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Aviation materials and technologies №4, 2015

Contents

  • Yu.Yu. Klochkova, G.G. Klochkov, V.A. Romanenko, V.I. Popov

    Structure and properties of sheets from high-strength aluminum-lithium alloy V-1469

    3-8
  • S.A. Krylov, E.S. Markova, A.I. Shcherbakov, N.A. Yakusheva

    Metallurgical features of smelting process of high-strength maraging steel VKS180-ID microalloyed by REM

    14-20
  • S.V. Ovsepyan, M.V. Akhmedzyanov, I.S. Mazalov, O.I. Rastorgueva

    Alloying by carbon of superalloy of the Ni-Co-Cr-W-Ti system strengthened by thermo-chemical treatment

    21-24
  • D.E. Kablov, M.S. Belyaev, V.V. Sidorov, P.G. Min

    The influence of sulfur and phosphorus impurities on low cycle fatigue of single crystals of ZhS36-VI alloy

    25-28
  • E.N. Azarovsky, S. A. Muboyadzhyan

    Surface modification of parts from structural steel in vacuum-arc titanium plasma. Part III

    29-37
  • E.N. Kablov, O.V. Startsev

    The basic and applied research in the field of corrosion and ageing of materials in natural environments (review)

    38-52
  • S.S. Vinogradov, A.A. Nikiforov, S.V. Balakhonov

    Cadmium replacement. Part 1. Improving of protective property of zinc coatings: thermo-immersed and modified coatings

    53-60
  • I.A. Kozlov, V.A. Duyunova

    Influence of filling in solution of sodium silicate solute on electrochemical properties of theVML20 alloy plasma electrolytic coating

    61-66
  • Y.A. Khokhlov, V.A. Bogatov, A.G. Krynin, O.V. Popkov

    Control of reactive deposition of ITO coating on the emission spectrum of the plasma magnetron discharge

    67-71
  • S.I. Voinov, G.F. Zhelezina, N.A. Solovieva, G.A. Yamshchikova

    Environmental effects on properties of aramid fiber reinforced plastic manufactured by RTM method

    72-78
  • A.V. Stepanov, E.I. Kosarina, A.A. Demidov

    Computer radiograghy using photostimulated plates

    79-85
  • V.V. Murashov, S.I. Trifonova

    Quality control of polymer composite materials using ultrasonic time-of-flight velocimetric technique

    86-90
  • V.S. Erasov, E.I. Oreshko, A.N. Lutsenko

    Damageability of materials in tension testing

    91-94
Содержание номера
1.

DOI: 10.18577/2071-9140-2015-0-4-3-8

UDC: 669.715:669.884

Pages:: 3-8

Yu.Yu. Klochkova1, G.G. Klochkov1, V.A. Romanenko1, V.I. Popov2

[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

Structure and properties of sheets from high-strength aluminum-lithium alloy V-1469

An increase in weight efficiency of perspective aircraft is possible using aluminum-lithium alloys with low density. At present there is a problem of manufacturing of thin sheets from aluminum-lithium alloys by cold coil rolling in view of their low technological plasticity. Perspective high-strength alloy V-1469 developed by VIAM based on Al-Cu-Li system and additionally alloyed by Ag, Sc and Zr, possesses the improved technological plasticity. Industrial technology of coil rolling of thin sheets from V-1469 alloy has been developed. Temperature of hot rolling has been chosen. Effect of thermomechanical treatment on structure and mechanical properties of the sheets has been studied. Results of comprehensive investigation of mechanical, corrosion and operational properties are presented.

Keywords: alloy V-1469, Al–Cu–Li system, alloying, silver, scandium, zirconium, coil rolling, heat treatment, structure, mechanical properties, corrosion resistance

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3.

DOI: 10.18577/2071-9140-2015-0-4-14-20

UDC: 669.14.046.516

Pages:: 14-20

S.A. Krylov1, E.S. Markova1, A.I. Shcherbakov1, N.A. Yakusheva2

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute», admin@viam.ru
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Metallurgical features of smelting process of high-strength maraging steel VKS180-ID microalloyed by REM

One of the most promising high-strength steel for the production of high-loaded parts of landing gear, airframe and engine is steel VKS-180. However for achievement of high properties, including on large-size semi-finished products it is necessary to apply a multi-stage high-temperature heat treatment. The object of the study was deve-lopment of melting technology of steel VKS-180, which allows providing the decrease in carbon content, nitrogen, oxygen in steel (carbon - to 0,005%, nitrogen - to 0,003%, oxygen - to 0,004%) for the subsequent optimization of heat treatment process. Metallurgical features of melting of high-strength maraging steel VKS-180-ID in a vacuum induction (VI) furnace with remelting in a vacuum arc (VA) furnace using the chosen system of microalloying on the basis of REM and introduction of nickel oxide has been investigated.

