Articles
In this work, the determination of low contents (less than 0,0005 wt. %) of arsenic in complex alloyed samples of nickel alloys was carried out by means of inductively coupled plasma mass spectrometry (ICP-MS) and atomic absorption spectrometry with electrothermal atomization. Also, the ICP-MS method was used to determine the arsenic content in chromium, which is an alloying component of nickel alloys. A technique for dissolving a sample and preparing it for analysis is presented. Spectral interferences are eliminated by applying mathematical correction equations, a reaction-collision cell and using corrective additives. The correctness of the results obtained is confirmed by the analysis of certified reference materials of nickel alloys and chromium.
2. Kablov E.N., Ospennikova O.G., Svetlov I.L. Highly efficient cooling of GTE hot section blade. Aviacionnye materialy i tehnologii, 2017, no. 2 (47), pp. 3–14. DOI: 10.18577/2071-9140-2017-0-2-3-14.
3. Bazyleva O.A., Ospennikova O.G., Arginbaeva E.G., Letnikova E.Yu., Shestakov A.V. Development trends of nickel-based intermetallic alloys. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 104–115. DOI: 10.18577/2071-9140-2017-0-S-104-115.
4. Petrushin N.V., Ospennikova O.G., Svetlov I.L. Single-crystal Ni-based superalloys for turbine blades of advanced gas turbine engines. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 72–103. DOI: 10.18577/2071-9140-2017-0-S-72-103.
5. Kablov E.N., Chabina E.B., Morozov G.A., Muravskaya N.P. Conformity assessment of new materials using high-level CRM and MI. Kompetentnost, 2017, no. 2, pp. 40–46.
6. State Standard 6689.13–92. Nickel, nickel and copper-nickel alloys. Methods for the determination of arsenic. Moscow: Publishing house of standards, 1992, pp. 1–4.
7. State Standard 1293.4–83. Lead-antimony alloys. Methods for the determination of arsenic. Moscow: Publishing house of standards, 1983, pp. 8–11.
8. State Standard 1652.8–77. Copper-zinc alloys. Methods for the determination of arsenic. Moscow: Publishing house of standards, 1977, pp. 9–12.
9. State Standard 12358–2002. Alloyed and high-alloyed steels. Methods for determining the weasel. Moscow: Standartinform, 2002, pp. 11–13.
10. Maiorova A.V., Belozerova A.A., Melchakova S.Yu. et al. Determination of Arsenic and Antimony in Ferrotungsten by Inductively Coupled Plasma Atomic Emission Spectrometry. Journal of Analytical Chemistry, 2019 vol. 74, pp. S18–S26.
11. State Standard 24018.6–80. Nickel-based heat-resistant alloys. Methods for the determination of arsenic. Moscow: Publishing house of standards, 1980, pp. 12–19.
12. Hu J., Wang H. Determination of Trace Elements in Super Alloy by ICP-MS. Mikrochimica Acta, 2001, vol. 137, pp. 149–155.
13. Pupyshev A.A., Epova E.N. Spectral interference of polyatomic ions in the method of mass spectrometry with inductively coupled plasma. Analytika i kontrol, 2001, vol. 5, no. 4, pp. 335–369.
14. Alekseev A.V., Yakimovich P.V. Determination of arsenic and selenium in high-temperature nickel alloys by ICP-MS method with hydride generation of vapor. Trudy VIAM, 2014, no. 11, paper no. 09. Available at: http://www.viam-works.ru (accessed: September 03, 2020). DOI: 10.18557/2307-6046-2014-0-11-9-9.
15. Leikin A.Yu., Karandashev V.K., Lisovskiy S.V., Volkov I.A. The use of a reaction-collision cell for the determination of impurity elements in rare-earth metals by the ICP-MS method. Zavodskaya laboratory. Diagnostika materialov, 2014, vol. 80, no. 5, pp. 6–9
Considers the features of powders obtained by various methods, their technological properties in relation to additive and granular manufacturing. The sequence of operations upon receipt of metal powder compositions is presented. The factors affecting the process of vibration sieving of metal powders and granules are described. The features and advantages of vibratory sieving on horizontally arranged circular sieves using ultrasonic cleaning to obtain specified trajectories of motion are shown. Criteria for evaluating the sieving efficiency are given and explanations are given for determining the particle size distribution of powders and granules.
