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Aviation materials and technologies №S6, 2014

Contents

  • A.A. Berlin, A.S. Shteinberg, E.I. Krasnov, A.A. Shavnev, S.B. Lomov, B.M. Serpova

    Experimental study of receipt of layer composite materials by the method of electro-thermal explosion. Аssessment of residual stresses

    5-10
  • O.Y. Sorokin, S.S. Solntsev, S.A. Evdokimov, I.V. Osin

    Hybrid spark plasma sintering method: principle, posiibilities, future prospects

    11-16
  • V.V. Berezovsky, A.A. Shavnev, S.B. Lomov, Y.A. Kurganova

    RECEIVING AND THE ANALYSIS OF STRUCTURE OF THE DISPERSE STRENGTHENED COMPOSITE MATERIALS OF AL-SIC SYSTEM WITH THE DIFFERENT MAINTENANCE OF THE REINFORCING PHASE

    17-23
  • O.I. Grishina, A.A. Shavnev, V.M. Serpova

    Features of influence of structural parameters on mechanical properties of metallic composite material based on particle-reinforced aluminum alloys by silicon carbide

    24-27
  • A.N. Nayfkin, O.I. Grishina, A.A. Shavnev, Y.V. Loshhinin, S.I. Pahomkin

    THE INFLUENCE OF COMPOSITION OF HETEROGENEOUS SYSTEMS WITH A HIGH OF THE CARBIDE PHASE ON THERMO-PHYSICAL PROPERTIES

    28-34
  • E.I. Kurbatkina, D.V. Kosolapov, L.G. Khodykin, M.S. Nigmetov

    Influence of the silicon addition on the phase composition of aluminum composite materials reinforced with silicon carbide particles

    35-38
  • O.I. Grishina, V.M. Serpova, A.N. Zhabin, E.I. Kurbatkina

    The effect of heat treatment on specific electrical conductivity in aluminum composite material

    39-44
  • A.S. Chanikova, M.V. Voropaeva, L.A. Alexeeva, L.A. Orlova, V.I. Samsonov

    Current state of developments in the field of radio transparent cordierite glass-ceramics

    45-51
  • A.S. Chainikova, L.A. Orlova, N.V. Popovich, Yu.E. Lebedeva, S.St. Solncev

    Functional composites based on glass/glass-ceramics matrixes and discrete fillers: properties and possible applications

    52-58
  • Yu.E. Lebedeva, N.V. Popovich, L.A. Orlova, A.S. Chaynikova

    Synthesis and perspective application of materials in the Y2O3-Al2O3-SiO2 system

    59-66
  • Yu.E. Lebedeva, N.V. Popovich, L.A. Orlova, A.S. Chaynikova, D.V. Grachshencov

    Investigation of rheological properties at sol-gel synthesis of materials in Y2O3-SiO2 system

    67-72
Содержание номера
1.

DOI: 10.18577/2071-9140-2014-0-s6-5-10

UDC: 669.018.95

Pages:: 5-10

A.A. Berlin1, A.S. Shteinberg1, E.I. Krasnov2, A.A. Shavnev3, S.B. Lomov3, B.M. Serpova2

[1] FEDERAL STATE INSTITUTION OF SCIENCE INSTITUTE OF CHEMICAL PHYSICS N.N. SEMENOV OF THE RUSSIAN ACADEMY OF SCIENCES
[2] FEDERAL STATE UNITARY ENTERPRISE ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS
[3] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Experimental study of receipt of layer composite materials by the method of electro-thermal explosion. Аssessment of residual stresses

Described the study of the synthesis of layered metal composite material systems Ti-TiAl 3 obtained by the method of electro-thermal explosion. Research conducted at the facility electrothermal analyzer (ETA-100) belongs to the class of devices of thermal analysis (DTA, DSC and TGA), used to study mechanisms of physical-chemical transformations in condensed systems. For example, two systems layered composite materials: titanium-titanium diboride and titanium-titanium carbide shows the influence of residual stresses arising during cooling of the material in the process of synthesis and properties of layered materials, quantitative assessment of the impact of cooling from the temperature of the melting of titanium to room temperature.

