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Aviation materials and technologies №3, 2016

Contents

  • N.Yu. Serebrennikova, V.V. Antipov, O.G. Senatorova, V.S. Erasov, V.V. Kashirin

    Hybrid multilayer materials based on aluminum-lithium alloys applied to panels of plane wing

    3-8
  • B.D. Annin, V.M. Fomin, E.V. Karpov, A.G. Malikov, A.M. Orishich

    Complex research of laser welding of high-strength alloy V-1469

    9-16
  • M.G. Kurs, V.V. Antipov, A.N. Lutsenko, A.E. Kutyrev

    Integral figure of corrosion damage of deformed aluminum alloys

    24-32
  • Yu.I. Dimitrienko, A.N. Lutsenko, E.A. Gubareva, E.I. Oreshko, O.A. Bazyleva, S.V. Sborschikov

    Calculating of mechanical characteristics of heat resistant intermetallic alloys on the basis of nickel by method of multi-scale modeling of structure

    33-48
  • D.V. Kosolapov, A.A. Shavnev, A.N. Nyavkin, O.I. Grishina

    Research of forming of structure of composition granules of Al-SiC

    49-52
  • B.V. Shchetanov, I.U. Efimochkin, S.V. Paegle, F.N. Karachevtsev

    Study of high-temperature strength of Nb-Si-Ti in-situ-composites reinforced by single-crystal α-Al2O3

    53-59
  • A.M. Chaykun, I.S. Naumov, M.A. Venediktova, E.V. Alifanov

    New researches of special purpose fluorosilicone rubber

    60-65
  • A.E. Sorokin, E.Ya. Beider, T.F. Izotova, E.V. Nikolaev, A.K. Shvedkova

    Investigation of carbon fiber reinforced plastic on polyphenylenesulfide resin after accelerated and natural climatic test

    66-72
  • V.V. Murashov

    Assessment of accumulation degree of microdamages of PCM structure in structures determined by nondestructive methods

    73-81
  • S.A. Evdokimov, S.St. Solntsev, G.V. Yermakova, D.I. Davletchin

    High-temperature protective coating for C-C composite materials

    82-87
  • E.I. Kosarina, A.V. Stepanov, A.A. Demidov, O.A. Krupnina

    Sensitometer for technical radiographic films

    88-94
Содержание номера
1.

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

UDC: 669.018.29

Pages:: 3-8

N.Yu. Serebrennikova1, V.V. Antipov1, O.G. Senatorova1, V.S. Erasov1, V.V. Kashirin2

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

Hybrid multilayer materials based on aluminum-lithium alloys applied to panels of plane wing

It is an opportunity to improve weight efficiency by application of laminated skin from hybrid material which consists of high-strength Al-Li alloy sheets and aluminium-glassplastic Laminate SIAL-type. Such materials have high resistance of fatigue crack growth, lower density and high strength in comparison with monolithic materials. The structure and properties of prototype of hybrid wing panel of Tu-204 aircraft were evaluated was produced in commercial conditions, OAO «Voronezh Aircraft JVC» (VASO). Standard samples were used for tensile, compression low fatigue tests and for determination of FGGR (dl/dN). Hybrid laminated materials are recommended to use for lower and upper wing panels. The work is executed within implementation of the complex scientific direction 6.2. «Layered crack resistant, high-strength metal polymer materials» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: hybrid laminated material, wing panel, skin, stringer, Al–Li alloy, SIAL.

Reference List

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    7. Antipov V.V., Senatorova O.G., Lukina N.F. i dr. Sloistye metallopolimernye kompozicionnye materialy [Layered metalpolymeric composite materials] // Aviacionnye materialy i tehnologii. 2012. №S. S. 226–230. 

    8. Senatorova O.G., Antipov V.V., Lukina N.F., Sidel\'nikov V.V., Shestov V.V., Popov V.I., Ershov A.S. Vysokoprochnye, treshhinostojkie, legkie alyumostekloplastiki SIAL – perspektivnye materialy dlya aviacionnyh konstrukcij [High-strength, treshchinostoyky, easy alyumostekloplastiki SIAL – perspective materials for aviation designs] // TLS. 2009. №2. S. 29–31. 

    9. Antipov V.V., Lavro N.A., Suhoivanenko V.V., Senatorova O.G. Opyt primeneniya Al–Li splava 1441 i sloistogo materiala na ego osnove v gidrosamoletah [Experience of application of Al–Li of alloy 1441 and layered material on its basis in seaplanes] // Tsvetnye metally. 2013. №8. S. 46–50.

    10. Laminate of metal sheets and polymer: pat. 0256370 US; publ. 20.10.11.

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    15. 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. 