2. Kablov E.N. Present and future of additive technologies. Metally Evrazii, 2017, no. 1, pp. 2–6.
3. Kablov E.N. 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, no. 1 (34), pp. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
4. Alishin M.I., Knyazev A.E. Production of metal-powder high-purity titanium alloy compositions by induction gas atomization for application in additive manufacturing. Trudy VIAM, 2017, no. 11 (59), paper no. 05. Available at: http://www.viam-works.ru (accessed: June 09, 2020). DOI: 10.18577/2307-6046-2017-0-11-5-5.
5. Kablov E.N. Powders get rid of unnecessary things. Ekspert, 2014, no. 49 (926), pp. 46–51.
6. Kablov E.N. Additive technologies – the dominant of the national technological initiative. Intellekt i tekhnologii, 2015, no. 2 (11), pp. 52–55.
7. Petrov I.M. Main trends of the Russian market of metal powders for additive technologies. Additivnyye tekhnologii, 2019, no. 1, pp. 24–26.
8. Kudrolli A. Size separation in vibrated granular matter. Reports оn Progress in Physics, 2004, vol. 67, pp. 209–247. DOI: 10.1088/0034-4885/67/3/R01.
9. Khodkin V.I. Research of processes and creation of technology for pulse-mechanical and vacuum-heat treatment of granules of heat-resistant nickel alloys in the production of blanks for engine building: thesis, Dr. Sc. (Tech.). Moscow: VILS, 1982, 410 p.
10. Knyazev A.E., Nerush S.V., Alishin M.I., Kuko I.S. Researches of the technological properties of metal-powder compositions of VT6 and VT20 titanium alloys obtained by induction melting and gas atomization. Trudy VIAM, 2017, no. 11 (59), paper no. 06. Available at: http://www.viam-works.ru (accessed: June 09, 2020). DOI: 10.18577/2307-6046-2017-0-11-6-6.
11. Garibov G.S., Koshelev V.Ya. Influence of the density of filling granules of high-temperature nickel alloys on the shape change of capsules during hot isostatic pressing. Tekhnologiya legkikh splavov, 2013, no. 1, pp. 27–33.
12. Girshov V.L., Kotov S.A., Tsemenko V.N. Modern technologies in powder metallurgy: textbook. allowance. Saint Petersburg: Publishing house of Polytechnic. University, 2010, pp. 200–214.
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18. Nazarov K.S., Fet Sh. Analysis of modern design solutions that increase the efficiency of vibration classification of difficult-to-use materials. Gornyi informatsionno-analiticheskiy byulleten, 2009, vol. 16, no. 12, pp. 383–393.
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23. A method of controlling a sieving machine: pat. 2486968 Rus. Federation; filed 13.02.12; publ. 10.07.13.
24. Denisov D.G. Separation of polydisperse materials on screens. Vestnik Ivanovskogo gosudarstvennogo energeticheskogo universiteta, 2006, no. 4, pp. 24–27.
25. Vostrikov A.V., Sukhov D.I. The production of powders by PREP method for addictive manufacturing – current situation and development prospects. Trudy VIAM, 2016, no. 8 (44), paper no. 03. Available at: http://www.viam-works.ru (accessed: June 09, 2020). DOI: 10.18577/2307-6046-2016-0-8-3-3.
In this paper a task in developing of industrial production of cold-worked thin-walled tubes from high-tech aluminum alloy V-1341 of Al–Mg–Si system was accomplished. Tubes are purposed for application in hydraulic and air conditioning systems of aircraft products. Results of investigation of the structure and mechanical properties of tubes during their technological process and heat treatment are presented. Forming of tubes was performed and construction elements of pipelines were produced, which are identical to pipelines of commercial airplanes.
2. Kablov E.N. Trends and guidelines for innovative development of Russia: Collection of information materials. Moscow: VIAM, 2015, 720 p.
3. Kablov E.N. Aviation materials science in the XXI century. Prospects and tasks. Vse materialy. Entsiklopedicheskiy spravochnik, 2007, no. 1, pp. 23–47.
