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Aviation materials and technologies №2, 2016

Contents

  • A.A. Smirnov, S.A. Budinovsky

    Improvement of heat resistance of condensation and diffusion coatings for turbine blades from ZHS32 alloy

    3-10
  • D.S. Gorlov, S.A. Muboyadzhyan, A.A. Shchepilov, D.A. Aleksandrov

    The research of erosion resistance and heat resistance of the ion-plasma damping coatings

    11-17
  • A.N. Zhabin, V.M. Serpova, O.I. Grishina, A.A. Shavnev

    Research of phase composition formation of the matrix forming aluminide alloy for high temperature metallic composite materials

    18-21
  • O.I. Grishina, A.A. Shavnev, A.N. Nyafkin

    Types of binders for casting silicon carbide powders (review)

    22-29
  • A.V. Solomentseva, V.M. Fadeeva, G.F. Zhelezina

    Antifriction organoplastics for heavy loaded sliding friction units of aircraft structures

    30-34
  • P.N. Timoshkov

    Equipment and materials for the technology of automated calculations prepregs

    35-39
  • N.I. Shvets, O.B. Zastrogina, V.T. Minakov, I.A. Matveeva

    Influence of tin carboxylates on the process of organosilicic oligomer binder curing and properties of the three-dimensional reinforced material on its base

    40-44
  • E.M. Shuldeshov, V.V. Lepeshkin, M.M. Platonov, A.M. Romanov

    Method of definition of acoustic characteristics of sound-proof materials in the range of frequencies expanded to 15 kHz

    45-49
  • E.I. Oreshko, V.S. Erasov, A.N. Lutsenko

    Mathematical modeling of deformation constructional carbon fiber at a bend

    50-59
  • V.S. Erasov, A.V. Lavrov, A.N. Lucenko, A.V. Grinevich

    About the question of the interaction of hardened core with ceramic barrier

    69-75
  • S.S. Vinogradov, S.A. Dyomin, S.V. Balakhonov, O.G. Kirillova

    Inorganic composite coatings - a perspective direction in the field of anticorrosive protectoin of carbon steels

    76-87
  • M.G. Kurs

    Atmospheric corrosion resistance of advanced Al-Li alloys by nature full-scale accelerated tests in the conditions of temperate warm climate

    88-94
Содержание номера
1.

DOI: 10.18577/2071-9140-2016-0-2-3-10

UDC: 629.7.023.224

Pages:: 3-10

A.A. Smirnov1, S.A. Budinovsky2

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

Improvement of heat resistance of condensation and diffusion coatings for turbine blades from ZHS32 alloy

The influence of composite barrier nitride and carbide layers on heat resistance and modification kinetics of the elemental composition from the ZHS32 superalloy combinations with heat-resistant coatings is studied. The investigations of microstructure of «alloy-coating» compositions in its original form and after the test for heat resistance at temperatures 1150 and 1200°C at 500 and 100 hours bases respectively are conducted. It is found that the use in the structure of the protective heat-resistant coating composition (Ni-Cr-Al-Ta-Re-Y-Hf)+(Al-Ni-Y) nitride barrier significantly increases the heat resistance of the «alloy-coating» composition and does not reduce the mechanical properties of the ZHS32 alloy (long-term strength and cycle fatigue). Work is executed within implementation of the complex scientific direction 17.3. «Multi layer heat resisting and heat-protective coatings, nanostructural strengthening erosive and corrosion resistant, anti wear, antifrettingovy coatings for protection of details of hot path and the GTЕ and GTU compressor» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: heat-resistant coatings, ion-plasma technology, high-temperature nickel alloys, the secondary reaction zone, topologically close-packed phases

Reference List

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    2. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharoprochnye splavy novogo pokoleniya [Nickel foundry heat resisting alloys of new generation] // Aviacionnye materialy i tehnologii. 2012. №S. C. 36–52.

    3. Zharoprochnyj splav na nikelevoj osnove dlya monokristallicheskogo litya: pat. 2439184 Ros. Federaciya [Hot strength alloy on nickel basis for single-crystal molding: pat. 2439184 Russian Federation]; opubl. 05.10.10.

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    5. Zharoprochnyj litejnyj splav na osnove nikelya i izdelie, vypolnennoe iz nego: pat. 2365656 Ros. Federaciya [Heat resisting cast alloy on the basis of nickel and the product which has been executed of it: pat. 2365656 Russian Federation]; opubl. 30.01.08.

    6. Petrushin N.B., Ospennikova O.G., Visik E.M. i dr. Zharoprochnye nikelevye splavy nizkoj plotnosti [Heat resisting nickel alloys of low density] // Litejnoe proizvodstvo. 2012. №6. S. 5–11.

    7. 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.

    8. Matveev P.V., Budinovskij S.A., Muboyadzhyan S.A., Kosmin A.A. Zashhitnye zharostojkie pokrytiya dlya splavov na osnove intermetallidov nikelya [High-temperature coatings for intermetallic nickel-based alloys] //Aviacionnye materialy i tehnologii. 2013. №2. S. 12–15.

    9. Kablov E.N., Muboyadzhyan S.A. Heat-resistant coatings for the high-pressure turbine blades of promising GTES // Russian metallurgy (Metally). 2012. №1. P. 1–7.

    10. Budinovskij S.A., Matveev P.V., Smirnov A.A. Issledovanie zharostojkosti litejnyh zharoprochnyh nikelevyh splavov v oblasti temperatur 1000–1200°C [Research of heat resistance of cast heat resisting nickel alloys in the field of temperatures 1000-1200°C] // Aviacionnaya promyshlennost. 2014. №2. S. 48–52.

    11. 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.

