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Aviation materials and technologies №4, 2013

Contents

  • D.K. Ryabov, N.I. Kolobnev

    Evolution of mechanical properties of 1913 aluminium alloy during two-stage aging

    3-7
  • A.L. Yakovlev, N.A. Nochovnaya

    Effect of heat treatment on properties of sheets of high-strength titanium alloy VT23M

    8-13
  • E.G. Arginbaeva, O.A. Bazyleva

    The research the structure, physical and mechanical properties of the intermetallic nickel alloys

    14-19
  • P.G. Min, V.V. Sidorov

    The experience of GS32-VI alloy scrap recycling at the VIAM scientific and production complex for cast bars production

    20-25
  • D.P. Farafonov, V.P. Migunov

    Manufacturing of porous fibrous material of ultralow density for sound-proof designs of aircraft engines

    26-30
  • A.G. Krynin, J.A. Khokhlov

    Optical performances thermostabilised polyethyleneterephtalate film used for the functional materials of a glass cover

    31-34
  • E.A. Ponomareva, T.V. Jakovenko

    Influence of preparations with nanoparticle of silver on properties of textile materials

    35-38
  • N.I. Nefyodov, L.V. Semyonova

    The application of paint and varnish coatings by method «crude on crude»

    39-42
  • D.A. Chubarov, P.V. Matveev

    New ceramic materials for thermal barrier coatings using in GTE turbine blades

    43-46
  • V.A. Bol’shakov, V.M. Aleksashin

    A way to increase the residual compression strength after low-speed impact of cfrps produced by vacuum infusion technology

    47-50
  • O.V. Kuzmin, E.A. Tikhomirova, M.Yu. Sundukov, T.N. Azizov, E.F. Sidokhin

    A new thermo-cyclic testing method to measure thermal fatigue resistance of materials in aeronautical engineering

    51-53
  • V.D. Krylov

    Test methods and features of fracture of thin-sheet materials

    54-57
  • D.S. Lozhkova, M.A. Dalin

    The measure of FBH’s parameters, which is using for equipment set-up for inspection of the pulsation absorber diaphragm

    58-61
  • V.V. Shirokov, A.M. Romanov

    Waveguide method research of honeycomb glass fibre plastics dielectric characteristics

    62-68
Содержание номера
1.

DOI:

UDC: 669.715

Pages:: 3-7

D.K. Ryabov1, N.I. Kolobnev2

[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» of National Research Center «Kurchatov Institute», admin@viam.ru

Evolution of mechanical properties of 1913 aluminium alloy during two-stage aging

Al–Zn–Mg and Al–Zn–Mg–Cu are heat treatment alloys. By applying different types of quenching and artificial aging it is possible to vary mechanical and corrosion properties in semi-products. It is reasonable to apply multistage aging that allows to intensify decomposition of solid solution to receiving the best complex of characteristics and to achieve improved characteristics of durability with high corrosion resistance. The results of study of evolution of mechanical properties of cold-rolled sheets of Russian corrosion resistant 1913 alloy (alloyed with small addition of Cu) during two-staged aging are introduced. The short assessment of expediency of a choice of temperature of the first and second steps of a step of aging is given.

Keywords: 1913 alloy, multi-stage aging, strength, heat treatment, Al–Zn–Mg

Reference List

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    10. Ying Deng, Zhimin Yin, Kai Zhao, Jiaqi Duan, Jian Hu, Zhenbo He. Effects of Sc and Zr microalloying additions and aging time at 120°C on the corrosion behaviour of an Al–Zn–Mg alloy //Corrosion Science. 2012. V. 65. R. 288–298.

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    19. Ling-Mei Wu, Seyring M., Rettenmayr M., Wen-Hsiung Wang. Characterization of precipitate evolution in an artificially aged Al–Zn–Mg–Sc–Zr alloy //Materials Science and Engineering A. 2010. V. 527. R. 1068–1073.

     

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2.

DOI:

UDC: 621.78:669.295

Pages:: 8-13

A.L. Yakovlev1, N.A. Nochovnaya1

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

Effect of heat treatment on properties of sheets of high-strength titanium alloy VT23M

The influence of heat treatment and thickness parameters on the properties of sheets of high-strength titanium alloy VT23M have been considered. The mechanical tests for the properties determination (UTS, EL) have been carried out in longitudinal and transverse directions. There have been selected the optimal heat treatment modes of thin sheets. Micro-/macrostructure analysis as well as XRD analysis have been also accomplished. The obtained results allowed to determine the effect of sheets thickness on the properties in longitudinal and transverse directions.

Keywords: titanium alloy VT23M, heat treatment, longitudinal direction, transverse direction, VTMO, annealing, ageing, sheet, ultimate tensile strength

Reference List

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    6. Antipov V.V. Strategija razvitija titanovyh, magnievyh, berillievyh i aljuminievyh splavov [Strategy of development of titanic, magnesian, beryllium and aluminum alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 157−167.

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    8. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [The strategic directions of development of materials and technologies of their processing for the period till 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7−17.

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    11. Il'in A.A., Kolachev B.A., Pol'kin I.S. Titanovye splavy. Sostav, struktura, svojstva [Titanic alloys. Composition, structure, properties]: Spravochnik. M.: VILS–MATI. 2009. 520 s.

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    13. Logachev I.A., Razumovskij V.I., Razumovskij I.M., Kosyrev K.L., Logacheva A.I. Razrabotka teoreticheskoj procedury ocenki sbalansirovannosti himicheskogo sostava zharoprochnogo titanovogo splava novogo pokolenija i sozdanie na jetoj osnove metodiki optimizacii sostavov titanovyh splavov [Development of theoretical procedure of an assessment of balance of a chemical composition of a heat resisting titanic alloy of new generation and creation on this basis of a technique of optimization of structures of titanic alloys] //Titan. 2012. №4 (38). S. 27−32.

    14. Horev A.I. Osnovnye nauchnye i prakticheskie napravlenija povyshenija stabil'nosti mehanicheskih svojstv (α+β)-titanovyh splavov vysokoj i sverhvysokoj prochnosti [The main scientific and practical directions of increase of stability of mechanical properties (α+β)-titanium alloys of high and ultrahigh durability] /V sb. Ti−2010 v SNG. Ekate-rinburg. 2010. S. 227−235.

    15. Horev A.I. Razrabotka teoreticheskih i prakticheskih osnov povyshenija konstrukcionnoj prochnosti titanovyh splavov putem kompleksnogo legirovanija i mikrolegirovanija [Development of theoretical and practical bases of increase of constructional durability of titanic alloys by a complex alloying and a microalloying] /V sb. Ti–2007 v SNG. Jalta. 2007. S. 226−234.

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    17. Horev A.I., Nochovnaja N.A., Jakovlev A.L. Mikrolegirovanie redkozemel'nymi metallami titanovyh splavov [Microalloying rare-earth metals of titanic alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 206−212.

     

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3.

