Archive - Электронный научный журнал "ТРУДЫ ВИАМ"

Articles

dx.doi.org/ 10.18577/2307-6046-2018-0-4-3-8

УДК 669.018.44:669.295

O.A. Bazyleva, Lutskaya S.A.

WAYS OF INCREASING CORROSION RESISTANCE OF SUPERALLOYS (review)

Ni-based superalloys are widely used in the aviation, energy and nuclear industries. They are used in conditions of high temperatures, stresses and corrosive medium, which is why the issue of oxidation resistance is actual. The article describes the results of recent studies aimed at increasing the corrosion resistance of high-temperature Ni-based alloys. Traditionally, the issue of increasing corrosion resistance is solved by a variation in the chemical composition. Elements such as aluminum and chromium contribute to the formation of a complex oxide film on the metal surface. This has a beneficial effect on the operational characteristics of the alloy. When analyzing the literature data, the results of studies carried out by the authors on intermetallic alloys were confirmed: doping of alloys with refractory elements such as Mo and Re has a negative effect on the corrosion resistance. Most actively carried out research work in the direction of additional alloying of materials with

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dx.doi.org/ 10.18577/2307-6046-2018-0-4-9-19

УДК 699.715:621.785.784

Antipov K.V., Astashkin A.I., Ovsyannikov B.V.

OPTIMIZATION OF ARTIFICIAL AGING OF FORGED AND ROLLED SEMI-FINISHED PRODUCTS FROM HEAT-RESISTANT ALUMINUM ALLOY AK4-1h.

The article presents the results of the study of the effect of aging regimes on the mechanical and corrosion properties of semi-finished products from AK4-1 alloy - rolled plates from 12 to 60 mm thick and forgings 135 and 225 mm thick. The temperature of artificial aging was varied in the range 190–200C, the holding time varied from 5 hours to 22 hours. It was found that with an increase in the holding time from 5 to 18 hours at a temperature of 190 and 200°C, the temporary resistance and the yield strength of the plates is reduced by 10–30 MPa, and in the interval of exposures of 14–18 hours the relative elongation of the plates decreases, especially in the altitude direction . The influence of the temperature-time parameters of aging on the propensity of plates to delaminating and intergranular corrosion in the investigated interval of aging regimes has not been revealed. The study of forgings from the AK4-1h alloy aged at 190 and at 200°C showed that the temporary resistance (

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Reference list

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dx.doi.org/ 10.18577/2307-6046-2018-0-4-20-27

УДК 669.175::669.884

M.V. Grigoriev, M.S. Oglodkov

INFLUENCE OF MACHINING ON MECHANICAL AND FATIGUE PROPERTIES OF SHEETS FROM ALUMINUM-LITHIUM ALLOYS 1441 AND V-1481

The state-of-the-art review of domestic and foreign literature on technologies of laser-beam and hydroabrasive cutting of semi-finished products from aluminum alloys is carried out. The main tendencies of development are revealed and the assessment of the current level of researches is carried out. Technological modes of milling, hydroabrasive and laser-beam cutting of sheets from alloy V-1481T1 1,5 and 3,0 mm thick and sheets from alloy 1441Т1 the 1,5 mm thick are investigated and fulfilled. It is established that at laser-beam cutting for sheets from alloy 1481 lack of defects (fin, not cuts) is provided at the radiant power not less than 3 and 4 kW respectively, thus the best quality of edges of the machine cut corresponds to the speed of 10 m/min. for both thickness, and for sheets from alloy 1441 – at the radiant power not less than 2 kW respectively, thus the best quality of edges of the machine cut corresponds to the speed of 7,5 m/min. The best quality of edge of leaf after

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dx.doi.org/ 10.18577/2307-6046-2018-0-4-28-37

УДК 667.621:678.8

R.R. Mukhametov, A.P. Petrova, Ponomarenko S.A., Dolgova E.V., Pavlyuk B.Ph.

PROPERTIES OF BINDER EDT-69N AND POLYMER COMPOSITES ON ITS BASIS

The binder EDT-69N is widely and efficiently used in industry as a part of different polymer composites. The article specifies the main types of materials, created on the basis of these binder, their compositions and application fields in the aviation industry. If it is necessary to obtain materials with improved properties, it is also recommended to modify the composition of the binder and its curing program. Evaluation of the influence of the filler type was carried out by comparing physico-chemical characteristics of the curing process of prepregs on the basis of the binder and the fillers used immediately after the preparation of the samples. For the analysis, thermal analysis methods (differential scanning calorimetry, differential thermal analysis (DTA), thermogravimetric analysis (TGA) and differential thermogravimetric analysis) and IR spectroscopy were used. Comparison of IR spectra of the binder before and after curing at different temperatures made it possible to reveal th