Keywords: high-strength steel, maraging steel, melting, remelting, microalloying by REM, nickel oxide, deoxidation, gases, impurities, homogenization, forging, rolling, annealing, heat treatment, tensile strength, impact strength, ductility, nonmetallic inclusions, carbides, carbonitrides, grain size

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4.

DOI: 10.18577/2071-9140-2015-0-4-21-24

UDC: 669.245:621.78

Pages:: 21-24

S.V. Ovsepyan1, M.V. Akhmedzyanov2, I.S. Mazalov1, O.I. Rastorgueva2

[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

Alloying by carbon of superalloy of the Ni-Co-Cr-W-Ti system strengthened by thermo-chemical treatment

Influence of alloying by carbon on phase structure and properties of heat-resistant Ni-based superalloy of a new class of Ni-Co-Cr-W-Ti system strengthened by special chemical and thermal treatment is investigated. It is established that carbides, forming at high-temperature nitriding, restrain growth of grains and reduce the speed of nitrogen diffusion, form thermostable carboborides strengthening an alloy. The additive of carbon leads to increase in heat resistance and long-term strength.

Keywords: nitriding, nitrides, structure, thermo-chemical treatment, heat resistant Ni-based superalloy, alloying

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    14. Latyshev V.B. Zharoprochnye deformiruemye svarivaemye splavy dlja kamer sgoranija [Heat resisting deformable welded alloys for combustion tubes] /V kn. Aviacionnye materialy na rubezhe XX–XXI vekov: Nauch.-tehnich. sb. M.: VIAM. 1994. S. 273–278.

    15. Ahmedzjanov M.V., Skugorev A.V., Ovsepjan S.V., Mazalov I.S. Razrabotka resursosbe-regajushhej tehnologii poluchenija holodnokatanogo lista iz vysokozharoprochnogo sva-rivaemogo splava VZh171 [Development of resource-saving technology of receiving cold-rolled sheet from high-heat resisting welded alloy VZh171] //Proizvodstvo prokata. 2015. №1. S. 14–17.

    16. Bykov Ju.G., Ovsepjan S.V., Mazalov I.S., Romashov A.S. Primenenie novogo zharo-prochnogo splava VZh171 v konstrukcii perspektivnogo dvigatelja [Application of new VZh171 hot strength alloy in design of the perspective engine] //Vestnik dvigatelestroenija. 2012. №2. S. 246–249.

    17. Cobalt-Chromium-Iron-Nickel alloys amenable to nitride strengthening: pat. 8075839 US; publ. 13.12.2011.

    18. Petrova L.G., Chudina O.V. Primenenie metodologii upravlenija strukturoobrazova-niem dlja razrabotki uprochnjajushhih tehnologij [Application of methodology of management by structurization for development of strengthening technologies] //MiTOM. 2010. №5. S. 31–41.

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DOI: 10.18577/2071-9140-2015-0-4-25-28

UDC: 669.018.44:669.245

Pages:: 25-28

D.E. Kablov1, M.S. Belyaev2, V.V. Sidorov1, P.G. Min1

[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

The influence of sulfur and phosphorus impurities on low cycle fatigue of single crystals of ZhS36-VI alloy

The influence of sulfur and phosphorus impurities on low cycle fatigue of single crystals of ZhS36-VI alloy was investigated. The harmful sulfur and phosphorus influence on middle quantity of cycles to failure was established. Introduction of lanthanum, as additive, allowed neutralizing the harmful sulfur and phosphorus influence and lowering sulfur contents in the alloy thereby increasing middle quantity of cycles to failure.

Keywords: single crystal, sulfur, phosphorus, superalloy, low cycle fatigue, lanthanum

Reference List

    1. 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 heat resisting ZhS30-VI nickel alloy and development of effective ways of its refinement] //Aviacionnye materialy i tehnologii. 2012. №2. S. 32–36.

    2. Kablov D.E., Chabina E.B., Sidorov V.V., Min P.G. Issledovanie vlijanija azota na strukturu i svojstva monokristallov iz litejnogo zharoprochnogo splava ZhS30-VI [Research of influence of nitrogen on structure and properties of monocrystals from foundry ZhS30-VI hot strength alloy] //MiTOM. 2013. №8. S. 3–7.

    3. Kablov D.E., Sidorov V.V., Min P.G. Zakonomernosti povedenija azota pri poluchenii monokristallov zharoprochnogo nikelevogo splava ZhS30-VI i ego vlijanie na jekspluatacionnye svojstva [Patterns of behavior of nitrogen when receiving monocrystals of heat resisting ZhS30-VI nickel alloy and its influence on operational properties] //MiTOM. 2014. №1. S. 8–12.