4. Antipov V.V. Prospects for development of aluminium, magnesium and titanium alloys for aerospace engineering. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 186–194. DOI: 10.18577/2071-9140-2017-0-S-186-194.
5. Antipov V.V., Klochkova Yu.Yu., Romanenko V.A. Modern aluminum and aluminum-lithium alloys. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 195–211. DOI: 10.18577/2071-9140-2017-0-S-195-211.
6. Benarieb I., Ber L.B., Antipov K.V., Sbitneva S.V. Trends in development of wrought alloys of Al–Mg–Si–(Cu) system. Part 1 (review). Aviacionnye materialy i tehnologii, 2019, no. 3 (56), pp. 14–22. DOI: 10.18577/2071-9140-2019-0-3-14-22.
7. Kolykhalov D.G., Maryin B.N., Sysoev O.E. Structural and technological analysis of liquid-bone-gas systems of aircraft. Uchenyye zapiski Komsomolskogo-na-Amure gosudarstvennogo tekhnicheskogo universiteta, 2016, vol. 1, no. 3, pp. 4–10.
8. Kolykhalov D.G., Sysoev O.E., Ivanov I.N. Assessment of the manufacturability of pipeline systems of aircraft at the early stages of design. Trudy MAI, 2016, no. 90, pp. 1–22.
9. Feoktistov S.I., Maryin B.N., Maryin S.B., Kolykhalov D.G. Theory and practice of manufacturing elements of pipelines for aircraft: textbook. Komsomolsk-on-Amur: KnAGTU, 2013, 88 p.
10. Maksimenkov V.I., Fedoseev V.I., Shevchenko O.I. Investigation of the technology of manufacturing pipeline systems of medium-range aircraft. Vestnik Voronezhskogo gosudar-stvennogo tekhnicheskogo universiteta, 2011, no. 11-12, pp. 76–79.
11. Maryin B.N., Kim V.A., Sysoev O.E. et al. Analysis of defects in operating hydro-gas systems of pipelines. Uchenyye zapiski Komsomolskogo-na-Amure gosudarstvennogo tekhnicheskogo universiteta, 2017, vol. 1, no. 1, pp. 79–89.
12. Maryin B.N., Maryin S.B., Shport R.V. Production of assembly blanks for pipelines. Uchenyye zapiski Komsomolskogo-na-Amure gosudarstvennogo tekhnicheskogo universiteta, 2014, vol. 1, no. 3, pp. 60–63.
13. Gureeva M.A., Grushko O.E. Aluminum alloys in welded structures of modern vehicles. Mashinostroyeniye i inzhenernoye obrazovanie, 2009, no. 3, pp. 27–41.
14. Kuznetsov E.A., Sysoev O.E., Kolykhalov D.G. Forecasting the limiting states of high-pressure pipelines of hydro-gas systems at the stage of commissioning. Trudy MAI, 2016, no. 88, pp. 1–17.
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17. Fridlyander I.N., Grushko O.E., Bersenev V.V., Shmeleva L.M., Ivanova L.A. Influence of the type of structure on the properties of cold-rolled sheets from aluminum alloys. Tekhnologiya legkikh splavov, 2002, no. 4, pp. 47–52.
18. Klochkov G.G., Grushko O.E., Popov V.I., Ovchinnikov V.V., Shamray V.F. Structure, technological properties and weldability of B-1341 (Al–Mg–Si) sheets. Aviacionnye materialy i tehnologii, 2011, no. 1, pp. 3–8.
19. Mouritz A.P. Aluminum alloys for aircraft structures. Introduction to aerospace materials, Woodhead Publishing Ltd, 2012, pp. 188–216.
20. Klochkov G.G., Ovchinnikov V.V., Klochkova Yu.Yu., Romanenko V.A. Structure and properties of sheets from workable aluminium alloy V-1341 of Al–Mg–Si system. Trudy VIAM, 2017, no. 12 (60), paper no. 03. Available at: http://www.viam-works.ru (accessed: February 15, 2020). DOI: 10.18577/2307-6046-2017-0-12-3-3.
