ARCHIVE

Aviation materials and technologies №3, 2014

Contents

  • E.V. Kolyadov, V.V. Gerasimov

    The influence of the reduced size of the casting on the axial temperature gradient and the macro-structure of castings for directional solidification at the facility UVNK-15

    3-9
  • E.V. Filonova, M.M. Bakradze, A.Ya. Kotchoubey, N.L. Vavilin

    Structural-phase evolution of VZH175-alloy during hot deformation and heat treatment

    10-13
  • O.G. Ospennikova

    Influence research of fillers on properties and stability of modelling compositions, a choice of optimum structures

    14-17
  • O.G. Ospennikova

    Research and working out of parametres of technological process of manufacturing of models from modelling compositions on the basis of synthetic waxes

    18-21
  • P.V. Matveev, S.A. Budinovskiy

    Research of the properties of protective heat-resistant coatings for intermetallic nickel alloys operating at temperatures up to 1300°С

    22-26
  • O.A. Tonysheva, N.M. Voznesenskaya

    Perspective high-strength corrosion-resistant steels alloyed with nitrogen (comparative analysis)

    27-32
  • M.I. Vavilova, N.S. Kavun

    The properties of glass filler for constructions of fiberglass

    33-37
  • L.V. Semyonova, N.I. Nefyodov

    Application of modified epoxy primers in the painting systems

    38-44
  • A.S. Chainikova, L.A. Orlova, N.V. Popovich, Yu.E. Lebedeva, S.St. Solncev

    Dispersion reinforced composites based on glass/glass-ceramics matrixes: properties and possible applications (review)

    45-54
  • A.M. Zimichev, E.P. Solovjeva

    Zirconia fiber for High Temperature Application (review)

    55-61
  • A.V. Ilichev, A.E. Raskutin

    Research of stress concentrator influence on stress-strain state of carbon by digital images correlation method

    62-66
  • M.M. Grigoriev, D.I. Kogan, Y.A. Gusev, Y.M. Gurevich

    Features of producing composites вy vacuum molding of prepreg

    67-71
Содержание номера
1.

DOI: 10.18577/2071-9140-2014-0-3-3-9

UDC: 669.018.44:66.065.5

Pages:: 3-9

E.V. Kolyadov1, V.V. Gerasimov2

[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», admin@viam.ru

The influence of the reduced size of the casting on the axial temperature gradient and the macro-structure of castings for directional solidification at the facility UVNK-15

In the article directional solidification parameters that affect the appearance of the castings developed dendrites axes of order. Conducted simplified calculations of heat released from the castings, the maximum crystallization rate at which there is no deflection of the crystallization front. The experimental work to determine the temperature gradient for castings with different cross-sectional area, their macrostructure. Ways of improving the quality of the structure by increasing the cross section castings.

Keywords: superalloys, directionally solidified, units for single crystal casting, temperature gradient

Reference List

    1. Kablov E.N., Tolorajja V.N. VIAM – osnovopolozhnik otechestvennoj tehnologii lit'ja monokristallicheskih turbinnyh lopatok GTD i GTU [VIAM – founder of the national casting technology monocrystalline turbine blades GTE and GTU] //Aviacionnye materialy i tehnologii. 2012. №S. S. 105–117.

    2. Kablov E.N., Gerasimov V.V., Visik E.M., Demonis I.M. Rol' napravlennoj kristallizacii v resursosberegajushhej tehnologii proizvodstva detalej GTD [The role of directional solidification technology in resource-producing parts of GTE] //Aviacionnye materialy i tehnologii. 2008. №1. S. 3–9.

    3. Bondarenko Ju.A., Kablov E.N. Napravlennaja kristallizacija zharoprochnyh splavov s povyshennym temperaturnym gradientom [Directional solidification of superalloys with a high temperature gradient] //MiTOM. 2002. №7. S. 20–23.

    4. Kablov E.N., Orlov M.R., Ospennikova O.G. Mehanizmy obrazovanija poristosti v monokristallicheskih lopatkah turbiny i kinetika ee ustranenija pri gorjachem izostaticheskom pressovanii [Mechanisms of formation porosity in single-crystal turbine blades and its elimination kinetics during hot isostatic pressing] //Aviacionnye materialy i tehnologii. 2012. №S. S. 117–129.

    5. Gerasimov V.V., Visik E.M., Nikitin V.A., Zernova M.G. Opyt osvoenija tehnologii lit'ja sektorov soplovyh lopatok s monokristallicheskoj strukturoj iz splava VKNA-4U [Experience in developing casting technology sectors vane with single-crystal structure of the alloy VKNA-4U] //Aviacionnye materialy i tehnologii. 2012. №4. S. 13–18.

    6. Gerasimov V.V., Visik E.M. Tehnologicheskie aspekty lit'ja detalej gorjachego trakta GTD iz intermetallidnyh nikelevyh splavov tipa VKNA s monokristallicheskoj strukturoj [Technological aspects of the casting of the hot section of GTE intermetallic nickel alloys of VKNA with single-crystal structure] //Litejshhik Rossii. 2012. №2. S. 19–23.

    7. Gerasimov V.V., Koljadov E.V. Tehnicheskie harakteristiki i tehnologicheskie vozmozhnosti ustanovok UVNK-9A i VIP-NK dlja poluchenija monokristallicheskih otlivok iz zharoprochnyh splavov [Specifications and technological capabilities installations UVNK-9A and VIP NC for single crystal casting of superalloys] //Litejshhik Rossii. 2012. №11. S. 33–38.

    8. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [Strategic directions of development of materials and technologies to process them for the period up to 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

    9. Kablov E.N., Svetlov I.L., Petrushin N.V. Nikelevye zharoprochnye splavy dlja lit'ja lopatok s napravlennoj i monokristallicheskoj strukturoj [Nickel superalloys for blades casting with directional and single-crystal structure] //Materialovedenie. 1997. №4. S. 32–38; №5. S. 14–17.

    10. 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 [Structure and properties of single crystals of high-temperature <001> vysokorenievogo nickel superalloy prepared under the high-gradient directional crystallization] //Aviacionnye materialy i tehnologii. 2011. №4. S. 25–31.

    11. Bondarenko Ju.A., Echin A.B., Surova V.A., Narskij A.R. O napravlennoj kristallizacii zharoprochnyh splavov s ispol'zovaniem ohladitelja [On the directional solidification of superalloys using cooler] //Litejnoe proizvodstvo. 2011. №5. S. 36–39.

    12. Bondarenko Ju.A., Bazyleva O.A., Echin A.B., Surova V.A., Narskij A.R. Vysokogradientnaja napravlennaja kristallizacija detalej iz splava VKNA-1V [High-gradient directional solidification of alloy parts VKNA-1B] //Litejnoe proizvodstvo. 2012. №6. S. 12–16.