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18. Aleksashin V.M., Antyufeeva N.V. Razvitie metodov termicheskogo analiza v issledo-vaniyah polimernyh kompozicionnyh materialov [Development of methods of the thermal analysis in researches of polymeric composite materials] // 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: yubil. nauch.-tehnich. sb. M.: VIAM, 2007. S. 245–249.
19. Antyufeeva N.V., Aleksashin V.M., Zhelezina G.F., Stolyankov Yu.V. Metodicheskie podhody termoanaliticheskih issledovanij dlya ocenki svojstv prepregov i ugleplastikov [Methodical approaches of thermoanalytical researches for assessment of properties of prepregs and carbonfibers] // Prilozhenie k zhurnalu «Vse materialy. Enciklopedicheskij spravochnik». 2012. №4. S. 18–28.
20. Kutsevich K.E., Aleksashin V.M., Petrova A.P., Antyufeeva N.V. Issledovanie kinetiki reakcij otverzhdeniya kleevyh svyazuyushhih [Research of kinetics of reactions of curing of the glue binding] // Klei. Germetiki. Tehnologii. 2014. №11. S. 27–31.

dx.doi.org/ 10.18577/2307-6046-2018-0-4-38-50

УДК 669.046.516.2:669.018.95

B.V. Schetanov, R.M. Dvoretskov

RESEARCH OF PECULIARITIES OF MECHANICAL DECOMPOSITION IN SYNTHESIS OF IN-SITU COMPOSITES BASED ON REFRACTORY METALS

The article describes the method of mechanical alloying as an alternative for obtaining high-temperature materials based on niobium, the obtaining of which by traditional methods (casting technologies) entails great difficulties. Particular attention was paid to the control of intermediate operations related to the process of mechanical alloying. The evolution of the microstructure, phase and granulometric compositions of composite powders (CP) of the Nb–Si–Ti system at various stages of mechanical doping is considered. It is established that the process of mechanical doping consists of two processes: the actual alloying process, which is controlled by the time of powder formation with the X-ray amorphous structure and the process of creating a fractional composition controlled by a histogram of powder distribution in size. The choice of the most effective method of quality control of alloying KP was made. This method is XRF, the criterion of which is the amorphization of the structu

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10.Babich B.N., Kolupaeva S.Ya., Kustov Yu.A., Chernyak A.I., Shhetanov B.V. O poluchenii dispersno-uprochnennogo nikel-hromovogo splava metodom mehanicheskogo legirovaniya [About receiving disperse strengthened nickel-chrome alloy method of mechanical alloying] // Poroshkovaya metallurgiya. 1977. №2 (170). S. 53–57.
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15. Honghui X., Yong D., Zhaohui Y. et al. Phase equilibria of the Fe–Nb–Ti system at 900°C // Journal of Alloys and Compounds. 2005. P. 151–155.

dx.doi.org/ 10.18577/2307-6046-2018-0-4-51-58

УДК 620.197:669.017.165

D.S. Gorlov, D.A. Aleksandrov, Zaklyakova O.V., Azarovskiy E.N.

INVESTIGATION OF THE POSSIBILITY OF PROTECTION OF INTERMETALLIC TITANIUM ALLOY AGAINST FRETTING WEAR BY ION-PLASMA COATING

Analyzing the causes of failures of units and units of GTE in the course of their long-term operation, as well as the results of bench tests, came to the conclusion that the main cause of the origin of most fatigue defects, leading to destruction, is fretting. Among the various methods of applying protective and hardening coatings on contacting surfaces to prevent fretting, the most technological are vacuum-plasma and ion-implant processing technologies, as well as their combinations. This work was carried out within the framework of strategic direction 17. «Comprehensive anticorrosive protection, hardening, wear-resistant protective and heat-protective coatings». Complex problem 17.3. «Multi-Layer heat-resistant and heat-protective coatings, nanostructured reinforcing erosion and corrosion-resistant, wear-resistant, antifretting coatings to protect parts of the hot tract and compressor GTE and GTU» («Strategic directions of development of materials and technologies for their processi

