Articles
RETRACTED 06.08.2018
The influence of residual austenite on the strength maraging steels 08Х15Н5Д2Т and 03Н18К9М5Т. To assess the content of residual austenite was measured the magnetic properties of the samples taken from two maraging steels after different heat treatment. Ways of improving the viscosity characteristics and of reducing the threshold of cold brittleness due to the formation in the martensitic structure of the steels in austenite to the special morphology depending on the heat treatment technology.
2. 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.
3. Kablov E.N., Ospennikova O.G., Lomberg B.S. Strategicheskie napravleniya razvitiya konstrukcionnyh materialov i tehnologij ih pererabotki dlya aviacionnyh dvigatelej nasto-yashhego i budushhego [The strategic directions of development of constructional materials and technologies of their processing for aircraft engines of the present and the future] // Avtomaticheskaya svarka. 2013. №10. S. 23–32.
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9. 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.
10. Gromov V.I., Voznesenskaya N.M., Pokrovskaya N.G., Tonysheva O.A. Vysokoprochnye konstrukcionnye i korrozionnostojkie stali FGUP «VIAM» dlya izdelij aviacionnoj tehniki [High-strength constructional and corrosion-resistant steels developed by VIAM for aviation engineering] // Aviacionnye materialy i tehnologii. 2017. №S. S. 159–174. DOI: 10.18577/2071-9140-2017-0-S-159-174.
11. Silin A.A., Krikushenko E.S., Alekseev V.V., Silina V.I., Belousov V.V. Sposob termicheskoj obrabotki martensitno-stareyushhih stalej 08H15N5D2T, 06H14N6D2MBT i 07H16N6 [Way of thermal processing maraging steels 08H15N5D2T, 06H14N6D2MBT and 07H16N6] // Metallovedenie i termicheskaya obrabotka metallov. 2013. №3. S. 23–26.
12. Mahneva T.M. Priroda nestabilnosti urovnya udarnoj vyazkosti i nizkoj tehnologicheskoj plastichnosti pri proizvodstve krupnogabaritnyh polufabrikatov iz korrozionnostojkih martensitno-stareyushhih stalej, sovershenstvovanie tehnologii ih obrabotki: dis. … d-r tehn. nauk [The nature of instability of level of impact strength and low technological ductility by production of large-size semi-finished products from corrosion-resistant maraging steels, improvement of technology of their processing: thesis, Doctor Sci. (Tech.)]. Izhevsk, 2012. 376 s.
13. Gorkunov E.S., Mitropol'skaya S.Yu., Zadvorkin S.M. i dr. Osobennosti deformacionnogo povedeniya magnitnyh harakteristik martensitno-stareyushhej stali s razlichnoj stepen'yu dispersionnogo tverdeniya [Features of deformation behavior of magnetic characteristics of maraging steel with different extent of dispersion hardening] // Defektoskopiya. 2007. №9. S. 3–14.
14. Vylezhnev V.P., Kokovyakina S.A., Simonov Yu.N., Suhih A.A. Povyshenie harakteristik nadezhnosti martensitno-stareyushhej stali 03N18K9M5T putem sozdaniya struktury tipa «nanotripleks» [Increase of characteristics of reliability of maraging steel 03N18K9M5T by creation of structure of the nanotriplex type] // Metallovedenie i termicheskaya obrabotka metallov. 2010. №11. S. 39–47.
15. Stashkov A.H., Somova B.M., Sazhina E.Yu., Stashkova L.A., Nichipuruk A.P. Magnitnyj metod opredeleniya kolichestva ostatochnogo austenita v martensitno-stareyushhih stalyah [Magnetic method of definition of amount of residual austenite in maraging steels] // Defektoskopiya. 2011. №12. S. 36–42.
16. Suhih Ar.A., Dementev V.B., Suhih An.A. O prichinah vysokoj prochnosti ostatochnogo i revertirovannogo austenita martensitno-stareyushhej stali N18K9M5T [About the reasons of high strength of residual and reverted austenite of N18K9M5T maraging steel] // Himicheskaya fizika i mezoskopiya. 2008. T. 10. №2. S. 200–206.