    13. Bondarenko Ju.A., Echin A.B., Surova V.A., Narskij A.R. Vlijanie uslovij naprav-lennoj kristallizacii na strukturu detalej tipa lopatki GTD [Effect of directional solidification conditions on the structure of parts such as blades of GTE] //Litejnoe proizvodstvo. 2012. №7. S. 14–16.

    14. Koljadov E.V., Gerasimov V.V., Visik E.M. Poluchenie krupnogabaritnyh zagotovok pod diski turbiny GTD iz splava VZh175 metodom napravlennoj kristallizacii na ustanovke UVNK-10 [Preparation of large workpieces under the wheels of alloy turbine GTE VZH175 directional crystallization method for installing UVNK-10] //Litejnoe proizvodstvo. 2013. №10. S. 28–31.

    15. Gerasimov V.V., Visik E.M., Koljadov E.V. O neispol'zovannyh rezervah napravlennoj kristallizacii v povyshenii jekspluatacionnyh harakteristik detalej GTD i GTU [About untapped reserves of directional solidification in improving the performance of gas-turbine and gas turbine] //Litejnoe proizvodstvo. 2013. №9. S. 30–32.

    16. Kablov E.N. Litye lopatki gazoturbinnyh dvigatelej (splavy, tehnologii, pokrytija) [Alloy blades of gas turbine engines (alloys, technology, coverage)]. M.: MISiS. 2001. S. 293–398.

    17. Kurc V., Zam P.R. Napravlennaja kristallizacija jevtekticheskih materialov [Directional solidification of eutectic materials]. M.: Metallurgija. 1980. S. 118–147.

    18. Gerasimov V.V., Visik E.M., Koljadov E.V. Vlijanie drejfa fronta kristallizacii na strukturu monokristallicheskih otlivok splava ZhS32U, poluchennyh na ustanovke VIP-NK [Influence of the drift on the structure of the crystallization front monocrystalline alloy castings ZHS32U obtained at the VIP NC] //Metallurgija mashinostroenija. 2013. №3. S. 14–17.

    19. Reed R.C. The Superalloys Fundamentals and Applications. New York: Cambridge University Press. 2006. S. 121–147.

    20. Artjunov V.A., Mitkalinnyj V.I., Stark S.B. Metallurgicheskaja teplotehnika [Metallurgical heat engineering]. M.: Metallurgija. 1974. T. 1. S. 292–356.

    21. Alekseev G.N. Obshhaja teplotehnika [Overall firing]. M.: Vysshaja shkola. 1980. S. 206–229.

    22. Kabardin O.F. Fizika [Physics]. M.: Prosveshhenie. 1991. 96 s.

    23. Kutateladze S.S., Borishanskij V.M. Spravochnik po teploperedache [Handbook of heat transfer]. M.-L.: Mashgiz, 1959. S. 148–155.

     

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2.

DOI: 10.18577/2071-9140-2014-0-3-10-13

UDC: 669.018.44:669.245

Pages:: 10-13

E.V. Filonova1, M.M. Bakradze1, A.Ya. Kotchoubey2, N.L. Vavilin2

[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

Structural-phase evolution of VZH175-alloy during hot deformation and heat treatment

The effect of thermomechanical deformation parameters (temperature and speed) and heat treatment on the recrystallization process of nickel-based superalloy VZH175 has been investigated in this article. The structural diagram and the conditions for the formation a recrystallized homogeneous fine-grained alloy microstructure were obtained.

Keywords: deformation, temperature, speed, heat treatment, recrystallization, grain, structure

Reference List

    1. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [Strategic directions of development of materials and technologies to process them for the period up to 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

    2. Kablov E.N., Lomberg B.S., Ospennikova O.G. Sozdanie sovremennyh zharoprochnyh materialov i tehnologij ih proizvodstva dlja aviacionnogo dvigatelestroenija [The creation of modern high-temperature materials and manufacturing technologies for aircraft engine] //Kryl'ja Rodiny. 2012. №3–4. S. 34.

    3. Lomberg B.S., Bakradze M.M., Chabina E.B., Filonova E.V. Vzaimosvjaz' struktury i svojstv vysokozharoprochnyh nikelevyh splavov dlja diskov gazoturbinnyh dvigatelej [Relationship between structure and properties of nickel-base superalloys for turbine engine disks] //Aviacionnye materialy i tehnologii. 2011. №2. S. 25–30.

    4. Kablov E.N., Bondarenko Ju.A., Echin A.B., Surova V.A. Razvitie processa napravlennoj kristallizacii lopatok GTD iz zharoprochnyh splavov s monokristallicheskoj i kompozicionnoj strukturoj [The development process of directional solidification of GTE blades with single crystal superalloys and composite structure] //Aviacionnye materialy i tehnologii. 2012. №1. 

    S. 3–8.

    5. Novikov I.I. Teorija termicheskoj obrabotki metallov i splavov [The theory of heat treating metals and alloys]. M.: Metallurgija. 1982. 392 s.

    6. Gorelik S.S., Dobatkin S.V., Kaputkina L.M. Rekristallizacija metallov i splavov [Recrystallization of metals and alloys]. M.: MISiS. 2005. 432 s.

    7. Vajnblat Ju.M., Sharshagin N.A., Varfalomeeva Je.A. Diagrammy strukturnyh sostojanij i mehanizmov deformacii aljuminievyh splavov [Diagrams of structural states and deformation mechanisms of aluminum alloys]. M.: VILS.1985. 123 s.

    8. Lomberg B.S., Ovsepjan S.V., Bakradze M.M. Osobennosti legirovanija i termicheskoj obrabotki zharoprochnyh nikelevyh splavov dlja diskov gazoturbinnyh dvigatelej novogo pokolenija [Features alloying and heat treatment heat-resistant nickel alloys for turbine engine drives the new generation] //Aviacionnye materialy i tehnologii. 2010. №2. S. 3–8.

    9. Lomberg B.S., Ovsepjan S.V., Bakradze M.M. Novyj zharoprochnyj nikelevyj splav dlja diskov gazoturbinnyh dvigatelej (GTD) i gazoturbinnyh ustanovok (GTU) [New heat resistant nickel alloy disc turbine engine (GTE) and gas turbine units (GTU)] //Materialovedenie. 2010. №7. 

    S. 24–28.

    10. Zharoprochnyj deformiruemyj splav na osnove nikelja i izdelie, vypolnennoe iz jetogo splava [Heat-resistant wrought alloys based on nickel and a product made from this alloy]: pat. 2365657 Ros. Federacija; opubl. 27.08.2009 Bjul. №24. 