21. Klochkov G.G., Klochkova Yu.Yu., Romanenko V.A. Influence of deformation temperature on structure and properties of extruded products of Al–Mg–Si alloy V-1341. Trudy VIAM, 2016, no. 9 (45), paper no. 01. Available at: http://www.viam-works.ru (accessed: February 15, 2020). DOI: 10.18577/2307-6046-2016-0-9-1-1.
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23. Gureeva M.A., Grushko O.E. Influence of calcium alloying additives on the structure and phase composition of alloy ingots of the Al–Mg–Si system. Zagotovitelnye proizvodstva v mashinostroenii, 2014, no. 8, pp. 36–40.
24. Kablov E.N., Lukina E.A., Sbitneva S.V., Khokhlatova L.B., Zaitsev D.V. Formation of meta-stable phases during the decomposition of a solid solution in the process of artificial aging of Al-alloys. Tekhnologiya legkikh splavov, 2016, no. 3, pp. 7–17.
A review of the scientific technical literature in the field of modern research on silicone rubber compositions with high temperature resistance, including those with fire-resistant properties, is presented. The polymer bases and heat-stabilizing and flame-retardant additives used in the developments, as well as methods for preparing rubber mixes and rubbers are shown. Features of compounding materials with a combination of heat resistance and fire-resistance are noted. The relevance of research for the needs of aviation equipment is shown.
2. Chaikun A.M., Venediktova M.A., Bryk Ya.A. Development of the compounding of rubber extremely high heat resistance with temperature range of exploitation from the -60 to +500°С. Trudy VIAM, 2019, no. 1 (73), paper no. 03. Available at: http://viam-works.ru (accessed: August 30, 2020). DOI: 10.18577/2307-6046-2019-0-1-21-30.
3. Kablov E.N. 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, no. 1 (34), pp. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
4. Kablov E.N. Materials of a new generation – the basis of innovation, technological leadership and national security of Russia. Intellekt i technologii, 2016, no. 2 (14), pp. 16–21.
5. Kablov E.N., Startsev V.O. Systematical analysis of the climatics influence on mechanical properties of the polymer composite materials based on domestic and foreign sources (review). Aviacionnye materialy i tehnologii, 2018, no. 2 (51), pp. 47–58. DOI: 10.18577/2071-9140-2018-0-2-47-58.
6. Kablov E.N. The role of chemistry in the creation of new generation materials for complex technical systems. Reports of XX Mendeleev Congress on General and Applied Chemistry. Ekaterinburg: UB of RAS, 2016, pp. 25–26.
7. Laptev A.B., Barbotko S.L., Nikolaev E.V. The main research areas of the persistence properties of materials under the influence of climatic and operational factors. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 547–561. DOI: 10.18577/2071-9140-2017-0-S-547-561.
8. Naumov I.S., Petrova A.P., Barbotko S.L., Vaniev M.A., Demidov D.V. Colored and black sealing rubbers of low combustibility based on siloxane rubbers. Vse materialy. Entsiklopedicheskiy spravochnik, 2017, no. 5, pp. 24–31.
9. Reznichenko S.V., Morozov Yu.L. Great reference book of the rubber-maker. Moscow: Techinform, 2012., 744 p.
10. High temperature mixing silicone rubber as well as preparation method and application thereof: pat. CN104761911B; filed 03.04.15; publ. 22.02.17.
11. Heat-resistant composition based on siloxane block copolymer: pat. 2196154C2 Rus. Federation; filed 26.12.00; publ. 20.01.03.
12. Todd H.E., Miazga J.F. Properties of Silicone Rubber for High-Temperature Static Seals. SAE Transactions, 1960, vol. 68, pp. 224–231.
13. Heat resistant silicone rubber composition: pat. US9803062B2; filed 23.05.14; publ. 31.10.17.
14. High-temperature resistant silicon rubber and preparation method thereof: pat. CN102061093A; filed 18.11.10; publ. 18.05.11.
15. Mixed rubber for high-temperature-resistant silicon rubber die: pat. CN102796290A; filed 31.08.12; publ. 28.11.12.
16. A kind of low cost high-temperature resisting methyl vinyl silicone rubber: pat. CN108102385A; filed 25.11.17; publ. 01.06.18.