17. Mahneva T.M. Hladnolomkost korrozionnostojkoj martensitno-stareyushhej stali 08H15N5D2T [Cold brittleness of corrosion-resistant maraging steel 08H15N5D2T] // Metallovedenie i termicheskaya obrabotka metallov. 2011. №12. S. 3–7.
The main methods of making billets from molybdenum and its alloys were examined in this paper such as powder metallurgy and vacuum remilting. The influence of the methods making billets on the formation of the strength and plastic characteristics of molybdenum alloys is analyzed. To increase the low-temperature plasticity of molybdenum alloys, it is necessary to use more pure raw materials, rational alloying and technological methods which make it possible to obtain an alloy with a fine-grained structure.
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The aim of the work is to study the technology of obtaining forms using self-hardening mixtures based on phenolic binders. The article gives statistical data about using different types of mixtures for the cores production. The classification of the most common resins used in molding using cold-hardening mixtures is given. The specific characteristics, advantages and disadvantages of cast alkaline phenolic resins are discussed. Time characteristics and strength parameters are analyzed on the basis of the curing curve of self-hardening mixtures. Examples of defects in forms, cores and castings associated with strength of the mixtures are given. The mechanism of strength formation of alkaline phenolic resins is considered (alpha-set process).
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The article describes properties of epoxy binder VS-2526K in an initial condition and after curing, and influence of fillers of various types on properties polymer composites on their basis. The results of research of binder and some materials on its basis by methods of differential thermal analysis, thermogravimetric analysis and IR-spectroscopy are given and discussed. It is shown the influence of filler nature on structure and water resistance of polymer composites. The polymer matrix between glass fibers is characterized be more tension, than for carbon fibers.
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The advantages of non-autoclaved molding technology in comparison with autoclave molding are considered in this article. The use of an autoclave ensures a high-quality curing of the polymer matrix, but because of the high cost of the apparatus, a non-autoclave method is widely used. Also, a molding scheme is given, the properties of the prepregs and resins for non-autoclaved molding of various manufacturers, the properties of the fiber fillers, the process of consolidating the prepreg with non-autoclave curing are analyzed.
2. Dushin M.I., Hrulkov A.V., Karavaev R.Yu. Parametry, vliyayushhie na obrazovanie poristosti v izdeliyah iz polimernyh kompozicionnyh materialov, izgotavlivaemyh bezavtoklavnymi metodami (obzor) [Parameters that influence the formation of porosity in the products made of polymer composite materials (PCM) produced by out-of-autoclave methods (review)] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №2. St. 11. Available at: http://www.viam-works.ru (accessed: January 10, 2018). DOI: 10.18577/2307-6046-2015-0-2-11-11.
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4. Dushin M.I., Doneckij K.I., Karavaev R.Yu. Ustanovlenie prichin obrazovaniya poristosti pri izgotovlenii PKM [Identification of the reasons of porosity formation when manufacturing composites] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №6 (42). St. 08. Available at: http://www.viam-works.ru (accessed: January 10, 2018). DOI: 10.18577/2307-6046-2016-0-6-8-8.
5. Gusev Yu.A., Grigorev M.M., Timoshina L.N. Izgotovlenie etalonnyh obrazcov iz PKM s zadannoj poristostyu metodom vakuumnoj infuzii [Production of standard polymer composite samples with the set porosity by vacuum infusion] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №11. St. 06. Available at: http://www.viam-works.ru (accessed: January 10, 2018). DOI: 10.18577/2307-6046-2014-0-11-6-6.
6. Dushin M.I., Muhametov R.R., Platonov A.A., Merkulova Yu.I. Issledovanie filtracionnyh harakteristik armiruyushhih napolnitelej i svyazuyushhih pri razrabotke tehnologii bezavtoklavnogo formovaniya polimernyh kompozicionnyh materialov [Study of filtration characteristics of reinforcing fillers and binders in the development of non-out-autoclave technology for polymer composite material] // Aviacionnye materialy i tehnologii. 2013. №2. S. 22–25.