Keywords: layered composite material, titanium, aluminium, titanium diboride, titanium carbide, intermetallide, electrothermal analyzer, synthesis, residual stresses

Reference List

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    16. Krasnov E.I., Shtejnberg A.S., Shavnev A.A., Berezovskij V.V. Issledovanie sloistogo metallicheskogo kompozicionnogo materiala sistemy Ti–TiAl3 [Research of layered metal composite material of Ti–TiAl3 system] //Aviacionnye materialy i tehnologii. 2013. №3. S. 16–19.

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2.

DOI: 10.18577/2071-9140-2014-0-s6-11-16

UDC: 621.365.5

Pages:: 11-16

O.Y. Sorokin1, S.S. Solntsev2, S.A. Evdokimov2, I.V. Osin2

[1] FEDERAL STATE UNITARY ENTERPRISE ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Hybrid spark plasma sintering method: principle, posiibilities, future prospects

The key principles and possibilities of a hybrid spark-plasma sintering method are highlighted. It was shown that the use of the hybrid spark-plasma sintering method comprising both conventional FAST/SPS, and induction heating by an induction coil can lead to the substantial decrease of the temperature across the sized samples. The main advantages of the hybrid FAST/SPS method versus the conventional hot pressing technique are listed. It was shown that a wide range of various materials can be manufactured by means of this method - high-temperature, composite, nanostructured and functionally graded ones.

Keywords: hybrid spark-plasma sintering, FAST/SPS, composite, ceramics, matrix

Reference List

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3.

DOI: 10.18577/2071-9140-2014-0-s6-17-23

UDC: 669.018.95

Pages:: 17-23

V.V. Berezovsky1, A.A. Shavnev2, S.B. Lomov2, Y.A. Kurganova3

[1] FEDERAL STATE UNITARY ENTERPRISE ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[3] Bauman Moscow State Technical University

RECEIVING AND THE ANALYSIS OF STRUCTURE OF THE DISPERSE STRENGTHENED COMPOSITE MATERIALS OF AL-SIC SYSTEM WITH THE DIFFERENT MAINTENANCE OF THE REINFORCING PHASE

Preparing of dispersion-reinforced Al-SiC with different SiC consist composite by powder metallurgy and mechanical alloying technology is offered. Experimental party of samples for mechanical properties researches is fabricated. Microstructure of fabricated samples is studied. Influence of source components technological treatment on MMC structure is searched. Depending of the mechanical properties from the reinforcement volume is studied.

Keywords: dispersion-reinforced composites, metal matrix composites, Al–SiC

Reference List

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4.

DOI: 10.18577/2071-9140-2014-0-s6-24-27

UDC: 669.018.95

Pages:: 24-27

O.I. Grishina1, A.A. Shavnev2, V.M. Serpova2

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

Features of influence of structural parameters on mechanical properties of metallic composite material based on particle-reinforced aluminum alloys by silicon carbide

This article provides an over view of hardening features of aluminum metal matrix composite reinforced with heat-resistant silicon carbide particles. We described the influence on mechanical properties of the difference in thermal expansion coefficient of matrix and reinforcing component and availability of residual thermal stress that arise in composite during producting. Was considered the mechanism of crack formation and growth during fatigue fracture, wich is observed at the interface, on within the reinforcing particles. Also examined the effect of interfacial interaction on the mechanism of fatigue failure and the influence of the interface condition on mechanical properties of the composite material.

Keywords: a metal composite material, silicon carbide particles, aluminum alloy

Reference List

    1. Aljuminievye splavy [Aluminum alloys] /V kn. Istorija aviacionnogo materialovedenija. VIAM – 80 let: gody i ljudi; Pod obshh. red. E.N. Kablova. M.: VIAM. 2012. S. 143–156. 

    2. 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.

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

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

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

    6. Kablov E.N., Gerasimov V.V., Visik E.M., Demonis I.M. Rol' napravlennoj kristallizacii v resursosberegajushhej tehnologii proizvodstva detalej GTD [Role of the directed crystallization in the resource-saving production technology of details of GTD] //Trudy VIAM. 2013. №3. St. 01 (viam-works.ru).

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

    8. 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 [Development of process of the directed crystallization of blades of GTD from hot strength alloys with single-crystal and composition structure] //Aviacionnye materialy i tehnologii. 2012. №1. S. 3–8.