17. Su Z.-T., Wang J.-H. Properties of silicone rubber at high or low temperature. 2006. Available at: https://www.researchgate.net/publication/296737966_Properties_of_silicone_rubber_at_high_or_low_temperature (дата обращения: 30.08.2020).
18. High-temperature-resistant silicon rubber additive and method: pat. CN102643550A; filed 28.04.12; publ. 22.08.12.
19. High-temperature resisting methyl vinyl silicone rubber: pat. CN101735620B; filed 27.12.09; publ. 03.08.11.
20. Heat-resistant silicone rubber composition and its molded product: pat. JP2001348481A; filed 09.06.00; publ. 18.12.01.
21. Heat-resistant silicone rubber composition and molded article obtained by curing the composition: pat. JP2002220532A; filed 25.01.01; publ. 09.08.02.
22. High-temperature-resisting silicon rubber and preparation method thereof: pat. CN104725862A; filed 17.12.14; publ. 24.06.15.
23. Flame-retardant silicone rubber: pat. JP2006176778A; filed 21.12.05; publ. 06.07.06.
24. Flame-retardant silicone rubber composition and flame-retardant silicone rubber molding using the same: pat. JPH09188815A; filed 05.01.96; publ. 03.02.04.
25. Novel high-temperature-resistant silicon rubber and preparation method thereof: pat. CN111040454A; filed 30.12.19; publ. 21.04.20.
26. Highly heat-resistant silicone rubber composition: pat. JP2006182902A; filed 27.12.04; publ. 13.07.06.
Questions of development of decorative and finishing materials for wall panels of passenger cab and the crew cockpit of air vehicles in the Russian Federation and abroad are considered. The structure and structure of such materials are described, examples of implementation of their different options are given. The main ways of manufacturing of materials, and also requirements to them which performance is necessary for the admission to application in aviation engineering, and the requirements providing competitive advantage of materials in comparison with analogs are provided. The main directions of development of decorative and finishing materials are evaluated.
2. Kablov E.N., Kashapov O.S., Medvedev P.N., Pavlova T.V. Study of a α+β-titanium alloy based on a system of Ti–Al–Sn–Zr–Si–β-stabilizing alloying elements. Aviacionnye materialy i tehnologii, 2020, no. 1 (58), pp. 30–37. DOI: 10.18577/2071-9140-2020-0-1-30-37.
3. Kablov E.N., Startsev V.O., Inozemtsev A.A. The moisture absorption of structurally similar samples from polymer composite materials in open climatic conditions with application of thermal spikes. Aviacionnye materialy i tehnologii, 2017, no. 2 (47), pp. 56–68. DOI: 10.18577/2071-9140-2017-0-2-56-68.
4. Shuldeshova P.M., Zhelezina G.F. An influence of atmospheric condition and dust loading on properties of structural organic plastics. Aviacionnye materialy i tehnologii, 2014, no. 1, pp. 64–68. DOI: 10.18577/2071-9140-2014-0-1-64-68.
5. Lexan F6000. Available at: www.sabic.com (accessed: May 18, 2020).
6. Nesterova T.A., Barbotko S.L., Nikolaeva M.F., Gerter Yu.A. Multi-layer protective and decorative material for decorating details in the cabin of aircraft and helicopters. Trudy VIAM, 2013, no. 8, paper no. 04. Available at: http://www.viam-works.ru (accessed: May 18, 2020).
7. Decorative-sheet manufacturing method: pat. US2017217145А1; filed 21.10.15; publ. 03.08.17.
8. Decorative multilayer material: pat. RU141769U1; filed 28.08.13; publ. 10.06.14.
9. Product decorative laminates: pat. FR2380879A1; filed 18.02.77. publ. 15.09.78.
10. Decorative element and decorative item: pat. RU65530U1; filed 09.03.07; publ. 10.08.07.
11. Decorative layered material and method of obtaining it (options): pat. RU2151063C1; filed 09.07.99; publ. 20.06.00.
12. Flexible laminate for coating and protection of surfaces, and manufacturing method of the same: pat. US2005042438A1; filed 24.09.03; publ. 24.02.05.
13. Soft decorative film and UV coating technology and application thereof: pat. CN107471788 (A); filed 07.06.16; publ. 15.12.17.
