Articles
The influence of heat treatment on the formation of structure and properties in the nickel-beryllium alloy 97NL-VI is considered in the article. The dissolution in the structure of the γ-matrix of the NiBe hardening intermetallic phase as a function of the quenching temperature is analyzed. It is found that when aging, the Guinier–Preston zones are initially formed, contributing a small contribution to the hardening, which later transform into a metastable γʹ-phase. The optimum aging temperature interval with a high complex of mechanical properties and a low level of specific electrical resistance has been specified.
2. Kablov E.N. Shestoj tekhnologicheskij uklad [Sixth technological way] // Nauka i zhizn. 2010. №4. S. 2–7.
3. Kablov E.N. Materialy i khimicheskie tekhnologii dlya aviatsionnoj tekhniki [Materials and chemical technologies for aviation engineering] // Vestnik Rossijskoj akademii nauk. 2012. T. 82. №6. S. 520–530.
4. Kablov E.N., Ospennikova O.G., Petrushin N.V. Novyj monokristallicheskij intermetallidnyj (na osnove γʹ-fazy) zharoprochnyj splav dlya lopatok GTD [New single crystal heat-resistant intermetallic γʹ-based alloy for GTE blades] // Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 34–40. DOI: 10.18577/2071-9140-2015-0-1-34-40.
5. Khimushin F.F. Zharoprochnye stali i splavy. 2-e izd., pererab. i dop. [Heat resisting there were also alloys. 2nd ed., rev. and add.]. M.: Metallurgiya, 1969. 752 s.
6. Arginbaeva E.G., Bazyleva O.A. Issledovanie struktury i fiziko-mehanicheskih svojstv intermetallidnyh nikelevyh splavov [The research the structure, physical and mechanical properties of the intermetallic nickel alloys] // Aviacionnye materialy i tehnologii. 2013. №4. S. 14–19.
7. Bazyleva O.A., Arginbaeva E.G. Vliyanie termicheskoj obrabotki na strukturu i zharoprochnost renijsoderzhashhego intermetallidnogo splava na osnove nikelya [Effect of heat treatment on the structure and heat resistance rhenium containing intermetallic nickel-based alloy] // Aviacionnye materialy i tehnologii. 2014. №2. S. 21–26. DOI: 10.18577/2071-9140-2014-0-2-21-26.
8. Bazyleva O.A., Ospennikova O.G., Arginbaeva E.G., Letnikova E.Yu., Shestakov A.V. Tendencii razvitiya intermetallidnyh splavov na osnove nikelya [Development trends of nickel-based intermetallic alloys] // Aviacionnye materialy i tehnologii. 2017. №S. S. 104–115. DOI: 10.18577/2071-9140-2017-0-S-104-115.
9. Arginbaeva E.G., Nazarkin R.M., Shestakov A.V., Karachevtsev F.N. Issledovanie vliyaniya termicheskoj obrabotki na strukturno-fazovye parametry intermetallidnykh splavov na osnove nikelya [Research of heat treatment influence on structural-phase parameters of intermetallic nickel based alloys] // Aviacionnye materialy i tehnologii. 2017. №3 (48). S. 8–13. DOI: 10.18577/2071-9140-2017-0-3-8-13.
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14. Borisov V.A., Rakhshtadt A.G., Shpitsberg A.L. Svojstva legirovannykh splavov nikel-berillij [Properties of doped alloys nickel-beryllium] // Metallovedenie i termicheskaya obrabotka metallov. 1966. №6. S. 12–16.
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The article contains the results of microstructure investigations in the cross section of an ingot from wrought intermetallic titanium ortho alloy doped with yttrium. The effect of heat treatment in a two-phase (b/В2+α2)-area on microstructure of the yttrium doped ortho alloy ingot has been studied. Thermal analysis has been performed with differential scanning calorimetry (DSC) curves plotting which specify phase transformation temperatures of the alloy in focus. Rheological curves for the upset cylindrical samples have been plotted, which revealed deformation strain reduction with upsetting temperature increase from 850 to 1050°C. It has been shown that doping of ortho alloys with rare-earth elements (REE) results in rolling temperature increase.