    9. Kablov E.N., Shhetanov B.V., Grashhenkov D.V., Shavnev A.A., Njafkin A.N. Metallomatrichnye kompozicionnye materialy na osnove Al–SiC [Metalmatrix composite materials on the basis of Al–SiC] //Aviacionnye materialy i tehnologii. 2012. №S. S. 373–380.

    10. Kablov E.N., Chibirkin V.V., Vdovin S.M. Izgotovlenie, svojstva i primenenie teplootvodjashhih osnovanij iz MMK Al–SiC v silovoj jelektronike i preobrazovatel'noj tehnike [Manufacturing, properties and application of the heat-removing bases from Al–SiC MMK in power electronics and converting equipment] //Aviacionnye materialy i tehnologii. 2012. №2. S. 20–22.

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

    12. Zhang F., Sun P., Li X., Zhang G. A comparative study on microplastic deformation behavior in a SiCp/2024Al composite and its unreinforced matrix alloy //J. Mater. Lett. 2001. V. 49. №2. P. 69–74.

    13. Arsenault R.J., Taya M. Thermal residual stress in metal matrix composite //Acta Metall. 1987. V. 35. №3. P. 651–659.

    14. Lur'e S.A., Soljaev Ju.O. Modificirovannyj metod Jeshelbi v zadache opredelenija jeffektivnyh svojstv so sfericheskimi mikro- i nanovkljuchenijami [The modified method of Eshelbi in problem of determination of effective properties with spherical micro and nanoinclusions] //Vestnik PGTU. Mehanika. 2010. №1. S. 80–90.

    15. Beljaev M.S., Koshkin S.B., Gorbovec M.A. Opredelenie predela ustalosti zharoprochnogo splava sposobom stupenchatogo izmenenija nagruzki [Definition of fatigue value of hot strength alloy by way of step change of loading] //Aviacionnye materialy i tehnologii. 2011. №1. S. 27–30.

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    17. Erasov V.S., Nuzhnyj G.A. Zhestkij cikl nagruzhenija pri ustalostnyh ispytanijah [Rigid cycle of loading at fatigue tests] //Aviacionnye materialy i tehnologii. 2011. №4. S. 35–40.

    18. Volkov V.M., Mironov A.A. Ob#edinennaja model' obrazovanija i rosta ustalostnyh treshhin v koncentratorah naprjazhenij [The integrated model of education and growth of fatigue cracks in concentrators of tension] //Problemy prochnosti i plastichnosti. 2005. Vyp. 67. S. 20–25.

    19. Kumai S., King J.E., Knott J.F. Fatigue in SiC-particulate-reinforced aluminum alloy composites //Mater. Sci. and Eng. A. 1991. V. 146. P. 317–326.

    20. Treninkov I.A., Alekseev A.A., Zajcev D.V., Filonova E.V. Issledovanija fazovyh i strukturnyh izmenenij, a takzhe ostatochnyh naprjazhenij v processe vysokotemperaturnoj polzuchesti v splave VZhM4 [Researches of phase and structural changes, and also residual stresses in the course of high-temperature creep in VZhM4 alloy] //Aviacionnye materialy i tehnologii. 2011. №2. S. 11–19.

    21. King J.E., Bhattacharjee D. Interfacial effects on fatigue and fracture in discontinuously reinforced metal matrix composites //Materials Science Forum. 1995. V. 189–190. P. 43–56.

    22. Shan D., Nayeb-Hashemi H. Fatigue-life prediction of SiC particulate reinforced aluminum alloy 6061 matrix composite using AE stress delay concept //J. Mater. Sci. 1999. V. 34. №13. P. 3263–3270.

    23. 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 non-destructive testing] //Aviacionnye materialy i tehnologii. 2013. №1. S. 64–69.

    24. Li Y., Mohamed F.A. An investigation of creep behavior in an SiC–2124 Al composite //Acta Mater. 1998. V. 45. №11. P. 4775–4785.

    25. Tham L.M., Gupta M., Cheng L. Effect of limited matrix-reinforcement interfacial reactions on enhancing the mechanical properties of aluminum-silicon carbide composites //Acta Mater. 2001. V. 49. №16. P. 3243–3253.

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5.