DOI:

UDC: 621.74:669.018.44

Pages:: 14-19

E.G. Arginbaeva1, O.A. Bazyleva1

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

The research the structure, physical and mechanical properties of the intermetallic nickel alloys

Results of research of strength properties anisotropy and microstructure of single-crystal intermetallic alloys VKNA-1V and VKNA-25 with different crystallographic orientations, are described. Of interest are the comparative research intermetallic alloys – low alloyed high-temperature VKNA-1V, with working temperatures up to 1250°C and heat-resisting rhenium-containing VKNA-25 with working temperatures up to 1200°C. It is established that the choice of crystallographic orientation due to working conditions of specific engine parts. Thus, the designer can choose as the material as its production technology, which would provide optimum physical and mechanical properties. The replacement standard superalloys by intermetallic nickel alloys with low-density series VKNA will increase working temperature at 50–100°C and weight engine efficiency, reduce emissions of CО х, NO х, as well as reduce the cost of batch ingots on 25–30%.

Keywords: VKNA, single-crystal bars, crystallographic orientation, microstructure, intermetallic compound Ni3Al, elastic modulus, high-temperature strength

Reference List

    1. Skibin V.A. Nauchnyj vklad v sozdanie aviacionnyh dvigatelej [Scientific contribution to creation of aviation engines]. M.: Mashinostroenie. 2000. T. 2. 750 s.

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

    3. Bazyleva O.A., Arginbaeva Je.G., Turenko E.Ju. Intermetallidnye splavy na osnove Ni3Al [Intermetallic alloys on the basis of Ni3Al] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. №5. S. 27–29.

    4. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlja vysokoteplo-nagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for high-heat – the loaded details of gas-turbine engines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №2. S. 13–19.

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

    6. Kablov E.N., Bondarenko Ju.A., Kablov D.E. Osobennosti struktury i zharoprochnyh svojstv monokristallov <001> vysokorenievogo nikelevogo zharoprochnogo splava, poluchennogo v uslovijah vysokogradientnoj napravlennoj kristallizacii [Features of structure and heat-resisting properties of monocrystals of <001> high-rhenium nickel heat-resisting alloys received in the conditions of high-gradient directed crystallization] //Aviacionnye materialy i tehnologii. 2011. №4. S. 25–31.

    7. Kablov E.N., Bondarenko Ju.A., Echin A.B., Surova V.A. Razvitie processa napravlen-noj kristallizacii lopatok GTD iz zharoprochnyh splavov s monokristallicheskoj i kompozicionnoj strukturoj [Development of process of the directed crystallization of shovels of GTD from heat-resisting alloys with single-crystal and composite structure] //Aviacionnye materialy i tehnologii. 2012. №1. S. 3–8.

    8. Bondarenko Ju.A., Bazyleva O.A., Echin A.B., Surova V.A., Narskij A.R. Vysokogradientnaja napravlennaja kristallizacija detalej iz splava VKNA-1V [The high-gradient directed crystallization of details from VKNA-1V alloy] //Litejnoe proizvodstvo. 2012. №6. S. 12–16.

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    11. Badamshin I.H. Prochnost' jelementov konstrukcij iz jevtekticheskih  kompozitov na osnove jelektrostaticheskoj prirody uprugosti [Strength of structural elements from the eutectic composites on the basis of the electrostatic nature of elasticity]: Avtoref. dis. d.t.n. 2010. 35 s.

    12. Bazyleva O.A., Bondarenko Ju.A., Timofeeva O.B., Hvackij K.K. Vlijanie kristallo-graficheskoj orientacii na strukturu i fiziko-mehanicheskie svojstva intermetallidnogo splava VKNA-1V [Influence of crystallographic orientation on structure and physicomechanical properties of an intermetallic alloy of VKNA-1V] //Metallurgija mashinostroenija. 2012. №4. S. 8–12.

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    14. Golubovskij E.R., Svetlov I.L. Temperaturno-vremennaja zavisimost' anizotropii harakteristik dlitel'noj prochnosti monokristallov nikelevyh zharoprochnyh splavov [Temperature and time dependence of anisotropy of characteristics of long durability of monocrystals of nickel heat resisting alloys] //Problemy prochnosti. 2002. №2. S. 5–19.

     

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4.

DOI:

UDC: 669.018.44:669.245

Pages:: 20-25

P.G. Min1, V.V. Sidorov1

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

The experience of GS32-VI alloy scrap recycling at the VIAM scientific and production complex for cast bars production

In VIAM was developed the resource-saving technology of refining remelting in vacuum induction furnaces of all formed scraps which allows to receive from 100% scraps the alloys completely answering on purity and properties the requirements of active specification. The given technology enables to save an expensive and deficient alloying metals and toreduce alloys costs on 30–50% without decreasing their quality. There was demonstrated the negative influencing of silicon on alloy GS32-VI.

Keywords: silicon, scrap, superalloys, vacuum induction furnace, bar stock, single crystal, structure

Reference List

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    6. Kablov D.E., Sidorov V.V., Min P.G. Vlijanie primesi azota na strukturu monokristallov zharoprochnogo nikelevogo splava ZhS30-VI i razrabotka jeffektivnyh sposobov ego rafinirovanija [Influence of impurity of nitrogen on structure of monocrystals of a heat resisting nickel alloy of ZhS30-VI and development of effective ways of its refinement] //Aviacionnye materialy i tehnologii. 2012. №2. S. 32–36.

    7. Kablov D.E., Sidorov V.V., Gerasimov V.V., Simonov V.N., Min P.G. Issledovanie zakonomernostej povedenija azota pri poluchenii monokristallov zharoprochnogo nikelevogo splava ZhS30-VI [Research of regularities of behavior of nitrogen when receiving monocrystals of a heat resisting nickel alloy of ZhS30-VI] //Nauka i obrazovanie: jelektronnoe nauchno-tehnicheskoe izdanie.

    8. Sidorov V.V. Metallurgija litejnyh zharoprochnyh splavov [Metallurgy of foundry heat-resisting alloys] /V sb. Litye lopatki gazoturbinnyh dvigatelej (splavy, tehnologii, pokrytija). M.: Nauka. 2006. S. 119–186.

    9. Kablov E.N., Sidorov V.V., Rigin V.E. Metallurgija litejnyh zharoprochnyh splavov [Metallurgy of foundry heat-resisting alloys] /V sb. Aviacionnye materialy. Izbrannye trudy 1932–2007: Jubilejnyj nauch.-tehnich. sb. M.: VIAM. 2007. S. 125–132.

    10. Kablov E.N., Ospennikova O.G., Sidorov V.V., Rigin V.E., Kablov D.E. Osobennosti tehnologii vyplavki i razlivki sovremennyh litejnyh vysokozharoprochnyh nikelevyh splavov [Features of technology of smelting and pouring of modern foundry high-heat resisting nickel alloys] //Vestnik MGTU im. N.Je. Baumana. Ser. Mashinostroenie. Spec. vyp. Perspektivnye konstrukcionnye materialy i tehnologii. 2011. S. 68–78.

    11. Kablov E.N., Ospennikova O.G., Sidorov V.V., Rigin V.E. Proizvodstvo lityh prutkovyh (shihtovyh) zagotovok iz sovremennyh litejnyh vysokozharoprochnyh nikelevyh splavov [Production cast the bar stock (charge billets) from modern foundry high-heat resisting nickel alloys] /V sb. Trudy nauch.-tehnich. konf. Problemy i perspektivy razvitija metallurgii i mashinostroenija s ispol'zovaniem zavershennyh fundamental'nyh issledovanij. 2011. S. 31–38.

    12. Sidorov V.V., Rigin V.E., Gorjunov A.V., Kablov D.E. Vysokojeffektivnye tehnologii i sovremennoe oborudovanie dlja proizvodstva shihtovyh zagotovok iz litejnyh zharoprochnyh splavov [Highly effective technologies and the modern equipment for production the charge billets from foundry heat resisting alloys] //Metallurg. 2012. №5. S. 26–30.