    4. Sidorov V.V., Min P.G., Burcev V.T., Kablov D.E., Vadeev V.E. Komp'juternoe modeli-rovanie i jeksperimental'noe issledovanie reakcij rafinirovanija v vakuume slozhnolegirovannyh renijsoderzhashhih nikelevyh rasplavov ot primesej sery i kremnija [Computer modeling and pilot study of reactions of refinement in vacuum complex-alloyed reniysoderzhashchy nickel rasplavov from sulfur and silicon impurity] //Vestnik RFFI. 2015. №1 (85). S. 32–36.

    5. Min P.G., Gorjunov A.V., Vadeev V.E. Sovremennye zharoprochnye nikelevye splavy i jeffektivnye resursosberegajushhie tehnologii ih izgotovlenija [Modern heat resisting nickel alloys and effective resource-saving technologies of their manufacturing] //Tehnologija metallov. 2014. №8. S. 12–23.

    6. Kablov E.N., Bondarenko Ju.A., Echin A.B., Surova V.A., Kablov D.E. Razvitie processa napravlennoj kristallizacii lopatok GTD iz zharoprochnyh i intermetallidnyh splavov s monokristallicheskoj strukturoj [Development of process of the directed crystallization of blades of GTD from heat resisting and intermetallidny alloys with single-crystal structure] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. № SP. S. 20–25.

    7. 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 hot strength alloys received in the conditions of high-gradient directed crystallization] //Aviacionnye materialy i tehnologii. 2011. №4. S. 25–31.

    8. Birger I.A., Balashov B.F., Dul'nev R.A. i dr. Konstrukcionnaja prochnost' materialov i detalej gazoturbinnyh dvigatelej [Constructional durability of materials and details of gas turbine engines]. M.: Mashinostroenie. 1981. 222 s.

    9. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitija materialov i tehnologij ih pererabotki na period do 2030 goda» [Innovative development of VIAM Federal State Unitary Enterprise of GNTs Russian Federation on implementation «The strategic directions of development of materials and technologies of their processing for the period till 2030»] //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 3–33.

    10. Schijve J. Fatique of structures and materials. Berlin Heidelberg: Springer-Verlag. 2009. 185 s.

    11. Kablov E.N., Lomberg B.S., Ospennikova O.G. Sozdanie sovremennyh zharoprochnyh mate-rialov i tehnologij ih proizvodstva dlja aviacionnogo dvigatelestroenija [Creation of modern heat resisting materials and technologies of their production for aviation engine building] //Kryl'ja Rodiny. 2012. №3–4. S.34–38.

    12. Kablov E.N., Ospennikova O.G., Lomberg B.S., Sidorov V.V. Prioritetnye napravlenija razvitija tehnologij proizvodstva zharoprochnyh materialov dlja aviacionnogo dvigatelestroenija [The priority directions of development of production technologies of heat resisting materials for aviation engine building] //Problemy chernoj metallurgii i materialovedenie. 2013. №3. S. 47–54.

    13. Sposob poluchenija izdelija iz deformiruemogo zharoprochnogo nikelevogo splava [Way of receiving product from deformable heat resisting nickel alloy]: pat. 2387733 Ros. Federacija; opubl. 31.03.2009.

    14. Stepnov M.N., Shavrin A.V. Statisticheskie metody obrabotki rezultatov mehanicheskih ispytanij [Statistical methods of processing of results of mechanical tests]: Spravochnik. M.: Mashinostroenie. 2005. 400 s.

    15. Troshhenko V.T., Sosnovskij L.A. Soprotivlenie ustalosti metallov i splavov [Resistance of fatigue of metals and alloys]: Spravochnik. Ch. 1. K.: Naukova dumka. 1987. 510 s.

    16. Mehanik E.A., Min P.G., Gundobin N.V., Rastegaeva G.Ju. Opredelenie massovoj doli sery v zharoprochnyh nikelevyh splavah i staljah v diapazone koncentracij ot 0,0001 do 0,0009% (po masse) [Definition of mass fraction of sulfur in heat resisting nickel alloys and stalyakh in the range of concentration from 0,0001 to 0,0009% (on weight)] //Trudy VIAM. 2014. №9. St. 12. (viam-works.ru).

    17. 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.

    18. Kablov E.N., Logunov A.V., Sidorov V.V. Mikrolegirovanie RZM – sovremennaja tehnologija povyshenija svojstv litejnyh zharoprochnyh nikelevyh splavov [RZM microalloying – modern technology of increase of properties of cast heat resisting nickel alloys] //Perspektivnye materialy. 2001. №1. S. 23–24.

    19. Sidorov V.V., Min P.G. Rafinirovanie slozhnolegirovannogo nikelevogo rasplava ot primesi sery pri plavke v vakuumnoj indukcionnoj pechi (chast' 2) [Refinement complex-alloyed nickel rasplava from sulfur impurity when melting in the vacuum induction furnace (part 2)] //Jelektrometallurgija. 2014. №5. S. 26–30.