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    15. Muboyadzhyan S.A., Budinovskij S.A., Gayamov A.M., Matveev P.V. Vysokotemperaturnye zharostojkie pokrytiya i zharostojkie sloi dlya teplozashhitnyh pokrytij [High-temperature heat resisting coverings and heat resisting layers for heat-protective coverings] //Aviacionnye materialy i tehnologii. 2013. №1. S. 17–20.

    16. Budinovskij S.A., Muboyadzhyan S.A., Gayamov A.M., Kosmin A.A. Zharostojkie ionno-plazmennye pokrytiya dlya lopatok turbin iz nikelevyh splavov, legirovannyh reniem [Heat resisting ion-plasma coverings for blades of turbines from the nickel alloys alloyed by reniye] // MiTOM. 2008. №6. C. 31–36.

    17. Budinovskij S.A., Muboyadzhyan S.A., Gayamov A.M., Stepanova S.V. Ionno-plazmennye zharostojkie pokrytiya s kompozicionnym bar\'ernym sloem dlya zashhity ot okisleniya splava ZhS36-VI [Ion-plasma heat resisting coverings with composition barrier layer for protection against oxidation of alloy ZhS36-VI] // MiTOM. 2011. №1. C. 34–40.

    18. Gayamov A.M. Zharostojkoe pokrytie s kompozicionnym bar\'ernym sloem dlya zashhity vneshnej poverhnosti rabochih lopatok GTD iz renijsoderzhashhih zharoprochnyh nikelevyh splavov [Heat resisting covering with composition barrier layer for protection of exterior surface of working blades of GTD from reniysoderzhashchy heat resisting nickel alloys] / V sb. materialov XI Rossijskoj ezhegodnoj konf. molodyh nauch. sotrudnikov i aspirantov «Fiziko-himiya i tehnologiya neorganicheskih materialov». M.: IMET RAN, 2012. C. 473–475.

    19. 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: March, 02 2015). DOI: 10.18577/2307-6046-2014-0-1-1-1.

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2.

DOI: 10.18577/2071-9140-2016-0-2-11-17

UDC: 629.7.023.224

Pages:: 11-17

D.S. Gorlov1, S.A. Muboyadzhyan1, A.A. Shchepilov1, D.A. Aleksandrov1

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

The research of erosion resistance and heat resistance of the ion-plasma damping coatings

Тhe damping capacity, erosion resistance and also the heat resistance of the samples of titanium alloy VT6 with ion-plasma coatings was researched. It is shown that to assess the effectiveness of the damping capacity of the ion-plasma coating, it is possible to use the criterion of merit of the oscillating system, as well as the oscillating amplitude the free end of the coated samples. The dependences of the oscillating amplitude of the free end of titanium alloy VT6 of stress in the dangerous section. Erosion resistance of VT6 titanium alloy samples with ion-plasma coatings and without the exposure to abrasive flow with SiO2 particles with a grain size of up to 700 mkm at angles of attack dusty stream 70 (direct impact) and 20 degrees (tangential flow), as well as heat resistance on the basis of 200 hours at a temperature of 400°C is investigated. Work is executed within implementation of the complex scientific direction 17.3. «Multi layer heat resisting and heat-protective coatings, nanostructural strengthening erosive and corrosion resistant, anti wear, antifrettingovy coatings for protection of details of hot path and the GTЕ and GTU compressor» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: vacuum-plasma technology of high-energy, ion-plasma damping coating, quality factor, erosion resistance, heat resistance

Reference List

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    3. Kablov E.N., Muboyadzhyan S.A., Budinovskij S.A., Pomelov Ya.A. Ionno-plazmennye zashhitnye pokrytiya dlya lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] // Konversiya v mashinostroenii. 1999. №2. S. 42–47.

    4. Muravchenko F.M., Sheremetev A.V. Aktualnye problemy dinamiki, prochnosti i nadezhnosti sovremennyh aviadvigatelej [Actual problems of dynamics, durability and reliability of modern aircraft engines] // Vibracii v tehnike i tehnologiyah. 2001. №4 (20). S. 2–5.

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    7. Paton B.E., Movchan B.A. Composite Materials Deposited from the Vapour Phase in Vacuum Soviet Technologies Review // Weld and Surfacing. 1991. V. 2. P. 43–64.

    8. Muboyadzhyan S.A., Aleksandrov D.A., Gorlov D.S., Egorova L.P., Bulavinceva E.E. Zashhitnye i uprochnjayushhie ionno-plazmennye pokrytiya dlya lopatok i drugih otvetstvennyh detalej kompressora GTD [Protective and strengthening ion-plasma coverings for blades and other responsible details of the GTE compressor] //Aviacionnye materialy i tehnologii. 2012. №S. S. 71–81.

    9. Kablov E.N., Muboyadzhyan S.A. Ionnoe travlenie i modificirovanie poverhnosti otvetstvennyh detalej mashin v vakuumno-dugovoj plazme [Ion etching and modifying of surface of responsible details of machines in vacuum and arc plasma] // Vestnik MGTU im. N.E. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 149–163.

    10. Muboyadzhyan S.A., Kablov E.N. Vacuum plasma technique of protective coatings production of complex alloys // Metal Science and Heat Treatment. 1995. №2. Р. 15–18.

    11. Muboyadzhyan S.A., Pomelov Ya.A. Zashhitnye pokrytiya dlya lopatok kompressora GTD [Protecting covers for GTE compressor blades] / V sb.: Aviacionnye materialy i tehnologii. M.: VIAM, 2003. Vyp.: Vysokozharoprochnye materialy dlya sovremennyh gazoturbinnyh dvigatelej i progressivnye tehnologii ih proizvodstva. S. 116–131.