    13. Sidorov V.V., Rigin V.E., Kablov D.E. Organizacija proizvodstva lityh prutkovyh zagotovok iz sovremennyh litejnyh vysokozharoprochnyh nikelevyh splavov [The organization of production cast the bar stock from modern foundry high-heat resisting nickel alloys] //Litejnoe proizvodstvo. 2011. №10. S. 2–6.

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

     

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5.

DOI:

UDC: 678.6

Pages:: 26-30

D.P. Farafonov1, V.P. Migunov2

[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»

Manufacturing of porous fibrous material of ultralow density for sound-proof designs of aircraft engines

In article experience of manufacturing of porous fibrous material from metal fibers with use technology of receiving fibers by method of extraction of hanging drop of melt (EHDM) is provided. The received material is characterized by the low specific weight, high acoustic effectiveness and the service properties necessary for its application as filler of sound absorbing structures (SAS) of aviation gas turbine engines (GTE).

Keywords: porous-fibrous metal material, sound absorbing structures, gas turbine engine

Reference List

    1. Sobolev A.F. Polujempiricheskaja teorija odnoslojnyh sotovyh zvukopogloshhajushhih konstrukcij s licevoj perforirovannoj panel'ju [Semiempirical theory of single-layer cellular sound-absorbing designs with the front punched panel] //Akusticheskij zhurnal. 2007. T. 53. №6. S. 861–872.

    2. Sobolev A.F., Ushakov V.G., Filippova R.D. Zvukopogloshhajushhie konstrukcii gomogennogo tipa dlja kanalov aviacionnyh dvigatelej [Sound-absorbing designs of homogeneous type for channels of aviation engines] //Akusticheskij zhurnal. 2009. T. 55. №6. S. 749–759.

    3. Haleckij Ju.D. Jeffektivnost' kombinirovannyh glushitelej shuma aviacionnyh dvigatelej [Effectiveness of the combined mufflers of noise of aviation engines] //Akusticheskij zhurnal. 2012. T. 58. №4. S. 556–562.

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

    5. Migunov V.P., Farafonov D.P. Issledovanie osnovnyh jekspluatacionnyh svojstv novogo klassa uplotnitel'nyh materialov dlja protochnogo trakta GTD [Research of the main operational properties of a new class of sealing materials for a flowing path of GTD] //Aviacionnye materialy i tehnologii. 2011. №3. S. 15–20.

    6. Migunov V.P., Lomberg B.S. Poristovoloknistye metallicheskie materialy dlja zvukopogloshhajushhih i uplotnitel'nyh konstrukcij [Porous-fibrous metal materials for sound-absorbing and sealing designs] /V sb.: 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: Jubilejnyj nauch.-tehnich. sb. M.: VIAM. 2007. S. 270–275.

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

    8. Borisov B.V. Razrabotka tehnologii poluchenija volokon i poristyh materialov iz zharostojkih splavov metodom jekstrakcii visjashhej kapli rasplava [Development of technology of receiving fibers and porous materials from heat-resistant alloys a method of extraction of a hanging drop of fusion]: Avtoref. dis. k.t.n. M.: MATI–RGTU im. K.Je. Ciolkovskogo. 2011. 19 s.

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

    10. Zhengping X., Jilei Z., Huiping T., Qingbo A., Hao Z., Jianyong W., Cheng L. Progress of application researches of porous fiber metals //Materials. 2011. №4. R. 816–824.

    11. Antipov V.V. Strategija razvitija titanovyh, magnievyh, berillievyh i aljuminievyh splavov [Strategy of development of titanic, magnesian, beryllium and aluminum alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 157–167.

    12. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [The strategic directions of development of materials and technologies of their processing for the period till 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

     

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6.

DOI:

UDC: 666.162:629.12.011.83

Pages:: 31-34

A.G. Krynin1, J.A. Khokhlov2

[1] Technoinfo ltd
[2] ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS, admin@viam.ru

Optical performances thermostabilised polyethyleneterephtalate film used for the functional materials of a glass cover

The optical properties of thermally stabilized polyethylene terephthalate (PETP) films of different thickness (75 and 125 microns). The calculations of the optical constants with and without interference effects. The optical constants thermostabilized PETP film in the visible and near infrared region of the spectrum (λ=0,4–20 μm).

Keywords: polyethyleneterephthalate, optical constants, transmittance, reflectivity

Reference List

    1. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [Strategical Areas of Developing Materials and Their Processing Technologies for the Period up to 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

    2. Grashhenkov D.V., Chursova L.V. Strategija razvitija kompozicionnyh i funkcional'nyh materialov [Development Strategics of Composite and Functional Materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 231–241.

    3. Rabotkin S.V., Solov'ev A.A., Sochugov N.S., Zaharov A.N., Oskomov K.V., Kovsharov N.F. Polimernaja plenka s nizkojemissionnym pokrytiem dlja snizhenija poter' cherez svetoprozrachnye konstrukcii [Polymeric film with a low-issue covering for decrease in losses through translucent designs] //Izv. vuzov. Ser. Fizika. 2011. T. 54. №11–12. S. 169–175.

    4. Bogatov V.A., Kondrashov S.V., Hohlov Ju.A. Mnogofunkcional'nye opticheskie pokrytija i materialy [Multifunctional optical coatings and materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 343–348.

    5. Berning P.H. Teorija i metody rascheta opticheskih svojstv tonkih plenok [Theory and methods of calculation of optical properties thin films/physics of thin films] /Fizika tonkih plenok. T. 1 /Pod red. G. Hassa. M.: Mir. 1967. 856 s.

    6. Furman Sh.A. Tonkoslojnye opticheskie pokrytija [Thin layer optical coverings]. L.: Mashinostroenie. 1977. 264 s.

    7. Kazuki T., Hiromi H., Yasusei Y., Masahisa O., Kazuki Y. Electrochromic switchable mirror foil with tantalum oxide thin film prepared by reactive DC magnetron sputtering in hydrogen-containing gas //Surface & Coatings Technology. 2011. V. 205. P. 3956–3960.

    8. Tajima K., Yamada Y., Bao S., Okada M., Yoshimura K. //Surface & Coatings Technology. 2008. V. 202. R. 5630–5633.

    9. Agnihotri O., Gupta B. Selektivnye poverhnosti solnechnyh ustanovok [Selective surfaces of solar installations]: Per. s angl. M.: Mir. 1984. 280 s.

    10. Hohlov Ju.A., Krynin A.G., Bogatov V.A., Kisljakov P.P. Opticheskie konstanty tonkih plenok oksida indija, legirovannogo olovom, osazhdennyh na polijetilentereftalatnuju plenku metodom reaktivnogo magnetronnogo raspylenija (blizhnjaja infrakrasnaja oblast' spektra) [Optical Constants of Thin Indium Oxide Films, Alloyed by Tin and Deposited onto Polyethylene Terephthalate Film by the Reactive Magnetron Sputtering Method (Spectrum Infrared Short-Range Region)] //Aviacionnye materialy i tehnologii. 2013. №1. S. 24–28.