2. Titanium and Titanium Alloys: Fundamental Applications / ed. by С. Leyens, M. Peters. KGaA, Weinheim: Wiley-VCH Verlag GmbH&Co., 2003. 513 p.
3. Chen W., Li J.W., Xu L., Lu B. Development of Ti2AlNb Alloys: Opportunities and Challenges // Advanced Materials and Processes. 2014. Vol. 172. No. 5. P. 23–27.
4. 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.
5. Splav na osnove titana i izdelie, vypolnennoe iz nego: pat. 2210612 Ros. Federaciya [Titanium-based alloy and the product which has been executed of it: pat. 2210612 Rus. Federation]; zayavl. 24.09.01; opubl. 20.08.03.
6. Intermetallidnyj splav na osnove titana: pat. 2405849 Ros. Federaciya [Intermetallic titanium-based alloy: pat. 2405849 Rus. Federation]; zayavl. 28.10.09; opubl. 10.12.10.
7. 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 aluminide alloy VТI-4] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2018. №2. St. 05. Available at: http://www.viam-works.ru (accessed: May 4, 2018). DOI: 10.18577/2307-6046-2018-0-2-5-5.
8. Alekseev E.B., Nochovnaya N.A., Ivanov V.I., Panin P.V., Novak A.V. Issledovanie vliyaniya alyuminiya na fazovyj sostav i termomekhanicheskij rezhim izotermicheskoj shtampovki intermetallidnogo splava VTI-4 [Research of influence of aluminum on phase structure and thermomechanical mode of isothermal punching of intermetallic alloy VTI-4] // Tekhnologiya legkikh splavov. 2015. №1. S. 57–61.
9. Zhang S.Z. et al. Phase transformation and microstructure evolution of differently processed Ti–45Al–9Nb–Y alloy // Intermetallics. 2012. Vol. 31. P. 208–216.
10. Liu Z.G., Chai L.H., Chen Y. Microstructure evolution in rapidly solidified Y added TiAl ribbons // Intermetallic. 2011. Vol. 19. P. 160–164.
11. Zhao L.L., Li G.Y., Zhang L.Q. Influence of Y addition on the long time oxidation behaviors of high Nb containing TiAl alloys at 900°C // Intermetallics. 2010. Vol. 18. P. 1586–1596.
12. Chen Y., Si Y., Kong F. Effects of yttrium on microstructures and properties of Ti–17Al–27Nb alloy // Transactions of Nonferrous Metals Society of China. 2006. Vol. 16. Issue 2. P. 316–320.
13. Li B., Kong F., Chen Y. Effect of yttrium addition on microstructures and room temperature tensile properties of Ti–47 Al alloy // Journal of Rare Earths. 2006. Vol. 24. Issue 3. P. 352–356.
14. Chen Y., Li B., Kong F. Microstructural refinement and mechanical properties of Y-bearing TiAl alloys // Journal of Alloys and Compounds. 2008. Vol. 457. Issues 1–2. P. 265–269.
15. Chen Y., Li B., Kong F. Effects of minor yttrium addition on hot deformability of lamellar Ti–45Al–5Nb alloy // Transactions of Nonferrous Metals Society of China. 2007. Vol. 17. P. 58–63.
16. Si Y., Chen Y., Liu Z., Kong F. Influence of yttrium on microstructure and properties of Ti–23Al–25Nb alloy after heat treatment // Transactions of Nonferrous Metals Society of China. 2006. Vol. 16. P. 849–853.
17. Chang X., Si J., Gao F., Jing Y., Zhang J. Effect of Gd аddition on heat treatment microstructure of wrought TiAl // Journal of Iron and Steel Research, International. 2007. Vol. 14. P. 26–29.
18. Lia W., Inksonb B., Horitac Z., Xiaa K. Microstructure observations in rare earth element Gd-modified Ti–44 at% Al // Intermetallics. 2000. Vol. 8. P. 519–523.
19. Shiriaev A.A., Antashev V.G. Osobennosti razrabotki vysokoprochnogo samozakalivaiushchegosia vysokotekhnologichnogo psevdo-β-titanovogo splava [Peculiarities of development of advanced high-strength self-hardening high-processable pseudo-β-titanium alloys] // Aviatsionnye materialy i tekhnologii. 2014. №4. S. 23–30. DOI: 10.18577/2071-9140-2014-0-4-23-30.