    12. Sposob polucheniya litogo trubnogo katoda iz splavov na osnove alyuminiya dlya ionno-plazmennogo naneseniya pokrytij: pat. 2340426 Ros. Federaciya [Way of receiving the cast pipe cathode from alloys on the basis of aluminum for ion-plasma drawing coverings: pat. 2340426 Russian Federation]; opubl. 16.04.07.

    13. Sposob polucheniya lityh trubnyh izdelij iz splavov na osnove nikelya i/ili kobal\'ta: pat. 2344019 Ros. Federaciya [Way of receiving cast tubular goods from alloys on the basis of nickel and/or cobalt: pat. 2344019 Russian Federation]; opubl. 16.04.07.

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    16. Muboyadzhyan S.A., Aleksandrov D.A., Konnova V.I. Metodika ispytanij na otnositelnuyu jerozionnuyu stojkost\' tverdyh pokrytij otvetstvennyh detalej kompressora GTD [Technique of tests for relative erosion resistance of hard coatings of responsible details of the GTE compressor] // Vse materialy. Jenciklopedicheskij spravochnik. 2014. №4. S. 7–18.

    17. Aleksandrov D.A., Muboyadzhyan S.A., Gorlov D.S., Konnova V.I. Povyshenie jerozionnoj i korrozionnoj stojkosti stal\'nyh lopatok kompressora GTD s pomoshh\'yu nanoslojnogo pokrytiya [Increase of erosion and corrosion resistance of steel compressor blades of GTD by means of nanolayer covering] // Problemy chernoj metallurgii i materialovedeniya. 2013. №4. S. 43–49.

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3.

DOI: 10.18577/2071-9140-2016-0-2-18-21

UDC: 669.715:669.018.95

Pages:: 18-21

A.N. Zhabin1, V.M. Serpova1, O.I. Grishina2, A.A. Shavnev1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[2] Federal state unitary enterprise «All-Russian scientific research institute of aviation materials

Research of phase composition formation of the matrix forming aluminide alloy for high temperature metallic composite materials

Research results of phase composition formation of matrix intermetallic alloy by method of reactionary impregnation are presented. Research works of fractional structure of matrix and neutral particles and calculation of their ratios are conducted. The influence of the content of the buffer particles of Al-O-N on the phase composition and structure of the matrix aluminide alloy is shown. The investigations on definition of phase composition of samples with the different contents of buffer material and reference samples after impregnation and after homogenizing annealing using the method of X-ray diffraction analysis are conducted. The data on the effect of homogenizing annealing on the phase composition of the matrix alloy are represented. Work is executed within implementation of the complex scientific direction 12.1. «The metal composite materials (MCM) reinforced by particles and fibers of high-melting connections» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: a metal composite material, nickel aluminide, nickel intermetallide

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.

    2. Istoriya aviacionnogo materialovedeniya. VIAM – 80 let: gody i lyudi / pod obshh. red. E.N. Kablova [History of aviation materials science. VIAM – 80 years: years and people / edition by E.N. Kablov]. M.: VIAM, 2012. 520 s. 

    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. 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.

    5. Kablov E.N., Lomberg B.S., Ospennikova O.G. Sozdanie sovremennyh zharoprochnyh materialov i tehnologij ih proizvodstva dlya aviacionnogo dvigatelestroeniya [Creation of modern heat resisting materials and technologies of their production for aviation engine building] // Krylya Rodiny. 2012. №3–4. S. 34–38.

    6. Letnikov M.N., Lomberg B.S., Ovsepyan S.V. Issledovanie kompozicij sistemy Ni–Al–Co pri razrabotke novogo zharoprochnogo deformiruemogo intermetallidnogo splava [Investigation experimental alloys based on Ni–Al–Co ternary system for development a new high-temperature intermetallic alloy for disk application] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. № 10. St. 01. Available at: http://www.viam-works.ru (accessed: February 18, 2015). 

    7. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharoprochnye splavy novogo pokoleniya [Nickel foundry heat resisting alloys of new generation] // Aviacionnye materialy i tehnologii. 2012. №S. C. 36–52.

    8. Kablov E.N., Golubovskij E.R. Zharoprochnost\' nikelevyh splavov: ucheb. posobie [Thermal stability of nickel alloys: studies. grant.]. M.: Mashinostroenie, 1998. 464 s.

    9. Bazyleva O.A., Turenko E.Yu., Shestakov A.V. Vliyanie termicheskoj obrabotki na mikrostrukturu i mehanicheskie svojstva splava na osnove intermetallida NiAl [An effect of heat treatment on microstructure and mechanical properties of NiAl-based intermetallic alloy] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №9. St. 02. Available at: http://www.viam-works.ru (accessed: February 18, 2015). DOI: 10.18577/2307-6046-2014.0-9-2-2.

    10. Arginbaeva E.G., Bazyleva O.A., Kolodochkina V.G., Khvatskij K.K. Vliyanie kristallograficheskoj orientacii na strukturu i fiziko-mehanicheskie svojstva intermetallidnogo splava na osnove Ni3Al [The influence of crystallographic oriental on structure, physical and mechanical properties of intermetallic alloys based on Ni3Al] // Aviacionnye materialy i tehnologii. 2013. №2. S. 3–7.

    11. Bazyleva O.A., Bondarenko Yu.A., Timofeeva O.B., Chabina E.B. Intermetallidnye kompozicii na osnove Ni3Al, legirovannye reniem [Интерметаллидные композиции на основе Ni3Al, легированные рением] // Metallurgiya mashinostroeniya. 2011. №4. S. 31–34.

    12. 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.

    13. Povarova K.B., Bannyh O.A. Principy soznaniya konstrukcionnyh splavov na osnove intermetallidov (Ch. I) [Principles of consciousness of structural alloys on the basis of intermetallic compound (Part I)] // Materialovedenie. 1999. №2. S. 27–33.