    20. Samsonov G.V., Vinickij I.M. Tugoplavkie soedinenija [High-melting connections]. M.: Metallurgija. 1976. 240 s.

    21. Filippov K.S., Burcev V.T., Sidorov V.V., Rigin V.E. Issledovanie poverhnostnogo natjazhenija i plotnosti rasplava nikelja, soderzhashhego primesi sery, fosfora i azota [Research of surface tension and density rasplava the nickel containing impurity of sulfur, phosphorus and nitrogen] //Fizika i himija obrabotki materialov. 2013. №1. S. 52–56.

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DOI: 10.18577/2071-9140-2015-0-4-29-37

UDC: 669.018.29

Pages:: 29-37

E.N. Azarovsky1, S. A. Muboyadzhyan2

[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

Surface modification of parts from structural steel in vacuum-arc titanium plasma. Part III

In this paper we consider the process of ion modifying of the surface of samples from compressor steel EI961 and EP866 in the titanium plasma by high-current vacuum-arc discharge (VAD) of ion-plasma unit (IPU) MAP-3 at constant vacuum arc current, identical processing time intervals and given parameters of bias voltage. The dependence of the temperature of the samples in deposition chamber of MAP-3 and the rate of specific weight change of the samples on bias voltage is obtained. Elemental composition of the samples after ion treatment is studied. It is shown that at VAD current of 300 A and bias voltage of 600 V the temperature of the samples from compressor steels does not exceed 600°C, as well as inversion voltage that determines transition from the condensation process to the process of ion etching is ~380 V for steel EP866 and is ~600 V for steel EI961.

Keywords: steel, vacuum arc, plasma, ion modification, thermally stimulated ion diffusion, ion etching, microstructure, electron microscopy

Reference List

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

    4. Kablov E.N., Mubojadzhjan S.A. Zharostojkie i teplozashhitnye pokrytija dlja lopatok tur-biny vysokogo davlenija perspektivnyh GTD [Heat resisting and heat-protective coverings for turbine blades of high pressure of perspective GTE] //Aviacionnye materialy i tehnologii. 2012. №S. S. 60–70.

    5. Kablov E.N., Mubojadzhjan S.A., Budinovskij S.A., Pomelov Ja.A. Ionno-plazmennye za-shhitnye pokrytija dlja lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] //Konversija v mashinostroenii. 1999. №2. S. 42–47.

    6. Kablov E.N., Mubojadzhjan S.A., Budinovskij S.A., Lucenko A.N. Ionno-plazmennye za-shhitnye pokrytija dlja lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] //Metally. 2007. №5. S. 23–34.

    7. Mubojadzhjan S.A., Aleksandrov D.A., Gorlov D.S. i dr. Zashhitnye i uprochnjajushhie ionno-plazmennye pokrytija dlja lopatok i drugih otvetstvennyh detalej kompressora GTD [Protective and strengthening ion-plasma coverings for blades and other responsible details of the GTE compressor] //Aviacionnye materialy i tehnologii. 2012. №S. S. 71–81.

    8. Mubojadzhjan S.A. Perspektivnye pokrytija dlja detalej aviadvigatelej [Perspective coverings for details of aircraft engines] //Voennyj parad. 2009. №1(91). S. 33–34.

    9. Kablov E.N., Mubojadzhjan S.A. Teplozashhitnye pokrytija dlja lopatok  turbiny vysoko-go davlenija perspektivnyh GTD [Heat-protective coverings for turbine blades of high pressure of perspective GTE] //Metally. 2012. №1. S. 5–13.

    10. Mubojadzhjan S.A., Galojan A.G. Kompleksnye termodiffuzionnye zharostojkie pokry-tija dlja bezuglerodistyh zharoprochnyh splavov na nikelevoj osnove [Complex thermodiffusion heat resisting coatings for carbon-free hot strength alloys on nickel basis] //Aviacionnye materialy i tehnologii. 2012. №3. S. 25–30.

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    12. 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 analytical model of determination of elastic stresses in multi-layer system at the solution of tasks on creation of high-temperature heat resisting coverings for working blades of aviation turbines] //Vestnik MGTU im. N.Je. Baumana. 2011. №SP2. S. 26–37.

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

    16. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitija materialov i tehnologij ih pererabotki na period do 2030 goda» [Innovative development of VIAM Federal State Unitary Enterprise of GNTs Russian Federation on implementation «The strategic directions of development of materials and technologies of their processing for the period to 2030»] //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 3–33.