    16. Shestov V.V., Antipov V.V., Senatorova O.G., Sidelnikov V.V. Konstrukcionnye sloistye alyumostekloplastiki 1441-SIAL [Constructional layered aluminum glass plastics 1441-SIAL] // MiTOM. 2013. №9. S. 28–32. 

    17. Skornyakov V.I., Antipov V.V. Innovacionnyj harakter sotrudnichestva OAO «KUMZ» i FGUP «VIAM» [Innovative nature of cooperation of JSC «KUMZ» and FSUE «VIAM»] // Aviacionnye materialy i tehnologii. 2012. №2. S. 11–14. 

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    19. Antipov V.V., Senatorova O.G., Beumber T., Lipma M. Investigation of a new fibre metal laminate (FML) family on the base of Al–Li alloy with lower density // Materials Science and Engineering Techology. 2012. №4. P. 350–355. 

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    21. Erasov V.S., Nuzhnyj G.A., Grinevich A.V., Terehin A.L. Treshhinostojkost aviacionnyh materialov v processe ispytaniya na ustalost [Crack growth resistance of aviation materials in fatigue testing] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №10. St. 06. Available at: http://www.viam-works.ru (accessed: October 14, 2015).

    22. 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.

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2.

DOI: 10.18577/2071-9140-2016-0-3-9-16

UDC: 621.791:669018.44

Pages:: 9-16

B.D. Annin1, V.M. Fomin2, E.V. Karpov1, A.G. Malikov2, A.M. Orishich2

[1] Siberian branch of Russian academy of sciences Lavrentev Institute of hydrodynamic
[2] Federal State Budgetary Institution Khristianovich institute of theoretical and applied mechanics Siberian Branch of Russian Academy of Sciences

Complex research of laser welding of high-strength alloy V-1469

Complex experimental research of laser welding of aluminum-lithium alloy В-1469 in order to obtain heat-resistant welded joint is considered in the work. It is found, that plastic deformation of the welded joint allows increasing weld strength by 5-10% in comparison with non-deformed welded joint. Heat treatment of welded joint increases it`s strength, however it essentially reduces strength of the main alloy out of thermal influence zone of welding process. Application of heat treatment allows obtaining the strength of welded joint equal to 0,85 from strength of the main alloy as received state T1.

Keywords: laser welding, aluminum-lithium alloy, strength, heat treatment.

Reference List

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

    3. Splav na osnove alyuminiya i izdelie, vypolnennoe iz nego: pat. 2237098 Ros. Federaciya [Alloy on the basis of aluminum and the product which has been executed of it: stalemate. 2237098 Ros. Federation]; opubl. 24.07.03.

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    6. Petrovic M., Veljic D., Rakin M., Radovic N., Sedmak A., Bajic N. Friction-stir welding of highstrength aluminium alloys and a numerical simulation of plunge stage // Materials in technology. 2012. V. 46. №3. P. 215–221.

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    9. Annin B.D., Fomin V.M., Antipov V.V., Ioda E.N., Karpov E.V., Malikov A.G., Orishich A.M., Cherepanov A.N. Issledovanie tehnologii lazernoj svarki alyuminievogo splava 1424 [Research of technology of laser bonding of aluminum alloy 1424 ] // Doklady akademii nauk. 2015. T. 465. №4. S. 419–424.

    10. Annin B.D., Fomin V.M., Karpov E.V., Malikov A.G., Orishich A.M., Cherepanov A.N. Development of a technology for laser welding of the 1424 aluminum alloy with a high strength of the welded joint // Journal of Applied Mechanics and Technical Physics. 2015. V. 56. №6. P. 945–950.

    11. Lukin V.I., Ioda E.N., Panteleev M.D., Skupov A.A. Vliyanie termicheskoj obrabotki na harakteristiki svarnyh soedinenij vysokoprochnyh alyuminijlitievyh splavov [Heat treatment influence on characteristics of welding joints of high-strength aluminum-lithium alloys] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №4. St. 06. Available at: http://www.viam-works.ru (accessed: April 20, 2016). DOI: 10.18577/2307-6046-2015-0-4-6-6.

    12. Klochkova Yu.Yu., Klochkov G.G., Romanenko V.A., Popov V.I. Struktura i svojstva listov iz vysokoprochnogo alyuminij-litievogo splava V-1469 [Structure and properties of sheets from high-strength aluminum-lithium alloy V-1469] // Aviacionnye materialy i tehnologii. 2015. №4 (37). S. 3–8. DOI: 10.18577/2071-9140-2015-0-4-3-8.

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4.