    11. Bogatov V.A., Zaharov C.S., Kisljakov P.P., Krynin A.G., Hohlov Ju.A. Vlijanie rezhimov magnetronnogo napylenija na optiko-fizicheskie svojstva mednyh nanopokrytij [Influence of modes of a magnetron dusting on optiko-physical properties of copper nanocoverings] //Nanotehnologii i nanomaterialy. 2011. №4. S. 45–54. 

    12. Bogatov V.A., Kondrashov S.V., Hohlov Ju.A. Poluchenie gradientnogo pokrytija oksinitrida aljuminija metodom reaktivnogo magnetronnogo raspylenija [Application of gradient aluminium oxynitride coating by the reactive magnetron sputtering method] //Aviacionnye materialy i tehnologii. 2010. №3. S. 19–21. 

    13. Lau K., Weber J., Bartzsch H., Frach P. Reactive pulse magnetron sputtered SiOxNy coatings on polymers //Thin Solid Films. 2009. V. 517. P. 3110–3114.

    14. Kerstin Taeschner, Hagen Bartzsch, Peter Frach, Eberhard Schultheiss. Scratch resistant optical coatings on polymers by magnetron-plasma-enhanced chemical vapor deposition //Thin Solid Films. 2012. V. 520. P. 4150–4154.

    15. Bogatov V.A., Hohlov Ju.A., Sytyj Ju.V., Zhadova N.S. Vlijanie obrabotki v razrjade s zamknutym drejfom jelektronov na adgezionnye svojstva i prochnost' kleevyh soedinenij polimerov [Processing influence in the category with the closed drift of electrons on adhesive properties and durability of glue compounds of polymers]//Klei. Germetiki. Tehnologii. 2011. №9. S. 27–31.

     

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7.

DOI:

UDC: 677.017

Pages:: 35-38

E.A. Ponomareva1, T.V. Jakovenko1

[1] ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS, admin@viam.ru

Influence of preparations with nanoparticle of silver on properties of textile materials

Influence of preparations with nanoparticles of silver on microbiological and physicomechanical properties of textile materials is investigated. Also the preliminary choice of ways of their protection from microbiological defeat is made.

Keywords: technical fabrics, cellulose materials, synthetic fibres, nanoparticles of silver, biocide preparations, bio-destruction, impregnation, aerosol application, magnetron sputtering, fungus resistance, thermal ageing

Reference List

    1. Semenov S.A., Gumargalieva K.Z., Zaikov G.E. Biopovrezhdenija materialov i izdelij tehniki. Gorenie, destrukcija i stabilizacija polimerov [Biodamages of materials and equipment products. Burning, destruction and stabilization of polymers]. SPb.: Nauchnye osnovy i tehnologii. 2008. S. 73–99.

    2. Kozinda Z.Ju., Gorbacheva I.N., Suvorova E.G. Metody poluchenija tekstil'nyh materialov so special'nymi svojstvami (antimikrobnymi i ognezashhitnymi) [Methods of receiving textile materials with special properties (antimicrobic and fireproof)]. M.: Legprombytizdat. 2008. 112 s.

    3. Sadova S. Polimernye preparaty dlja tekstil'noj promyshlennosti [Polymeric preparations for the textile industry] //Bar'er bezopasnosti. 2012. №1. S. 87–89. 

    4. Gagarin M.V., Baranov D.E., Turchenkov V.A. Modelirovanie pronicaemosti nanokompozitov [Modeling of permeability of nanocomposites] //Aviacionnye materialy i tehnologii. 2012. №3. S. 36–39.

    5. Krutjakov Ju.A., Kudrinskij A.A., Olenin A.Ju., Lisichkin G.V. Sintez i svojstva nanochastic serebra: dostizhenija i perspektivy [Synthesis and properties of nanoparticles of silver: achievements and prospects] //Uspehi himii. 2008. T. 77. №3. S. 211–315.

    6. Mekalina I.V., Sentjurin E.G., Klimova S.F., Bogatov V.A. Novye «serebrostojkie» organichekie stekla [New «silver-resistent» organic glasses] //Aviacionnye materialy i tehnologii. 2012. №4. S. 45–48.

    7. Lisiecki I., Pileni P. //Amer. Chem. Soc. 1993. V. 115. P. 3887–3896.

    8. Parsons H.L. //J. of Society Dyers and Colourists. 1970. V. 86. №12. S. 504–512.

    9. Muhametov R.R., Ahmadieva K.R., Chursova L.V., Kogan D.I. Novye polimernye svjazujushhie dlja perspektivnyh metodov izgotovlenija konstrukcionnyh voloknistyh PKM [New polymeric binding for perspective methods of production of constructional fibrous PKM] //Aviacionnye materialy i tehnologii. 2011. №2. S. 38–42.

    10. Kalontarov I.Ja., Liverant I.V. Pridanie tekstil'nym materialam biocidnyh svojstv i ustojchivosti k mikroorganizmam [Giving to textile materials of biocidal properties and resistance to microorganisms]. Dushanbe: Donish. 2011. 98 s.

    11. Gunjaev G.M., Chursova L.V., Komarova O.A., Gunjaeva A.G. Konstrukcionnye ugleplastiki, modificirovannye nanochasticami [The constructional coal plastics modified by nanoparticles] //Aviacionnye materialy i tehnologii. 2012. №S. S. 277–286.

    12. Ponomarev A.N. //Nanotehnologija i nanokonstrukcija. 2012. №1. S. 12–17.

     

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8.

DOI:

UDC: 667.6

Pages:: 39-42

N.I. Nefyodov1, L.V. Semyonova2

[1] ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS, admin@viam.ru
[2] Limited Liability corporation «Aviation equipment and materials»

The application of paint and varnish coatings by method «crude on crude»

In the present-day world of the requirement to paint and varnish materials steadily increase as concerning increase of their quality, expansion of the range, and regarding improvement of technology of their application. One of technological ways of decrease in expenses is coatings deposition by method «crude on crude». In a basis of a method formation of system of coatings when deposition the subsequent layers of paint and varnish materials on underdried previous layers is necessary. Properties of systems of paint and varnish coatings in a combination with various primers are investigated.

Keywords: paint and varnish materials, painting procedure, coatings, adhesion, permeability, aviation materials

Reference List

    1. Chebotarevskij V.V., Kondrashov Je.K. Tehnologija lakokrasochnyh pokrytij v mashinostroenii [Teсhnology of paint and varnish coverings in mechanical engineering]. M.: Mashinostroenie 1978. 295 s.

    2. Kondrashov Je.K., Kuznecova V.A., Semenova L.V., Lebedeva T.A., Malova N.E. Razvitie aviacionnyh lakokrasochnyh materialov [Development of aviation paintwork materials] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. №5. S. 49–54.

    3. Istorija aviacionnogo materialovedenija: VIAM – 75 let poiska, tvorchestva, otkrytij [History of aviation materials science: VIAM – 75 years of search, creativity, opening] /Pod obshh. red. E.N. Kablova. M.: Nauka. 2007. S. 152–158.

    4. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [The strategic directions of development of materials and technologies of their processing for the period till 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

    5. Semenova L.V., Malova N.E., Kuznecova V.A., Pozhoga A.A. Lakokrasochnye materialy i pokrytija [Paintwork materials and coverings] //Aviacionnye materialy i tehnologii. 2012. №S. S. 315–327.