DOI: 10.18577/2071-9140-2014-0-s6-28-34

UDC: 669.018.95

Pages:: 28-34

A.N. Nayfkin1, O.I. Grishina2, A.A. Shavnev3, Y.V. Loshhinin3, S.I. Pahomkin3

[1] FEDERAL STATE UNITARY ENTERPRISE ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS
[2] Federal state unitary enterprise «All-Russian scientific research institute of aviation materials
[3] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

THE INFLUENCE OF COMPOSITION OF HETEROGENEOUS SYSTEMS WITH A HIGH OF THE CARBIDE PHASE ON THERMO-PHYSICAL PROPERTIES

This article shows the theoretical aspects of the factors that determine the stacking density of silicon carbide particles in the volume of the composite material. Studies were carried out to determine the complex of thermo-physical properties (thermal conductivity, thermal expansion coefficient, specific heat), including a wide range of temperatures of aluminum composite materials reinforced with silicon carbide particles. Also in the article is presented the study of variance regularities of thermo-physical properties depending of the composition in order to create new multifunctional heterogeneous systems.

Keywords: thermo-physical properties, thermal conductivity, specific heat, thermal conductivity, thermal expansion coefficient, metal matrix composite (MMC), aluminum alloy, silicon carbide particles

Reference List

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

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

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    10. Aksenov A.A. Metallicheskie kompozicionnye materialy, poluchaemye zhidkofaznymi metodami [The metal composite materials received by liquid-phase methods] //Izvestija vuzov Cvetnaja metallurgija. 1996. №2. C. 34–46.

    11. Aljuminievye splavy [Aluminum alloys] /V kn. Istorija aviacionnogo materialovedenija. VIAM – 80 let: gody i ljudi; Pod obshh. red. E.N. Kablova. M.: VIAM. 2012. S. 143–156. 

    12. Kablov E.N., Shhetanov B.V., Grashhenkov D.V., Shavnev A.A., Njafkin A.N. Metallomatrichnye kompozicionnye materialy na osnove Al–SiC [Metalmatrix composite materials on the basis of Al–SiC] //Aviacionnye materialy i tehnologii. 2012. №S. S. 373–380.

    13. Kablov E.N., Grashhenkov D.V., Shhetanov B.V., Shavnev A.A., Njafkin A.N., Vdovin S.M., Nishhev K.N., Chibirkin V.V., Eliseev V.V., Jemih L.A. Metallicheskie kompozicionnye materialy na osnove Al–SiC dlja silovoj jelektroniki [Metal composite materials on the basis of Al–SiC for power electronics] //Mehanika kompozicionnyh materialov i konstrukcij. 2012. T. 2. №3. S. 359–368.

    14. Kablov E.N., Chibirkin V.V., Vdovin S.M. Izgotovlenie, svojstva i primenenie teplootvodjashhih osnovanij iz MMK Al–SiC v silovoj jelektronike i preobrazovatel'noj tehnike [Manufacturing, properties and application of the heat-removing bases from Al–SiC MMK in power electronics and converting equipment] //Aviacionnye materialy i tehnologii. 2012. №2. S. 20–22.

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

    16. Grinevich A.V., Lucenko A.N., Karimova S.A. Raschetnye harakteristiki metallicheskih materialov s uchetom vlazhnosti [Rated characteristics of metal materials taking into account humidity] //Trudy VIAM. 2014. №7. Ct. 10 (viam-works.ru).

    17. Goncharenko E.S., Trapeznikov A.V., Ogorodov D.V. Litejnye aljuminievye splavy (k 100-letiju so dnja rozhdenija M.B. Al'tmana) [Cast aluminum alloys (to the 100 anniversary since the birth of M.B. Altman)] //Trudy VIAM. 2014. №4. Ct. 02 (viam-works.ru).

    18. Kumai S., King J.E., Knott J.F. Fatigue in SiC-particulate-reinforced aluminum alloy composites //Mater. Sci. and Eng. A. 1991. V. 146. P. 317–326.

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    20. Dyban' Ju.P., Sichkar' Z.V., Shipilova L.A. Vlijanie frakcionnogo sostava formovochnyh smesej na svojstva samosvjazannogo karbida kremnija [Influence of fractional structure of forming mixes on properties of the self-connected silicon carbide] //Poroshkovaja metallurgija. 1982. №6. S. 16–23.