    11. Lomberg B.S., Ovsepjan S.V., Bakradze M.M., Mazalov I.S. Vysokotemperaturnye zharoprochnye nikelevye splavy dlja detalej gazoturbinnyh dvigatelej [High-temperature heat-resistant nickel alloys for turbine engine parts] //Aviacionnye materialy i tehnologii. 2012. №S. S. 52–57.

    12. Ovsepyan S., Lomberg B., Bakradze M., Mazalov I. New nickel-base wrought superalloys for high temperature rotor and stator parts of gas turbine engines /In: Materials Science and Engineering Conference. 2012. http://www.dgm.de/tagungen.

    13. Ryndenkov D.V., Perevozov A.S., Lomberg B.S., Bakradze M.M. Pervyj opyt proizvodstva krupnogabaritnyh shtampovok iz splava VZh175-ID v OAO «SMK» [The first experience of production of large forgings alloy VZH175-ID JSC «QMS»] /V sb. tezisov dokl. konf. «Sovremennye deformiruemye zharoprochnye splavy i stali dlja detalej GTD». M.: VIAM. 2013 (CD-disk).

    14. Bakradze M.M., Lomberg B.S., Ovsepjan S.V. i dr. Razrabotka novogo zharoprochnogo deformiruemogo splava na nikelevoj osnove dlja diskov GTD [Development of a new heat-resistant nickel alloy deformed basis for GTE disks] /V sb. tezisov dokl. Mezhdunarodnoj nauch.-tehnich. konf. «Aktual'nye voprosy aviacionnogo materialovedenija». M.: VIAM. 2007. S. 146.

    15. Lomberg B.S., Bubnov M.V., Bakradze M.M., Arbina V.P. Izgotovlenie pokovok diskov gazoturbinnyh dvigatelej iz splava VZh175 [Manufacturing forgings drives turbine engines alloy VZH175] //Kuznechno-shtampovochnoe proizvodstvo. Obrabotka materialov davleniem. 2013. №9. S. 21–23.

    16. Kablov E.N., Ospennikova O.G., Lomberg B.S. Kompleksnaja innovacionnaja tehnologija izotermicheskoj shtampovki na vozduhe v rezhime sverhplastichnosti diskov iz superzharoprochnyh splavov [Integrated innovative technology isothermal forging in air superplasticity disks from superzharoprochnyh alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 129–141.

    17. Kablov E.N., Ospennikova O.G., Lomberg B.S., Sidorov V.V. Prioritetnye napravlenija razvitija tehnologij proizvodstva zharoprochnyh materialov dlja aviacionnogo dvigatelestroenija [Priority development of technologies for the production of refractory materials of aviation engine] //Problemy chernoj metallurgii i materialovedenija. 2013. №3. S. 47–54.

     

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3.

DOI: 10.18577/2071-9140-2014-0-3-14-17

UDC: 621.74.045

Pages:: 14-17

O.G. Ospennikova1

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

Influence research of fillers on properties and stability of modelling compositions, a choice of optimum structures

On the basis of the spent researches concentration dependences are defined and the base structure of a modelling composition on the basis of synthetic waxes is developed. In quality of filler compositions in quantity from 30 to 50 % (it is entered over 100 %) terephthalic acid is used. Terephthalic acid (in difference from a carbamide) in quality of filler provides necessary quality of geometry and cleanliness of a surface of models and physicomechanical characteristics of modelling compositions. Thus its optimum substance is in the range from 30 to 50%. Carbamide use in quality of filler is inexpedient because it partially co-operates with components of a modelling composition, coagulates and is partially dissolved in it. The new developed modelling composition mark Salut-7 is appropriated.

Keywords: modelling compositions, moulding on melted models, concentration of components, durability, linear seat, penetration, filler, a carbamide, terephthalic acid

Reference List

    1. Ospennikova O.G. Model'nye kompozicii na osnove sinteticheskih materialov dlja lit'ja po vyplavljaemym modeljam detalej GTD [Model formulation based on synthetic materials for investment casting parts of GTE]: Avtoref. dis. k.t.n. M.: MMPP «Saljut». 2000. 32 s. 

    2. Ospennikova O.G., Hajutin S.G. Struktura model'nyh kompozicij dlja lit'ja po vyplavljaemym modeljam [The structure of the model compositions for investment casting] //Materialovedenie. 2009. №10. S. 46–51.

    3. Ospennikova O.G., Shutov A.N., Pikulina A.V., Dushkin A.M. Pattern compounds based on synthetic materials for casting gas-turbine engine blades //Litejnoe proizvodstvo. 2003. №1. 

    S. 21–29.

    4. Ospennikova O.G., Kablov E.N., Shunkin V.N. Model'nye kompozicii na osnove sinteticheskih materialov dlja lit'ja lopatok GTD [Model formulation based on synthetic materials for casting gas turbine engine blades] /V sb. Aviacionnye materialy i tehnologii. M.: VIAM. 2002. №3. 

    S. 64–67.

    5. Ospennikova O.G., Kablov E.N., Shunkin V.N. Razrabotka i issledovanie plastifikatora dlja model'nyh kompozicij na osnove prirodnyh voskov [Development and research of a plasticizer for model formulations based on natural waxes] /V sb. Aviacionnye materialy i tehnologii. M.: VIAM. 2002. №3. S. 68–70.

    6. Ospennikova O.G., Pikulina L.V., Shunkin V.N. Рattern compositions for casting gas-turbine engine blades //Litejnoe proizvodstvo. 2001. №10. S. 23–24.

    7. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2447968 Ros. Federacija; opubl. 14.12.2010.

    8. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2447969 Ros. Federacija; opubl. 14.12.2010.

    9. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2182057 Ros. Federacija; opubl. 31.05.2000.

    10. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2162386 Ros. Federacija; opubl. 17.03.2000.

    11. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2177387 Ros. Federacija; opubl. 31.05.2000.

    12. Repjah S.I. Tehnologicheskie osnovy lit'ja po vyplavljaemym modeljam [Technological bases of investment casting]. Dnepropetrovsk: Lira. 2006. 1056 s.

    13. Kablov E.N., Deev V.V., Narskij A.R., Bondarenko O.A. Tehnologija udalenija model'nyh mass iz keramicheskih form dlja lit'ja po vyplavljaemym modeljam [Removal technology model masses of ceramic molds for investment casting] //Litejnoe proizvodstvo. 2005. №3. S. 20–22.

     

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4.