    6. Kondrashov Je.K., Kuznecova V.A., Semenova L.V., Lebedeva T.A. Osnovnye napravlenija povyshenija jekspluatacionnyh, tehnologicheskih i jekologicheskih harakteristik lakokrasochnyh pokrytij dlja aviacionnoj tehniki [The main directions of increase of operational, technical and ecological characteristics on paint and varnish coverings for the aircraft equipment] //Rossijskij himicheskij zhurnal. 2010. T. LIV. №1. S. 96–102.

    7. Bejder Je.Ja., Donskoj A.A., Zhelezina G.F., Kondrashov Je.K., Sytyj Ju.V., Surnin E.G. Opyt primenenija ftorpolimernyh materialov v aviacionnoj tehnike [Experience of application of polymericfluorine materials in the aircraft equipment] //Rossijskij himicheskij zhurnal. 2008. T. LII. №3. S. 30–44.

    8. Kondrashov Je.K., Kozlova A.A., Malova N.E. Issledovanie kinetiki otverzhdenija ftorpoliuretanovyh jemalej alifaticheskimi poliizocianatami razlichnyh tipov [Research of kinetics of an curing fluoro-polyuretane enamels aliphatic polyisocyanates of various types] //Aviacionnye materialy i tehnologii. 2013. №1. S. 48–49.

    9. Buznik V.M. Sverhgidrofobnye materialy na osnove ftorpolimerov [Superhydrophobic materials on the basis of fluoropolimer] //Aviacionnye materialy i tehnologii. 2013. №1. S. 29–34.

    10. Semenova L.V., Kondrashov Je.K. Modificirovannyj bromjepoksidnyj lak VL-18 dlja zashhity polimernyh kompozicionnyh materialov [The modified bromine-epoxy varnish of VL-18 for protection of polymeric composite materials] //Aviacionnye materialy i tehnologii. 2010. №1. S. 29–32.

    11. Kondrashov Je.K. Sverhtonkie vzaimodejstvija i diffuzija v polimerah [Superthin interactions and diffusion in polymers]. M.: Sputnik. 2004. 77 s.

    12. Nefedov N.I., Semenova L.V. Tendencii razvitija v oblasti konformnyh pokrytij dlja vlagozashhity i jelektroizoljacii plat pechatnogo montazha i jelementov radio-jelektronnoj apparatury [Development tendencies in the field of conformal coverings for moisture protection and electrical insulation of payments of printed circuit wiring and elements of the radio-electronic equipment] //Aviacionnye materialy i tehnologii. 2013. №1. S. 50–52.

    13. Grashhenkov D.V., Chursova L.V. Strategija razvitija kompozicionnyh i funkcional'nyh materialov [Strategy of development of composite and functional materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 231–242.

    14. Semenova L.V., Rodina N.D., Nefedov N.I. Vlijanie sherohovatosti sistem lakokrasochnyh pokrytij na jekspluatacionnye svojstva samoletov [Influence of a roughness of systems of paint and varnish coverings on operational properties of planes] //Aviacionnye materialy i tehnologii. 2013. №2. S. 37–40.

     

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9.

DOI:

UDC: 678.84

Pages:: 43-46

D.A. Chubarov1, P.V. Matveev2

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

New ceramic materials for thermal barrier coatings using in GTE turbine blades

The ceramic materials using in thermal barrier coatings (TBC) for GTE turbine blades was investigated. The compositions and characteristics of new ceramic layers based on zirconium, hafnium or cerium, doped with one or more rare earth elements and perspective of their using in developing new generation TBC are also discussed.

Keywords: thermal barrier coating (TBC), YSZ, gas turbine engine

Reference List

    1. Budinovskij S.A., Mubojadzhjan S.A., Gajamov A.M. Sovremennoe sostojanie i osnovnye tendencii razvitija vysokotemperaturnyh teplozashhitnyh pokrytij dlja rabochih lopatok turbin aviacionnyh GTD [Current state and the main tendencies of development of high-temperature heat-shielding coverings for working shovels of turbines of aviation GTE] //Aviacionnaja promyshlennost'. 2008. №4. S. 33–37.

    2. Mubojadzhjan S.A., Budinovskij S.A., Gajamov A.M., Matveev P.V. Vysokotemperaturnye zharostojkie pokrytija i zharostojkie sloi dlja teplozashhitnyh pokrytij [High-temperature heat-resistant coverings and heat-resistant layers for heat-shielding coverings] //Aviacionnye materialy i tehnologii. 2013. №1. S. 17–20.

    3. Bisson J.-F., Fournier D., Poulain M., Lavigne O., Mevrel R. Thermal conductivity of yttria–zirconia single crystals, determinedwith spatially resolved infrared thermography //Jornal American Ceramic Society. 2000. V. 83. №8. R. 1993–1998.

    4. Mevrel R., Laizet J.C., Azzopardi A., Leclercq B., Poulain M., Lavigne O., Demange D. Thermal diffusivity and conductivity of Zr1-xYxO2-x/2 (x=0; 0,084 and 0,179) single crystals //J. Eur. Ceram. Soс. 2004. V. 24. №10–11. Р. 3081–3089.

    5. Shiladitya P. Pore Architecture in ceramic thermal barrier coatings. University of Cambridge. 2007. P. 1–30.

    6. Miller R.A. Thermal Barrier Coatings for Aircraft Engines: History and Directions //Journal of Thermal Spray Technology. 1997. V. 6(1). P. 36–42.

    7. Matveev P.V., Budinovskij S.A., Mubojadzhjan S.A., Kos'min A.A. Zashhitnye zharostojkie pokrytija dlja splavov na osnove intermetallidov nikelja[Protective heat-resistant coverings for alloys based on intermetallic nickel] //Aviacionnye materialy i tehnologii. 2013. №2. S. 12–25.

    8. Tsipas S. Thermophysical properties of Plasma Sprayed thermal Barrier Coatings. University of Cambridge. 2005. P. 1–25.

    9. Merchev S. Termobar'ernye pokrytija.[Thermal barrier coatings] ZAO «Plakart». 2011. http://www.rusnanonet.ru/ articles/53958/.

    10. Miller R.A., Smialek J.L., Garlick R.G. Phase stability in plasmasprayed, partially stabilized zirconia–yttria /In: Science and technology of zirconia. Advances in ceramics. The American Ceramic Society. 1981. V. 3. P. 241–253.

    11. Mubojadzhjan S.A., Budinovskij S.A., Gajamov A.M., Smirnov A.A. Poluchenie keramicheskih teplozashhitnyh pokrytij dlja rabochih lopatok turbin aviacionnyh GTD magnetronnym metodom [Receiving ceramic heat-shielding coverings for working shovels of turbines of aviation GTE a magnetron method] //Aviacionnye materialy i tehnologii. 2012. №4. S. 3–8.

    12. Kablov E.N., Mubojadzhjan S.A. Zharostojkie i teplozashhitnye pokrytija dlja lopatok turbiny vysokogo davlenija perspektivnyh GTD [Heat-resistant and heat-shielding coverings for shovels of the turbine of a high pressure of perspective GTE] //Aviacionnye materialy i tehnologii. 2012. №S. S. 60−70.

    13. Kablov E.N., Mubojadzhjan S.A. Teplozashhitnye pokrytija dlja lopatok turbin vysokogo davlenija perspektivnyh GTD [Heat-shielding coverings for shovels of turbines of a high pressure of perspective GTE] //Metally. 2012. №1. S. 1–9.