7. Raskutin A.E., Goncharov V.A. Komp'yuternoe modelirovanie tehnologicheskogo processa izgotovleniya PKM metodom vakuumnoj infuzii [Computer modeling of technological process of manufacturing of PCM by method of vacuum infusion] // Aviacionnye materialy i tehnologii. 2012. №S. S. 286–291.
8. Kirillov V.N., Vapirov Yu.M., Drozd E.A. Issledovanie atmosfernoj stojkosti polimernyh kompozicionnyh materialov v usloviyah atmosfery teplogo vlazhnogo i umerenno teplogo klimata [Research of atmospheric firmness of polymeric composite materials in the conditions of the atmosphere of warm wet and moderately warm climate] // Aviacionnye materialy i tehnologii. 2012. №4. S. 31–38.
9. 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.
10. Kablov E.N. Rossii nuzhny materialy novogo pokoleniya [Materials of new generation are necessary to Russia] // Redkie zemli. 2014. №3. S. 8–13.
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.
12. Kablov E.N. Kompozity: segodnya i zavtra [Composites: today and tomorrow] // Metally Evrazii. 2015. №1. S. 36–39.
13. Kablov E.N. Iz chego sdelat budushhee? Materialy novogo pokoleniya, tehnologii ih sozdaniya 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.
14. Grunenfelder L.K., Centea T., Hubert P., Nutt S.R. Effect of room-temperature out-time on tow impregnation in an out-of-autoclave prepreg // Composites Part A: Applied Science Manufacturing. 2013. Vol. 45. P. 119–126.
15. Centea T., Grunenfelder L.K., Nutt S.R. A review of out-of-autoclave prepregs – material properties, process phenomena and manufacturing considerations // Composites Part A: Applied Science Manufacturing. 2014. P. 132–154.
16. Thorfinnson B., Biermann T. Degree of Impregnation of Prepregs – Effects on Porosity // Proceedings 32nd International SAMPE Symposium, Anaheim, CA: Society for the Advancement of Materials and Process Engineering. 1987. P. 9.
17. Thorfinnson B., Biermann T. Production of Void Free Composite Parts Without Debulking // Proceedings 31st International SAMPE Symposium, Las Vegas, NV: Society for the Advancement of Materials and Process Engineering. 1986. P. 10.
18. Kratz J., Hubert P. Anisotropic air permeability in out-of-autoclave prepregs: Effect on honeycomb panel evacuation prior to cure // Composites Part A: Applied Science Manufacturing. 2013. Vol. 49. P. 179–191.
19. Grunenfelder L.K., Nutt S.R. Void formation in composite prepregs – Effect of dissolved moisture // Composites Science and Technology. 2010. Vol. 70. P. 2304–2309.
20. Tavares S.S., Michaud V., Månson J.A.E. Through thickness air permeability of prepregs during cure // Composites Part A: Applied Science Manufacturing. 2009. Vol. 40. P. 1587–1596.
A description is given of the developed fiber-optic system for monitoring structural loading (arch-bridge elements) operating in real time and warning of approaching the critical level of loading. The criteria for working capacity of the design of the a two-lane automobile arched bridge. The choice of the main criterion was made on the basis of the principle of assessing the structural stability of the structure taking into account the capabilities of the equipment used. It is shown that the relative axial deformation of the arched elements practically did not change over the period of observation.
2. Kablov E.N. Shestoj tehnologicheskij uklad [Sixth technological way] // Nauka i zhizn. 2010. №4. S. 2–7.
3. Doriomedov M.S., Daskovskij M.I., Skripachev S.Yu., Shein E.A. Polimernye kompozicionnye materialy v zheleznodorozhnom transporte Rossii (obzor) [Polymer com-posite materials in the Russian railways (review)] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №7. St. 12. Available at: http://www.viam-works.ru (accessed: February 27, 2018). DOI: 10.18577/2307-6046-2016-0-7-12-12.
4. 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.
5. Dyshenko V.S., Raskutin A.E., Zuev M.A. Dorozhnyj detektor v sistemah bezostanovochnogo avtomaticheskogo vzveshivaniya [The road detector in systems of Weigh-In-Motion] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №5. St. 12. Available at: http://www.viam-works.ru (accessed: February 27, 2018). DOI: 10.18577/2307-6046-2016-0-5-12-12.