DOI: 10.18577/2071-9140-2014-0-3-18-21

UDC: 621.74.045

Pages:: 18-21

O.G. Ospennikova1

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

Research and working out of parametres of technological process of manufacturing of models from modelling compositions on the basis of synthetic waxes

Reception of qualitative cast details with high geometrical accuracy a moulding method on melted models in many respects depends on properties of modelling compositions and their components as casting completely repeats model geometry. On the basis of the spent researches requirements to modelling structures are developed, the technique of definition of fluidity (by analogy to polymers), for studying of modelling compositions as fluidity is one of the basic properties defining a choice of technological parametres of manufacturing of models is fulfilled. The technique of definition of fluidity of modelling compositions allows to carry out selection of technological parametres of manufacturing of models depending on a fluidity indicator of melt compositions. Depending on size of an indicator of fluidity melt optimum intervals of temperatures of pressing of models from composition Salut-7 with the volume of filler 30, 40 and 50 % are defined.

Keywords: modelling compositions, moulding on melted models, models, a fluidity indicator of melt, filler, terephthalic acid, casting

Reference List

    1. Ospennikova O.G. Model'nye kompozicii na osnove sinteticheskih materialov dlja lit'ja po vyplavljaemym modeljam detalej GTD [Model formulation based on synthetic materials for investment casting parts of GTE]: Avtoref. dis. k.t.n. M.: MMPP «Saljut». 2000. 32 s.

    2. Ospennikova O.G., Hajutin S.G. Struktura model'nyh kompozicij dlja lit'ja po vyplavljaemym modeljam [The structure of the model compositions for investment casting] //Materialovedenie. 2009. №10. S. 46–51.

    3. Ospennikova O.G., Shutov A.N., Pikulina A.V., Dushkin A.M. Pattern compounds based on synthetic materials for casting gas-turbine engine blades //Litejnoe proizvodstvo. 2003. №1. 

    S. 21–29.

    4. Ospennikova O.G., Kablov E.N., Shunkin V.N. Model'nye kompozicii na osnove sinteticheskih materialov dlja lit'ja lopatok GTD [Model formulation based on synthetic materials for casting gas turbine engine blades] /V sb. Aviacionnye materialy i tehnologii. M.: VIAM. 2002. №3. 

    S. 64–67.

    5. Ospennikova O.G., Kablov E.N., Shunkin V.N. Razrabotka i issledovanie plastifikatora dlja model'nyh kompozicij na osnove prirodnyh voskov [Development and research of a plasticizer for model formulations based on natural waxes] /V sb. Aviacionnye materialy i tehnologii. M.: VIAM. 2002. №3. S. 68–70.

    6. Ospennikova O.G., Pikulina L.V., Shunkin V.N. Рattern compositions for casting gas-turbine engine blades //Litejnoe proizvodstvo. 2001. №10. S. 23–24.

    7. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2447968 Ros. Federacija; opubl. 14.12.2010.

    8. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2447969 Ros. Federacija; opubl. 14.12.2010.

    9. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2182057 Ros. Federacija; opubl. 31.05.2000.

    10. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2162386 Ros. Federacija; opubl. 17.03.2000.

    11. Kompozicija dlja izgotovlenija vyplavljaemyh modelej [The composition for the manufacture of cast models]: pat. 2177387 Ros. Federacija; opubl. 31.05.2000.

    12. Chernozhukov N.I., Vajnshtok V.V., Kartinin B.N. K voprosu o submikrostrukture tverdyh uglevodorodov v uglevodorodnoj srede [On the submicrostructure solid hydrocarbons in a hydrocarbon medium]. Ch. 1 //Izvestija vuzov. Neft' i gaz. 1961. №8. S. 83–85. 

    13. Chernozhukov N.I., Vajnshtok V.V., Kartinin B.N. K voprosu o submikrostrukture tverdyh uglevodorodov v uglevodorodnoj srede [On the submicrostructure solid hydrocarbons in a hydrocarbon medium]. Ch. 2 //Izvestija vuzov. Neft' i gaz. 1962. №11. S. 53–54.

    14. Kablov E.N., Deev V.V., Narskij A.R., Bondarenko O.A. Tehnologija udalenija model'nyh mass iz keramicheskih form dlja lit'ja po vyplavljaemym modeljam [Removal technology model masses of ceramic molds for investment casting] //Litejnoe proizvodstvo. 2005. №3. S. 20–22.

     

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DOI: 10.18577/2071-9140-2014-0-3-22-26

UDC: 629.7.023.224

Pages:: 22-26

P.V. Matveev1, S.A. Budinovskiy2

[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»

Research of the properties of protective heat-resistant coatings for intermetallic nickel alloys operating at temperatures up to 1300°С

Properties of heat-resistant coatings for intermetallic nickel alloys operating at temperatures up to 1250-1300°С were studied. Research of heat-resistance of alloys with coatings was made. Results of research showed that VSDP-4 and SDP-41 coatings have the best heat-resistan-ce.

Keywords: сoatings, heat-resistant coatings, ion-plasma coatings, ion-plasma technology, heat-resistance, intermetallic alloys

Reference List

    1. Kablov E.N., Petrushin N.V., Eljutin E.S. Monokristallicheskie zharoprochnye splavy dlja gazoturbinnyh dvigatelej [Single crystal superalloys for gas turbine engines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 38–52.

    2. Kablov E.N., Gerasimov V.V., Visik E.M., Demonis I.M. Rol' napravlennoj kristallizacii v resursosberegajushhej tehnologii proizvodstva detalej GTD [The role of directional solidification technology in resource-producing parts of GTE] //Trudy VIAM. 2013. №3. St. 01 (viam-works.ru).

    3. Kablov E.N., Ospennikova O.G., Vershkov A.V. Redkie metally i redkozemel'nye jelementy – materialy sovremennyh i budushhih vysokih tehnologij [Rare metals and rare earth elements – materials of current and future high-tech] //Trudy VIAM. 2013. №2 St. 01 (viam-works.ru).

    4. Bazyleva O.A., Arginbaeva Je.G., Turenko E.Ju. Zharoprochnye litejnye intermetallidnye splavy [Heat-resistant casting intermetallic alloys] //Aviacionnye materialy i tehnologii. 2012. №S. 

    S. 57–60.

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

    6. Gajamov A.M. Zharostojkoe pokrytie s kompozicionnym bar'ernym sloem dlja zashhity vneshnej poverhnosti rabochih lopatok GTD iz renijsoderzhashhih zharoprochnyh nikelevyh splavov [Reflective coating composite barrier layer to protect the outer surface of the working gas turbine engine blades of rhenium-containing heat-resistant nickel alloys] /V sb. trudov XI Rossijskoj ezhegodnoj konferencii molodyh nauchnyh sotrudnikov i aspirantov «Fiziko-himija i tehnologija neorganicheskih materialov». M.: IMET RAN. 2012. S. 473–475.

    7. Sposob obrabotki poverhnosti metallicheskogo izdelija [A method of surface treatment of metal articles]: pat. 2368701 Ros. Federacija; opubl. 27.09.2009.

    8. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlja vysokoteplonagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for high-thermal components of gas turbine engines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 13–19.