DOI: 10.18577/2071-9140-2016-0-3-24-32

UDC: 620.193.2

Pages:: 24-32

M.G. Kurs1, V.V. Antipov2, A.N. Lutsenko2, A.E. Kutyrev2

[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»

Integral figure of corrosion damage of deformed aluminum alloys

Based on the results of 4-years exposure of five aluminum alloys (2 mm thick sheets) at full-scale accelerated tests, calculating procedure for integral figure of corrosion damage was developed by two methods: for samples after full-scale accelerated tests (method A) and for constructions using nondestructive control methods (method B). Application of integral research methods of corrosion resistance of aluminum alloys and calculation of integrated corrosion figure will allow to estimate strength variations of constructions losses, made from sheet aluminum alloys in the case of their corrosion damages in the process of operation when performing a scheduled inspection and remedial maintenance of aviation articles.

Keywords: integral figure, aluminum alloys, corrosion, full-scale accelerated tests.

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. Antipov V.V. Strategiya razvitiya titanovyh, magnievyh, berillievyh i alyuminievyh splavov [Strategy of development of titanium, magnesium, beryllium and aluminum alloys] // Aviacionnye materialy i tehnologii. 2012. №S. S. 157–167.

    3. Kablov E.N., Startsev O.V., Medvedev I.M. Obzor zarubezhnogo opyta issledovanij korrozii i sredstv zashhity ot korrozii [Review of international experience on corrosion and corrosion protection] // Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 76–87.

    4. Grinevich A.V., Lutsenko A.N., Karimova S.A. Raschetnye harakteristiki metallicheskih materialov s uchetom vlazhnosti [The design characteristic of metallic materials taking into account the humidity] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №7. St. 10. Available at: http://www.viam-works.ru (accessed: January 29, 2016). DOI: 10.18577/2307-6046-2014-0-7-10-10.

    5. Kurs M.G., Karimova S.A. Naturno-uskorennye ispytaniya: osobennosti metodiki i sposoby ocenki korrozionnyh harakteristik alyuminievyh splavov [Salt-accelerated outdoor corrosion testing: methodology and evaluation of corrosion susceptibility of aluminum alloy] // Aviacionnye materialy i tehnologii. 2014. №1. S. 51–57.

    6. Semenychev V.V. Korrozionnaya stojkost listov splava D16ch.-T v morskih subtropikah [Corrosion resistance of alloy D16ch.-T sheets in marine subtropics] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №7. St. 11. Available at: http://www.viam-works.ru (accessed: December 15, 2015). DOI: 10.18577/2307-6046-2014-0-7-11-11.

    7. Zhirnov A.D., Strekalov P.V., Karimova S.A., Zhilikov V.P., Tararaeva T.I., Mishchenkov E.N. Sezonnaya dinamika protsessa korrozii metallov na beregovoy zone Chernogo moray [Seasonal dynamics of process of corrosion of metals on coastal zone of Black Sea] // Korroziya: materialy, zashchita. 2007. №8. S. 23–29.

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    9. Kurs M.G., Laptev A.B., Kutyrev A.E., Morozova L.V. Issledovanie korrozionnogo razrusheniya deformiruemyh alyuminievyh splavov pri naturno-uskorennyh ispytaniyah. Ch. 1 [Research of corrosion destruction of deformable aluminum alloys at natural accelerated tests. P.1] // Voprosy materialovedeniya. 2016. №1 (85). S. 116–126.

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5.

DOI: 10.18577/2071-9140-2016-0-3-33-48

UDC: 669.018.44:669.017.165

Pages:: 33-48

Yu.I. Dimitrienko1, A.N. Lutsenko2, E.A. Gubareva1, E.I. Oreshko2, O.A. Bazyleva2, S.V. Sborschikov3

[1] ul. Baumanskaya 2-ya, 5, Moscow, 105005
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[3] Bauman Moscow State Technical University

Calculating of mechanical characteristics of heat resistant intermetallic alloys on the basis of nickel by method of multi-scale modeling of structure

The article considers computational mathematical modeling of mechanical properties of heat resistant nickel alloys by method of multi-scale modeling of structure. Effect of crystallographic orientation (CGO) <001>, <011>, <111> on the microstructure of intermetallic alloy VKNA-1V is investigated. The decision to use two-level structure model of VKNA-1V alloy in the form of the periodic structure containing two phases with section boundary between them is made on the basis of performed metallographic analysis. The 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 systems» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: VKNA-1V, microstructure, crystallographic orientation, intermetallide Ni3Al, monocrystal alloys, mathematical modeling, method of multilarge-scale modelling, finite element method, damage.