6. Vlasenko F.S., Raskutin A.E. Primenenie polimernyh kompozicionnyh materialov v stroitelnyh konstrukcijah [Applying FRP in building structures] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №8. St. 03. Available at: http://viam-works.ru (accessed: February 27, 2018).
7. Vasilev S.A., Medvedkov I.O., Korolev I.G. i dr. Volokonnye reshetki pokazatelya prelomleniya i ih primenenie [Fiber grids of refraction index and their application] // Kvantovaya elektronika. 2005. T. 35. №12. S. 1085–1103.
8. Sposob izmereniya deformacii konstrukcii iz kompozicionnogo materiala: pat. 2427795 Ros. Federaciya [Way of measurement of deformation of design from composite material: pat. 2427795 Ros. Federation]; opubl. 03.12.09.
9. Kablov E.N., Sivakov D.V., Gulyaev I.N. i dr. Primenenie opticheskogo volokna v kachestve datchikov defopmacii v polimepnyh kompozicionnyh materialah [Application of optical fiber as deformation sensors in polymeric composite materials] // Vse materialy. Enciklopedicheskij spravochnik. 2010. №3. S. 10–15.
10. Kablov E.N., Sivakov D.V., Gulyaev I.N., Sorokin K.V., Fedotov M.Yu., Goncharov V.A. Metody issledovaniya konstrukcionnyh kompozicionnyh materialov s integrirovannoj el-ektromehanicheskoj sistemoj [Methods of research of constructional composite materials with the integrated electromechanical system] //Aviacionnye materialy i tehnologii. 2010. №4. S. 17–20.
11. Shhetanov B.V., Kuptsov R.S., Svistunov V.I. Metody polucheniya monokristallicheskih volokon oksida alyuminiya dlya sozdaniya kompozicionnyh materialov i vysokotemperaturnoj volokonnoj optiki [Methods of receiving single-crystal fibers of aluminum oxide for creation of composite materials and high-temperature fiber optics] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №4. St. 01. Available at: http://www.viam-works.ru (accessed: February 27, 2018).
12. Nikitina V.J., Kolyshev S.G., Kuptsov R.S. Sposoby opredeleniya ploshhadi secheniya monokristallicheskih volokon Al2O3 dlya rascheta prochnosti pri rastyazhenii [The methods of determination of Al2O3 single-crystal fibers cross-section area for tensile strength calculation] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №2. St. 03. Available at: http://www.viam-works.ru (accessed: February 27, 2018). DOI: 10.18577/2307-6046-2014-0-2-3-3.
13. Huang Y., Palek L., Strommen R. et al. Real-Time Weigh-In-Motion Measurement Using Fiber Bragg Grating Sensors // Sensors and Smart Structures Technologies for Civil, Mechanical and Aerospace Systems. 2014. Vol. 9061. P. 96–102.
14. Zhou Z., Liua W., Huang Y. et al. Optical Fiber Bragg Grating Sensor Assembly for 3D Strain Monitoring and Its Case Study in Highway Pavement // Mechanical Systems and Signal Pro-cessing. 2012. Vol. 28. P. 36–49.
15. Wang K., Wei Z., Zhang H. et al. Fiber-Bragg-grating-based weigh-in-motion system using fiber-reinforced composites as the load-supporting material // Optical Engineering. 2006. Vol. 45. No. 6. P. 33–39.
16. Zhan H., Wei Z., Fan L. et al. Sensing System and a High Performance Optical Fiber Bragg Grating (FBG) Demodulator // Sensors and Smart Structures Technologies for Civil, Mechanical and Aerospace Systems. 2010. Vol. 7647. P. 102–109.
The influence of climatic factors and fluids on the properties of CFRP VKU-27L, on the basis of reinforcing carbon fabric and binder VST-1208, manufactured by autoclave molding is investigated. It is shown that the CFRP VKU-27L has a high level of property preservation (not less than 82% of the initial value) when exposed to environmental factors (thermal and hydrothermal aging, resistance to water, moisture, fuel, oil, anti-icing fluid and solvent).