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Reference list

1. Smyslov A.M., Selivanov K.S. Razrabotka i issledovanie tehnologicheskih metodov povysheniya fretting-stojkosti rabochih lopatok iz titanovyh splavov [Development and research of technological methods of increase fretting firmness of working blades from titani-um alloys] // Vestnik UGATU. Ser.: Mashinostroenie. T. 9. №1 (19). C. 77–83.
2. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlya vysokoteplonagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for the high-heatloaded details of gas turbine engines] // Vestnik MGTU im. N.E. Baumana. Ser.: Mashinostroenie. 2011. № SP2. S. 13–19.
3. Kablov E.N. Litye lopatki gazoturbinnyh dvigatelej. Splavy, tehnologii, pokrytiya. 2-e izd. [Cast blades of gas turbine engines. Alloys, technologies, coverings. 2nd ed.]. M.: Nauka, 2006. S. 531–534.
4. Muboyadzhyan S.A., Aleksandrov D.A., Gorlov D.S., Egorova L.P., Bulavinceva E.E. Zashhitnye i uprochnyayushhie ionno-plazmennye pokrytiya dlya 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.
5. Gorlov D.S., Skripak V.I., Muboyadzhyan S.A., Egorova L.P. Issledovanie fretting-iznosa tverdosmazochnogo, shlikernogo i ionno-plazmennogo pokrytij [The research of fretting-wear slip and ion-plasma coatings] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2017. №3. St. 07. Available at: http://www.viam-works.ru (accessed: March 12, 2018). DOI: 10.18577/2307-6046-2017-0-3-7-7.
6. Lesnevskij L.N. Fretting-korroziya pokrytij tipa «tverdaya smazka» v ekstremalnyh usloviyah ekspluatacii [Fretting corrosion of coverings of the solid lubricant type in extreme operating conditions] // Vestnik nauchno-tehnicheskogo razvitiya. 2009. №2 (18). S. 31–35.
7. Putyrskij S.V., Arislanov A.A., Artemenko N.I., Yakovlev A.L. Razlichnye metody povysheniya iznosostojkosti titanovyh splavov i sravnitelnyj analiz ih effektivnosti primen-itelno k titanovomu splavu VT23M [Different methods of wear resistance increase of titanium alloys and comparative analysis of their efficiency for VT23M titanium alloy] // Aviacionnye materialy i tehnologii. 2018. №1. S. 19–24. DOI: 10.18577/2071-9240-2018-0-1-19-24.
8. Muboyadzhyan S.A., Budinovskij S.A. Ionno-plazmennaja tehnologiya: perspektivnye processy, pokrytiya, oborudovanie [Ion-plasma technology: prospective processes, coatings, equipment] // Aviacionnye materialy i tehnologii. 2017. №S. S. 39–54. DOI: 10.18577/2071-9140-2017-0-S-39-54.
9. Kablov E.N., Muboyadzhyan S.A., Budinovskij S.A., Pomelov Ya.A. Ionno-plazmennye zashhitnye pokrytiya dlya lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] // Konversiya v mashinostroenii. 1999. №2. S. 42–47.
10. Sibileva S.V., Kozlova L.S. Obzor tehnologij polucheniya pokrytij na titanovyh splavah plazmennym elektroliticheskim oksidirovaniem [Review of technologies of applying coatings to titanium alloys by plasma electrolytic oxidation] // Aviacionnye materialy i tehnologii. 2016. №S2 (44). S. 3–10. DOI: 10.18577/2071-9140-2016-0-S2-3-10.
11. Selivanov K.S., Galiakbarov R.F. Povyshenie fretting-stojkosti detalej mashin kompleksnoj vakuumnoj plazmennoj obrabotkoj [Increase fretting firmness of details of machines com-plex vacuum plasma processing] // Aviacionno-kosmicheskaya tehnika i tehnologiya. 2011. №7 (84). S. 29–32.
12. Kablov E.N., Nochovnaya N.A., Panin P.V., Alekseev E.B., Novak A.V. Issledovanie struktury i svojstv zharoprochnyh splavov na osnove alyuminidov titana s mikrodobavkami gadoliniya [Research of structure and properties of hot strength alloys on the basis of titanium aluminides with gadolinium microadditives] // Materialovedenie. 2017. №3. S. 3–10.
13. Antipov V.V. Perspektivy razvitiya alyuminievyh, magnievyh i titanovyh splavov dlya izdelij aviacionno-kosmicheskoj tehniki [Prospects for development of aluminium, magnesium and titanium alloys for aerospace engineering] // Aviacionnye materialy i tehnologii. 2017. №S. S. 186–194. DOI: 10.18577/2107-9140-2017-0-S-186-194.
14. Novak A.V., Alekseev E.B., Ivanov V.I., Dzunovich D.A. Izuchenie vliyaniya parametrov zakalki na strukturu i tverdost intermetallidnogo titanovogo orto-splava VTI-4 [The study of the quenching parameters influence on structure and hardness of orthorhombic titanium alu-minide alloy VТI-4] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2018. №2. St. 05. Available at: http://www.viam-works.ru (accessed: March 12, 2018). DOI: 10.18577/2307-6046-2018-0-2-5-5.
15. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.
16. Kurzina I.A., Popova N.A., Nikonenko E.L. i dr. Formirovanie nanorazmernyh in-termetallidnyh faz v usloviyah implantacii ionami alyuminiya titanovyh mishenej [Forming of nanodimensional intermetallidny phases in the conditions of implantation by ions of aluminum of titanic targets ] // Izvestiya RAN. Ser.: Fizicheskaya. 2012. T. 76. №1. S. 74–78.