    14. Thermal Barrier Coatings With High Fracture Toughness Underlayer For Improved Impact Resistance: rat. 7255940 US. 26.06.2004.

    15. Vaben R., Mack D.-E. New Thermal Barrier Coatings (TBC), Forschungszentrum Jülich Online. 10.11.2006 URL: http://www.fz-juelich.de/ief/ief-1/

    16. Xu Qiang, Pan Wei, Wan Chunlei, Qi Longhao, Miao Hezhuo, Wang Fuchi. Promising LaSmZr2O7 Ceramic with Pyrochlore Structure for Thermal Barrier Coatings //Key Engineering Materials Vols. 2008. V. 368–372. P. 1328–1330.

    17. Wen Ma, Yue Ma, Shengkai Gong, Huibin Xu and Xueqiang Cao. Thermal Cycling Behavior of Lanthanum-Cerium Oxide Thermal Barrier Coatings Prepared by Air Plasma Spraying //Key Engineering Materials Vols. 2007. V. 336–338. P. 1759–1761.

    18. Jingdong Wang, Wei Pan, Qiang Xu, Kazutaka Mori, Taiji Torigoe. Thermal Conductivity of the New Candidate Materials for Thermal Barrier Coatings //Key Engineering Materials Vols. 2005. V. 280–283. P. 1503–1506.

    19. Jogender Singh, Douglas E. Wolfe, Robert Miller, Jeff Eldridge, Dong-Ming Zhu. Thermal Conductivity and Thermal Stability of Zirconia and Hafnia Based Thermal barrier Coatings by EB-PVD For High Temperature Applications //Materials Science Forum Vols. 2004. V. 455–456. P. 579–586.

    20. Ma W., Mack D., Malzbender J., Vaßen R., Stöver D. Yb2O3 and Gd2O3 doped strontium zirconate for thermal barrier coatings //Journal of the European Ceramic Society. 2008. V. 28. P. 3071–3081.

    21. Bansal N.P., Dongming Zhu, Maryam Eslamloo-Grami. Effects of Doping on Thermal Conductivity of Pyrochlore Oxides for Advanced Thermal Barrier Coatings. NASA/TM–2006-214483.

     

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10.

DOI:

UDC: 678.747.2:620.1

Pages:: 47-50

V.A. Bol’shakov1, V.M. Aleksashin2

[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»

A way to increase the residual compression strength after low-speed impact of cfrps produced by vacuum infusion technology

In the Russian Federation, aviation-purposed parts and components are manufactured by the solvent impregnation in autoclave. However, foreign companies usually use the non-solvent techniques based on melting resins. Non-autoclave molding technologies (such as infusion molding or vacuum impregnation) allow one to decreases sufficiently production costs of CFRPs. Vacuum impregnation is the matter of a particular interest because the usage of complex production equipment can be eliminated. CFRP parts and units made by means of infusion molding possess high impact resistance due to cladding layers and introduction of thermoplastic additives in the reinforcement stack. It provides an improvement of serviceability of such materials in case of low speed impact loading.

Keywords: carbon fiber-reinforced plastic, infusion molding or vacuum and pressure impregnation, residual compression strength after impact

Reference List

    1. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 g. [Strategical Areas of Developing Materials and Their Processing Technologies for the Period up to 2030]  //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

    2. Grashhenkov D.V., Chursova L.V. Strategija razvitija kompozicionnyh i funkcional'nyh materialov [Development Strategics of Composite and Functional Materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 231–242.

    3. Muhametov R.R., Ahmadieva K.R., Chursova L.V., Kogan D.I. Novye polimernye svjazujushhie dlja perspektivnyh metodov izgotovlenija konstrukcionnyh voloknistyh PKM [Novel polymer binders for advanced production methods of structural fibrous polymer composites] //Aviacionnye materialy i tehnologii. 2011. №2. S. 38–42.

    4. Muhametov R.R., Ahmadieva K.R., Kim M.A., Babin A.N. Rasplavnye svjazujushhie dlja perspektivnyh metodov izgotovlenija PKM novogo pokolenija [Melt Binders for Advanced Production Methods for PCM of New Generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 260–265.

    5. Hrul'kov A.V., Dushin M.I., Popov Ju.O., Kogan D.I. Issledovanija i razrabotka avtoklavnyh i bezavtoklavnyh tehnologij formovanija PKM [Studies and Development of Autoclave and Autoclave-Free Technologies for PCM Moulding] //Aviacionnye materialy i tehnologii. 2012. №S. S. 292–302.

    6. Dushin M.I., Hrul'kov A.V., Muhametov R.R., Chursova L.V. Osobennosti izgotovlenija izdelij iz PKM metodom propitki pod davleniem [Characteristic features of manufacturing PC products by the pressure infiltration method] //Aviacionnye materialy i tehnologii. 2012. №1. S. 18–26. 

    7. Perepelkin K.E. Armirujushhie volokna i voloknistye polimernye kompozity [Reinforcing fibers and fibrous polymeric composites]. SPb: Nauchnye osnovy i tehnologii. 2009. S. 171–185.

    8. Cherepanov G.P. Mehanika razrushenija kompozicionnyh materialov[Mechanics of destruction of composite materials]. M.: Nauka. 1983. S. 32–37.

    9. Aleksashin V.M., Antjufeeva N.V. Razvitie metodov termicheskogo analiza v issledovanii polimernyh kompozicionnyh materialov [Development of methods of the thermal analysis in research of polymeric composite materials] /V sb. 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: Jubilejnyj nauch.-tehnich. sb. M.: VIAM. 2007. S. 345–349.

    10. Antjufeeva N.V., Aleksashin V.M., Zhelezina G.F., Stoljankov Ju.V. Metodicheskie podhody termoanaliticheskih issledovanij dlja ocenki svojstv prepregov i ugleplastikov [Methodical approaches of thermoanalytical researches for an assessment of properties of prepregs and coal plastics] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. №4. S. 18–28.

    11. Kirillov V.N., Efimov V.A., Shvedkova A.K., Nikolaev E.V. Issledovanie vlijanija klimaticheskih faktorov i mehanicheskogo nagruzhenija na strukturu i mehanicheskie svojstva PKM [Testing of climatic factors and the mechanical loading effect upon the polymer composite structure and properties] //Aviacionnye materialy i tehnologii. 2011. №4. S. 41–45.

    12. Generalov A.S., Murashov V.V., Dalin M.A., Bojchuk A.S. Diagnostika polimernyh kompozitov ul'trazvukovym reverberacionno-skvoznym metodom [Polymer composite diagnostics by the ultrasonic reverberative-through method] //Aviacionnye materialy i tehnologii. 2012. №1. S. 42–47.

    13. Murashov V.V., Rumjancev A.F. Defektoskopija i diagnostika polimernyh kompozicionnyh materialov akusticheskimi metodami [Defectoscopy and diagnostics of polymeric composite materials by acoustic methods] /V sb. 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: Jubilejnyj nauch.-tehnich. sb. M.: VIAM. 2007. S. 342–348.

     

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11.