Reference List

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    2. Kablov E.N., Buntushkin V.P., Bazyleva O.A. Konstrukcionnye zharoprochnye materialy na osnove soedineniya Ni3Al dlya detalej goryachego trakta GTD [Constructional heat resisting materials on the basis of Ni3Al connection for details of hot path of GTD] // Tehnologiya legkih splavov. 2007. №2. S. 75–80.

    3. Kablov E.N., Petrushin N.V., Elyutin E.S. Monokristallicheskie zharoprochnye splavy dlya gazoturbinnyh dvigatelej [Single-crystal hot strength alloys for gas turbine engines] // Vestnik MGTU im. N.E. Baumana. Ser.: Mashinostroenie. 2011. №SP2. S. 38–52.

    4. Povarova K.B., Bazyleva O.A., Kazanskaya N.K., Drozdov A.A. i dr. Konstrukcionnye zharoprochnye splavy na osnove Ni3Al: poluchenie, struktura i svojstva [Constructional hot strength alloys on the basis of Ni3Al: receiving, structure and properties] // Materialovedenie. 2011. №4. S. 39–48.

    5. Bazyleva O.A., Arginbaeva E.G., Turenko E.Yu. Zharoprochnye litejnye intermetallidnye splavy [Heat resisting cast intermetallic alloys] // Aviacionnye materialy i tehnologii. 2012. №S. S. 57–60.

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DOI: 10.18577/2071-9140-2016-0-3-49-52

UDC: 669.018.95

Pages:: 49-52

D.V. Kosolapov1, A.A. Shavnev1, A.N. Nyavkin1, O.I. Grishina2

[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 forming of structure of composition granules of Al-SiC

The influence of mechanical alloying time on formation of composition structure of granules based on high-strength aluminum alloy is shown. Aluminum alloy of Al-Zn-Mg-Cu system and SiC silicon carbide powders were used as initial components. Stages of structure forming are shown. In the process of mechanical alloying under the influence of grinding bodies the initial components mixing, deformation, destruction and welding occurred. As time of mechanical alloying increased the forming of monolithic structure of composition granules occurred. The fractional structure of the received composition granules is shown. The conclusion about influence of mechanical alloying time on structure of composition granules is made. The work is executed within implementation of the complex scientific direction 12.1. «Metal composite materials (MCM) reinforced by particles and fibers of high-melting compositions» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: a metal matrix composite (MMC), aluminum, silicon carbide particles.

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DOI: 10.18577/2071-9140-2016-0-3-53-59

UDC: 669.293:669.018.95

Pages:: 53-59

B.V. Shchetanov1, I.U. Efimochkin1, S.V. Paegle1, F.N. Karachevtsev1

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

Study of high-temperature strength of Nb-Si-Ti in-situ-composites reinforced by single-crystal α-Al2O3

A set of experimental samples of fibrous composite materials (CMs) was fabricated by hot pressing techniques from mechanically alloyed powder of ternary Nb-Si-Ti system and continuous single-crystal α-Al2O3 fibers with and without TiN coating. The microstructure and phase composition of fibrous CMs were characterized by X-ray diffraction and electron probe microanalysis. Matrix phase composition consists: Nbs.s., Tis.s., Nb5Si3, Nb3Si, TiSi, Ti5Si4 and Nb4FeSi. It is established that the structure in the interaction zone of the matrix-fiber interface is changed due to the mutual elements diffusion of matrix and fiber (coating). Nb5Si3 phase is depleted by diffusion of silicon from a matrix interaction zone to the fiber that leads to formation of Nb3Si phase. High-temperature bending strength of Nb-Si-Ti in-situ composites reinforced by single-crystal fibers with and without barrier coating is investigated. It is found that the high-temperature bending strength of CM reinforced by fibers without covering at 1300°C is 1,5 times higher than for the pure (Nb-Si-Ti) matrix; and the one of CM reinforced by fibers with covering is 2,5 times higher. The work is executed within implementation of the complex scientific direction 12.3. «Metal composite materials (MCМ) on the basis of Nb, Mo and their intermetallic compound» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: Nb–Si–Ti composites, single-crystal α-Al2O3 fibers, diffusion barrier TiN coating, high-temperature bending strength, X-ray diffraction analysis and electron probe microanalysis.

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    13. Basargin O.V., Shheglova T.M., Nikitina V.Yu., Svistunov V.I. Sposob opredeleniya prochnosti pri rastyazhenii monokristallicheskih volokon Al2O3 pri temperature 1400°S [High-temperature tensile strength determination of single crystal alumina fibers] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №4. St. 03. Available at: http://www.viam-works.ru (accessed: March 25, 2015). DOI: 10.18577/2307-6046-2014-0-4-3-3.