dx.doi.org/ 10.18577/2307-6046-2018-0-4-59-65

УДК 669.715

V.V. Antipov, I.A. Kozlov, I.A. Volkov, A.P. Petrova

SURFACE PREPARATION ALUMINUM ALLOY V-1469 BEFORE USE IN THE COMPOSITION OF LAYERED HYBRID MATERIAL

Despite the increased interest of designers to composite polymeric materials (PCM), aluminum alloys are the main structural material of the aviation industry. Particular attention is paid to aluminum-lithium alloys and hybrid materials based on them, such as SIAL, which are layered materials of a new generation. SIALs are layered hybrid metal-polymer materials, which consist of thin sheets of structural aluminum alloys and GRP based on adhesive melt-type binders and glass fiber fillers with different reinforcement structures. The article provides information on the preparation of the surface of the aluminum-lithium alloy V-1469, which was selected for use in SIAL for the manufacture of wing panel panels. In this paper, the issue of protecting such alloys from corrosion and giving their surfaces special properties, in particu-lar, ensuring good adhesion of epoxy adhesive binders, is considered. Various types of anodic oxidation of the surface of aluminum alloys for bonding are conside

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Reference list

1. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitiya materialov i tehnologij ih pererabotki na period do 2030 goda» [In-novative 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.
2. Kablov E.N. Strategicheskie napravleniya razvitiya 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 to 2030] // Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.
3. Karimova S.A., Pavlovskaya T.G. Razrabotka sposobov zashhity ot korrozii konstrukcij, rabotayushhih v usloviyah kosmosa [Development of corrosion protection methods for structures operating under space conditions] // Aviacionnye materialy i tehnologii. 2013. №S1. S. 35–40.
4. Antipov V.V. Strategiya razvitiya titanovyh, magnievyh, berillievyh i alyuminievyh splavov [Strategy of development of titanium, magnesium, beryllium and aluminum alloys] // Aviacionnye materialy i tehnologii. 2012. №S. S. 157–167.
5. Kablov E.N. Korroziya ili zhizn [Corrosion or life] // Nauka i zhizn. 2012. №11. S. 16–21.
6. Anihovskaya L.I., Pavlovskaya T.G., Dementeva P.A., Petrova A.P. Podgotovka poverhnosti pod skleivanie [Surface preparation under pasting] // Klei. Germetiki. Tehnologii. 2008. №7. S. 32–35.
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8. Kolobova Z.N., Pavlovskaya T.G., Anihovskaya L.I., Karimova S.A. Razrabotka sposobov podgotovki poverhnosti pri remonte kleenyh konstrukcij iz alyuminievyh splavov [Development of ways of surface preparation at repair of glued designs from aluminum alloys] // Aviacionnye materialy i tehnologii. M.: VIAM, 2002. Vyp.: Remontnye tehnologii v aviastroenii. S. 73–76.
9. Fridlyander I.N., Senatorova O.G., Lukina N.F., Antipov V.V. Sloistye alyumopolimernye materialy SIAL [SIAL layered aluminapolymeric materials] // 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007. M.: VIAM, 2007. S. 188–192.
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11. Karimova S.A., Pavlovskaya T.G., Petrova A.P. Podgotovka alyuminievyh splavov s primeneniem anodnogo oksidirovaniya [Preparation of aluminum alloys using anodic oxida-tion] // Klei. Germetiki. Tehnologii. 2014. №1. S. 34–48.
12. Averyanov E.E. Spravochnik po anodirovaniyu [Directory on anodizing]. M.: Mashinostroenie, 1988. 132 s.
13. Karimova S.A., Kutyrev A.E., Pavlovskaya T.G., Zaharov K.E. Nizkotemperaturnoe uplotnenie anodno-oksidnyh pokrytij na detalyah iz alyuminievyh splavov [Low temperature sealing of anodic oxide coatings on parts of aluminum alloys] // Aviacionnye materialy i tehnologii. 2014. №4. S. 9–17. DOI: 10.18577/2071-9140-2014-0-4-9-17.
14. Kurs M.G., Karimova S.A. Naturno-uskorennye ispytaniya: osobennosti metodiki i sposoby ocenki korrozionnyh harakteristik alyuminievyh splavov [Salt-accelerated outdoor corrosion testing: methodology and evaluation of corrosion susceptibility of aluminum alloy] // Aviacionnye materialy i tehnologii. 2014. №1. S. 51–57. DOI: 10.18577/2071-9140-2014-0-1-51-57.
15. Karimova S.A., Zhilikov V.P., Mihajlov A.P. Naturno-uskorennye ispytaniya alyuminievyh splavov v usloviyah vozdejstviya morskoj atmosfery [Natural accelerated tests of aluminum alloys in the conditions of influence of the sea atmosphere] // Korroziya: materialy i zashhita. 2012. №10. S. 1–3.
16. Petrova A.P., Donskoj A.A. Kleyashhie materialy. Germetiki: spravochnik [Gluing materials. Hermetics: directory]. SPb.: Professional, 2008. 589 s.
17. Petrovа A.P., Dementyevа L.A., Lukina N.F., Chursova L.V. [Adhesive binders for polymer composite materials based on carbon- and glass fillers] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №9. St. 11. Available at: http://www.viam-works.ru (accessed: Marcht 20, 2018). DOI: 10.18577/2307-6046-2015-0-9-11-11.