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DOI: 10.18577/2071-9140-2016-0-2-22-29

UDC: 621.74.043.2

Pages:: 22-29

O.I. Grishina1, A.A. Shavnev2, A.N. Nyafkin2

[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»

Types of binders for casting silicon carbide powders (review)

This paper presents an overview in foreign press on the use of various types of binders for casting silicon carbide powders under pressure to obtain the metal composite materials on the base of aluminum alloy. We observe the influence of various types of binders on the properties of the final products. Basic information on the technology of casting powder mixtures is presented. Work is executed within implementation of the complex scientific direction 12.1. «The metal composite materials (МСМ) reinforced by particles and fibers of high-melting connections» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: molding powders under pressure, a metal composite material, silicon carbide, aluminum, binders, ceramic injection molding

Reference List

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5.

DOI: 10.18577/2071-9140-2016-0-2-30-34

UDC: 678.83

Pages:: 30-34

A.V. Solomentseva1, V.M. Fadeeva1, G.F. Zhelezina1

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

Antifriction organoplastics for heavy loaded sliding friction units of aircraft structures

Research works on the tribological properties of the self-lubricating antifriction material Orgalon AF-1M based on the combined fabrics of polyimide Аramid fibers and Рolyphemus PTFE fibers with phenolic and rubber binder, intended for heavy loaded sliding friction units of aircraft structures are presented. The material is manufactured by machine impregnation of fabric by binder solution. The results of tribological investigations are provided. The graphical dependences of the friction coefficient of the material on the unit load, sliding speed and temperature and also the linear wear of friction units on the work time for bushings and spherical plain bearings are given. Work is executed within implementation of the complex scientific direction 13 «Polymeric composite materials» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: organoplastics, antifriction materials, units of sliding friction, tribological properties, friction factor

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.

    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. Materialy i himicheskie tehnologii dlya aviacionnoj tehniki [Materials and chemical technologies for aviation engineering] // Vestnik Rossijskoj akademii nauk. 2012. T. 82. №6. S. 520–530.

    4. Kablov E.N. Himiya v aviacionnom materialovedenii [Chemistry in aviation materials science] // Rossijskij himicheskij zhurnal. 2010. T. LIV. №1. S. 3–4.

    5. Bejder E.Ya., Donskoj A.A., Zhelezina G.F., Kondrashov E.K., Sentyurin E.G., Surnin E.G., Sytyj Yu.V. Opyt primeneniya ftorpolimernyh materialov v aviacionnoj tehnike [Experience of application of ftorpolimerny materials in aviation engineering] // Rossijskij himicheskij zhurnal. 2008. T. LII. №3. S. 30–44.

    6. Eremin E.N., Negrov D.A. Sovershenstvovanie tehnologii izgotovleniya podshipnikov skolzheniya iz kompozicionnyh materialov na osnove politetraftorjetilena [Improvement of manufacturing techniques of sliding bearings from composite materials on the basis of polytetrafluoroethylene] // Tehnologiya mashinostoroeniya. 2010. №1. S. 30–32.

    7. Negrov D.A., Eremin E.N., Putincev V.Yu. Issledovanie vliyaniya energii ultrazvukovyh kolebanij na strukturu kompozicionnogo materiala [Research of influence of energy of ultrasonic fluctuations on structure of composite material] // Spravochnik. Inzhenernyj zhurnal 2014. №7. S. 3–5.

    8. Negrov D.A., Eremin E.N. Vliyanie parametrov ultrazvukovogo pressovaniya na mehanicheskie i tribotehnicheskie svojstva strukturno-modificirovannogo politetraftorjetilena [Influence of parameters of ultrasonic pressing on mechanical and tribotekhnichesky properties structural the modified polytetrafluoroethylene] // Omskij nauchnyj vestnik. 2009. №2 (80). S. 58–60.

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    10. Gunyaev G.M., Krivonos V.V., Rumyantsev A.F., Zhelezina G.F. Polimernye kompozicionnye materialy v konstrukciyah letatelnyh apparatov [Polymeric composite materials in designs of flight vehicles] // Konversiya v mashinostroenii. 2004. №4 (65). S. 65–69.

    11. Zhelezina G.F. Konstrukcionnye i funkcionalnye organoplastiki novogo pokoleniya [Constructional and functional organoplastics of new generation] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №4. St. 06. Available at: http://www.viam-works.ru (accessed: March 02, 2015). 

    12. Buznik V.M., Yurkov G.Yu. Primenenie ftorpolimernyh materialov v tribologii: sostoyanie i perspektivy [Application of ftorpolimerny materials in tribologiya: condition and perspectives] // Voprosy materialovedeniya. 2012. №4 (72). S. 133–150.

    13. Davydova I.F., Kavun N.S. Teplostojkie antifrikcionnye tekstolity [Heat-resistant anti-friction textolites] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №11. St. 04. Available at: http://www.viam-works.ru (accessed: March 02, 2015). DOI: 10.18577/2307-6046-2014-0-11-4-4.

    14. Deev I.S., Kablov E.N., Kobets 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. (accessed: March 02, 2015). DOI: 10.18577/2307-6046-2014-0-7-6-6.

    15. Timoshkov P.N., Kogan D.I. Sovremennye tehnologii proizvodstva polimernyh kompozicionnyh materialov novogo pokoleniya [Modern production technologies of polymeric composite materials of new generation] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №4. St. 07. Available at: http://www.viam-works.ru (accessed: March 02, 2015).

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6.

DOI: 10.18577/2071-9140-2016-0-2-35-39

UDC: 678.8

Pages:: 35-39

P.N. Timoshkov1

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

Equipment and materials for the technology of automated calculations prepregs

At present time the composite parts of aircraft, produced by the technology of automatic prepreg placement (AFP/ATL) replacing the traditional manual prepreg placement technology are increasingly popular,. The introduction of such technologies allows to fully implement by engineer the entire potential of composite construction. To do this, development of new types of materials having different advantages in comparison with known before, as well as a number of technologies of processing and production equipment. Work is executed within 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: automatic prepreg placement (AFP/ATL), prepreg slitting equipment, slitted prepreg winding

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.