    14. Zhao J.-C., Jackson M.R., Peluso L.A. Mapping of the Nb–Ti–Si phase diagram using diffusion multiples // Materials Science and Engineering A372. 2004. P. 21–27.

    15. Bowman R.R., Misra A.K., Arnold S.M. Processing and Mechanical Properties of Al2O3 Fibwe-Reinforced NiAl Composites // Metallurgical and Materials Transactions. 1995. V. 26A. P. 615–628.

    16. Svetlov I.L., Abuzin Yu.A., Babich B.N., Vlasenko S.Ya., Efimochkin I.Yu., Timofeeva O.B. Vysokotemperaturnye niobievye kompozity, uprochnennye silicidami niobiya [The high-temperature niobic composites strengthened by silicides of niobium] // Zhurnal funkcional\'nyh materialov. 2007. T. 1. №2. S. 48–53.

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DOI: 10.18577/2071-9140-2016-0-3-60-65

UDC: 621.315.616.7

Pages:: 60-65

A.M. Chaykun1, I.S. Naumov2, M.A. Venediktova2, E.V. Alifanov2

[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»

New researches of special purpose fluorosilicone rubber

The article shows modern tendencies in synthesis of fluorosilicone raw rubbers and vulcanizate stock based thereon. The subscribed problem is very actual since remarkable increase of aircraft operation intensity dictates new requirements to used rubbers. First of all they are the increase in temperature range of operation and improvement of performance parameters. That is why the improvement of rubber compounds based on fluorosilicone raw rubbers is of particular interest since they provide wide temperature range of operation and have high performance characteristics. Rubbers based on silicone raw rubbers can work in air at wide temperature range. However they have low fuel- and oil resistance. High-molecular fluorosilicone raw and vulcanizate rubbers have balanced combination of resistance to aggressive environment and good working ability in wide temperature range. Improving rubber compositions based on above-mentioned raw rubbers allows improving their performance parameters and thus increase the life time of aircraft. The patterns revealed in this work allow to research and compose new. The work is executed within implementation of the complex scientific direction 15.2. «Elastomeric and sealing materials» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: rubber, rubber compounds, fluorosilicone rubbers.

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. 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.

    3. Vlasenko F.S., Raskutin A.E. Primenenie polimernyh kompozicionnyh materialov v stroitelnyh konstrukciyah [Applying FRP in building structures] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №8. St. 03. Available at: http://viam-works.ru (accessed: March 20, 2015).

    4. Eliseev O.A., Krasnov L.L., Zajceva E.I., Savenkova A.V. Razrabotka i modificirovanie elastomernyh materialov dlya primeneniya vo vseklimaticheskih usloviyah [Development and modifying of elastomeric materials for application in all weather conditions] // Aviacionnye materialy i tehnologii. 2012. №S. S. 309–314.

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

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    11. Tehnologiya reziny: Recepturostroenie i ispytaniya: per. s angl. / pod red. Dzh.S. Dika [Compounding structure and tests: trans. from English / ed. by J. S. Dick]. SPb.: Nauchnye osnovy i tehnologii, 2010. 620 s.

    12. Shvejcer F.A. Korroziya plastmass i rezin [Corrosion of plastic and rubbers]. SPb.: Nauchnye osnovy i tehnologii, 2010. 637 s.

    13. Martin Dzh.M., Smit U.K. Proizvodstvo i primenenie rezinotehnicheskih izdelij: per s angl. / pod red. S.Ch. Bhati [Production and application of industrial rubber products: trans. from English]. SPb.: Professiya, 2006. 480 s.

    14. Chaikun A.M., Eliseev O.A., Naumov I.S., Venediktova M.A. Osobennosti morozostojkih rezin na osnove razlichnyh kauchukov [Features of old-resistant rubbers on the basis on different unvulcanized rubbers] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №12. St. 04. Available at: http://www.viam-works.ru (accessed: March 20, 2015).

    15. Chaykun A.M., Eliseev O.A., Naumov I.S., Venediktova M.A. Osobennosti postroeniya receptur dlya morozostojkih rezin [Compounding principles in the field of frost resistant rubbers] // Aviacionnye materialy i tehnologii. 2013. №3. S. 53–55.

    16. Ito M., Noguchi T., Ueki H., Inukai H., Ino S., Takeuch K., End M. Adhesion and Reinforcement of CNT-fluoroelastomers Composite for Oilfield Application // Journal of The Adhesion Society of Japan. 2011. V. 47 (4). P. 146–153.