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. Gunyaev G.M., Krivonos V.V., Rumyancev A.F., Zhelezina G.F. Polimernye kompozicionnye materialy v konstrukciyah letatelnyh apparatov [Polymeric composite materials in designs of flight vehicles] // Konversiya v mashinostroenii. 2004. №4 (65). S. 65–69.
4. Kablov E.N. Materialy i himicheskie tehnologii dlya aviacionnoj tehniki [Materials and chemical technologies for aviation engineering] // Vestnik Rossijskoj akademii nauk. 2012. T. 82. №6. S. 520–530.
5. Hrulkov A.V., Dushin M.I., Popov Yu.O., Kogan D.I. Issledovaniya i razrabotka avtoklavnyh i bezavtoklavnyh tehnologij formovaniya PKM [Researches and development autoclave and out-of-autoclave technologies of formation of PCM] // Aviacionnye materialy i tehnologii. 2012. №S. S. 292–301.
6. Gulyaev I.N., Zelenina I.V., Raskutin A.E. Ugleplastiki na osnove uglerodnyh tkanej importnogo proizvodstva i rossijskih rastvornyh svyazuyushhih [Carbomplastics on the basis of carbon fabrics of import production and the Russian solution binding] // Voprosy materialovedeniya. 2014. №1 (77). S. 116–125.
7. Platonov A.A., Dushin M.I. Konstrukcionnyj ugleplastik VKU-25 na osnove odnonapravlennogo preprega [Carbon composites VKU-25 based on unidirectional prepregs] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2015. №11. St. 06. Available at: http://www.viam-works.ru (accessed: February 28, 2018). DOI: 10.18577/2307-6046-2015-0-11-6-6.
8. Efimov V.A., Shvedkova A.K., Korenkova T.G., Kirillov V.N. Issledovanie polimernyh konstrukcionnyh materialov pri vozdejstvii klimaticheskih faktorov i nagruzok v laboratornyh i naturnyh usloviyah [Investigation of polymer composite materials under effect of climatic factors and loads in laboratory and environmental conditions] // Aviacionnye materialy i tehnologii. 2013. №S2. S. 68–73.
9. Kablov E.N., Starcev O.V., Krotov A.S., Kirillov V.N. Klimaticheskoe starenie kompozicionnyh materialov aviacionnogo naznacheniya. III. Znachimye faktory stareniya [Climatic aging of composite materials of aviation assignment. III. Significant factors of aging] // Deformaciya i razrushenie materialov. 2011. №1. S. 34–40.
10. Kablov E.N., Starcev O.V., Krotov A.S., Kirillov V.N. Klimaticheskoe starenie kompozicionnyh materialov aviacionnogo naznacheniya. I. Mehanizmy stareniya [Climatic aging of composite materials of aviation assignment. I. Aging mechanisms] // Deformaciya i razrushenie materialov. 2010. №11. S. 19–27.
11. Kirillov V.N., Startsev O.V., Efimov V.A. Klimaticheskaya stojkost i povrezhdaemost polimernyh kompozicionnyh materialov, problemy i puti resheniya [Climatic firmness and damageability of polymeric composite materials, problems and solutions] // Aviacionnye materialy i tehnologii. 2012. №S. S. 412–423.
12. Kablov E.N., Starcev O.V., Krotov A.S., Kirillov V.N. Klimaticheskoe starenie kompozicionnyh materialov aviacionnogo naznacheniya. II. Relaksaciya ishodnoj strukturnoj neravnovesnosti i gradient svojstv po tolshhine [Climatic aging of composite materials of aviation assignment. II. Relaxation of initial structural non-equilibrium and gradient of properties on thickness] // Deformaciya i razrushenie materialov. 2010. №12. S. 40–46.
13. Kablov E.N., Grashhenkov D.V., Erasov V.S. i dr. Stend dlya ispytaniya na klimaticheskoj stancii GCKI krupnogabaritnyh konstrukcij iz PKM [The stand for testing for the GTCT cli-matic stations of large-size designs from PCM] // Sb. dokl. IX Mezhdunar. nauch. konf. po gidroaviacii «Gidroaviasalon–2012», 2012. S. 122–123.