    2. Prepreg i izdelie, vypolnennoe iz nego: pat. 2427594 Ros. Federaciya [Prepreg and the product which has been executed of it: stalemate. 2427594 Rus. Federation]; opubl. 21.12.09.

    3. Sposob polucheniya izdeliya iz kompozicionnogo materiala: pat. 2448808 Ros. Federaciya [Way of receiving product from composite material: stalemate. 2448808 Rus. Federation]; opubl. 05.10.10.

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    14. 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.

    15. McClain M., Goering J. Overview of Recent Developments in 3D Structures / ICCM 17. 3D Textiles & Composites. Edinburgh. 2009.

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    19. Timoshkov P.N., Kogan D.I. Sovremennye tehnologii proizvodstva polimernyh kompozicionnyh materialov novogo pokoleniya [Modern production technologies of polymeric composite materials of new generation] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №4. St. 07. Available at: http://www.viam-works.ru (accessed: August 01, 2015).

    20. Crossley R.J., Schubel P.J., Warrior N.A. The experimental characterisation and investigate on of prepreg tack // Proceedings of ICCM-18. Edinburgh. 2009. P. 1–11.

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7.

DOI: 10.18577/2071-9140-2016-0-2-40-44

UDC: 678.049:678.8

Pages:: 40-44

N.I. Shvets1, O.B. Zastrogina1, V.T. Minakov1, I.A. Matveeva1

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

Influence of tin carboxylates on the process of organosilicic oligomer binder curing and properties of the three-dimensional reinforced material on its base

Method of pressure impregnation is applied for manufacture of parts from composite materials based on 3D-reinforcment and provids low porosity and stability of properties in the volume of products. Binder for such technology should not contain a passive solvent, but it should have specific viability and rheological characteristics for effective impregnation of a filler. Application of liquid and solid poly-reactive oligomers allows avoiding the use of passive solvents, directionally change rheology of the binder and be cured in its composition with formation of a polymer with 3D-structure. The process of curing the binder on the basis of two organosilicic oligomers on the base of two organosilicic oligomer - oligo methylphenyl siloxane and oligomer which is a product of transesterification of oligophenylbutoxisiloxane with p and p¢-diphenylolpropane and influence of four - and bivalent tin carboxylates on it are studied. By means of IR-spectroscopy method it is shown that curing of the binder occurs within temperature interval of 100-200°C with the help of a number of consecutive reactions of polycondensation and leads to formation of the three-dimensional sewed polymeric matrix which is a product of interaction of initial oligomers. It is found that change of the organic substituent and carboxyl group in a molecule of the catalyst allows changing technological properties of the organosilicic binder (viscosity, viability and processing mode) in the wide range. Physical-mechanical properties of the received composite material on the basis of this binder and quartz filler with 3D-structures do not change. Work is executed within implementation of the complex scientific direction 13.1 «Binding for polymeric and composite materials of constructional and special purpose» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: organosilicic oligomer, tin carboxylates, viability, viscosity, outlet of insoluble polymer, IR-spectroscopy

Reference List

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    3. Dospehi dlya «Burana». Materialy i tehnologii VIAM dlya MKS «Energiya–Buran» / pod. obshh. red. E.N. Kablova [Armor for «Buran». Materials and VIAM technologies for ISS of «Energiya–Buran» / ed. by E.N.Kablov]. M.: Fond «Nauka i zhizn», 2013. S. 10–27.

    4. Minakov V.T., Grushko V.E., Donskoj A.A. Teplo- i ognezashhitnye materialy i pokrytiya [Warm and fireproof materials and coverings] / V kn. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2002: yubilejnyj nauch.-tehnich. sb. M.: MISiS–VIAM, 2002. S. 345–354.

    5. Kablov E.N. VIAM. Prodolzhenie puti [Way continuation] // Nauka v Rossii. 2012. №3. S. 26–44.

    6. Gunyaev G.M., Rumyancev A.F., Ivanova G.A. Metod avtoklavnogo formovaniya detalej iz polimernyh kompozicionnyh materialov [Method of avtoklavny formation of details from polymeric composite materials] // Aviacionnye materialy i tehnologii. 2002. Vyp.: Polimernye kompozicionnye materialy. S. 35–40.

    7. Vavilova M.I., Kavun N.S. Svojstva i osobennosti armiruyushhih steklyannyh napolnitelej, ispolzuemyh dlya izgotovleniya konstrukcionnyh stekloplastikov [The properties of glass filler for constructions of fiberglass] // Aviacionnye materialy i tehnologii. 2014. №3. S. 33–37.

    8. Babin A. N. Svyazujushhie dlya polimernyh kompozicionnyh materialov novogo pokoleniya [Binding for polymeric composite materials of new generation] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №4. St. 11. Available at: http://www.viam-works.ru (accessed: February, 12 2015).

    9. 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.

    10. Zheleznyak V.G., Chursova L.V. Modifikaciya svyazujushhih i matric na ih osnove s celyu povysheniya vyazkosti razrusheniya [Modification of binders and matrixes based on them to increase fracture toughness] // Aviacionnye materialy i tehnologii. 2014. №1. S. 47–50.

    11. Shiryaev V.I. Himiya i tehnologiya olovoorganicheskih soedinenij [Chemistry and technology of organotin connections] // Vse materialy. Enciklopedicheskij spravochnik. 2010. №11. S. 27–32. 