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    20. Azarovskij E.N., Mubojadzhjan S.A. Modificirovanie poverhnosti detalej iz konstrukcionnyh stalej v vakuumno-dugovoj plazme titana. Ch. I. [Modifying of surface of details from constructional staly in vacuum and arc plasma of titanium. P. I] //Aviacionnye materialy i tehnologii. 2013. №3. S. 20–25.

    21. Azarovskij E.N., Mubojadzhjan S.A. Modificirovanie poverhnosti detalej iz konstrukcionnyh stalej v vakuumno-dugovoj plazme titana. Ch. II. [Modifying of surface of details from constructional staly in vacuum and arc plasma of titanium. P. II] //Aviacionnye materialy i tehnologii. 2014. №1. S. 3–11.

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DOI: 10.18577/2071-9140-2015-0-4-38-52

UDC: 620.193

Pages:: 38-52

E.N. Kablov1, O.V. Startsev1

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

The basic and applied research in the field of corrosion and ageing of materials in natural environments (review)

The review of the researches in the field of corrosion and ageing of materials was performed based on the proceedings of the II All-Russian scientific conference «Basic and applied research in the field of corrosion and ageing of materials in natural environments: problems and solutions». The review contains examples of modeling and prediction of the polymer composites stability in the natural environments, corrosion properties of aluminum alloys and parts of gas turbine engines, the efficiency of protective coatings, testing methods of building materials and objects of infrastructure. The most important issues of corrosion and climatic testing were reviewed and systematized.

Keywords: aviation materials, climatic testing, corrosion, ageing, microbiologically-influenced corrosion, protective coatings, modeling

Reference List

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Полнотекстовая версия
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DOI: 10.18577/2071-9140-2015-0-4-53-60

UDC: 621.357.74

Pages:: 53-60

S.S. Vinogradov1, A.A. Nikiforov1, S.V. Balakhonov2

[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»

Cadmium replacement. Part 1. Improving of protective property of zinc coatings: thermo-immersed and modified coatings

The comparative accelerated corrosion tests of modified and thermo-immersed zink and cadmium coatings, as well as adhesion and mechanical tests of properties of 30KhGSA and 30KhGSN2A steels has been carried out. Modified coatings were shown to have comparable protective properties with cadmium coatings in salt spray environment during 2060 hours test. The investigated coatings possess satisfactory adhesion to steel substrate that is approximately equal to laquer and paint coating. The technology of putting of the thermo-immersed and modified coatings does not affect on tendency of steels (including high-strength) to slow-brittle-destruction. The modified coating decreases short-term durability of the steel according to slow-brittle-destruction test after 48 hours immersion in salt spray chamber. In addition, the modified coating negatively influences on low-cyclic fatigue of the steels. Therefore, the modified coatings can be recommended for anti-corrosion protection of steels with strength less than 1350 MPa.

Keywords: thermo-immersed, modified, cadmium coatings, protection property, adhesion, mechanical properties of 30ХHGSA and 30HGSN2А steels

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9.

DOI: 10.18577/2071-9140-2015-0-4-61-66

UDC: 666.1.056:621.793.7

Pages:: 61-66

I.A. Kozlov1, V.A. Duyunova1

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

Influence of filling in solution of sodium silicate solute on electrochemical properties of theVML20 alloy plasma electrolytic coating

Magnesium alloys are of the utmost interest for modern aircraft industry thanks to the high-performance capabilities of specific strength, however currently the problem of protecting them from corrosion is not completely solved. The most perspective method of protection of magnesium alloys is plasma electrolytic oxidation. In this work efficiency of increase of protective properties of plasma electrolytic coating on cast magnesium alloy VML20 in a way of filling in a solution of sodium waterglass is investigated. The plasma electrolytic coating filled in solutions with different concentration of sodium waterglass solution was investigated by electrochemical method. Dependence of electrochemical properties of magnesium alloy-coating system from filling solution concentration of was determined.

Keywords: microarc oxidation, plasma electrolytic oxidation, anodic oxidation, anode oxide coatings, impregnation, magnesium alloys

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    23. Kozlova A.A., Kondrashov Je.K. Sistemy lakokrasochnyh pokrytij dlja protivokorro-zionnoj zashhity magnievyh splavov [Systems of paint coatings for anticorrosive protection of magnesium alloys] //Aviacionnye materialy i tehnologii. 2014. №2. S. 44–47.

    24. Kozlov I.A., Karimova S.A. Korrozija magnievyh splavov i sovremennye metody ih zashhity [Corrosion of magnesium alloys and modern methods of their protection] //Aviacionnye materialy i tehnologii. 2014. №2. S. 15–20.

    25. Karimova S.A., Kozlov I.A., Volkov I.A. Povyshenie zashhitnyh svojstv nemetallicheskih neorganicheskih pokrytij na magnievyh splavah [Increase of protective properties of non-metallic inorganic on magnesium alloys] //Trudy VIAM. 2014. №9. St. 09 (viam-works.ru).