20. Nochovnaya N.A., Alekseev E.B., Panin P.V., Novak A.V. Issledovanie struktury i mekhanicheskikh svojstv deformiruemogo intermetallidnogo titanovogo splava VIT5, legirovannogo gadoliniem [Research of structure and mechanical properties of the deformable intermetallic VIT5 titanium alloy alloyed by gadolinium] // Titan. 2017. №2. S. 21–29.
21. Kablov E.N., Nochovnaya N.A., Panin P.V., Alekseev E.B., Novak A.V. Issledovanie struktury i svojstv zharoprochnykh 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.
22. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskikh napravlenij razvitiya materialov i tekhnologij ikh pererabotki na period do 2030 goda» // Aviacionnye materialy i tekhnologii. 2015. №1 (34). S. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
23. Antipov V.V. Strategiya razvitiya titanovykh, magnievykh, berillievykh i alyuminievykh splavov // Aviacionnye materialy i tekhnologii. 2012. №S. S. 157–167.
24. Kablov E.N. Bez novykh materialov – net budushchego // Metallurg. 2013. №12. S. 4–8.
25. Bazyleva O.A., Arginbaeva E.G., Fesenko T.V., Kolodochkina V.G. Issledovanie vliyaniya likvacionnoj neodnorodnosti na strukturu i dolgovechnost intermetallidnykh splavov na osnove nikelya // Materialy budushchego. 2014. №6. S. 7–12.
26. Bazyleva O.A., Arginbaeva E.G., Fesenko T.V., Kolodochkina V.G. Study of the effect of liquation on structure and durability of intermetallic alloys based on nickel // Inorganic Materials: Applied Research. 2015. Vol. 6. No. 1. P. 5–10.
27. Bazyleva O.A., Bondarenko Yu.A., Morozova G.I., Timofeeva O.B. Struktura, khimicheskij i fazovyj sostavy intermetallidnogo splava VKNA-1V posle vysokotemperaturnykh obrabotok i tekhnologicheskikh nagrevov // Zharoprochnye splavy. 2014. №5. S. 3–6.
28. Povarova K.B., Drozdov A.A., Bazyleva O.A., Bondarenko Yu.A., Bulakhtina M.A., Arginbaeva E.G., Antonova A.V., Morozov A.E., Nefedov D.G. Vliyanie sposobov polucheniya monokristallov splavov na osnove Ni3Al na makro- i mikroodnorodnost raspredeleniya komponentov, strukturu, svojstva // Metally. 2014. №3. S. 40–51.
The effect of various modes and technological parameters of hardening heat treatment on mechanical properties and structure of sheets from an experimental composition of a high-strength metastable β-titanium alloy doped with rare-earth element yttrium have been studied.
It has been shown the possibility of wide variation within parameters and morphology of structural constituents of the experimental alloy composition. The experimental alloy can be effectively strengthened both by conventional heat treatment and low-temperature thermo-mechanical treatment (LTMT). Long-term low-temperature ageing makes it possible to provide high level of strength characteristics with satisfactory values of elongation and impact toughness.
2. Boyer R.R., Briggs R.D. The Use of β Titanium Alloys in the Aerospace Industry // Journal of Materials Engineering and Performance. 2005. Vol. 14 (6). P. 681–685.
3. Nyakana S.L., Fanning J.C., Boyer R.R. Quick Reference Guide for β Titanium Alloys in the 00s // Journal of Materials Engineering and Performance. 2005. Vol. 14 (6). P. 799–811.
4. Titanium and titanium alloys. Fundamentals and applications / Ed. by C. Leyens, M. Peters. Wiley–VCH, Germany. 2003. 513 p.
5. Ilin A.A., Kolachev B.A., Polkin I.S. Titanovye splavy. Sostav, struktura, svojstva: spravochnik [Titanium alloys. Structure, structure, properties: directory]. M.: VILS–MATI. 2009. 520 s.
6. 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.