dx.doi.org/ 10.18577/2307-6046-2018-0-4-66-74

УДК 669.018.29:539.42

V.B. Grigorenko, L.V. Morozova, S.S. Vinogradov

FEATURES OF DESTRUCTION OF DETAILS OF FIXTURE FROM THE CONSTRUCTIONAL STEEL

Features of destruction of samples from steel 30ХГСА with galvanotermic coatings on the basis of zinc are analyzed. At formation of a break of the samples tested for grain-boundary brittle destruction, three areas differing on a structure are created. In a near surface zone under a sheeting the area of the maleficiated relief with destruction on the mechanism of a viscous cut is formed. Further the area with a rough relief in which it is possible to allocate a zone of the slowed-down destruction with brittle facets and a zone viscous dimple rupture is created. It is established that when testing for low-cycle fatigue samples from steel 30ХГСА with galvanotermic coatings the centers of destruction are risks or other defects on a steel surface under a covering. In an focal zone the fan-shaped relief is most often observed. In process of removal from the center of destruction fatigue plateaus and grooves are created. In break viscous poles are formed. Research of the destroyed axis made

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Reference list

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2. Kobayashi J., Ina D., Yoshikawa N., Sugimoto K. Effects of the addition of Cr, Mo and Ni on the microstructure and retained austenite characteristics of 0,2% C–Si–Mn–Nb ultra-highstrength TRIP-aided bainitic ferrite steels // ISIJ International. 2012. Vol. 52. No. 10. P. 1894–1901.
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9. Nikiforov A.A., Zakirova L.I., Vinogradov S.S. Termoimmersionnoe pokrytie cink + olovo kontaktnoe [Thermoimmersion covering zinc + tin contact ] // Korroziya: materialy, zashhita. 2016. №8. S. 34–41.
10. Taranceva K.R., Nikolotov A.D. Elektroosazhdenie splava olovo-cink iz stabilizirovannogo pirofosfatnogo elektrolita kak alternativa kadmievomu pokrytiyu [Alloy electrosedimentation tin-zinc from the stabilized pirofosfatny electrolit as alternative to cadmic covering] // Korroziya: materialy, zashhita. 2014. №3. S. 27–30.
11. Grinevich A.V., Erasov V.S., Yakusheva N.A., Terehin A.L. Ustalostnaya dolgovechnost stali VKS-9 v usloviyah simmetrichnogo nagruzheniya «rastyazhenie–szhatie» i «izgib s vrashheniem» [Fatigue life of steel VKS-9 in conditions of symmetric loading «tension–compression» and «bending with rotation»] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2017. №9. St. 11. Available at: http://www.viam-works.ru (accessed: February 05, 2018.). DOI: 10.18577/2307-6046-2017-0-9-11-11.
12. Gromov V.I., Krotov V.N., Kurpyakova N.A., Sedov O.V., Doroshenko A.V. Vliyanie ostatochnogo austenita na strukturu i svojstva diffuzionnogo sloya stali martensitnogo klassa posle vakuumnoj cementacii [Influence of residual austenite on the structure and properties of diffusion layer of martensitic grade steel after vacuum carburization] // Aviacionnye materialy i tehnologii 2016. №4 (45) S. 3–8. DOI: 10.18577/2071-9140-2016-0-4-3-8.
13. Gordeeva T.A., Zhegina I.P. Analiz izlomov pri ocenke nadezhnosti materialov [The analysis of breaks at assessment of reliability of materials]. M.: Mashinostroenie, 1978. 200 s.
14. Fonshtejn N.M., Bronfin B.M., Shirman A.Z. et al. Kolichestvennoe mikrofrak-tograficheskoe issledovaniya vyazkogo razrusheniya v nizkolegirovannyh stalyah [Quantitative microfractographic researches of viscous destruction in low-alloy steels] // Fizika metallov i metallovedenie. 1982. T. 53. №1. S. 174–179.
15. Badikov K.A., Savkin A.N., Andronik A.V. Ocenka treshhinostojkosti nizkolegirovannoj stali pri neregulyarnom ciklicheskom nagruzhenii [The evaluation of fracture toughness of low-alloy steels by irregular cyclic loading] // Aviacionnye materialy i tehnologii. 2015. №S1 (38). S. 20–26. DOI: 10.18577/2071-9140-2015-0-S1-20-26.
16. Erasov V.S., Nuzhnyj G.A., Grinevich A.V. Ob ocenke povrezhdaemosti metallicheskih materialov metodami mehanicheskih ispytanij [About assessment of damageability of metal materials methods of mechanical tests] // Deformaciya i razrushenie materialov. 2015. №3. S. 42–47.
17. Kudrya A.V., Sokolovskaya E.A., Le Haj Nin, Trachenko V.A., Skorodumov S.V. i dr. Ocenka stroeniya izlomov i struktur v konstrukcionnyh stalyah s ispol'zovaniem kompyuterizirovannyh procedur [Assessment of structure of breaks and structures in constructional stalyakh with use of the computerized procedures] // Vektor nauki TGU. 2015. №4. S. 44–52.
18. Matvienko Yu.G. Modeli i kriterii mehaniki razrusheniya [Models and criteria of fracture mechanics]. M.: Fizmatlit, 2006. 328 s.
19. Grinevich A.V., Nuzhnyj G.A., Bakanov A.V., Ulkin M.Yu., Odincev I.N. Ocenka nesushhej sposobnosti elementov krepezha iz polimernyh kompozicionnyh materialov [As-sessment of bearing capacity of elements of fixture from polymeric composite materials ] // Deformaciya i razrushenie materialov. 2015. №12. S. 38–42.
20. Orlov M.R., Ospennikova O.G., Gromov V.I. Zamedlennoe razrushenie stali 38HN3MA v processe dlitelnoj ekspluatacii [Steel 38ХН3МА delayed fracture in the course of long opera-tion] // Vestnik MGTU im. N.E. Baumana. Ser.: Mashinostroenie. 2011. Specialnyj vypusk: Perspektivnye konstrukcionnye materialy i tehnologii. S. 5–10.
21. Bytsenko O.A., Grigorenko V.B., Lukina E.A., Morozova L.V. Razvitie metodov metallofizicheskih issledovanij: metodologicheskie voprosy i prakticheskaya znachimost [Development of methods for metal-physical research: methodological issues and practical significance] // Aviacionnye materialy i tehnologii. 2017. №S. S. 498–515. DOI: 10.18577/2071-9140-2017-0-S-498-515.