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    27. Gnedenkov S.V., Sidorova M.V., Sinebrjuhov S.L., Antipov V.V., Buznik V.M., Volkova E.F., Sergienko V.I. Stroenie i svojstva pokrytij, poluchennyh metodom plazmennogo jelektroliticheskogo oksidirovanija na aviacionnyh magnievyh splavah [Structure and properties of the coverings received by method of plasma electrolytic oxidation on aviation magnesium alloys] //Aviacionnye materialy i tehnologii. 2013. №SP2. S. 36–45.

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DOI: 10.18577/2071-9140-2015-0-4-67-71

UDC: 542.42:629.7.023

Pages:: 67-71

Y.A. Khokhlov1, V.A. Bogatov2, A.G. Krynin3, O.V. Popkov4

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute», admin@viam.ru
[2] Federal State Unitary Enterprise «All-Russian Scientific Research Institute of Aviation Materials»
[3] Technoinfo ltd
[4] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Control of reactive deposition of ITO coating on the emission spectrum of the plasma magnetron discharge

The effect of process parameters on the magnetron plasma composition during reactive deposition of the ITO coating has been studied. A method for stabilization of the process parameters based on controlling the oxygen flow involving the monitoring of the indium and oxygen emission spectra lines intensities is proposed.

Keywords: planar magnetron, reactive deposition, optical control, emission spectroscopy, ITO coating

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11.

DOI: 10.18577/2071-9140-2015-0-4-72-78

UDC: 678.83

Pages:: 72-78

S.I. Voinov1, G.F. Zhelezina2, N.A. Solovieva2, G.A. Yamshchikova1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute», admin@viam.ru
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Environmental effects on properties of aramid fiber reinforced plastic manufactured by RTM method

An influence of climatic factors and working fluids on properties of VKO-21 AFRP (aramid fiber reinforced plastic) manufactured by RTM (resin transfer moulding) technology was investigated. It was shown that the VKO-21 AFRP has a high level of properties conservation under the influence of environmental factors (at least 81% of the initial value) and in this regard is not inferior to the conventional structural VKO-19 AFRP manufactured by autoclave molding.

Keywords: AFRP, aramid fiber, RTM, polymer composites

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    10. Kogan D.I., Chursova L.V., Petrova A.P. Polimernye kompozicionnye materialy, polu-chennye putem propitki plenochnym svjazujushhim [The polymeric composite materials received by impregnation by the film binding] //Vse materialy. Jenciklopedicheskij spravochnik. Kompozicionnye materialy. 2011. №11. S. 2–6.

    11. Chursova L.V., Dushin M.I., Hrul'kov A.V., Muhametov R.R. Osobennosti tehnologii izgotovlenija detalej iz kompozicionnyh materialov metodom propitki pod davleniem [Features of manufacturing techniques of details from composite materials impregnation method under pressure] /V sb. tezisov dokladov mezhotraslevoj nauch.-teh. konf. «Kompozicionnye materialy v aviakosmicheskom materialovedenii». M.: VIAM. 2009. S. 17.

    12. Hrul'kov A.V., Dushin M.I., Popov Ju.O., Kogan D.I. Issledovanija i razrabotka avtoklavnyh i bezavtoklavnyh tehnologij formovanija PKM [Researches and development of avtoklavny and bezavtoklavny technologies of formation of PСM] //Aviacionnye materialy i tehnologii. 2012. №S. S. 292–301.

    13. Timoshkov P.N., Kogan D.I. Sovremennye tehnologii proizvodstva polimernyh kompozicionnyh materialov novogo pokolenija [Modern production technologies of polymeric composite materials of new generation] //Trudy VIAM. 2013. №4 (viam-works.ru).

    14. Muhametov R.R., Ahmadieva K.R., Kim M.A., Babin A.N. Rasplavnye svjazujushhie dlja perspektivnyh metodov izgotovlenija PKM novogo pokolenija [Molten binding for perspective methods of manufacturing of PСM of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 260–265.

    15. 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 manufacturing of constructional fibrous PСM] //Aviacionnye materialy i tehnologii. 2011. №2. S. 38–42.

    16. Babin A.N. Svjazujushhie dlja polimernyh kompozicionnyh materialov novogo pokolenija [Binding for polymeric composite materials of new generation] //Trudy VIAM. 2013. №4 (viam-works.ru).

    17. Efimov V.A., Shvedkova A.K., Koren'kova T.G., Kirillov V.N. Issledovanie polimernyh konstrukcionnyh materialov pri vozdejstvii klimaticheskih faktorov i nagruzok v labo-ratornyh i naturnyh uslovijah [Research of polymeric constructional materials at influence of climatic factors and loadings in laboratory and natural conditions] //Aviacionnye materialy i tehnologii. 2013. №S2. S. 68–73.