7. Vysokoprochnyj splav na osnove titana i izdelie, vypolnennoe iz vysokoprochnogo splava na osnove titana: pat. 2569285 Ros. Federaciya. №2014153690/02 [High-strength alloy on the basis of titanium and the product executed from high-strength alloy on the basis of titanium: pat. 2569285 Rus. Federation. No. 2014153690/02]; zayavl. 29.12.2014; opubl. 20.11.2015, Byul. №32.
8. Shiriaev A.A., Antashev V.G. Osobennosti razrabotki vysokoprochnogo samozakalivaiushchegosia vysokotekhnologichnogo psevdo-β-titanovogo splava [Peculiarities of development of advanced high-strength self-hardening high-processable pseudo-β-titanium alloys] // Aviatsionnye materialy i tekhnologii. 2014. №4. S. 23–30. DOI: 10.18577/2071-9140-2014-0-4-23-30.
9. Kablov E.N., Ospennikova O.G., Vershkov A.V. Redkie metally i redkozemelnye elementy – materialy sovremennyh i budushhih vysokih tehnologij [Rare metals and rare-earth elements are materials for modern and future high technologies] // Aviacionnye materialy i tehnologii. 2013. №S2. S. 3–10.
10. Kablov E.N., Volkova E.F., Filonova E.V. Vliyanie RZE na fazovyj sostav i svojstva novogo zharoprochnogo magnievogo splava sistemy Mg–Zn–Zr–RZE [Influence of RZE on phase structure and property of new heat resisting magnesium alloy of Mg-Zn-Zr-RZE system] // Metallovedenie i termicheskaya obrabotka metallov. 2017. №7 (745). S. 19–26.
11. Kashapov O.S., Pavlova T.V., Kalashnikov V.S., Kondrateva A.R. Issledovanie vliyaniya rezhimov termicheskoj obrabotki na strukturu i svojstva opytnykh pokovok iz splava VT41 s melkozernistoj strukturoj [The influence of heat treatment conditions on structure and properties of pilot forgings from VT41 alloy with fine grained structure] // Aviacionnye materialy i tehnologii. 2017. №3. S. 3–7. DOI: 10.18577/2071-9140-2017-0-3-3-7.
12. El-Chaikh A., Schmidt P., Christ H.-J. Study on the Beneficial Effects of Duplex Aging on Microstructure Phenomena Determining the Fatigue life of the Metastable β-titanium Alloy Ti 38-644 // Ti-2011 Science and Technology: Proceedings of the 12th World Conference on Titanium. Beijing: Science Press Beijing, 2011. Vol. 1. P. 745–749.
13. Santhosh R., Geetha M., Nageswara Rao M. Recent developments in heat treatment of beta titanium alloys for aerospace applications // Transactions Indian Institute of Metals. 2017. Vol. 70 (7). P. 1681–1688.
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15. Suzuki T., Niwa N., Goto K., Kobayashi M. et al. Effect of aging on the mechanical properties of beta titanium alloys of Ti–13V–11Cr–3Al, Ti–15V–3Cr–3Sn–3Al and Ti–3Al–8V–6Cr–4Mo–4Zr // Titanium 95: Science and technology. 1995. P. 1294–1301.
The process of casting of thin-walled shaped casting from the aluminum alloy AK7ch. with the use of two methods of casting: sand casting and investment casting was observed in this article. The plastic foundry pattern equipment got by 3D printing technology is used in both cases. The differences in the methods of casting were revealed, which affected the quality of the part. A comparative analysis of the experimental results was carried out. Based on the results of the experiment, an optimal method for casting a thin-walled casting «Housing» from the alloy AK7ch. was selected.
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3. Fasonnoe lite alyuminievykh splavov: ucheb. posobie / G.B. Stroganov, M.B. Altman, A.V. Melnikov i dr. [Shaped casting of aluminum alloys: studies. grant/G B. Stroganov, M. B. Altman, A.V.Melnikov et al.]. M.: Mashinostroenie, 1980. 296 s.
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10. Vlasova K.A., Klyukvina T.D., Leonov A.A., Larionov S.A. Vzaimodejstvie modelnykh sostavov s plastikovoj osnastkoj, izgotovlennoj s pomoshchyu tekhnologii 3D-pechati [Interaction of model compositions with plastic equipment made using 3D printing technology] // Trudy VIAM: elektron. nauch.-tekhnich. zhurn. 2018. №2. St. 07. URL: http://www.viam-works.ru (accessed: March 26, 2018). DOI: 10.18577/2307-6046-2018-0-2-7-7.