    9. Mubojadzhjan S.A., Aleksandrov D.A., Gorlov D.S. Nanoslojnye uprochnjajushhie pokrytija dlja zashhity stal'nyh i titanovyh lopatok kompressora GTD [Nanolayer strengthening coatings for protection of steel and titanium turbine engine compressor blades] //Aviacionnye materialy i tehnologii. 2011. №3. S. 3–8.

    10. Matveev P.V., Budinovskij S.A., Mubojadzhjan S.A., Kos'min A.A. Zashhitnye zharostojkie pokrytija dlja splavov na osnove intermetallidov nikelja [Heat-resistant protective coatings for intermetallic alloys based on nickel] //Aviacionnye materialy i tehnologii. 2013. №2. S. 12–15.

    11. Kablov E.N., Mubojadzhjan S.A. Zharostojkie i teplozashhitnye pokrytija dlja lopatok turbiny vysokogo davlenija perspektivnyh GTD [Heat-resistant and heat-resistant coatings for high-pressure turbine blades promising GTD] //Aviacionnye materialy i tehnologii. 2012. №S. S. 60–70.

    12. 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 coating and heat-resistant layers for thermal barrier coatings] //Aviacionnye materialy i tehnologii. 2013. №1. S. 17–20.

    13. Budinovskij S.A., Kablov E.N., Mubojadzhjan S.A. Primenenie analiticheskoj modeli opredelenija uprugih naprjazhenij v mnogoslojnoj sisteme pri reshenii zadach po sozdaniju vysokotemperaturnyh zharostojkih pokrytij dlja rabochih lopatok aviacionnyh turbin [Application of an analytical model of elastic stresses in a multilayer system with the task of building high-temperature coatings for aircraft turbine blades workers] //Vestnik MGTU im. N.Je. Baumana. 2011. №SP2. S. 26–37.

    14. Budinovskij S.A., Mubojadzhjan S.A., Gajamov A.M., Stepanova S.V. Ionno-plazmennye zharostojkie pokrytija s kompozicionnym bar'ernym sloem dlja zashhity ot okislenija splava ZhS36-VI [Ion-plasma heat-resistant composite coating with a barrier layer to prevent the oxidation of the alloy ZHS36-VI] //MiTOM. 2011. №1. S. 34–40.

     

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DOI: 10.18577/2071-9140-2014-0-3-27-32

UDC: 669.14.018.8

Pages:: 27-32

O.A. Tonysheva1, N.M. Voznesenskaya1

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

Perspective high-strength corrosion-resistant steels alloyed with nitrogen (comparative analysis)

The article considers perspective high-strength corrosion-resistant steels alloyed with nitrogen including increased content of nitrogen steels which have developed at FSUE «Аll-Russian scientific research institute of aviation materials» and also in conjunction with the institute of Metallurgy and material science in recent years. It is described mechanical and corrosion properties of these steels and their welds and also methods of their production. It is revealed alloying principles of corrosion-resistant nitrogen steels and shown the possibility of increasing of their properties by means of high-temperature thermo-mechanical processing.

Keywords: corrosion-resistant steels, nitrogen, properties

Reference List

    1. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [Strategic directions of development of materials and technologies to process them for the period up to 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

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

    3. Kablov E.N. VIAM. Napravlenie glavnogo udara [VIAM. Direction of the main attack] //Nauka i zhizn'. 2012. №6. S. 14–19.

    4. Tonysheva O.A., Voznesenskaja N.M., Eliseev Je.A., Shal'kevich A.B. Novaja vysokoprochnaja jekonomnolegirovannaja azotsoderzhashhaja stal' povyshennoj nadezhnosti [New high ehkonomnolegirovannyh nitrogen-containing steel increased reliability] //Aviacionnye materialy i tehnologii. 2012. №S. S. 84–88.

    5. Berezovskaja V.V., Kostina M.V., Blinov E.V., Bobrova B.E., Bannyh I.O. vlijanie termicheskoj obrabotki na strukturu vysokoazotistyh austenitnyh korrozionnostojkih stalej 04H22AG17N8M2F i 07H20AG9N8MF [Effect of heat treatment on the structure vysokoazotistyh austenitic stainless steels 04H22AG17N8M2F and 07H20AG9N8MF] //Metally. 2009. №2. S. 61–68.

    6. Blinov E.V., Hadyev M.S. Issledovanie struktury i mehanicheskih svojstv korrozionnostojkih vysokoazotistyh stalej 04H22AG15N8M2F i 05H19AG10N7MBF [Investigation of the structure and mechanical properties of corrosion-resistant high-nitrogen steels 04H22AG15N8M2F and 05H19AG10N7MBF] //Metally. 2009. №2. S. 93–99.

    7. Berezovskaja V.V., Bannyh O.A., Kostina M.V., Blinov E.V., Shestakov A.I., Savraj R.A. Vlijanie termicheskoj obrabotki na strukturu i svojstva vysokoazotistoj austenitnoj korrozionnostojkoj stali 03H20AG11N7M2 [Effect of heat treatment on the structure and properties of vysokoazotistoy austenitic stainless steel 03H20AG11N7M2] //Metally. 2010. №2. S. 34–44. 

    8. Ustinovshhikov Ju.I., Blinov V.M., Strukturnye i fazovye prevrashhenija vysokoazotistoj stali 05H20AG10N3MF pri termicheskom vozdejstvii [Structural and phase transitions in high-nitrogen steels 05H20AG10N3MF thermal exposure] //Metally. 2012. №1. S. 72–79.

    9. Blinov E.V., Terent'ev V.F., Prosvirnin D.V., Blinov V.M., Bakunova N.V. Cikliche-skaja prochnost' korrozionnostojkoj austenitnoj azotosoderzhashhej stali 05H22AG15N8MF v uslovijah povtornogo rastjazhenija [Cyclic strength nitrogen-containing austenitic stainless steel 05H22AG15N8MF under restretching] //Metally. 2012. №1. S. 80–87.

    10. Naumenko V.V., Shljamnev A.P., Filippov G.A. Azot v austenitnyh nerzhavejushhih staljah razlichnyh sistem legirovanija [Nitrogen austenitic stainless steels of different alloying systems] //Metallurg. 2011. №6. S. 46–53.

    11. Korolev M.L. Azot kak legirujushhij jelement stali [Nitrogen as an alloying element in steel]. M.: Metallurgizdat. 1961. S. 4.

    12. Vysokoprochnaja korrozionnostojkaja stal' austenitno-martensitnogo klassa [High-strength corrosion-resistant steel austenitic-martensitic class]: pat. 2164546 Ros. Federacija; opubl. 27.03.2001.