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DOI: 10.18577/2071-9140-2016-0-3-66-72

UDC: 678.747.2:620.165.79

Pages:: 66-72

A.E. Sorokin1, E.Ya. Beider1, T.F. Izotova1, E.V. Nikolaev1, A.K. Shvedkova1

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

Investigation of carbon fiber reinforced plastic on polyphenylenesulfide resin after accelerated and natural climatic test

This article contains a properties study of structural thermoplastic carbon fiber reinforced plastic (CFRP) based on polyphenylenesulfide matrix after accelerated and full-scale climatic tests. CFRP has high resistance to tropical climate, water and humid environment at normal and elevated temperatures. It is shown that CFRP is characterized by low water- and moisture absorption. Thermal aging of CFRP is accompanied by increasing of its’ glass transition temperature, because of structuration processes. Effects arising during full-scale climatic tests of CFRP resulted in slight reducing of its’ strength characteristics and increasing of fireproof properties. The 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: polymer composite material, carbon fiber plastic, thermoplastic matrix, accelerated aging, full-scale climatictests.

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DOI: 10.18577/2071-9140-2016-0-3-73-81

UDC: 678.8:620.179

Pages:: 73-81

V.V. Murashov1

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

Assessment of accumulation degree of microdamages of PCM structure in structures determined by nondestructive methods

It is suggested to assess the micro-damage accumulation degree in polymer composites by their strength characteristics determined by the nondestructive method using the integrated parameter that contains the ultrasonic testing pulse velocity values in the product plane and the main ultrasonic testing impulse spectral component frequency values that got through the product dimension direct and reverse. The work is executed within implementation of the complex scientific direction 2.3 «Methods of nondestructive research and control» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: non-destructive testing, polymer composite materials, micro-damages, strength characteristics.

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.

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    3. Kablov E.N. Kontrol kachestva materialov – garantiya bezopasnosti ekspluatacii aviacionnoj tehniki // Aviacionnye materialy i tehnologii [Quality control of materials – security accreditation of operation of aviation engineering]. M.: VIAM, Vyp.: Metody ispytanij i kontrolya kachestva metallicheskih i nemetallicheskih materialov. 2001. S. 3–8.

    4. Kablov E.N. Shestoj tehnologicheskij uklad //Nauka i zhizn\'. 2010. №4. S. 2–7.

    5. Murashov V.V., Mishurov K.S. Ocenka prochnostnyh harakteristik ugleplastikov akusticheskim metodom //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 81–85.

    6. Generalov A.S., Murashov V.V., Kosarina E.I., Bojchuk A.S. Postroenie i analiz korrelyacionnyh svyazej dlya ocenki prochnostnyh svojstv ugleplastikov reverberacionno-skvoznym metodom //Aviacionnye materialy i tehnologii. 2014. №1. S. 58–63.

    7. Murashov V.V., Kosarina E.I., Generalov A.S. Kontrol\' kachestva aviacionnyh detalej iz polimernyh kompozicionnyh materialov i mnogoslojnyh kleenyh konstrukcij //Aviacionnye materialy i tehnologii. 2013. №3. S. 65–70.

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    10. Maksimov R.D., Ponomarev V.M. Predposylki kompleksnogo diagnostirovaniya nakopleniya povrezhdenij pri deformirovanii gibridnogo kompozita //Metody i sredstva diagnostiki nesushhej sposobnosti izdelij iz kompozitov. Riga: Zinatne. 1983. S. 150–155.

    11. Sorokin K.V., Murashov V.V., Fedotov M.Yu., Goncharov V.A. Prognozirovanie razvitiya defektov v konstrukciyah iz PKM sposobom opredeleniya izmenenij zhestkosti pri aktyuirovanii materiala [Forecasting of development of defects in designs from PCM in the way of definition of changes of rigidity at material actuation conditions] // Aviacionnye materialy i tehnologii. 2011. №2. S. 20–22.

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    15. Murashov V.V., Rumyancev A.F., Buznikov Yu.N. Ocenka fiziko-mehanicheskih harakteristik ugleplastikov kompleksnym akusticheskim metodom [Assessment of physicomechanical characteristics ugleplastikov complex acoustic method] // Voprosy aviacionnoj nauki i tehniki. Ser.: Aviacionnye materialy. M.: VIAM, 1986. Vyp.: Nemetallicheskie kompozicionnye materialy. S. 105–111.

    16. 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.

    17. Kablov E.N., Startsev O.V., Krotov A.S., Kirillov V.N. Klimaticheskoe starenie kompozicionnyh materialov aviacionnogo naznacheniya. I. Mehanizmy stareniya [Climatic aging of composite materials of aviation assignment. I. Aging mechanisms] // Deformaciya i razrushenie materialov. 2010. №11. S. 19–27.

    18. 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.