11. Petrova G.N., Sapego Yu.A., Larionov S.A., Platonov M.M., Laptev A.B. Pozharobezopasnye termoplastichnye materialy dlya 3D-tehnologii [Fireproof thermoplastic materials for 3D-technologies] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2017. №9 (57). St. 07. Available at: http://www.viam-works.ru (accessed: March 26, 2018). DOI: 10.18577/2307-6046-2017-0-9-7-7.
12. Kablov E.N. Additivnye tekhnologii – dominanta nacionalnoj tekhnologicheskoj iniciativy [The dictionary reference on foundry production] // Intellekt i tekhnologii. 2015. №2 (11). S. 52–55.
13. Ospennikova O.G. Issledovanie i razrabotka parametrov tehnologicheskogo processa izgotovleniya modelej iz modelnyh kompozicij na osnove sinteticheskih voskov [Research and working out of parametres of technological process of manufacturing of models from modelling compositions on the basis of synthetic waxes] // Aviacionnye materialy i tehnologii. 2014. №3. S. 18–21. DOI: 10.18577/2071-9140-2014-0-3-18-21.
14. Duyunova V.A., Volkova E.F., Uridiya Z.P., Trapeznikov A.V. Dinamika razvitiya magnievyh i litejnyh alyuminievyh splavov [Dynamics of the development of magnesium and cast aluminum alloys] // Aviacionnye materialy i tehnologii. 2017. №S. S. 225–241. DOI: 10.18577/2071-9140-2017-0-S-225-241.
15. Duyunova V.A., Kozlov I.A. Kholodnotverdeyushchie formovochnye smesi: perspektivy ispolzovaniya pri lite magnievykh splavov [Cold-hardering forming mixes: use perspectives when molding magnesium alloys] // Vse materialy. Enciklopedicheskij spravochnik. 2011. №1. S. 41–43.
In article results of researches on impact assessment of large-scale factor on level of the physical and mechanical properties rigid foamed polyacrylimide sheet brands VPP-5, made of sheet prepolymer on basis acrylimide are given.
Dependences of values of apparent density, durability are considered at stretching and factors of their variation from overall dimensions foam concrete block. It is established that the factor of variation has values less than 10%, and extent of dispersion of the obtained data is insignificant.
Results of the carried-out work will allow to predict properties of blocks foamed polyacrylimide different dimensions.
2. Popov Yu.O., Kolokol’tseva T.V., Khrulkov A.V. Novoe pokolenie materialov i tehnologij dlya izgotovleniya lonzheronov lopastej vertoleta [The new generation of materials and technologies for helicopter blade spars] // Aviacionnye materialy i tehnologii. 2014. №S2. S. 5–9.
3. 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.
4. Beider E.Ya., Petrova G.N., Izotova T.F., Gureeva E.V. Kompozicionnye termoplastichnye materialy i penopoliimidy [Thermoplastic composite materials and foam polyimides] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №11. St. 01. Available at: http://www.viam-works.ru (accessed: May 17, 2018).
5. Doroshenko N.I., Chursova L.V. Evolyuciya materialov dlya lopastej vertoletov [Evolution of materials for blades of helicopters] // Aviacionnye materialy i tehnologii. 2012. №2. S. 16–18.
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8. Shuldeshov E.M., Kraev I.D., Platonov M.M. Polimernaya kompozicionnaya zvukopogloshhayushhaya panel [Polymeric composition sound absorbing panel] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2017. №5 (53). St. 07. Available at: http://www.viam-works.ru (accessed: May 17, 2018). DOI: 10.18577/2307-6046-2017-0-5-7-7.
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The paper presents the results of a study of the structure formation of in-thermetallide-oxide high-temperature metal composite materials based on nickel alloys reinforced with monocrystalline aluminum oxide plastids. Samples for research were obtained by the method of reaction impregnation. nickel powder with a diameter of 5–10 µm and nanosized nickel alumina particles with a diameter of 1–10 nm were used as matrix-forming agents. The results of the study of the microstructure and phase composition of samples of metal composite materials with different NiAl particle content (10; 15 and 20%) are shown. In order to identify individual intermetallic phases, microhardness studies were conducted.