    13. Lukin V.I., Banas I.P., Koval'chuk V.G., Golev E.V. Argono-dugovaja svarka vysokoprochnoj cementuemoj stali VNS-63 [Argon-arc welding of high strength carburized steel VNS-63] //Trudy VIAM. 2013. №8. St. 01 (viam-works.ru). 

    14. Vysokoprochnaja korrozionnostojkaja stal' martensitnogo klassa i izdelie, vypolnennoe iz nee [High-strength corrosion-resistant steel and martensitic class product made from it]: pat. 2291912 Ros. Federacija; opubl. 10.11.2005.

    15. Vysokoprochnaja korrozionnostojkaja stal' [High-strength corrosionresistant steel]: pat. 2318068 Ros. Federacija; opubl. 21.11.2005.

    16. Mokrinskij V.I. Proizvodstvo boltov holodnoj obꞌꞌemnoj shtampovkoj [Production of cold forging bolts]. M.: Metallurgija. 1978. 71 s.

    17. Misozhnikov V.M., Grinberg M.Ja. Tehnologija holodnoj vysadki metalla [Technology cold heading metal]. M.: Mashgiz. 1951. 310 s.

    18. Vysokoprochnaja korrozionnostojkaja stal' i izdelie, vypolnennoe iz nee [High-strength and corrosion-resistant steel product made from it]: pat. 2214474 Ros. Federacija; opubl. 20.10.2003.

    19. Tonysheva O.A., Voznesenskaja N.M., Eliseev Je.A., Shal'kevich A.B. Issledovanie novoj vysokoprochnoj jekonomnolegirovannoj azotosoderzhashhej stali povyshennoj nadezhnosti [Investigation of a new high-nitrogen-containing steel ehkonomnolegirovannyh increased reliability] //Vestnik MGTU im. N.Je. Baumana. 2011. №SP2. S. 17–20.

    20. Lukin V.I., Voznesenskaja N.M.. Koval'chuk V.G., Golev E.V., Samorukov M.L. Svarka vysokoprochnoj korrozionno-stojkoj stali VNS-72 [Welding of high-strength corrosion-resistant steel VNS-72] //Svarochnoe proizvodstvo. 2012. №10. S. 31–35.

    21. Tonysheva O.A., Voznesenskaja N.M., Shal'kevich A.B., Petrakov A.F. Issledovanie vlijanija vysokotemperaturnoj termomehanicheskoj obrabotki na strukturu, tehnologicheskie, mehanicheskie i korrozionnye svojstva vysokoprochnoj korrozionnostojkoj stali perehodnogo klassa s povyshennym soderzhaniem azota [Investigation of the influence of high-temperature thermomechanical treatment on the structure, process, mechanical and corrosion properties of high-grade stainless steel transition with a high content of nitrogen] //Aviacionnye materialy i tehnologii. 2012. №3. S. 31–36.

    22. Panin V.E., Kablov E.N., Pleshanov V.S., Klimenov V.A., Ivanov Ju.F., Pochivalov Ju.I., Kibitkin V.V., Naprjushkin A.A., Nehoroshkov O.N., Lukin V.I., Sapozhnikov S.V. Vlijanie ul'trazvukovoj udarnoj obrabotki na strukturu i soprotivlenie ustalosti svarnyh soedinenij vysokoprochnoj stali VKS-12 [Effect of ultrasonic treatment on the structure of the shock and fatigue resistance of welded joints of high-strength steel VKS-12] //Fizicheskaja mezomehanika. 2006. T. 9. №2. S. 85–96.

    23. Markova E.S., Jakusheva N.A., Pokrovskaja N.G., Shal'kevich A.B. Tehnologicheskie osobennosti proizvodstva martensitostrejushhej stali VKS-180 [Technological features of production martensitostreyuschey steel VKS-180] //Trudy VIAM. 2013. №7. St. 01 (viam-works.ru). 

    24. Shherbakov A.I., Mosolov A.N., Kalicev V.A. Vosstanovlenie tehnologii poluchenija berillijsoderzhashhej stali VNS-32-VI [Recovery technology of beryllium steel VNS-32-VI] //Trudy VIAM. 2014. №5. St. 01 (viam-works.ru).

    25. Razuvaev E.I., Kapitanenko D.V. Vlijanie termomehanicheskoj obrabotki na strukturu i svojstva austenitnyh stalej [Effect of thermomechanical treatment on the structure and properties of austenitic steels] //Trudy VIAM. 2013. №5. St. 01 (viam-works.ru).

     

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7.

DOI: 10.18577/2071-9140-2014-0-3-33-37

UDC: 678.067.5

Pages:: 33-37

M.I. Vavilova1, N.S. Kavun2

[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

The properties of glass filler for constructions of fiberglass

In article is shown the properties of different types of glass fiber, fiber glass cloth uses in constructions of fiberglass. The results of investigations the fiberglass properties based on different types epoxy resin are present.

Keywords: filler, glass fiber, fiber glass cloth, polymeric composite material, fiberglass

Reference List

    1. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [Strategic directions of development of materials and technologies to process them for the period up to 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

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

    3. Kablov E.N. Aviakosmicheskoe materialovedenie [Aerospace Materials] //Vse materialy. Jenciklopedicheskij spravochnik. 2008. № 3. S. 2–14.

    4. Gutnikov S.I., Lazorjak B.I., Seleznjov A.N. Stekljannye volokna [Glass fibers]: Ucheb. posob. M.: MGU im. M.V. Lomonosova. 2010. 53 s.

    5. Borodulin A.S. Svojstva i osobennosti struktur stekljannyh volokon, ispol'zuemyh pri izgotovlenii stekloplastikov [Properties and features structures of glass fibers used in the manufacture of GRP] //Materialovedenie. 2012. №7. S. 34–37.

    6. Demonis I.M., Petrova A.P. Materialy VIAM v kosmicheskoj tehnike [VIAM materials in space technology] //Vse materialy. Jenciklopedicheskij spravochnik. 2011. №6. S. 2–9.

    7. Davydova I.F., Kavun N.S. Stekloplastiki – mnogofunkcional'nye kompozicionnye materialy [GRP – multifunctional composite materials] //Aviacionnye materialy i tehnologii. 2012. №S. 

    S. 253–260.

    8. Mihajlin Ju.A. Konstrukcionnye polimernye kompozicionnye materialy [Structural polymer composite materials]. M.: «HOT». 2008. 820 s.

    9. Melehina M.I., Kavun N.S., Rakitina V.P. Vlijanie himicheskogo sostava i struktury stekljannyh napolnitelej na svojstva jepoksidnyh stekloplastikov [Effect of chemical composition and structure of glass fillers on properties of epoxy GRP] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. №10. S. 44–47.