14. Kablov E.N., Starcev O.V., Medvedev I.M., Panin S.V. Korrozionnaya agressivnost primorskoj atmosfery. Ch. 1. Faktory vliyaniya (obzor) [Corrosion aggression of the seaside atmosphere. P.1. Factors of influence (overview)] // Korroziya: materialy, zashhita. 2013. №12. S. 6–18.
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.
The paint and varnish material filled with finely divided quasicrystals, and system of coverings on its basis is developed. As basis for polymeric matrix epoxies, as the most demanded material for anti wear coatings have been chosen. Optimum degree of dispersion of quasicrystal fillers and its content in epoxy and polyamide matrix is defined. The paint coatings filled with quasicrystals, possess the increased wear resistance, and its physico-mechanical properties do not concede to let-out analogs.
2. Istoriya aviacionnogo materialovedeniya. VIAM – 80 let: gody i lyudi / pod obshh. red. E.N. Kablova [History of aviation materials science. VIAM is 80: years and people / gen. ed. by E.N. Kablov]. M.: VIAM, 2012. 520 s.
3. Kablov E.N. Materialy i himicheskie tehnologii dlya aviacionnoj tehniki [Materials and chemical technologies for aviation engineering] // Vestnik Rossijskoj akademii nauk. 2012. T. 82. №6. S. 520–530.
4. Kablov E.N. Aviacionnoe materialovedenie: itogi i perspektivy [Aviation materials science: results and perspectives] // Vestnik Rossijskoj akademii nauk. 2002. T. 72. №1. S. 3–12.
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» [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.
6. Kablov E.N. Himiya v aviacionnom materialovedenii [Chemistry in aviation materials science] // Rossijskij himicheskij zhurnal. 2010. T. LIV. №1. S. 3–4.
7. Abuzin Yu.A., Yudin A.S. Issledovanie osobennostej kvazikristallov pri sozdanii materialov dlya kosmosa, aviacii, motorostroeniya i drugih otraslej narodnogo hozyajstva [Research of features of quasicrystals at creation of materials for space, aircraft, motor industry and other industries of national economy] // Sb. dokl. Pervogo Vseros. soveshhaniya po kvazikristallam. M., 2003. C. 15–18.
8. Rybin V.V., Ulin I.V., Farmakovskij B.F., Yurkov M.A. Izuchenie vozmozhnosti prakticheskogo ispolzovaniya kvazikristallov v kachestve funkcionalnyh pokrytij [Studying of possibility of practical use of quasicrystals as functional coverings] // Sb. dokl. Pervogo Vseros. soveshhaniya po kvazikristallam. M., 2003. S. 53–56.
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13. Gohardani O. Impact of erosion testing aspects on current and future flight conditions // Progress in Aerospace Science. 2011. Vol. 47. P. 280–303.
14. Tibor «Anpassung–Integration–Offenheit» // Werkstatt und Betr. 2011. Vol. 144. No. 7–8. P. 46–49.
15. Deev I.S., Kablov E.N., Kobets L.P., Chursova L.V. Issledovanie metodom skaniruyushhej elektronnoj mikroskopii deformacii mikrofazovoj struktury polimernyh matric pri me-hanicheskom nagruzhenii [Research of the scanning electron microscopy method deformation of microphase structure of polymeric matrix at mechanical loading] // Trudy VIAM: elektron. nauch-tehnich. zhurn. 2014. №7. St. 06. Available at: http://www.viam-works.ru (accessed: January 31, 2018). DOI: 10.18577/2307-6046-2014-0-7-6-6.
A method is proposed for obtaining thick chrome coatings in a self-regulating electrolyte with chromium plating with a positive microhardness gradient in thickness. The adhesion strength of the graded chromium coating was estimated by the temperature change method and the impact method on the vertical copra U-2M and metallographic studies of the individual layers of chromium deposited under various electrolysis regimes. The results of the investigation of residual macrostresses by x-ray diffractometric method in chromium coatings of various microhardness are presented.