    21. Dyban' Ju.P. Strukturno-tehnologicheskie aspekty prochnosti samosvjazannogo karbida kremnija (SKK) [Structural and technological aspects of durability of the self-connected silicon carbide (SSC)] /Prepr. NAN Ukrainy. 98-1. Kiev: IPM im. I.N. Francevicha NAN Ukrainy. 1998. 64 s.

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6.

DOI: 10.18577/2071-9140-2014-0-s6-35-38

UDC: 669.018.95

Pages:: 35-38

E.I. Kurbatkina1, D.V. Kosolapov1, L.G. Khodykin2, M.S. Nigmetov2

[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

Influence of the silicon addition on the phase composition of aluminum composite materials reinforced with silicon carbide particles

This article describes the analysis of the Al-Si-C phase diagram. Were calculated the isothermal and polythermal sections. Silicon concentration in the matrix aluminum alloy was theoretically substantiated, which excludes the formation of aluminum carbide (Al4C3). To confirm theoretical calculations were conducted experimental studies, which confirm that in samples, containing silicon in an amount of ≥12% in the matrix aluminum alloy, the aluminum carbide formation does not occur. It was shown that the experimental values of Al4C3 amount significantly lower than estimated, due to short time of contact of molten aluminum and silicon carbide particles

Keywords: аluminum matrix composite material, silicon, silicon carbide, aluminum carbide, Al‒Si‒C phase diagram

Reference List

    1. Yang Z., Hea X., Wang L., Liu R., Hu H., Wang L., Qu X. Microstructure and thermal expansion behavior of diamond/SiC/(Si) composites fabricated by reactive vapor infiltration //Journal of the European Ceramic Society. 2014. V. 34, №5. P. 1139–1147.

    2. Aksenov A.A. Metallicheskie kompozicionnye materialy, poluchaemye zhidkofaznymi metodami [The metal composite materials received by liquid-phase methods] //Izvestija vuzov. Cvetnaja metallurgija. 1996. №2. S. 34–40.

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

    4. Aljuminievye splavy [Aluminum alloys] /V kn. Istorija aviacionnogo materialovedenija. VIAM – 80 let: gody i ljudi. Pod obshh. red. E.N. Kablova. M.: VIAM. 2012. S. 143–156. 

    5. 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.

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

    7. Kablov E.N., Grashhenkov D.V., Shhetanov B.V., Shavnev A.A., Njafkin A.N. Metallomatrichnye kompozicionnye materialy na osnove Al–SiC [Metalmatrix composite materials on the basis of Al–SiC] //Aviacionnye materialy i tehnologii. 2012. №S. S. 373–380.

    8. Kablov E.N., Grashhenkov D.V., Shhetanov B.V., Shavnev A.A., Njafkin A.N., Vdovin S.M., Nishhev K.N., Chibirkin V.V., Eliseev V.V., Jemih L.A. Metallicheskie kompozicionnye materialy na osnove Al–SiC dlja silovoj jelektroniki [Metal composite materials on the basis of Al–SiC for power electronics] //Mehanika kompozicionnyh materialov i konstrukcij. 2012. T. 2. №3. S. 359–368.

    9. Lee J.C., Ahn J.P., Shim J.H., Shi Z., Lee H.I. Control of the interface in SiC/Al composites // Scripta Materialia. 1999. V. 41. №8. P. 895–900.

    10. Mandal D., Viswanathan S. Effect of heat treatment on microstructure and interface of SiC particle reinforced 2124 Al matrix composite // Materials Characterization. 2013. V. 85. P. 73–81.

    11. Grinevich A.V., Lucenko A.N., Karimova S.A. Raschetnye harakteristiki metallicheskih materialov s uchetom vlazhnosti [Rated characteristics of metal materials taking into account humidity] //Trudy VIAM. 2014. №7. Ct. 10 (viam-works.ru).

    12. Goncharenko E.S., Trapeznikov A.V., Ogorodov D.V. Litejnye aljuminievye splavy (k 100-letiju so dnja rozhdenija M.B. Al'tmana) [Cast aluminum alloys (to the 100 anniversary since the birth of M.B. Altman)] //Trudy VIAM. 2014. №4. Ct. 02 (viam-works.ru).

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

    14. Li K., Jin X.-D., Yan B.-D., Li P.-X. Effect of SiC particles on fatigue crack propagation in SiC/Al composites // Composites. 1992. V. 23. №1. P. 54–58.