    12 Savenkova A.V., Chursova L.V., Eliseev O.A., Shragin D.I., Kopylov V.M., Glazov P.A. Vosstanovitel\'nye tehnologii izgotovleniya teplomorozostojkih germetikov na osnove kremnijorganicheskih kauchukov, sintezirovannyh po novym promyshlennym tehnologiyam [Recovery manufacturing techniques of heatcold-resistant hermetics on the basis of the organic silicon rubbers synthesized on new industrial technologies] // Aviacionnye materialy i tehnologii. 2012. №4. S. 25–31.

    13. Savenkova A.V., Chursova L.V., Eliseev O.A., Glazov P.A. Germetiki aviacionnogo naznacheniya [Hermetics of aviation assignment] // Aviacionnye materialy i tehnologii. 2012. №3. S. 40–43.

    14. Savenkova A.V., Tihonova I.V., Trebukova E.A. Teplomorozostojkie germetiki [Heatcold-resistant hermetics] / V kn. Aviacionnye materialy na rubezhe HH–HHI vekov: nauch.-tehnich. sb. M.: VIAM. 1994. S. 432–439.

    15. Clarke M.L. Recent advances in homogeneous catalysis using platinum complexes // Polyhedron. 2001. V. 20. P. 159–160.

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DOI: 10.18577/2071-9140-2016-0-2-45-49

UDC: 62-758.34

Pages:: 45-49

E.M. Shuldeshov1, V.V. Lepeshkin1, M.M. Platonov2, A.M. Romanov1

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

Method of definition of acoustic characteristics of sound-proof materials in the range of frequencies expanded to 15 kHz

This article is devoted to attenuation coefficient research in the range of frequencies from 6 to 15 kHz for samples of sound-proof polymeric composite materials. Features of measurement of attenuation coefficient of samples are described. The stand for carrying out measurements of attenuation coefficient of sound-proof materials is described. The calculation procedure necessary for obtaining of the above described characteristics is described. Accuracy of method of measurement is determined. Work is executed within implementation of the complex scientific direction 15.3. «Materials and coverings 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: sound-proof material, attenuation coefficient, sound wave, intensity

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.

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

    3. 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.

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

    5. Zhelezina G.F., Shuldeshova P.M. Konstrukcionnye organoplastiki na osnove plenochnyh kleev [Constructional organoplasty on the basis of film glues] // Klei. Germetiki. Tehnologii. 2014. №2. S. 9–14.

    6. Shuldeshova P.M., Zhelezina G.F. Aramidnyj sloisto-tkanyj material dlya zashhity ot ballisticheskih i udarnyh vozdejstvij [The aramid layered and woven material for protection against impact and ballistic influences] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №9. St. 06. Available at: http://www.viam-works.ru (accessed: March 09, 2015). DOI: 10.18577/2307-6046-2014-0-9-6-6.

    7. Obraztsova E.P., Kraev I.D., Shuldeshov E.M., Yurkov G.Yu. Gibridnye funkcionalnye materialy, sochetayushhie v sebe zvukopogloshhayushhie i radiopogloshhayushhie svojstva // Materialovedenie. 2016 (v pechati).

    8. Platonov M.M., Zhelezina G.F., Nesterova T.A. Poristovoloknistye polimernye materialy dlya izgotovleniya shirokodiapazonnyh ZPK i issledovanie ih akusticheskih svojstv [Porous fibrous polymer materials for wide range sound absorbing structures and investigation of their acoustical properties] // Trudy VIAM: elektron. nauch-tehnih. zhurn. 2014. №6. St. 09. Available at: http://viam-works.ru (accessed: March 09, 2015). DOI: 10.18577/2307-6046-2014-0-6-9-9.

    9. 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.

    10. Sytyj Yu.V., Sagomonova V.A., Maksimov V.G., Babashov V.T. Zvukoteploizoliruyushhij material gradientnoj struktury VTI-22 [VTI-22 sound and thermal insulation material of gradient structure] // Aviacionnye materialy i tehnologii. 2013. №2. S. 47–49.

    11. Sagomonova V.A., Kislyakova V.I., Tyumeneva T.Yu., Bol\\\'shakov V.A. Vliyanie kleevogo sloya na dempfiruyushhie svojstva vibropogloshhayushhego materiala na osnove termoplastichnogo poliuretana [Influence of glue layer on dempfiruyushchy properties of vibropogloshchayushchy material on the basis of thermoflexible polyurethane] // Klei. Germetiki. Tehnologii. 2015. №2. S. 23–27.

    12. Sagomonova V.A., Kislyakova V.I., Bolshakov V.A., Dolgopolov S.S. Vliyanie armiruyushhego sloya na kojefficient mehanicheskih poter\\\' vibropogloshhayushhih materialov [Influence of reinforcing layer on factor of mechanical losses of vibropogloshchayushchy materials] // Plasticheskie massy. 2015. №3–4. S. 13–16.

    13. Kraev I.D., Obraztsova E.P., Yurkov G.Yu. Vliyanie morfologii magnitnogo napolnitelya na radiopogloshhayushhie harakteristiki kompozicionnyh materialov [Influence of morphology of magnetic filler on radar-absorbing characteristics of composite materials] // Aviacionnye materialy i tehnologii. 2014. №S2. S. 10–14.

    14. Belyaev A.A., Romanov A.M., Shirokov V.V., Shuldeshov E.M. Izmerenie dielektricheskoj pronicaemosti steklosotoplasta v svobodnom prostranstve [Measurement of honeycomb glass fiber plasticspermittivity in free space] // Trudy VIAM: elektron. nauch-tehnih. zhurn. 2014. №5. St. 06. Available at: http://viam-works.ru (accessed: March 09, 2015). DOI: 10.18577/2307-6046-2014-0-5-6-6.