DOI:

UDC: 620.172.251.2

Pages:: 51-53

O.V. Kuzmin1, E.A. Tikhomirova2, M.Yu. Sundukov1, T.N. Azizov3, E.F. Sidokhin4

[1] OAO «KLIMOV», klimov@klimov.ru
[2] Join Stock Company «Klimov»
[3] CHERNYSHEV MOSCOW MACHINE-BUILDING ENTERPRISE, azizov-06@yandex.ru
[4] Limited Liability Company «CB Rentgen devices»

A new thermo-cyclic testing method to measure thermal fatigue resistance of materials in aeronautical engineering

A method of thermo-cyclic testing of materials available for production control convenient for evaluation tests at assignment of materials in a construction (or an article) is considered. The developed self-contained unit is an absolutely rigid frame in respect of the rigidity of a sample. With the task to preset a value of elasto-plastic strain ( Δε ) at thermo-cyclic tests the frame has to be made from a material different from that of a sample in terms of linear thermal expansion coefficient (LTEC).

Keywords: thermal fatigue, thermo-cyclic testing, linear thermal expansion coefficients, stiffness

Reference List

    1. Dul'nev R.A., Kotov P.I. Termicheskaja ustalost' metallov [Termal fatigue of metals]. M.: Mashinostroenie. 1980. 200 s.

    2. Gecov L.B., Dobina N.I., Rybnikov A.I., Semenov A.S., Starosel'skij A., Tumanov N.V. Soprotivlenie termicheskoj ustalosti monokristallicheskogo splava [Thermal fatigue resistance of   single-crystal alloy] //Problemy prochnosti. 2008. №5. S. 54−71.

    3. Henkin M.L., Lokshin I.H. Razmernaja stabil'nost' metallov i splavov v tochnom mashi-nostroenii i priborostroenii [Dimensional stability of metals and alloys in exact mechanical engineering and instrument making]. M.: Mashinostroenie. 1974. S. 17.

    4. Dul'nev R.A., Svetlov I.L., Bychkov N.G., Rybina T.V., Suhanov N.N., Gordeeva T.A., Dobrohvalova E.N., Epishin A.I., Krivko A.I., Nazarova M.P. Orientacionnaja zavisimost' termicheskoj ustalosti monokristallov nikelevogo splava [Orientation dependence of thermal fatigue of monocrystals of a nickel alloy]//Problemy prochnosti. 1988. №11. S. 3−9.

     

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12.

DOI:

UDC: 620.1

Pages:: 54-57

V.D. Krylov1

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

Test methods and features of fracture of thin-sheet materials

Fracture toughness K I and K III and puncture-testing methods for thin-sheet materials were considered. A method for determination of yield strength of foils at bending was offered and yield strength of foils was tested. General features of self-oscillation process of thin film fracture were revealed and experimentally verified by the use of aluminum foil samples. The morphology and geometry of foil fractures, as well as the mechanics of fracture process were analyzed. A method for processing of fracture relief images and a procedure of detection of self-oscillation process were offered.

Keywords: thin-sheet material, self-oscillation, fracture mode, fracture toughness, bending test

Reference List

    1. http://www.triz-journal.com/archives/2002/06/e/index.htm.

    2. Antipov V.V., Senatorova O.G., Lukina N.F., Sidel'nikov V.V., Shestov V.V. Sloistye metallopolimernye kompozicionnye materialy [Layered metal-polymer composite materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 226–230.

    3. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 g [The strategic directions of development of materials and technologies of their processing for the period till 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

    4. Antipov V.V. Strategija razvitija titanovyh, magnievyh, berillievyh i aljuminievyh splavov [Strategy of development of titanic, magnesian, beryllium and aluminum alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 157–167.

    5. GOST 618‒73 Fol'ga aljuminievaja dlja tehnicheskih celej. Tehnicheskie uslovija [Foil aluminum for the technical purposes. Specifications].

    6. GOST 25905–83 Fol'ga aljuminievaja dlja kondensatorov. Tehnicheskie uslovija [Foil aluminum for condensers. Specifications].

    7. Orlov M.R. Strategicheskie napravlenija razvitija Ispytatel'nogo centra FGUP «VIAM» [Strategic directions of development of the Test center Federal State Unitary Enterprise VIAM] //Aviacionnye materialy i tehnologii. 2012. №S. S. 387–393.

    8. Bayart E., Boudaoud A., Adda-Bedia M. Finite-Distance Singularities in the Tearing of Thin Sheets //Phys. Rev. Letters. 2011. V. 106. (jelektronnyj zhurnal).

    9. Ghatak A., Mahadevan L. Crack street: The cycloidal wake of a cylinder tearing through a thin sheet //Phys. Rev. Letters. 2003. V. 91. (jelektronnyj zhurnal).

    10. Audoly B., Reis P.M., Roman B. Cracks in thin sheets: when geometry rules the fracture path //Phys. Rev. Letters. 2005. V. 95. (jelektronnyj zhurnal).

    11. Chernatkin S.E., Jakovlev N.O., Kuz'ko E.I., Arsenkin A.M., Shtremel' M.A. Opredelenie soprotivlenija KIII razdiru tonkih listov [Determination of resistance to tearing of thin sheets KIII] //Zavodskaja laboratorija. Diagnostika materialov. 2008. №5. S. 54–57.

    12. Kuz'ko E.I., Chernatkin S.E., Jakovlev N.O., Shtremel' M.A. Processy razrushenija mody KI i KIII v tonkom liste [Fracture processes mode KI and KIII in thin sheet]: Tezisy dokladov. III Evrazijskaja nauchno-prakticheskaja konferencija «Prochnost' neodnorodnyh struktur». 2006. S. 137–139.

    13. Jakovlev N.O., Chernatkin S.E., Kuz'ko E.I., Shtremel' M.A. Sootnoshenie podobija pri prokole tonkogo lista [Relation of similarity at a puncture of a thin leaf] //FMM. 2009. T. 108. №2. S. 217–221.

    14. Vandeparre H., Pineirua M. Wrinkling Hierarchy in Constrained Thin Sheets from Suspended Graphene to Curtains //Phys. Rev. Lett. 2011 V. 106. P. 224–301.

     

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13.

DOI:

UDC: 620.192.63

Pages:: 58-61

D.S. Lozhkova1, M.A. Dalin1

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

The measure of FBH’s parameters, which is using for equipment set-up for inspection of the pulsation absorber diaphragm

The problems of resin pulsation absorber diaphragms of the helicopter’s hydraulic system ultrasonic non-destructive testing under production conditions are observed. The problem of making FBH’s in resin test sample, which is using for equipment set-up was successfully solved. The method of FBH’s parameters measure with laser scanned and optical inverted microscopes is shown.

Keywords: pulse-echo method of ultrasonic non-destructive testing, sensitivity, FBH, test specimen certification, optical microscopy

Reference List

    1. Dalin M.A., Generalov A.S., Bojchuk A.S., Lozhkova D.S. Osnovnye tendencii razvitija akusticheskih metodov nerazrushajushhego kontrolja [Main tendencies of development of acoustic methods of nondestructive control] //Aviacionnye materialy i tehnologii. 2013. №1. S. 64–69.

    2. Generalov A.S., Murashov V.V., Dalin M.A., Bojchuk A.S. Diagnostika polimernyh kompozitov ul'trazvukovym reverberacionno-skvoznym metodom [Diagnostics of polymeric composites by an ultrasonic reverberation and through method] //Aviacionnye materialy i tehnologii. 2012. №1. S. 42–47.

    3. Generalov A.S., Murashov V.V., Bojchuk A.S. Kontrol' prochnosti ugleplastikov na kleevyh prepregah ul'trazvukovym metodom [Control of durability of coal plastics on glue prepregs an ultrasonic method] //Klei. Germetiki. Tehnologii. 2012. №5. S. 27–32.