    15. Bruzzi M.S., McHugh P.E. Micromechanical investigation of the fatigue crack growth behaviour of Al–SiC MMCs // International Journal of Fatigue. 2004. V. 26. №8. P. 795–804.

    16. Lee J.C., Subramanian K.N. Failure behaviour of particulate-reinforced aluminium alloy composites under uniaxial tension // Journal of Materials Science. 1992. V. 27. P. 5453–5462.

    17. Lee J.-C., Byun J.-Y., Park S.-B., Lee H.-I. Prediction of Si contents to suppress the formation of Al4C3 in the SiCp/Al composite // Acta Materialia. 1998. V. 46. №5. P. 1771–1780. 

    18. Shin C.S., Huang J.C. Effect of temper, specimen orientation and test temperature on the tensile and fatigue properties of SiC particles reinforced PM 6061 Al alloy //International Journal of Fatigue. 2010. V. 32. №10. P. 1573–1581.

    19. Milejko S.T. Kompozity i nanostruktury [Composites and nanostructures] //Kompozity i nanostruktury. 2009. №1. S. 6–37.

    20. Shi Z., Gu M., Liu J., Liu G., Lee J., Zhang D., Wu R. Interfacial reaction between the oxidized SiC particles and Al–Mg alloys //Chinese Science Bulletin. 2001. V. 46. №23. P. 1948–1952.

    21. Du X., Gao T., Wu Y., Liu X. Effects of copper addition on the in-situ synthesis of SiC particles in Al–Si–C–Cu system //Materials & Design. 2014. V. 63. P. 194–199.

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DOI: 10.18577/2071-9140-2014-0-s6-39-44

UDC: 669.018.28

Pages:: 39-44

O.I. Grishina1, V.M. Serpova2, A.N. Zhabin2, E.I. Kurbatkina2

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

The effect of heat treatment on specific electrical conductivity in aluminum composite material

The article presents the experimental results analysis of the effect of different heat treatment (annealing) on the value of the conductivity of a composite material based on aluminum alloy reinforced with discrete carbon fibers. The problem of wetting of the carbon fibers by molten aluminum during infiltration and suggested ways to improve it was shown. Samples of aluminum metal matrix composite material using liquid-phase technology, such as the method of forced infiltration were prepared. Article also shows the influence of the volume fraction of the reinforcing filler to a value of conductivity.

Keywords: metal matrix composite (MMC), carbon fibers, specific electrical conductivity, heat treatment

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

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

    4. Aljuminievye splavy [Aluminum alloys] /V kn. Istorija aviacionnogo materialovedenija. VIAM – 80 let: gody i ljudi; Pod obshh. red. E.N. Kablova. M.: VIAM. 2012. S. 143–156. 

    5. Milejko S.T. Kompozity i nanostruktury [Composites and nanostructures] //Kompozity i nanostruktury. 2009. №1. S. 6–37.

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

    7. Kablov E.N., Shhetanov B.V., Grashhenkov D.V., Shavnev A.A., Njafkin A.N. Metallomatrichnye kompozicionnye materialy na osnove Al–SiC [Metalmatrix composite materials on the basis of Al–SiC] //Aviacionnye materialy i tehnologii. 2012. №S. S. 373–380.

    8. Kablov E.N., Grashhenkov D.V., Shhetanov B.V., Shavnev A.A., Njafkin A.N., Vdovin S.M., Nishhev K.N., Chibirkin V.V., Eliseev V.V., Jemih L.A. Metallicheskie kompozicionnye materialy na osnove Al–SiC dlja silovoj jelektroniki [Metal composite materials on the basis of Al–SiC for power electronics] //Mehanika kompozicionnyh materialov i konstrukcij. 2012. T. 2. №3. S. 359–368.