    10. Kondratenko A.N., Golubkova T.A. Polimernye kompozicionnye materialy v izdelijah zarubezhnoj raketno-kosmicheskoj tehniki (obzor) [Polymer composite materials in products overseas rocket and space technology (Review)] //Konstrukcii iz kompozicionnyh materialov. 2009. №2. S. 24–34.

    11. Bazhenov S.L., Berlin A.A., Kul'kov A.A., Oshmjan V.G. Polimernye kompozicionnye materialy [Polymer composite materials]. Dolgoprudnyj: «Intellekt». 2010. 352 s.

    12. Muhametov R.R., Ahmadieva K.R., Chursova L.V., Kogan D.I. Novye polimernye svjazujushhie dlja perspektivnyh metodov izgotovlenija konstrukcionnyh voloknistyh PKM [New polymeric binders for advanced manufacturing techniques of structural fibrous RMB] //Aviacionnye materialy i tehnologii. 2011. №2. S. 38–42.

    13. Dushin M.I., Hrul'kov A.V., Muhametov R.R. Vybor tehnologicheskih parametrov avtoklavnogo formovanija detalej iz polimernyh kompozicionnyh materialov [Selection of process parameters autoclave molding parts made of polymer composites] //Aviacionnye materialy i tehnologii. 2011. №3. S. 20–26.

    14. Jepoksidnoe svjazujushhee, prepreg na ego osnove i izdelie, vypolnennoe iz nego [Epoxy binder prepreg on its base and a product made therefrom]: pat. 2424259 Ros. Federacija; opubl. 22.10.2009.

    15. Fiziko-himicheskie osnovy tehnologii kompozicionnyh materialov [Physico-chemical fundamentals of composite materials]: Ucheb. posob. M.: MISiS. 2011. 163 s.

    16. Sokolov I.I., Raskutin A.E. Ugleplastiki i stekloplastiki novogo pokolenija [Carbon and fiberglass new generation] //Trudy VIAM. 2013. №4 (viam-works.ru).

    17. 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 [Investigation of the influence of climatic factors and mechanical loading on the structure and mechanical properties of the PCM] //Aviacionnye materialy i tehnologii. 2011. №4. S. 41–45.

    18. Zorin V.A. Opyt primenenija kompozicionnyh materialov v izdelijah aviacionnoj i raketno-kosmicheskoj tehniki [Experience of using composite materials in products aviation and space technology] //Konstrukcii iz kompozicionnyh materialov. 2011. №4. S. 44–58.

    19. Vlasenko F.S., Raskutin A.E. Primenenie polimernyh kompozicionnyh materialov v stroitel'nyh konstrukcijah [Application of polymer composites in structures] //Trudy VIAM. 2013. №8. St. 03 (viam-works.ru).

     

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8.

DOI: 10.18577/2071-9140-2014-0-3-38-44

UDC: 667.638.2

Pages:: 38-44

L.V. Semyonova1, N.I. Nefyodov2

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

Application of modified epoxy primers in the painting systems

To improve the reliability of protection products aviation technology (AT) developed modified epoxy primer VG-27, VG-34 and EP-0215M. The results of comparative tests with domestic and imported materials. Developed in VIAM primer VG-27, VG-34 and EP-0215M have better adhesion properties, water resistance, heat resistance, resistance to aviation fluids, as well as more environmentally friendly compared with domestic and foreign analogs. Modified epoxy primer can be used in coating systems with acrylic, epoxy, polyurethane enamels and able to protect a new generation of AT products.

Keywords: paint-and-lacquer materials, modified epoxy primers, painting systems, aviation materials

Reference List

    1. Chebotarevskij V.V., Kondrashov Je.K. Tehnologija lakokrasochnyh pokrytij v mashinostroenii [Coatings technology in mechanical engineering]. M.: Mashinostroenie. 1978. S. 214–220.

    2. Istorija aviacionnogo materialovedenija: VIAM – 75 let poiska, tvorchestva, otkrytij [History of aviation materials: VIAM – 75 years of searching, creativity, discovery] /Pod obshh. red. E.N. Kablov. M.: Nauka. 2007. S. 326–330.

    3. Kablov E.N. Korrozija ili zhizn' [Corrosion or life] //Nauka i zhizn'. 2012. №11. S. 16–21.

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

    5. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [Strategic directions of development of materials and technologies to process them for the period up to 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.

    6. Kondrashov Je.K., Kuznecova V.A., Semenova L.V., Lebedeva T.A., Malova N.E. Razvitie aviacionnyh lakokrasochnyh materialov [Development of aircraft paints and varnishes] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. №5. S. 49–54.

    7. 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 [Main directions of operational, technological and environmental performance coatings for aircraft] //Rossijskij himicheskij zhurnal. 2010. T. LIV. №1. S. 96–102.

    8. Chursova L.V., Kim M.A., Panina N.N., Shvecov E.P. Nanomodificirovannoe jepoksidnoe svjazujushhee dlja stroitel'noj industrii [Nanomodified epoxy binder for the construction industry] //Aviacionnye materialy i tehnologii. 2013. №1. S. 40–47.

    9. Kuznecova V.A., Kondrashov Je.K., Semenova L.V., Kuznecov G.V. O vlijanii formy chastic oksida cinka na jekspluatacionnye svojstva polimernyh pokrytij [On the influence of the form of zinc oxide particles on the performance properties of polymer coatings] //Materialovedenie. 2012. №12. S. 12–14.

    10. Kuznecova V.A., Deev M.S., Kondrashov Je.K., Kuznecov G.V. Vlijanie otverditelej na mikrostrukturu i svojstva modificirovannogo jepoksidnogo svjazujushhego dlja toplivostojkogo pokrytija [Effect hardeners microstructure and properties of the modified epoxy coating binder toplivostoykogo] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. №11. S. 38–41.

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9.

DOI: 10.18577/2071-9140-2014-0-3-45-54

UDC: 666.9-16

Pages:: 45-54

A.S. Chainikova1, L.A. Orlova2, N.V. Popovich3, Yu.E. Lebedeva1, S.St. Solncev4

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[2] Dmitry Mendeleev University of Chemical Technology of Russia
[3] D. MENDELEEV UNIVERSITY OF CHEMICAL TECHNOLOGY OF RUSSIA, rector@muctr.ru
[4] ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS, admin@viam.ru

Dispersion reinforced composites based on glass/glass-ceramics matrixes: properties and possible applications (review)