dx.doi.org/ 10.18577/2307-6046-2018-0-4-75-83

УДК 620.197.6

A.A. Kozlova, E.K. Kondrashov, S.L. Barbotko, Vereninova N.P.

HEAT-REFLECTIVE COATING FOR PROTECTION OF EXPANDABLE STRUCTURE ON AGAINST INFLUENCE OF THE HEAT TRANSFER RATE

Passenger evacuation in the event of a flight accident is often carried out using of inflatable life designs, and in the event of a fire it is important to save the air-tightness and efficiency of the life rafts. In defence of the membranous tissue materials, whereof inflatable life designs are manufacture, heat-reflecting enamel VE-72 is developed from influence of thermal radiation. Research has shown that the heat-reflecting coating of the VE-72 has high technical charac-teristics and also has proved the high efficiency of the heat-reflecting properties of the coating: the duration of the preset overpressure preservation of 20 kPa from exposure of an external heat current of 1,7 W/c2 is 15 minutes even with glue seams, which is 5 times higher than the requirements of the standard TSO-C69c and 3 times higher than the foreign equivalent of art. M-11673 (Air Cruisers Company, USA). Tests of materials on the preservation of leakage under the influence of radiant heat current were carr

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Reference list

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21. Marker T.R. Evacuation Slide Materials Test Method: Round Robin 5 // International Aircraft Materials Fire Test Working Group (Mobile, AL. March 7, 2017). 2017. 18 p.
22. Marker T.R. Evacuation Slide Test Method: Comparison of Radiant Heaters Used for Revised Evacuation Slide Test Method // International Aircraft Materials Fire Test Working Group (Cologne, Germany. June 7–8, 2017). 2017. 13 p.
23. Do D. Evacuation Slide Test Method: The Revised Test Method used for The Evacuation Slide Test // International Aircraft Materials Fire Test Working Group (Atlantic City, NJ, US. October 30–31, 2017). 2017. 14 p.
24. Zhelezina G.F., Gulyaev I.N., Soloveva N.A. Aramidnye organoplastiki novogo pokoleniya dlya aviacionnyh konstrukcij [Aramide organic plastics of new generation for aviation designs] // Aviacionnye materialy i tehnologii. 2017. №S. S. 368–378. DOI: 10.18577/2071-9140-2017-0-S-368-378.
25. Polimernaya teplootrazhayushhaya kompoziciya dlya pokrytiya: pat. 2467042 Ros. Federaciya [Polymeric heatreflecting composition for coating: pat. 2467042 Rus. Federation]; zayavl. 07.06.11; opubl. 20.11.12.
26. Semenova L.V., Malova N.E., Kuznetsova V.A., Pozhoga A.A. Lakokrasochnye materialy i pokrytiya [Paint and varnish materials and coatings] // Aviacionnye materialy i tehnologii. 2012. №S. S. 315–327.

10.

dx.doi.org/ 10.18577/2307-6046-2018-0-4-84-90

УДК 629.7.023

Alifanov E.V., A.М. Chaykun, D.S. Gorlov, M.A. Venediktova

TRIBOLOGICAL CHARACTERISTICS OF THE ALKYD COVERINGS FILLED WITH ABRASIVE FILLERS OF DIFFERENT SIZE

In article results of research of tribological properties of model systems of nonskid coatings based on one-component alkyd binding with abrasive fillers like sand and electrocorundum of different fractions was applied. Submitted data can be used when developing nonskid coatings which are actively applied, both in the aviation industry, and in other spheres of national economy. Intelligent approach to the nature and the size of the chosen filler will allow not only to improve considerably functionality of nonskid coating, but also to increase term of its operation. Values of friction coefficient, as one of the main characteristics of this type of coatings, are given. Observations concerning surface qualities and resistance to abrasion are showed. Definition of friction coefficient were carried out on the tribometer CETR UMT-3MT with use of drive of R33HE350 for reciprocating motion on the mode modeling the beginning of slipping of shoe sole on dry nonskid coating. It is shown that ex