    15. Barbotko S.L., Kirillov V.N., Shurkova E.N. Ocenka pozharnoj bezopasnosti polimernyh kompozicionnyh materialov aviacionnogo naznacheniya [Assessment of fire safety of polymeric composite materials of aviation assignment] // Aviacionnye materialy i tehnologii. 2012. №3. S. 56–63.

    16. Shuldeshova P.M., Zhelezina G.F. Vliyanie atmosfernyh uslovij i zapylennosti sredy na svojstva konstrukcionnyh organoplastikov [An influence of atmospheric condition and dust loading on properties of structural organic plastics] // Aviacionnye materialy i tehnologii. 2014. №1. S. 64–68.

    17. Shuldeshov E.M., Lepeshkin V.V., Romanov A.M. Metod nerazrushajushhego kontrolja kompleksnoj dielektricheskoj pronicaemosti vhodnyh slabo napolnennyh sloev gradientnyh radiopogloshhajushhih polimernyh kompozicionnyh materialov [Method of non-destructive testing of complex dielectric permittivity of the entrance poorly filled layers of gradient radio absorbing polymeric composite materials] // Trudy VIAM: elektron. nauch-tehnih. zhurn. 2014. №10. St. 11. Available at: http://viam-works.ru (accessed: March 09, 2015). DOI: 10.18577/2307-6046-2014-0-10-11-11.

    18. Shul\\\'deshov E.M., Lepeshkin V.V., Romanov A.M. Metod nerazrushayushhego kontrolya kojefficienta otrazheniya radiopogloshhayushhih polimernyh kompozicionnyh materialov [Method of non-destructive testing of reflection coefficient of radio absorbing polymeric composite materials] // Kontrol. Diagnostika. 2015. №6. S. 44–48.

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DOI: 10.18577/2071-9140-2016-0-2-50-59

UDC: 678.747.2:620.177

Pages:: 50-59

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»

Mathematical modeling of deformation constructional carbon fiber at a bend

The article presents the numerical mathematical modeling simulation of bending carbon fiber. In the mathematical model of deformation of constructional carbon fiber were used, the coefficients of the equations of deformation of a polymeric matrix and a reinforcing filler. The mathematical model considers the different resistance of sintered layers deformation in tension and compression, resulting in bending. To account for possible variation of the volume content of reinforcement calculations were carried out for samples from constructional carbon-fiber VKU-25 with a volume content of filler 0,65 and 0,55%. To compare the developed mathematical model with known models strain diagrams of constructional carbon in three-point bending using finite element software are constructed. Comparison of the experimental and model deformations curve in three-point bending sample constructional carbon VKU-25 is conducted. Work is executed within implementation of the complex scientific direction 3.3. «Technology of forecasting of properties, modeling and implementation of modern processes of designing and production of products from non-metallic and composite materials with use of the digital methods compatible to CAD/CAM/CAE and PLM by systems» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: filler, polymer matrix composite material, a mathematical model, three-point bending, shear force, bending moment, longitudinal displacement, deflection, finite element method

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.

    2. 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.

    3. Kablov E.N., Shchetanov 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: February 12, 2015).

    4. 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.

    5. 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.

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

    7. 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: February 12, 2015).

    8. 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.

    9. Erasov V.S., Grinevich A.V., Senik V.Ya., Konovalov V.V., Trunin Yu.P., Nesterenko G.I. Raschetnye znacheniya harakteristik prochnosti aviacionnyh materialov [Calculated values of characteristics of durability of aviation materials] // Aviacionnye materialy i tehnologii. 2012. №2. S. 14–16.

    10. Belyaev M.S., Gorbovec M.A., Komarova T.I. Sposob ispytanij i raschetnoe opredelenie predela vynoslivosti dlya gorizontalnogo uchastka krivoj ustalosti [Way of tests and rated definition of limit of endurance for horizontal site of curve fatigue] // Aviacionnye materialy i tehnologii. 2012. №3. S. 50–55.

    11. Majorova I.A. Matematicheskoe modelirovanie processa teploperenosa i optimizaciya konstrukcii mnogoslojnogo teplozashhitnogo pokrytiya [Mathematical modeling of heat  transfer and optimization of multilayer thermal protective system] // Aviacionnye materialy i tehnologii. 2013. №2. S. 16–18.

    12. Samorukov M.L. Analiticheskij podhod k matematicheskomu modelirovaniyu temperaturnoj sostavlyayushhej rotacionnoj svarki treniem [Analytical approach to mathematical modeling of temperature component of direct drive friction welding] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №9. St. 03. Available at: http://www.viam-works.ru (accessed: February 12, 2015).

    13. Novozhilov V.V. Teoriya tonkih obolochek [Theory of thin covers]. L.: Sudpromgiz. 1951. 344 s.

    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., 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. 2016 (v pechati).

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

    17. 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 intermetallidny alloys on the basis of the microstructural numerical analysis] // Matematicheskoe modelirovanie i chislennye metody. 2015. №2. S. 3–22.

    18. Dimitrienko Yu.I., Lucenko A.N., Gubareva E.A., Oreshko E.I., Bazyleva O.A., Sborshhikov S.V. Raschet mehanicheskih harakteristik zharoprochnyh intermetallidnyh splavov na osnove nikelya metodom mnogomasshtabnogo modelirovaniya 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).

    19. Oreshko E.I., Erasov V.S., Podzhivotov N.Yu., Lutsenko A.N. Raschet na prochnost gibridnoj paneli kryla na baze listov i profilej iz vysokoprochnogo alyuminijlitievogo splava i sloistogo alyumostekloplastika [Calculation on durability of the hybrid panel of wing on the basis of sheets and profiles from high-strength alyuminiylitiyevy alloy and layered alyumostekloplastika] // Aviacionnye materialy i tehnologii. 2016. №1 (40). S. 53–61.

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11.