    18. Kablov E.N., Starcev O.V., Krotov A.S., Kirillov V.N. Klimaticheskoe starenie kompozicionnyh materialov aviacionnogo naznachenija. III. Znachimye faktory starenija [Climatic aging of composite materials of aviation assignment. III. Significant factors of aging] //Deformacija i razrushenie materialov. 2011. №1. S. 34–40.

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

    20. Kirillov V.N., Starcev O.V., Efimov V.A. Klimaticheskaja stojkost' i povrezhdaemost' polimernyh kompozicionnyh materialov, problemy i puti reshenija [Climatic firmness and damageability of polymeric composite materials, problems and solutions] //Aviacionnye materialy i tehnologii. 2012. №S. S. 412–423.

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12.

DOI: 10.18577/2071-9140-2015-0-4-79-85

UDC: 620.192.63

Pages:: 79-85

A.V. Stepanov1, E.I. Kosarina2, A.A. Demidov2

[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»

Computer radiograghy using photostimulated plates

The article presents the results of research into the physical foundations of detection of radiation images in which ionic crystals with the addition of certain impurities, also known as photostimulated phosphors, play an important role. The photostimulated phosphors transform energy of the primary charged particles or x-ray photon into visible or ultraviolet spectrum. Saved energy is released by means of thermal and optical stimulation that leads to the light emission in the visible spectrum. The article gives the information about testing of hardware-software complex for x-ray control of the aircraft. Testing results including such parameters as attainable sensitivity of control, resolution limit, detectability of artificial and natural defects, cost and performance are compared with the corresponding results obtained by radiographic control. The area of possible application of the hardware-software complex for x-ray non-destructive control of aircraft was defined.

Keywords: radiography, radioscopic testing, standard X-ray images, flaws, quality levels, CR-plates

Reference List

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

    4. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Litejnye zharoprochnye nikelevye splavy dlja perspektivnyh aviacionnyh GTD [Cast heat resisting nickel alloys for perspective aviation GTD] //Tehnologija legkih splavov. 2007. №2. S. 6–16.

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    6. Stepanov A.V., Kosarina E.I., Savvina N.A., Usachev V.E. Makro- i mikroporistost' v splavah na osnove aljuminija i nikelja, obnaruzhenie ee rentgenoskopicheskimi metodami nerazrushajushhego kontrolja [The macro- and microporosity in alloys on the basis of aluminum and nickel, detection by its roentgenoscopic methods of non-destructive testing] //Aviacionnye materialy i tehnologii. 2012. №S. S. 423–430.

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    11. Zscherpel U., Ewert U., Bavendiek K.I. Possibilities and Limits of Digital Industrial Radiology: The new high contrast sensitivity technique – Examples and system theoretical analysis. DIR 2007 /In: International Symposium on Digital industrial Radiology and Computed Tomography. Lyon. 2007. P. 3–27.

    12. Lozhkova D.S., Stepanov A.V., Kosarina E.I. Komp'juternaja radiografija, rezul'taty prakticheskih issledovanij i vozmozhnost' zameny plenochnyh tehnologij [Computer radiography, results of practical researches and possibility of replacement of film technologies] //Vestnik MJeI. 2011. №3. S. 57–62.

    13. Sasanpur M.T., Kosarina E.I. Rekomendacii po vyboru anodnyh naprjazhenij pri rentgenovskom kontrole stal'nyh ob#ektov [Recommendations about choice of anode voltages at x-ray control of steel objects] //Defektoskopija. 2011. №5. S. 48–53.

    14. Lozhkova D.S., Stepanov A.V., Kosarina E.I. Komp'juternaja radiografija: rezul'taty prakticheskih issledovanij i vozmozhnost' zameny plenochnyh tehnologij [Computer radiography: results of practical researches and possibility of replacement of film technologies] /V sb. tezisov dokl. XVII Mezhdunarodnoj nauch.-tehnich. konf. «Radiojelektronika, jelektrotehnika i jenergetika». M.: MJeI TU. 2011. S. 468–469.

    15. Kosarina E.I., Stepanov A.V., Usachev V.E. Rentgenoskopicheskie ustanovki dlja reshenija nekotoryh zadach promyshlennoj defektoskopii [Roentgenoscopic installations for the solution of some problems of industrial defektoskopiya] /V sb. tezisov dokl. XIX Vserossijskoj nauch.-tehnich. konf. «Sovremennye metody i sredstva nerazrushaju-shhego kontrolja i tehnicheskoj diagnostiki». Samara. 2011. S. 245–246.

    16. ISO 17636-2 Non-destructive testing of welds Radiographic. Part 2. X- and gamma ray techniques with digital detectors. 2013. (E). 49 p.

    17. ISO 16371-1 Non-destructive testing – Industrial computed radiography with storage phosphor imaging plates. Part 1. Classification of systems. 2011(E). 25 p.