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Reference list

1. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitiya materialov i tehnologij ih pererabotki na period do 2030 goda» [Innovative developments of FSUE «VIAM» SSC of RF on realization of «Strategic directions of the development of materials and technologies of their processing for the period until 2030»] // Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
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5. Kablov E.N. Iz chego sdelat budushhee? Materialy novogo pokoleniya, tehnologii ih soz-daniya i pererabotki – osnova innovacij [Of what to make the future? Materials of new generation, technology of their creation and processing – basis of innovations] // Krylya Rodiny. 2016. №5. S. 8–18.
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7. Mudrov O.A., Savchenko I.M., Shitov V.S. Spravochnik po elastomernym pokrytiyam i germetikam v sudostroenii [The directory on elastomeric coverings and hermetics in ship-building]. L.: Sudostroenie, 1982. 184 s.
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11. Semenova L.V., Malova N.E., Kuznetsova V.A., Pozhoga A.A. Lakokrasochnye materialy i pokrytiya [Paint and varnish materials and coatings] // Aviacionnye materialy i tehnologii. 2012. №S. S. 315–327.
12. Nefyodov N.I., Semyonova L.V. Nanesenie lakokrasochnyh pokrytij metodom «syroj po syromu» [The application of paint and varnish coatings by method «crude on crude»] // Aviacionnye materialy i tehnologii. 2013. №4. S. 39–42.
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14. Semenova L.V., Novikova T.A., Nefedov N.I. Klimaticheskaya stojkost i starenie lakokrasochnogo pokrytiya [Climatic stability and ageing paint coating] // Aviacionnye ma-terialy i tehnologii. 2014. №S3. S. 31–34. DOI: 10.18577/2071-9140-2017-0-S-393-404.
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18. Antislip coating materials: pat. KR20150024368 (A); publ. 06.03.15.
19. Antiskid elastic coating and mfg. technology thereof: pat. CN1483518 (A); publ. 24.03.04.
20. Williamson N., O’Donoghue M., Datta V.J. Overview of Anti-Slip Coatings for Structural Steel // Journal of Protective Coatings & Linings. 2003. June. P. 41–49. Available at: http://www.paintsquare.com/jpcl/ (accessed: March 20, 2018).
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11.

dx.doi.org/ 10.18577/2307-6046-2018-0-4-91-100

УДК 620.193:669.715

Morozova S.E.

CORROSION BEHAVIOR OF Al–Si–Mg ALLOY MADE BY SELECTIVE LASER MELTING METHOD

Selective laser melting (SLM) is a promising technology for complicated configuration details manufacture. Al-Si alloys are the most investigated alloys in selective laser melting manufacture at the time. A mechanical, corrosion and operational performance of SLM and as-cast details are deeply vary because cast structure stands in stark difference to SLM structure. In this article a corrosion behavior of synthesized and heat treated Al–Si–Mg alloy is shown. Also the results of general and intergranular corrosion are shown. The corrosion behavior of AlSi10Mg aluminum alloy with additives of Cu, Zr, Al–Si–Mg system Ce directly depends on structure of a material which in turn depends on manufacturing techniques and modes of thermal processing. In a cast condition the material shows the lowered corrosion resistance owing to formation of large dentritny structure in the course of crystallization. Development of corrosion processes in an alloy made by a SLS method, depends on quantity, the