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    21. Potapov A.I., Pekker F.P. Nerazrushayushhij kontrol konstrukcij iz kompozicionnyh materialov [Non-destructive testing of designs from composite materials]. L.: Mashinostroenie. 1977. 190 s.

    22. Gershberg M.V., Ilyushin S.V., Smirnov V.N. Nerazrushayushhie metody kontrolya sudostroitelnyh stekloplastikov [Nondestructive control methods of ship-building fibreglasses]. L.: Sudostroenie. 1971. 200 s.

    23. Ashkenazi E.K., Gershberg M.V., Ilyushin S.V. Kosvennyj sposob ocenki prochnosti stekloplastikov pri sdvige [Indirect way of assessment of durability of fibreglasses at shift] // Svojstva sudostroitelnyh stekloplastikov i metody ih kontrolya. L.: Sudostroenie, 1974. Vyp. 3. S. 198–202.

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11.

DOI: 10.18577/2071-9140-2016-0-3-82-87

UDC: 629.7.023

Pages:: 82-87

S.A. Evdokimov1, S.St. Solntsev1, G.V. Yermakova1, D.I. Davletchin1

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

High-temperature protective coating for C-C composite materials

The basic principles and possibilities of high-temperature chemical synthesis of protective coating on carbonaceous composite materials are regarded in the present article. It is shown that the application of high-temperature chemical synthesis allows to reach the necessary functional properties by means of varying the chemical composition of the coating. The results of thermo-gravimetric research of the carbonaceous composite material with anti-oxidant coating are given. The prospects of obtaining the high-temperature coating by high-temperature synthesis method on carbonaceous composite materials are shown. The work is executed within implementation of the complex scientific direction 14.1. «Constructional ceramic composite materials (ССM)» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: high-temperature chemical synthesis, carbonaceous composite material, anti-oxidant coating.

Reference List

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    7. Solntsev S.S., Shalin R.E., Isaeva N.V. Reakcionnospekaemye keramicheskie pokrytiya [Reactionary sintered ceramic coatings] // Sb. tr. 8-j Vsemir. konf. po keramike i novym materialam. 1995. T. 9. S. 237–242.

    8. Solntsev S.S., Isaeva N.V., Shvagireva V.V., Maksimov V.I. Vysokotemperaturnye pokrytiya dlya zashhity splavov i uglerodkeramicheskih kompozicionnyh materialov ot okisleniya [High temperature coatings for protection of alloys and carbon ceramic composite materials from oxidation] // Konversiya v mashinostroenii. 2004. №4. S. 77–80.

    9. Solntsev S.S., Shvagireva V.V., Isaeva N.V., Soloveva G.A. Zharostojkoe pokrytie dlya zashhity vysokoprochnyh slozhnolegirovannyh nikelevyh splavov ot vysokotemperaturnoj gazovoj korrozii [High temperature coating for protection of high-strength complex alloyed of nickel alloys of high-temperature gas corrosion] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №6. St. 04. Available at: http://www.viam-works.ru (accessed: September 18, 2015). DOI: 10.18577/2307-6046-2014-0-6-4-4.

    10. Solntsev S.S., Rozenenkova V.A., Mironova N.A., Soloveva G.A. Vysokotemperaturnye pokrytiya dlya voloknistyh substratov [High-temperature coatings for fibers substratum] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №10. St. 03. Available at: http://www.viam-works.ru (accessed: September 18, 2015).

    11. Solntsev S.St., Shvagireva V.V., Isaeva N.V., Soloveva G.A. Mnogocelevoe stekloemalevoe pokrytie dlya zashhity lityh fasonnyh detalej gazoturbinnyh dvigatelej [Multipurpose glass-enamel coating for protection of cast parts of gas turbine engines] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №3. St. 04. Available at: http://www.viam-works.ru (accessed: September 18, 2015). DOI: 10.18577/2307-6046-2014-0-3-4-4.

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

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

    14. Sorokin O.Yu., Solntsev S.St., Evdokimov S.A., Osin I.V. Metod gibridnogo iskrovogo plazmennogo spekaniya: princip, vozmozhnosti, perspektivy primeneniya [Hybrid spark plasma sintering method: principle, possibilities, future prospects] // Aviacionnye materialy i tehnologii. 2014. №S6. S. 11–16.

    15. Solntsev S.S., Rozenenkova V.A., Mironova N.A., Gavrilov S.V. Keramicheskie pokrytiya dlya zashhity vysokoprochnoj stali pri termicheskoj obrabotke [Ceramic coatings for protection of high-strength steel at thermal processing] // Aviacionnye materialy i tehnologii. 2011. №4. S. 3–8.