14. Coating mechanism of base layer in PVC decorative film forming device: pat. CN209502108 (U); filed 14.01.19; publ. 18.10.19.
15. Laminate film made of polyolefin-based resin: pat. JP2004002825A; filed 18.04.03; publ. 08.01.04.
16. Composite system of nano protective film, PVC decorative layer and aluminum-manganese alloy layer and composite method of composite system: pat. CN109334014 (A); filed 15.11.18; publ. 15.02.19.
17. Decorative film and method for producing same and decorated molded article: pat. US2019077134А1; filed: 23.05.16; publ. 14.03.19.
18. Decorative and finishing coatings that imitate the texture and relief of natural or artificial ornamental stones, shell rock or wood of various species: pat. RU2004133200A; filed 15.11.04; publ. 20.04.06.
19. A method of obtaining a protective coating on materials and products made of polycarbonate: pat. RU2561406C1; filed 05.05.14; publ. 27.08.15.
20. Decorative laminate: pat. RU2039661C1; filed 05.03.92; publ. 20.07.95.
21. Means of transport having a film for the coating of at least one of its surfaces: pat. WO2014/114566A1; filed 17.01.14; publ. 31.07.14.
22. Film from polyester resin for lamination of decorative material: pat. TW537962B; filed 30.11.99; publ. 21.06.03.
23. Bondable and tape/label-releasable top-coated overlays useful in the manufacture of decorative laminate panels: pat. US 5985595; filed 24.03.97; publ. 28.09.99.
24. Embossed reflective laminates: pat. US2003161997A1; filed 16.01.03; publ. 28.08.03.
25. Laminate floor panel: pat. EP2263867A1; filed 13.07.09; publ. 22.12.10.
26. Designed coating film: pat. JP09169933A; filed 19.12.95; publ. 30.06.97.
27. Laminated film or sheet substituted for coating, method for manufacturing the same, and laminate including laminated film or sheet substituted for coating: pat. JP2003034006A; filed 17.05.02; publ. 04.02.03.
28. Protective and decorative coating of a non-metallic product: pat. RU49738U1; filed 28.03.05; publ. 10.12.05.
29. Laminate film for decorating molded article, paint composition and decorative molded article: pat. JP2015145103 (A); filed 03.02.14; publ. 18.03.15.
30. Multilayer laminate having amorphous fluororesin coating film formed on water-repellent surface: pat. JP2016150584А; filed 19.02.15; publ. 22.08.16.
31. A method of producing films with a layer of mixtures of fluoropolymers and polyacrylates: pat. RU2254238C2; filed 03.12.99; publ. 20.06.05.
32. Method of applying fluoropolymer coatings for surface protection: pat. RU2394860C1; filed 24.10.08; publ. 20.07.10.
33. Laminate film for decorating three-dimensional molded article for vacuum molding, method for decorating three-dimensioanal molded article and decorative molded article: pat. JP2017007109А; filed 17.06.15; publ. 12.01.17.
34. Laminated polyester film: pat. JP2012223984A; filed 20.04.11; publ. 15.11.12.
35. Multilayer film: pat. RU2381104C2; filed 09.06.05; publ. 10.02.10.
36. Wiping coating method: pat. JP0833866A; filed 22.07.94; publ. 06.02.96.
37. Barbotko S.L. Fire safety of aviation materials. Aviacionnye materialy i tehnologii, 2012, no. S, pp. 431–439.
38. Barbotko S.L., Volny O.S., Kirienko O.A., Shurkova E.N. Assessment of fire safety of polymer materials for aviation purposes: state analysis, test methods, development prospects, methodological features: textbook. Ed. E.N. Kablov. Moscow: VIAM, 2018, 424 p.
39. Volny O.S., Kirienko O.A., Shurkova E.N., Barbotko S.L. Investigation of the influence of operational factors on the fire safety characteristics of decorative and finishing polymer materials for aviation purposes. Sovremennyye tekhnologii obespecheniya grazhdanskoy oborony i likvidatsii posledstviy chrezvychaynykh situatsiy, 2015, no. 1-1 (6), pp. 69–72.