    18. ASTM E 2445–05 Standard Practice for Qualification and long-Term Stability of Computed Radiology Systems. 2010. 8 p.

    19. Stepanov A.V. Metody rentgenovskogo nerazrushajushhego kontrolja v proizvodstve aviacionnyh dvigatelej [Methods of x-ray non-destructive testing in production of aircraft engines] //Aviacionnye materialy i tehnologii. 2010. №3. S. 28–32.

    20. Kosarina E.I., Mihajlova N.A., Demidov A.A., Turbin E.M. Rentgenovskij kontrol' krupnogabaritnyh otlivok slozhnoj formy iz splavov gruppy «silumin» [X-ray control of large-size otlivka of difficult form from silumin group alloys] //Aviacionnye materialy i tehnologii. 2013. №2. S. 55–58.

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DOI: 10.18577/2071-9140-2015-0-4-86-90

UDC: 620.179

Pages:: 86-90

V.V. Murashov1, S.I. Trifonova2

[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

Quality control of polymer composite materials using ultrasonic time-of-flight velocimetric technique

Features of PCM structures and components tests using ultrasonic time-of-flight velocimetric technique and some - factors limiting the control sensitivity are considered in this paper. It is shown that the difference between the considered technique and the through transmission method is an increase in time of the elastic waves pulse passing through the tested material, which is determined not only by an increase of the passed path, but also by a decrease of the propagation velocity caused by transformation of the wave type.

Keywords: polymer composite material, ultrasonic velocimetric technique, time-of-flight technique, normal waves, phase velocity, group velocity

Reference List

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    22. Murashov V.V., Generalov A.S. Kontrol' mnogoslojnyh kleenyh konstrukcij nizkochastotnymi akusticheskimi metodami [Control of multi-layer kleeny designs by low-frequency acoustic methods] //Aviacionnye materialy i tehnologii. 2014. №2. S. 59–67.

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    37. Lange Ju.V. Akusticheskie nizkochastotnye metody i sredstva nerazrushajushhego kontrolja mnogoslojnyh konstrukcij [Acoustic low-frequency methods and means of non-destructive testing of multi-layer designs]. M.: Mashinostroenie. 1991. 272 s.

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DOI: 10.18577/2071-9140-2015-0-4-91-94

UDC: 620.172.254

Pages:: 91-94

V.S. Erasov1, E.I. Oreshko1, A.N. Lutsenko1

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

Damageability of materials in tension testing

Modern design on the principle of «safe damage» allows emergence and development in construction of the damage is not critical size, which during exploitation must be detected, and the design is repaired. Therefore, the registration process damage is an important practical task. The paper presents the process of damage to the sample from the metal material in static tensile and describing this process function damaging ω. Function damage ω varies from 0 - initial state of the sample, up to 1 destroyed or depleted deformation resource sample. The obtained graphs damage. The proposed danger of destruction to evaluate two functions: a function of damage and function speed damageability. As the main parameters that shape these features, the proposed timing and size of the plastic deformation.

Keywords: the principle of «safe injury» test, static stretching, time, elastic deformation, plastic deformation, the critical value of plastic deformation, damage, speed damageability

Reference List

    1. Erasov V.S. Fiziko-mehanicheskie harakteristiki kak osnovnye integralnye pokazateli kachestva aviacionnyh konstrukcionnyh materialov [Physicomechanical characteristics as main integral figures of merit of aviation constructional materials]: Metod. posobie. M.: VIAM. 2011. 16 s.

    2. Erasov V.S., Yakovlev N.O., Nuzhnyj G.A. Kvalifikatsionnye ispytaniya i issledovaniya prochnosti aviatsionnyh materialov [Qualification tests and researches of durability of aviation materials] //Aviacionnye materialy i tehnologii. 2012. №S. S. 440–448.

    3. Erasov V.S., Bajramukov R.R. Rol faktora vremeni pri provedenii mehanicheskih ispytanij, obrabotke dannyh i predstavlenii rezultatov [Role of factor of time at carrying out mechanical tests, data processing and representation of results] //Aviacionnye materialy i tehnologii. 2013. №S2. S. 62–67.

    4. Erasov V.S., Bajramukov R.R., Nuzhnyj G.A. Opredelenie skorosti plasticheskoj deformacii pri ispytanii na rastyazhenie [Speed sensing of plastic strain at tension test] //Zavodskaya laboratoriya. Diagnostika materialov. 2014. T. 80. №5. S. 61–63.

    5. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitiya materialov i tehnologij ih pererabotki na period do 2030 goda» [Innovative developments of FSUE «VIAM» SSC of RF on realization of «Strategic directions of the development of materials and technologies of their processing for the period until 2030»] //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 3–33.

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