    16. Grashhenkov D.V., Solncev S.St., Shhegoleva N.E., Naumova A.S., Gaponov B.N. Steklokeramicheskij kompozicionnyj material [Glass-ceramic composite material] // Aviacionnye materialy i tehnologii. 2012. №S. S. 368–372.

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    18. Yao X.Y., Li H.J., Zhang Y.L., Wu H., Qiang X.F. A SiC–Si–ZrB2 multiphase oxidation protective ceramic coating for SiC-coated carbon/carbon composites // Ceram. Int. 2012. V. 38. P. 2095–2100.

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12.

DOI: 10.18577/2071-9140-2016-0-3-88-94

UDC: 620.179

Pages:: 88-94

E.I. Kosarina1, A.V. Stepanov2, A.A. Demidov1, O.A. Krupnina1

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

Sensitometer for technical radiographic films

This article is devoted to sensitometry of technical radiographic films. Features of the interaction of X-rays with microcrystals in the emulsion layer in contrast to the interaction of radiation in the optical range are shown. Variants of the emulsion film exposure are discussed so that the duration of exposure and the results of absorbance measurements obtained with the X-ray sensitometer, one can construct a characteristic curve of a radiographic film. The parameters of the two variants of Sensitometer with translational and rotational movement are calculated. The possibility of construction of the characteristic curves for different values of X-ray tube voltage is determined. It is possible to determine the relationship between mean gradient, sensitivity, resolution and the x-ray energy. The work is executed within implementation of the complex scientific direction 2.3. «Methods of nondestructive researches and control» («The strategic directions of development of materials and their processing technologies for the period till 2030»

Keywords: technical radiographic film, sensitometer, optical density, exposure dose of radiation, characteristic curve, mean gradient, sensitivity to radiation, resolution, spectral properties.

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

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

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

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

    6. Gorohovskij Yu.N., Levenberg T.M. Obshhaya sensitometriya. Teoriya i praktika [General sensitometry. Theory and practice]. M.: Iskusstvo, 1963. 302 s.

    7. Gorohovskij Yu.N., Baranova V.P. Svojstva cherno-belyh fotograficheskih plenok [Properties of black-and-white photographic films]. M.: Nauka, 1970. 388 s.

    8. Gorohovskij Yu.N. Spektralnye issledovaniya fotograficheskogo processa [Spectral researches of photographic process]. M.: Fizmatgiz, 1960. 391 s.

    9. Dzhejms T. Teoriya fotograficheskogo processa: per. s angl. [Theory of photographic process: trans. from English]. L.: Himiya, 1973. 672 s.

    10. Stepanov A.V., Kosarina E.I., Savvina N.A. Trebovaniya k rentgenovskomu kontrolyu i kachestvu rentgenograficheskih snimkov v evropejskih normah i rossijskih standartah [Requirements to x-ray control and quality of radiographic pictures in the European norms and the Russian standards] // Vestnik MEI. 2011. №4. S. 85–90.

    11. Stepanov A.V., Kosarina E.I., Savvina N.A. Razrabotka metodiki po ispytaniyu radiograficheskih plenok s cel\'yu opredeleniya celesoobraznosti ih primeneniya v defektoskopii [Development of technique on testing of radiographic films for the purpose of determination of expediency of their application in defect’s scope] // Kontrol. Diagnostika. 2011. №12. S. 65–67.

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

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

    14. Dobromyslov V.A. Radiacionnye metody nerazrushayushhego kontrolya [Radiation methods of non-destructive testing]. M.: Mashinostroenie, 1999. 104 s.

    15. Klyuev V.V., Sosnin F.R. Teoriya i praktika radiacionnogo kontrolya: ucheb. posobie [Theory and practice of radiation monitoring: manual]. M.: Mashinostroenie, 1998. 170 s.

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

    17. BS EN 584-1:2006. Nerazrushayushhij kontrol. Promyshlennaya radiograficheskaya plenka. Chast 1. Klassifikaciya plenochnyh sistem dlya promyshlennogo radiograficheskogo kontrolya [Non-destructive testing. Industrial radiographic film. Part 1. Classification of film systems for industrial radiographic control.].

    18. BS EN 584-2. Nerazrushayushhij kontrol. Plenka dlya promyshlennogo radiograficheskogo kontrolya. Chast 2. Kontrol za proyavleniem plenki s pomoshh\'yu etalonnyh znachenij [Non-destructive testing. Film for industrial radiographic control. Part 2. Control of film manifestation by means of reference values.]

    19. Zernov V.A. Fotograficheskaya sensitometriya [Photographic sensitometry]. M.: Iskusstvo, 1980. 

    351 s.

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