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Reference list

1. Kablov E.N. Additivnye tehnologii – dominanta nacionalnoj tehnologicheskoj iniciativy [The additive technologies – dominant of national technological initiative] // Intellekt i tehnologii. 2015. №2 (11). S. 52–55.
2. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.
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5. Dynin N.V., Ivanova A.O., Hasikov D.V., Oglodkov M.S. Selektivnoe lazernoe splavlenie alyuminievyh splavov (obzor) [Selective laser melting of aluminium alloy (review)] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2017. №8. St. 02. Available at: http://www.viam-works.ru (accessed: March 19, 2018). DOI: 10.18577/2307-6046-2017-0-8-2-2.
6. Aboulkhai N.T., Maskery I., Tuck C. The microstructure and mechanical properties of se-lectively laser melted AlSi10Mg: The effect of a conventional T6-like heat treatment // Materials Science & Engineering: A. 2016. Vol. 667. P. 139–146. DOI: 10.1016/j.msea.2016.04.092.
7. Read N., Wang W., Essa K. Selective laser melting of AlSi10Mg alloy: Process optimisation and mechanical properties development // Materials and Design. 2015. Vol. 65. P. 417–424. DOI: 10.1016/j.matdes.2014.09.044.
8. Aboulkhai N.T., Tuck C., Ashcroft I. et al. On the precipitation hardening of selective laser melted AlSi10Mg //The Minerals, Metals & Materials Society and ASM International 2015. Metallurgical and materials transactions A. Vol. 46a, August 2015–3337. DOI:10.1007/s11661-015-2980-7.
9. Pei W., Zhengying W., Zhen C. The AlSi10Mg samples produced by selective laser melting: single track, densification, microstructure and mechanical behavior // Applied surface sci-ence. 2007. DOI: 10.1016/j.apsusc.2017.02.215.
10. Prashanth K.G., Scudino S., Klauss H.J. Microstructure and mechanical properties of Al–12Si produced by selective laser melting: Effect of heat treatment // Materials Science & Engineering: A. 2014. Vol. 590. P. 153–160.
11. Kimura T. Effect of silicon content on densification, mechanical and thermal properties of Al-xSi binary alloys fabricated using selective laser melting // Materials Science & Engineer-ing: A. November 17, 2016. DOI: 10.1016/j.msea.2016.11.059.
12. Tang M., Pistorius P.C. Anisotropic Mechanical Behavior of AlSi10Mg Parts Produced by Selective Laser Melting // The Minerals, Metals & Materials Society. January, 2017. DOI: 10.1007/s11837-016-2230-5.
13. Ryabov D.K., Antipov V.V., Korolev V.A., Medvedev P.N. Vliyanie tehnologicheskih faktorov na strukturu i svojstva silumina, poluchennogo s ispolzovaniem tehnologii sel-ektivnogo lazernogo sinteza [Effect of technological factors on structure and properties of Al–Si alloy obtained by selective laser melting] // Aviacionnye materialy i tehnologii. 2016. №S1 (43). S. 44–51. DOI: 10.18577/2071-9140-2016-0-S1-44-51.
14. Ryabov D.K., Morozova L.V., Korolev V.A., Ivanova A.O. Izmenenie mehanicheskih svojstv splava AK9ch., poluchennogo po tehnologii selektivnogo lazernogo splavleniya [Alternation of mechanical features of alloy AK9ch manufactured by selective laser melting] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №9 (45). St. 02. Available at: http://www.viam-works.ru (accessed: May 25, 2017). DOI: 10.18577/2307-6046-2016-0-9-2-2.
15. Ryabov D.K., Zajcev D.V., Dynin N.V., Ivanova A.O. Izmenenie struktury splava AK9ch., poluchennogo selektivnym lazernym spekaniem, v processe termicheskoj obrabotki [Alternation of structure of selective laser melted aluminum alloy AK9ch during heat treatment] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №9. St. 03. Available at: http://www.viam-works.ru (accessed: March 19, 2018). DOI: 10.18557/2307-6046-2016-0-9-3-3.
16. Ivanova A.O., Zavodov A.V., Dynin N.V., Fomina M.A. Effektivnost vvedeniya malyh dobavok perehodnyh metallov v splavy tipa AlSi10Mg, prednaznachennye dlya polucheniya izdelij po tehnologii selektivnogo lazernogo splavleniya [Efficiency of complex alloying AlSi10Mg type alloy with transition metals for selective laser melting technologies] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2017. №7 (55). St. 01. Available at: http://www.viam-works.ru (accessed: March 19, 2018). DOI: 10.18577/2307-6046-2017-0-7-1-1.
17. Kablov E.N., Lukina E.A., Sbitneva S.V., Hohlatova L.B., Zajcev D.V. Formirovanie metastabilnyh faz pri raspade tverdogo rastvora v processe iskusstvennogo stareniya Al-splavov [Forming of metastable phases at disintegration of solid solution in the course of artificial aging of Al-alloys] // Tehnologiya legkih splavov. 2016. №3. S. 7–17.
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12.

dx.doi.org/ 10.18577/2307-6046-2018-0-4-101-110

УДК 620.1:669.017

Putyrskiy S.V., Yakovlev A.L., N.A. Nochovnaya

RESEARCHING OF MECHANICAL PROPERTIES OF DEFORMED SEMI-FINISHED PRODUCTS OF VT23M AND VT43 ALLOYS, ASSESSMENT OF THEIR CLIMATIC STABILITY IN THE ARCTIC CLIMATE

The studies, showed, that the structure of the manufactured semi-finished products from the alloys VT23M and VT43 is typical for deformable semi-finished of (α+β) titanium alloys. It was noted that the average size of structural components of semi-finished products of VT43 alloy is smaller than that of VT23M semi-finished products. Tensile tests to determine the mechanical properties of samples from sheets and bars of VT23M and VT43 alloys were carried out at room temperature (20°C) and lowered (-60°C) temperatures. Since the sheets of the VT43 alloy were first obtained within the framework of this work, in order to evaluate the anisotropy of the mechanical properties, tensile tests at a temperature of +20°C were carried out in the longitudinal and transverse directions of hot rolling. It is shown that under the same production conditions for the of sheets from the investigated alloys, the alloy VT43 has a 9,6% higher strength, with an equal elongation. The comparison is given for th

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