40. Polyvinyl chloride of reduced combustibility, including organophosphorus polymers containing organophosphorus fragments, and a method for their preparation: pat. RU2385327C1; filed 04.08.08; publ. 27.03.10.
41. Decorative laminates incorporating flame retardant engineering thermoplasticfilms: pat. US2010/0272976A1; filed. 27.04.10, publ. 28.10.10.
42. Decorative film having low gross heat of combustion: pat. US2014/0322473A1; filed 30.09.11; publ. 30.10.14.
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The article is devoted to the consideration of the world and Russian market of aramid fiber. Provides information about the approximate production of aramid fibers in general and by types: para- and meta-aramid. The main trade names of aramid fibers, production facilities, main aramid producers in the world and in Russia, information about the properties of some brands of aramid fiber and indicative percentages of various fields of application in the global and Russian consumption of aramid fibers are given.
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The results of investigation of thermal treatment influence on thermophysical properties of metal composite material (MCM) based on aluminium casting alloy АК9ч (АЛ4) grade of Al–Si–Mg system reinforced with silicon carbide particles with content of reinforcing particles of 69±1% (volume) are given. MCM is made by solid-phase method followed by vacuum annealing. There are also presented studies of thermophysical characteristics of the material: thermal conductivity, temperature coefficient of linear expansion in the temperature range from 20 to 400 °C and density. It is shown that thermophysical characteristics depend on structural characteristics of the material.
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A review of the scientific and technical literature in the field of the most used methods of physical vapor deposition for the manufacture of metal matrix composites (MMCs) reinforced silicon carbide fibers is presented. The most widespread methods of solid-phase technology for the manufacture of MMCs are briefly considered, and methods of electron-beam deposition and magnetron sputtering of a matrix titanium alloy on silicon carbide fibers are discussed in detail. The morphological structure of the surface of the deposited matrix alloy on fibers, obtained by different methods, is investigated.
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The efficiency of various variants of the component composition of alkaline electrolytes of plasma electrolytic oxidation (PEO) was studied. Technical liquid glass, NaOH, Na2B4O7, Na3PO4, and NaAlO2 were used as components of aqueous solutions. All of the studied components of electrolytes are the most common for use in PEO processes of aluminum alloys. The influence of the component composition of electrolytes on their stability during 30 days of exposure was evaluated, and the most stable compositions were selected. The structure and properties of coatings formed on samples of aluminum alloy AK6 during PEO are studied. The dependences of the hardness of coatings and their growth rate on the composition of the electrolyte are established. Possible variants of coating growth in the PEO process with different component composition of electrolytes are proposed.
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Рrovides an overview of the methods of chemical and electrochemical removal of hardening coatings based on titanium nitride (TiN) and zirconium nitride (ZrN) from the surface of parts made of various materials that can be used to remove defective and waste coatings from the surface of compressor blades and other parts of gas turbine engines (GTE) from titanium alloys. The main disadvantages of the described methods are shown in relation to the removal of hardening coatings from the surface of compressor blades and other GTE parts made of titanium alloys. Taking into account the shortcomings of the available methods, FSUE «VIAM» has developed effective methods for chemical removal of hardening coatings based on titanium nitride and zirconium nitride from the surface of parts made of titanium alloys, and recommendations are given for controlling the completeness of removal of coatings.
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8. Process for treating the surface of a component, made from a Ni based supperalloy, to be coated: pat. US6440238B1; filed 09.08.99; publ. 27.08.02.
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10. Method for removing titanium nitride film from the surface of stainless steel products: pat. 2039851С1 Rus. Federation; filed 17.08.92; publ. 20.07.95.
11. Method for repairing parts, mainly blades, gas turbine engines: pat. 2205734С2 Rus. Federation; filed 14.03.01; publ. 10.06.03.
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14. Method for removing coating from parts and solution for removing coating: pat. 2507311S2 Rus. Federation; filed 09.04.09; publ. 20.02.14.
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16. Method of electrolyte-plasma removal of coatings from titanium nitrides or nitrides of titanium compounds with metals: pat. 2467098C1 Rus. Federation; filed 25.04.11; opubl. 20.11.12.
17. Kablov E.N. 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, no. 1 (34), pp. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