    9. Karabasova Ju.S. Novye materialy [New materials]. M.: MISiS. 2002. 736 s.

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DOI: 10.18577/2071-9140-2014-0-s6-45-51

UDC: 666.266.51

Pages:: 45-51

A.S. Chanikova1, M.V. Voropaeva2, L.A. Alexeeva2, L.A. Orlova3, V.I. Samsonov2

[1] FEDERAL STATE UNITARY ENTERPRISE ALL-RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS
[2] OJSC «ORPE «TECHNOLOGIYA»
[3] Dmitry Mendeleev University of Chemical Technology of Russia

Current state of developments in the field of radio transparent cordierite glass-ceramics

In recent years increasing interest of scientists are attracted by the glass-ceramic materials having advantages of technology of glass and crystal materials. The greatest practical application was received by cordierite glass-ceramics. It is caused by their technological effectiveness, high mechanical and thermal properties, high radio transparency and chemical resistance. In this article the main achievements in the field of synthesis, researches and technology of cordierite glass-ceramics for the last one and a half decades on world patent, scientific and technical data are considered. The main russian and foreign producers of cordierite glass-ceramics are given, the most known among them are: Corning Inc. (USA), Schott (Germany), Ohara Inc. (Japan), JSC «Fazar» and OJSC «ORPE «Technology». Results of recent researches, devoted to clarification of role of different nucleating agents, such as TiO2 and ZrO2, in processes of phase formation and formation of structure of cordierite glass-ceramics are shown. The data on development of new compositions of glass and properties of cordierite glass-ceramics received on their basis are provided. In conclusion the results of researches on creation of the radio transparent cordierite glass-ceramics with the increased thermal properties, carried out in OJSC «ORPE «Technology» are given.

Keywords: radio transparent cordierite glass-ceramics, nucleating agent, TiO2, ZrO2

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DOI: 10.18577/2071-9140-2014-0-s6-52-58

UDC: 666.9-16

Pages:: 52-58

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

Functional composites based on glass/glass-ceramics matrixes and discrete fillers: properties and possible applications

One of the most important problems of modern materials science is creation of the multifunctional materials, being characterized resistance to influence of high temperatures, dynamic loads and hostile environment. This problem can be solved by development of glass/glass-ceramic composite materials (SKKM) with special functional properties. In this paper the overview of modern scientific and patent literature devoted to creation and studying of functional SKKM with discrete fillers is provided. The most popular glass/glass-ceramic matrixes and the fillers used for their development are given. The tendency to creation of functional nanocomposites on the basis of carbon nanotubes (UNT) is shown. Structure and properties of these fillers are described. Methods for the production and functional properties of glass/glass-ceramic composite materials (electric conductivity, heat conductivity, thermal expansivity, dielectric and optical properties) reached for the last decade are presented. It is shown that the greatest number of works are deal with modification of electric and thermophysical properties of matrixes. The maximum increase of these properties is reached by means of introduction of carbon nanotubes. As one of the perspective directions in creation of SKKM with discrete fillers is noted the creation of luminescent materials. Among the possible applications of functional SKKM is allocated the creation of solid oxide fuel cells. Besides the great attention of scientists attracts creation of low temperature co-fired ceramics on the basis of SKKM perspective for integration, packaging and connection of different elements in uniform electronic modules.

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

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10.

DOI: 10.18577/2071-9140-2014-0-s6-59-66

UDC: 661.183.4-911.48

Pages:: 59-66

Yu.E. Lebedeva1, N.V. Popovich2, L.A. Orlova3, A.S. Chaynikova1

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

Synthesis and perspective application of materials in the Y2O3-Al2O3-SiO2 system

Phase formation processes of Y2O3-Al2O3-SiO2 system are considered. High melting temperature, low oxygen tranmittivity, low value of thermal expansion close to silicon carbide one - all this does yttrium silicates excellent components for protection silicon carbide materials from influence of high temperatures in oxidation atmosphere now.

Keywords: yttrium silicates, high temperature coatings, silicon carbide

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11.

DOI: 10.18577/2071-9140-2014-0-s6-67-72

UDC: 666.113.641ꞌ:541.182.642/644:620.192.42

Pages:: 67-72

Yu.E. Lebedeva1, N.V. Popovich2, L.A. Orlova3, A.S. Chaynikova1, D.V. Grachshencov4

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

Investigation of rheological properties at sol-gel synthesis of materials in Y2O3-SiO2 system

Data of rheological properties investigation of sol-gel solutions in the Y2O3-SiO2 system are presented in this work. Influence of initial reagent kinds, concentration and molar ration of water and alkoxides on the rheological properties and gel-formation processes is determined.

Keywords: sol-gel method, yttrium-silicate system, rheological properties, gel-formation

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