.V., Gulyaev I.N., Aleksashin V.M., Antyufeeva N.V. Amorfnye metallicheskie materialy v sostave pezoelektricheskih sloistyh elementov-aktyuatorov [Amorphous metal materials in piezoelectric laminated actuators components] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №4. St. 03. Available at: http://viam-works.ru (accessed: April 15, 2015). DOI: 10.18577/2307-6046-2015-4-3-3.

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DOI: 10.18577/2071-9140-2016-0-1-72-78

UDC: 667.621:669.715

Pages:: 72-78

V.A. Kuznetsova1, I.S. Deev1, L.V. Semenova1

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

Influence of modification of epoxy film-forming compositions on their phase microstructure and adgesion to aluminium alloy

Influence of the modifier of epoxy priming coatings, cured by aminoalkoksisilany on their phase strucrure and adhesive strength at normal separation is investigated. It is established that adhesive strength at separation depends on the content of the modifier - acrylic copolymer - in polymeric binding. In order to determine the dependence of adhesive strength of coatings at separation on their phase structure influence of the content of the modifier (acrylic copolymer) in epoxy binding on phase structure of priming coatings, cured by aminoalkoksisilany AGM-9 has been investigated. For that the special attention was given to a change of the phase structure of studied priming coatings depending on curing duration under natural conditions.

Keywords: priming coatings, phase structure, adgesive strength at separation, curing duration

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    28. Deev I.S., Kablov E.N., Kobec L.P., Chursova L.V. Issledovanie metodom skaniruyushhej elektronnoj mikroskopii deformacii mikrofazovoj struktury polimernyh matric pri mehanicheskom nagruzhenii [Research of the scanning electron microscopy method deformation of microphase structure of polymeric matrix at mechanical loading] // Trudy VIAM: elektron. nauch-tehnich. zhurn. 2014. №7. St. 06. Available at: http://www.viam-works.ru (accessed: September 05, 2015). DOI: 10.18577/2307-6046-2014-0-7-6-6.

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DOI: 10.18577/2071-9140-2016-0-1-79-85

UDC: 678.8:620.1

Pages:: 79-85

V.D. Krylov1, N.O. Yakovlev1, Yu.A. Kurganova2, O.A. Lashov1

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

Interlayer fracture toughness of structural polymer composites

Methods for determining the static interlayer fracture toughness of laminated polymer composite materials (PCM) under loading in tearing-off condition, lateral shear and combined loading have been considered. The rates of interlayer fracture toughness GIс and GIIс for structural PCM based on carbon fibre HTS45, T800 and fabrics of Porsher (art. 4510, 3692, 14535, 7781) and epoxy matrix VSE-1212 with high fracture toughness and triazine (isocyanurate) matrix VST-1208 have been determined.

Keywords: layered polymer composite, crack resistance, interlayer fracture toughness, tearing-off, lateral shear, mode I, mode II

Reference List

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    2. Erasov V.S., Yakovlev N.O., Nuzhnyj G.A. Kvalifikatsionnye ispytaniya i issledovaniya prochnosti aviatsionnyh materialov [Qualification tests and researches of durability of aviation materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 440–448.

    3. Kablov E.N., Sivakov D.V., Gulyaev I.N., Sorokin K.V., Fedotov M.Yu., Goncharov V.A. Metody issledovaniya konstrukcionnyh kompozicionnyh materialov s integrirovannoj elektromehanicheskoj sistemoj [Methods of research of constructional composite materials with the integrated electromechanical system] // Aviacionnye materialy i tehnologii. 2010. №4. S. 17–20.

    4. 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.

    5. Dimitrienko Yu.I., Fedonyuk N.N., Gubareva E.A., Sborshhikov S.V., Prozarovskij A.A., Erasov V.S., Yakovlev N.O. Modelirovanie i razrabotka trehslojnyh kompozicicionnyh materialov s sotovym zapolnitelem [Modeling and development of three-layered kompozitsitsionny materials with cellular filler] // Vestnik MGTU im. N.E. Baumana. Ser. «Estestvennye nauki». 2014. №5 (56). S. 66–81.

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    7. 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.

    8. 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.

    9. Yakovlev N.O., Erasov V.S., Krylov V.D., Popov Yu.A. Metody opredeleniya sdvigovyh harakteristik polimernyh kompozicionnyh materialov [Methods of definition of shift characteristics of polymeric composite materials] // Aviacionnaya promyshlennost. 2014. №1. S. 20–23.

    10. Yakovlev N.O., Erasov V.S., Kolokoltseva T.V. Osobennosti opredeleniya harakteristik sdviga v ploskosti lista polimernyh kompozicionnyh materialov v razlichnyh standartah [Features of definition of characteristics of shift in the plane of leaf of polymeric composite materials in different standards] // Vse materialy. Entsiklopedicheskij spravochnik. 2014. №5. S. 12–16.

    11. Erasov V.S., Krylov V.D., Panin S.V., Goncharov A.A. Ispytaniya polimernogo kompozitsionnogo materiala na udar padayushhim gruzom [Drop-weight impact testing of polymer composite material] // Aviacionnye materialy i tehnologii. 2013. №3. S. 60–64.

    12. Finogenov G.N., Erasov V.S. Treshhinostojkost polimernyh kompozitov pri mezhslojnyh otryve i sdvige [Crack firmness of polymeric composites at interlaminar separation and shift] /V sb. Aviacionnye materialy i tehnologii. M.: VIAM. 2003. №3. S. 62–67.

    13. Yakovlev N.O., Lutsenko A.N., Artemeva I.V. Metody opredeleniya mezhsloevoj treshhinostojkosti sloistyh materialov [Methods of definition of mezhsloyevy treshchinostoykost of layered materials] // Vse materialy. Jenciklopedicheskij spravochnik: Prilozhenie «Kommentarii k standartam, TU, sertifikatam». 2015. №10. S. 7–14.

    14. Yakovlev N.O., Erasov V.S., Petrova A.P. Sravnenie normativnyh baz razlichnyh stran po ispytaniju kleevyh soedinenij materialov [Comparison of regulatory bases of the different countries on testing of glued joints of materials] // Vse materialy. Entsiklopedicheskij spravochnik. 2014. №7. S. 2–8.

    15. Erasov V.S., Yakovlev N.O., Avtaev V.V. Sovremennoe sostoyanie laboratorii imeni professora S.I. Kishkinoj [Contemporary state of laboratory after the named of professor S.I. Kishkina] //Aviacionnye materialy i tehnologii. 2014. №S4. S. 136–139.

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DOI: 10.18577/2071-9140-2016-0-1-86-94

UDC: 669.721.5

Pages:: 86-94

E.F. Volkova1

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

The analysis and results of the International conference «Magnesium-21. Broad horizons» (review)

The article represents the survey of the most interesting papers presented on the III International conference and exhibition «Magnesium-21. Broad horizons». An analysis of the results of researches of phase composition, physical and mechanical properties of new magnesium alloys that were worked out by foreign and domestic reseachers are hereby represented. It is shown that there is a strong trend towards widening use of rare earth elements as the alloying components of new magnesium alloys to improve their properties.

Keywords: magnesium-based alloys, phase composition, mechanical properties, surface treatments for the improvement of the corrosion resistance, rare-earth elements

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