DOI: 10.18577/2071-9140-2016-0-2-69-75

UDC: 678.84

Pages:: 69-75

V.S. Erasov1, A.V. Lavrov1, A.N. Lucenko1, A.V. Grinevich1

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

About the question of the interaction of hardened core with ceramic barrier

The engineering method of study the criteria of performance for the ceramic armor elements with the possibility of an integrated assessment after barrier action is suggested. For a series of model samples based on alumina ceramics depending to the main criteria for the operation of the thickness of the armor elements are received. The nature of the destruction of heat-treated core bullets B32 interaction with ceramic armor elements of different thicknesses is researched. Work is executed within implementation of the complex scientific direction 2 «Fundamental the oriented researches, qualification of materials, non-destructive testing» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: ceramic armor, core, bullet, criterion, model, energy capacity

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.

    2. Grinevich A.V., Petrova A.P. Soedinenie raznorodnyh materialov dlya detalej, podverzhennyh impulsnym nagruzkam [Joining materials of different types used in constructions subjected to pulse loading] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. № 10. St. 05. Available at: http://www.viam-works.ru (accessed: March 27, 2015).

    3. Istoriya aviacionnogo materialovedeniya. VIAM – 80 let: gody i lyudi / pod. obshh. red. E.N. Kablova [History of aviation materials science. VIAM – 80 years: years and people / ed. by E.N.Kablova]. M.: VIAM. 2012. 520 s. 

    4. Grigoryan V.A., Kobylkin I.F., Marinin V.M., Chistyakov E.N. Materialy i zashhitnye struktury dlya lokal\'nogo i individual\'nogo bronirovaniya [Materials and protective structures for local and individual armoring]. M.: RadioSoft. 2008. 406 s. 

    5. Zashhita tankov /Pod red. V.A. Grigoryana [Protection of tanks / ed. by of V.A.Grigoryan]. M.: Izd-vo MGTU im. N.E. Baumana, 2007. 327 s. 

    6. Kablov E.N. Aviakosmicheskoe materialovedenie [Calculated values of characteristics of durability of aviation materials] // Vse materialy. Enciklopedicheskij spravochnik. 2008. №3. S. 2–14. 

    7. Erasov V.S., Grinevich A.V., Senik V.Ya., Konovalov V.V., Trunin Yu.P., Nesterenko G.I. Raschetnye znacheniya harakteristik prochnosti aviacionnyh materialov [Calculated values of characteristics of durability of aviation materials] // Aviacionnye materialy i tehnologii. 2012. №2. S. 14–16.

    8. 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.

    9. Grinevich A.V., Yarosh V.V. Drobyashhij effekt keramicheskogo sloya kombinirovannoj broni [Splitting-up effect of ceramic layer of the combined reservation] // Voprosy oboronnoj tehniki. Ser. 15. 1999. Vyp. 1–2. S. 20–30. 

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12.

DOI: 10.18577/2071-9140-2016-0-2-76-87

UDC: 621.794.62:620.193

Pages:: 76-87

S.S. Vinogradov1, S.A. Dyomin2, S.V. Balakhonov2, O.G. Kirillova2

[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»

Inorganic composite coatings - a perspective direction in the field of anticorrosive protectoin of carbon steels

The composite coating for anticorrosive protection of carbon steel developed in VIAM is a continuation of international and Russian works devoted to composite coatings based on phosphates and aluminum powder. The composite coating possesses good adhesion with carbon steel after sandblasting. Anticorrosive tests in sea coast environment at the Center of Anticorrosive Tests (Gelendzhik city) and in salt spray chamber showed that the coating has high protection property (more than 5000 hours in salt spray chamber) including exploitation at 460°C. This result had been obtained after grinding of a top layer of the coating; after that the aluminum powder acted as protector. The electrochemical tests verified an anodic type of the composite coating. Mechanical tests showed a possibility of wearing of the composite coating onto high-strength steels. The coating is water resistant and is able to be used in different oils. Work is executed within implementation of the complex scientific direction 17.2. «The slip, gazodinamichesky and combined coverings for details from carbon steels, including high-strength» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: composite coating, coating based on phosphates and aluminum powder, protective property, grinding, mechanical tests, water resistance, oil resistance

Reference List

    1. Kablov E.N. 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.

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DOI: 10.18577/2071-9140-2016-0-2-88-94

UDC: 669.715:620.193

Pages:: 88-94

M.G. Kurs1

[1] Federal State Unitary Enterprise «All-Russian Scientific Research Institute of Aviation Materials»

Atmospheric corrosion resistance of advanced Al-Li alloys by nature full-scale accelerated tests in the conditions of temperate warm climate

It is now becoming an essential matter to get a reliable assessment of corrosion resistance in a short time when tested in harsh climatic conditions. The proposed method of full-scale accelerated tests allows getting data about corrosion resistance of the material 4-5 times faster in comparison with the tests in the open atmosphere. In the present paper the results of corrosion resistance research of plates made of perspective aluminum-lithium alloys 1441-T1, 1424-T1, V-1461-T1 and V-1469-T1 by full-scale accelerated tests are presented. The method is based on the acceleration of the corrosion process by periodically applying a sea salt solution on the surface of the sample exposed to atmospheric climate station stand of the Gelendzhik climatic testing center named after G.V. Akimov (GCTC of VIAM). It was shown that during 12 months of testing the maximum values of intergranular and pitting corrosion depth are achieved which further changed slightly. The examination of corrosion rate in its dynamics showed its considerable decrease after 6 months of exposition. It was found that 1424-T1 alloy has the highest corrosion resistance. Work is executed within implementation of the complex scientific direction 18.2. «Development of methods of climatic tests and tool methods of research» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: corrosion, aluminum-lithium alloys, full-scale accelerated tests, rates of corrosion resistance

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