2. Kablov E.N. Tendencii i orientiry innovacionnogo razvitiya Rossii: sb. inform. materialov. 3-e izd. [Tendencies and reference points of innovative development of Russia: collection of information materials. 3rd ed.]. M.: VIAM, 2015. 720 s.
3. 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.
4. Salahova R.K., Tihoobrazov A.B. Fiziko-himicheskie svojstva oksalatno-sulfatnogo elektrolita hromirovaniya, soderzhashhego nanorazmernye chasticy oksidov metallov [Physical and chemical properties of oxalate-sulfate chromium plating electrolyte, containing metal oxide nanoparticles] // Aviacionnye materialy i tehnologii. 2016. №4 (45). S. 31–39. DOI: 10.18577/2071-9140-2016-0-4-31-39.
5. Gubarevich G.P., Savchenko A.V., Fomichev V.T. Optimizaciya tehnologicheskih parametrov processa hromirovaniya iz samoreguliruyushhegosya elektrolita s kompleksnoj organo-neorganicheskoj dobavkoj [Optimization of technological parameters of process of chromizing from self-regulating electrolit with complex organo-inorganic additive] // VolgGASU: Internet-vestnik. 2015. Vyp. 4 (40). S. 1–5. URL: http://www.vestnik.vgasu.ru (data obrashheniya: 09.02.2018).
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13. Glyancev N.I., Kotov V.V., Stekolnikov Yu.A. Vliyanie hromirovaniya na fiziko-mehanicheskie svojstva metallov [Influence of chromizing on physicomechanical properties of metals] // Himiya i himicheskaya tehnologiya. 2006. T. 49. Vyp. 9. S. 74–78.
14. Semenychev V.V., Salahova R.K. Ocenka adgezii nikel-kobaltovogo pokrytiya k steklo- i ugleplastiku metodom carapanya [Evaluation of nickel-cobalt coating adhesion to fiberglass and carbon fiber–reinforced plastic by scratching] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №7 (43). St. 06. Available at: http://www.viam-works.ru (accessed: February 09, 2018). DOI: 10.18577/2307-6046-2016-0-7-6-6.
15. Pfeiffer W., Koplin C., Reisacher E., Wenzel J. Residual Stresses and Strength of Hard Chromium Coatings // Materials Science Forum. 2011. Vol. 681. Р. 133–138. DOI: 10.4028/www.scientific.net/MSF.681.133.
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As is well known, for tension test and stress-rupture test of titanium alloys applying to compressor blades and discs, in most cases are used the standard samples with 5 mm diameter and 25 mm gauge length. In a construction of gas turbine engines are applied the compressor blades of the small sizes made of fine dimensional stampings that causes the necessity of monitoring procedure of material of these compressor blades on small samples with a diameter of 3 mm and gage length of 15 mm. This work is devoted to effect of samples parameters on short-term strength and stress-rupture characteristics of heat-resistant titanium alloys VT3-1, VT9, VT18 and nickel alloys VGL12U, GS6U.
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The article analyzes the criteria for estimating the ballistic durability of ceramic materials. It is shown that the physicomechanical characteristics of ceramics obtained during static tests make it possible to assess the ballistic characteristics of ceramics only at a qualitative level, and therefore it is necessary to develop special test methods that ensure the ceramics work efficiency at high rates of its interaction with the impactor. A technique for direct estimation of the ballistic characteristics of ceramics using a trap with discrete screens is described. The results of a comparative evaluation of the ballistic characteristics of experimental batches of armored ceramics based on aluminum oxide and silicon carbide are presented. A close correspondence of the results of direct ballistic tests and calculations on the basis of the attached mass model is shown.
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Structural polymeric composite materials on the set of characteristics are at a level, and sometimes exceed the characteristics of other structural materials. Recently, modification of polymer composites by carbon nanoparticles is of particular interest, but due to their high cost and limited volume, a number of difficulties in their application may arise. Shungites are a natural rock containing fulleroid nanostructures. In addition, they have a significantly lower cost compared to synthesized carbon nanoparticles and their use in large volumes is not difficult. The purpose of this work is to study the effect of modification of polymeric composites with shungite.
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