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10. Goryunov A.V., Rigin V.E. Sovremennaya tehnologiya polucheniya litejnyh zharoprochnyh nikelevyh splavov [The modern technology of cast nickel base superalloys production] // Aviacionnye materialy i tehnologii. 2014. №2. S. 3–7. DOI: 10.18577/2071-9140-2014-0-2-3-7.
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Influence of mechanical properties of free films of priming coverings on operational properties of systems on the basis of the disperse reinforced paint coatings was studied, tensile strength at break for coating film was defined, relative lengthenings of film at break for primers ЭП-0214, ВГ-28, ЭП-076, ЭП-0215, and also the erosion resistant disperse reinforced cove-ring. For systems of coatings physical and mechanical properties are defined and the durability is evaluated. Mechanical properties of primers in coating system of erosion resistant coverings make essential impact on their operational properties.
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11. 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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In the study operational properties of coverings on the basis of varnish UR-231 are investigated. Comparison tests of varnish UR-231 with hardeners OS-17 and diethylene glycol urethane (DGU), and also coverings on their basis are carried out. Varnish UR-231 put on samples of alloy D16-AT and samples of printed circuit boards according to specifications 6-21-14–90. Comparing analysis of the received results was carried for the purpose to define possibility of replacement of DGU hardener on hardener OS-17 in interests of reduction of technological process of painting of varnish coatings at the expense of reduction of time of varnish filmforming.
2. Kablov E.N. Materialy i khimicheskie tekhnologii dlya aviatsionnoj tekhniki [Materials and chemical technologies for aviation engineering] // Vestnik Rossijskoj akademii nauk. 2012. T. 82. №6. S. 520–530.
3. Kablov E.N. Rol khimii v sozdanii materialov novogo pokoleniya dlya slozhnykh tekhnicheskikh system [Chemistry role in creation of materials of new generation for complex technical systems] // XX Mendeleevskij szd po obshchej i prikladnoj khimii: tez. dokl. v 5 t. UrO RAN, 2016. S. 25–26.
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5. Kablov E.N. Materialy novogo pokoleniya – osnova innovatsij, tekhnologicheskogo liderstva i natsionalnoj bezopasnosti Rossii [Materials of new generation – basis of innovations, technological leadership and national security of Russia] // Intellekt i tekhnologii. 2016. №2 (14). S. 16–21.
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Literature analysis on possibilities to obtain anti-icing coatings is presented. Solid surface wetting regimes and properties of superhydrophobic coatings, coatings based on elastomers, organogels, SLWL- and SLIP-surfaces are discussed. Influence of wetting angle and surface roughness on ice-to-surface adhesion and time of water droplet freezing is shown.
It seems that smooth surfaces based on elastomers and superhydrophobic coatings increase time of water droplet freezing and decrease ice adhesion. Such coatings supposed to be effective anti-icing coatings. SLWL- and SLIP-surfaces also possess low ice adhesion and high icing durability but have some deficiencies connected with mechanical and operational characteristics and need to be modified.
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In this work researches nature of change of area of localization of the maximum shear deformation have been provided when testing carbon plastic specimens in four planes on the ASTM D5379 standard (GOST R 56799). In article there are two kinds of carbon fiber-reinforced polymer. First based on carbon fabric and second based on carbon roving (with orientation of fibers only in one direction). Measurements of deformation field of sample were carried out by means of optical system of digital image correlation (DIC). The question of influence of different length of site of measurement of deformation as for digital extensometers (DIC), and for pasted strain gages, on reliability of the received values also is considered.
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Complex research of two cases of operational destructions of details of difficult configuration from alloy AK4-1 (impellers and fan wheels) is conducted. By methods of optical and electron microscopy, chemical analysis and mechanical tests it is evaluated macro- and microstructure, chemical composition and nature of destruction of details is studied. It is established that destruction of the impeller and wheel of the fan has occurred at action of cyclic load. Destruction of details was promoted by availability of rough surface and micro damages (scratches from machining) in zone of the increased tension.
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