Development of the defense and civil industry is impossible without development of new materials suitable for work in the conditions of high temperatures, dynamic loads and hostile environment. Perspective composites based on glass/glass-ceramic matrixes (SKKM). In this article the overview of modern scientific and patent literature devoted to creation and studying of dispersion reinforced SKKM is provided. Glass/glass-ceramic matrixes of different chemical and phase composition and discrete fillers of the different nature and form are considered. The tendency to application of hard silicate and alumina-silica glasses and glass-ceramics as matrixes, and high-temperature nonoxide substances (carbides or nitrides) as fillers is shown. As the specific areas development of biocomposites and creation of nanocomposites on the basis of carbon nanotubes are allocated. Methods for the production and mechanical properties of glass/glass-ceramic matrixes composites (fracture toughness, elastic modulus, flexural strength) reached for the last decade are presented. It is shown that the greatest value of fracture toughness (K 1 с=8,9 MPa √m) is reached for BAS glass-ceramics by means of introduction of 70% wt. of silicon nitride grains. At the smaller concentration of filler (up to 30%) the greatest K 1 с (6,7 MPa √m) is received for composites on the basis of SAS glass-ceramics and 30% vol. of α-Si 3N 4 particles. Possible toughening mechanisms of brittle matrixes at introduction of discrete fillers are considered (crack deflection and crack bridging, debonding and pull-out of filler). Possible applications of the dispersion reinforced glass/glass-ceramic composites in aviation and space engineering, power system and nuclear power, metallurgy, automotive industry and the chemical industry are shown.

Keywords: composite materials, glass, glass-ceramics, discrete fillers

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Полнотекстовая версия
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10.

DOI: 10.18577/2071-9140-2014-0-3-55-61

UDC: 621.775.8

Pages:: 55-61

A.M. Zimichev1, E.P. Solovjeva2

[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

Zirconia fiber for High Temperature Application (review)

Review of literature sources on receiving and use of zirconia fibers. The zirconia ceramics possesses low heat conductivity, high melting temperature, high chemical stability, especially water- and alkali resistance. Now developers consider zirconia fibers for use as high-temperature thermal insulation.

Keywords: zirconia, precursor, spinning solution, high temperature thermal insulation, sol-gel method

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    26. Grashhenkov D.V., Shhetanov B.V., Tinjakova E.V., Shheglova T.M. O vozmozhnosti ispol'zovanija kvarcevogo volokna v kachestve svjazujushhego pri poluchenii legkovesnogo teplozashhitnogo materiala na osnove volokon Al2O3 [The possibility of using a silica fiber as a binder in the preparation of a lightweight heat-fiber-based material Al2O3] //Aviacionnye materialy i tehnologii. 2011. №4. S. 8–14. 

    27. Kirienko T.A., Solov’eva E.P., Balinova Yu.A. Physical-chemical Properties of Spinning Solutions for Aluminum-Silicate Fibrous Materials //Glass and Ceramics. 2013. T. 70. №7–8. 

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    28. Shhetanov B.V., Balinova Ju.A., Ljuljukina G.Ju., Solov'eva E.P. Struktura i svojstva nepreryvnyh polikristallicheskih volokon α-Al2O3 [Structure and properties of continuous polycrystalline α-Al2O3 fibers] //Aviacionnye materialy i tehnologii. 2012. №1. S. 13–17. 

    29. Kablov E.N., Shhetanov B.V., Ivahnenko Ju.A., Balinova Ju.A. Perspektivnye armirujushhie vysokotemperaturnye volokna dlja metallicheskih i keramicheskih kompozicionnyh materialov [Prospective reinforcing fibers for high temperature ceramic composites and metal materials] //Trudy VIAM. 2013. №2. St. 05 (viam-works.ru).

    30. Kablov E.N., Shhetanov B.V., Ivahnenko Ju.A., Balinova Ju.A., Semenova E.V. Volokna dioksida cirkonija dlja novogo pokolenija materialov aviacii i kosmosa [Zirconia fibers for a new generation of materials Air and Space] /V sb. materialov 25-j Mezhdunarodnoj konf. «Kompozicionnye materialy v pro-myshlennosti». Jalta. 2005. S. 320–323. 

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    32. Ivahnenko Ju.A., Babashov V.G., Zimichev A.M., Tinjakova E.V. Vysokotemperaturnye teploizoljacionnye i teplozashhitnye materialy na osnove volokon tugoplavkih soedinenij [High-temperature and heat-insulating materials based on fibers of refractory compounds] //Aviacionnye materialy i tehnologii. 2012. №S. S. 380–386. 

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    34. Solncev St.S. Jerozionnostojkie vlagozashhitnye termoregulirujushhie pokrytija mnogorazovoj teplozashhity orbital'nogo korablja «Buran» [Erosion-resistant waterproof coating thermostatic reusable thermal protection orbiter «Buran»] //Aviacionnye materialy i tehnologii. 2013. №S1. S. 94–124.

     

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11.

DOI: 10.18577/2071-9140-2014-0-3-62-66

UDC: 620.17

Pages:: 62-66

A.V. Ilichev1, A.E. Raskutin1

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

Research of stress concentrator influence on stress-strain state of carbon by digital images correlation method

Researches of influence of the concentrator of tension (in the form of the filled and open hole) on deformation field of samples carbon composites are provided by optical method of correlation of digital images. In the course of research the local area intense the deformed condition, initiated by the concentrator has been revealed. Values of fields of deformations are compared at the filled and open hole.

Keywords: method of correlation of digital images, concentrator of tension, plastic strain, carbon composites, composite material

Reference List

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    14. Muhametov R.R., Ahmadieva K.R., Chursova L.V., Kogan D.I. Novye polimernye svjazujushhie dlja perspektivnyh metodov izgotovlenija konstrukcionnyh voloknistyh PKM [New polymeric binders for advanced manufacturing techniques of structural fibrous RMB] //Aviacionnye materialy i tehnologii. 2011. №2. S. 38–42.

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12.

DOI: 10.18577/2071-9140-2014-0-3-67-71

UDC: 678.8

Pages:: 67-71

M.M. Grigoriev1, D.I. Kogan1, Y.A. Gusev1, Y.M. Gurevich1

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

Features of producing composites вy vacuum molding of prepreg

The results of the research process of obtaining PCM vacuum-formed package prepreg. The data obtained by varying the thickness of samples of plastics, depending on the technology of semi-prepreg.

Keywords: out-of-autoclave molding, prepreg, semi-prepreg, resin content, porosity, thick-walled products, polymeric composites

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    22. Dushin M.I., Hrul#kov A.V., Muhametov P.P. Vybor tehnologicheskih parametrov avtoklavnogo formovanija detalej iz polimernyh kompozicionnyh materialov [Selection of process parameters autoclave molding parts made of polymer composites] //Aviacionnye materialy i tehnologii. 2011. №3. S. 20–26.

    23. Doneckij K.I., Hrul'kov A.V., Kogan D.I., Belinis P.G., Luk'janenko Ju.V. Primenenie objemno-armirujushhih preform pri izgotovlenii izdelij iz PKM [Application of space-reinforcing preforms during the production of PCM] //Aviacionnye materialy i tehnologii. 2013. №1. S. 35–39.

     

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