    4. Bojchuk A.S., Dalin M.A., Stepanov A.V., Generalov A.S. Nerazrushajushhij kontrol' tehnologicheskih narushenij sploshnosti T-obraznoj zony integral'noj konstrukcii iz PKM s ispol'zovaniem ul'trazvukovyh fazirovannyh reshetok [Nondestructive control of technological violations of a continuity of the T-shaped zone of an integrated design from PCM with use of the ultrasonic phased lattices] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. №10. S. 38–44.

    5. Generalov A.S., Murashov V.V., Dalin M.A., Bojchuk A.S. Opredelenie prochnosti ug-leplastikov ul'trazvukovym reverberacionno-skvoznym metodom [Determination of durability of coal plastics by an ultrasonic reverberation and through method] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. №11. S. 47–53.

    6. Bojchuk A.S., Stepanov A.V., Juhackova O.V. Nerazrushajushhij kontrol' PKM s ispol'zovaniem ul'trazvukovyh fazirovannyh reshetok [Nondestructive control of PCM with use of the ultrasonic phased lattices] //Promyshlennye ASU i kontrollery. 2013. №2. S. 54–58.

    7. Sorokin K.V., Murashov V.V., Fedotov M.Ju., Goncharov V.A. Prognozirovanie razvitija defektov v konstrukcijah iz PKM sposobom opredelenija izmenenij zhestkosti pri aktjuirovanii materiala [Forecasting of development of defects in designs from PCM in the way of definition of changes of rigidity at a material aktyuirovaniye] //Aviacionnye materialy i tehnologii. 2011. №2. S. 20–22.

    8. Dalin M.A., Lozhkova D.S., Smirnov D.N. Izmerenie tolshhiny sloja germetikov U-30MJeS-5NT i VGM-L v izdelijah aviacionnoj tehniki s ispol'zovaniem ul'trazvukovogo metoda nerazrushajushhego kontrolja [Measurement of thickness of a layer of sealants U-30MES-5NT and VGM-L in products of the aircraft equipment with use of an ultrasonic method of nondestructive control] //Klei. Germetiki. Tehnologii. 2012. №5. S. 32–35.

    9. Dalin M. A., Lozhkova D.S. Measurement of the Thickness of U-30MES-5NT and VGM-L Sealing Compound Layers in Aircraft Products Using the Ultrasonic Nondestructive Testing Method [Measurement of the Thickness of U-30MES-5NT and VGM-L Sealing Compound Layers in Aircraft Products Using the Ultrasonic Nondestructive Testing Method] //Polymer Science. Series D. Glues and Sealing Materials. 2012. №5. P. 305–308.

    10. Bronfin M.B., Alekseev A.A., Chabina E.B. Metallofizicheskie issledovanija. Vozmozhnosti i perspektivy [Metalphysical researches. Opportunities and prospects] /V sb. 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: Jubilejnyj nauch.-tehnich. sb. M.: VIAM. 2007. S. 353–365.

    11. Sidorov V.V., Ishodzhanova I.V., Rigin V.E., Folomejkin Ju.I. Ocenka jeffektivnosti fil'tracii pri razlivke slozhnolegirovannogo nikelevogo rasplava s povyshennym kolichestvom othodov [Assessment of efficiency of a filtration when pouring hard-doped nickel fusion with the increased quantity of waste] //Jelektrometallurgija. 2011. №11. S. 17–21.

    12. Svetlov I.L., Ishodzhanova I.V., Evgenov A.G., Naprienko S.A. Issledovanie vysokotemperaturnoj polzuchesti i defektnosti struktury monokristallov nikelevogo zharoprochnogo splava posle gorjachego izostaticheskogo pressovanija [Research of high-temperature creep and deficiency of structure of monocrystals of a nickel heat resisting alloy after hot isostatic pressing] //Deformacija i razrushenie materialov. 2011. №3. C. 28–32.

     

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14.

DOI:

UDC: 621.317.411:678.067.5

Pages:: 62-68

V.V. Shirokov1, A.M. Romanov1

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

Waveguide method research of honeycomb glass fibre plastics dielectric characteristics

Given article is devoted to research of honeycomb glass fibre plastics dielectric characteristics. Features of waveguide method measurement of honeycomb glass fibre plastics dielectric permittivity the definitions connected with a polysemy are described. The way of a choice of correct value is shown. Results of measurement of honeycomb glass fibre plastics dielectric permittivity in a wave guide are resulted.

Keywords: radio transparent material, dielectric permittivity, honeycomb glass fibre plastics, a waveguide measuring line

Reference List

    1. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [The strategic directions of development of materials and technologies of their processing for the period till 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

    2. Grashhenkov D.V., Chursova L.V. Strategija razvitija kompozicionnyh i funkcional'nyh materialov [Strategy of development of composite and functional materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 231–242.

    3. Davydova I.F., Kavun N.S. Stekloplastiki – mnogofunkcional'nye kompozicionnye materialy [Fibreglasses – multipurpose composite materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 253–260.

    4. Davydova I.F., Kablov E.N., Kavun N.S. Termostojkie negorjuchie poliimidnye steklotekstolity dlja izdelij aviacionnoj i raketnoj tehniki [Heat-resistent nonflammable polyimide fiberglass for products aviation and rocketry] //Vse materialy. Jenciklopedicheskij spravochnik. 2009. №9. S. 2–11.

    5. Davydova I.F., Kavun N.S. Termostojkie germetichnye steklotekstolity [Heat-resistent tight fiberglass] //Vse materialy. Jenciklopedicheskij spravochnik. 2011. №11. S. 18–20.

    6. Haritonov D.V. Radioprozrachnyj steklokeramicheskij material s uluchshennym raspredeleniem fiziko-tehnicheskih svojstv [A radiotransparent glass-ceramic material with the improved distribution of physics and technology properties] //Aviacionnye materialy i tehnologii. 2012. №3. S. 19–24.

    7. Strel'nikov S.V., Zastrogina O.B., Vekshin E.A., Shvec N.I. K voprosu o sozdanii vysokojeffektivnyh tehnologij izgotovlenija panelej inter'era v krupnoserijnom proizvodstve [To a question of creation of highly effective manufacturing techniques of panels of an interior in a large-lot production] //Aviacionnye materialy i tehnologii. 2011. №4. S. 18–24.

    8. Beljaev A.A., Kondrashov S.V., Lepeshkin V.V., Romanov A.M. Radiopogloshhajushhie materialy [Radio absorbing materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 348–352.

    9. Agafonova A.S., Beljaev A.A., Kondrashov Je.K., Romanov A.M. Osobennosti formirovanija monolitnyh konstrukcionnyh radiopogloshhajushhih materialov na osnove kompozitov, napolnennyh rezistivnym voloknom [Features of formation of monolithic constructional radio absorbing materials on the basis of the composites filled with resistive fiber] (v pechati).

    10. Kondrashov Je.K., Postnov V.I., Petuhov V.I., Kavun N.S., Abrosimov P.A., Barbot'ko S.L. Issledovanie svojstv trehslojnyh panelej na modificirovannom svjazujushhem FPR-520G [Research of properties of three-layer panels on modified binding FPR-520G] //Aviacionnye materialy i tehnologii. 2009. №3. S. 19–23.

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