Source: http://viam-works.ru/en/articles?year=2015&num=4
Timestamp: 2019-04-20 02:45:35+00:00

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The investigation results of the new weldable wrought alloy V-1208 based on Al–Cu–Mn system with addition of Sc, Ag and Zr are represented. Sheets from this alloy were manufactured at JSC «KUMW». It was shown that scandium, silver and zirconium complex additions increase strength and life-time characteristics, corrosion resistance and weldability. Influence of heat treatment modes on the sheets mechanical properties was studied. Complex investigations of mechanical, corrosion and operational charac-teristics are represented. Weldability with argon arc welding and friction stir welding are evaluated. Comparison with 1201 and 2219 alloys is carried out.
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Stolyankov Yu.V., Gulyaev I.N., Aleksashin V.M., Antyufeeva N.V.
The matter of amorphous metal bands application in the laminated metal-polymeric functional components (actuators) for smart materials is hereby considered. The remarkable feature of the metal amorphous materials is their structural and chemical homogeneity, high plasticity and their resistance to repeated bending and corrosion. It is suggested to use the amorphous metal materials as bands in conjunction with ferroelectric ceramics made of lead zirconium-titanate to create laminated piezoelectric cells. Phase transformation process in nickel-based amorphous alloy VPr51 of metal-metalloid type by means of differential scanning calorimetry and thermo-mechanical analysis methods is studied as well. It is determined that the given nickel-based amorphous alloy keeps its structural homogeneity and workability in the temperature range up to 380°C relevant to the piezoelectric materials based on lead titanate-zirconium operation.
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The method of raster electron microscopy and the fractographic analysis was applied to research surface and microstructure of heat resistant nickel alloys samples before and after destruction in order to identify pre-destruction signs after tests for short-term and long-term hardness and also for low-cyclic fatigue at temperatures of 20, 650 and 750°С. It is determined that exits density of slip planes on surface of studied samples depends on testing method, level of applied load and temperature of tests, there are differences in behavior of alloys during the loading. Difference in resistance to slip systems development and to destruction start after exhaustion of material ability for plastic deformation is shown for two alloys.
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23. Lomberg B.S., Ovsepjan S.V., Bakradze M.M. i dr. Vysokotemperaturnye zharoprochnye ni-kelevye splavy dlja detalej gazoturbinnyh dvigatelej [High-temperature heat resisting nickel alloys for details of gas turbine engines] //Aviacionnye materialy i tehno-logii. 2012. №S. S. 52–57.
24. Morozova G.I. Zakonomernost' formirovanija himicheskogo sostava γ′/γ-matricy mnogokomponentnyh nikelevyh splavov [Pattern of forming of chemical composition γ′/γ-матрицы multicomponent nickel alloys] //Doklady Akademii nauk. 1991. T. 320. №6. S. 1413–1416.
Budinovskiy S.A., Smirnov A.A., Matveev P.V., Chubarov D.A.
The complex thermal barrier coating (TBC) for rotor blades of jet prop engines made of nickel-base superalloy VZHM4 working at temperatures up to 1200°С is represented, and also application of high-temperature heat resistant coatings for intermetallic nickel-base alloys as a bond coatings for turbine nozzle blades working at temperatures up to 1250°С is considered. Results of high-temperature tests of VZhM4 and VKNA-25 alloys with applied TBC are represented. It is shown that [Ni–Cr–Al–Ta–Re–Y–Hf+Al–Ni–Y]+(Zr–Y–Gd)O TBC protects VZhM4 alloy at temperatures up to 1200°С and [Ni–Cr–Al–Hf+Al–Ni–Hf]+(Zr–Y–Gd)O HPC protects VKNA-25 alloy at temperatures up to 1250°С. Research of thermal conductivity of ceramic (Zr–Y–Gd)O material is made.
1. Petrushin N.B., Ospennikova O.G., Visik E.M. i dr. Zharoprochnye nikelevye splavy nizkoj plotnosti [Heat resisting nickel alloys of low density] //Litejnoe proizvodstvo. 2012. №6. S. 5–11.
2. Kuznecov V.P., Lesnikov V.P., Konakova I.P., Petrushin N.V., Mubojadzhjan S.A. Struktura i fazovyj sostav monokristallicheskogo splava VZhM4 s gazocirkuljacionnym zashhitnym pokrytiem [Structure and phase composition of VZhM4 single-crystal alloy with gazotsirkulyatsionny protecting cover] //MiTOM. 2011. №3. S. 28–32.
3. Bazyleva O.A., Arginbaeva Je.G., Turenko E.Ju. Zharoprochnye litejnye intermetallidnye splavy [Heat resisting cast intermetallidny alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 57–60.
4. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlja vysokoteplonagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for the high-heatloaded details of gas turbine engines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 13–19.
5. Budinovskij S.A. Primenenie analiticheskoj modeli opredelenija uprugih mehanicheskih i termicheskih naprjazhenij v mnogoslojnoj sisteme v reshenii zadach po sozdaniju zharostojkih aljuminidnyh pokrytij [Application of analytical model of determination of elastic mechanical and thermal stresses in multi-layer system in the solution of tasks on creation of heat resisting alyuminidny coverings] //Uprochnjajushhie tehnologii i pokrytija. 2013. №3. S. 3–11.
6. Budinovskij S.A., Kablov E.N., Mubojadzhjan S.A. Primenenie analiticheskoj modeli opredelenija uprugih naprjazhenij v mnogoslojnoj sisteme pri reshenii zadach po sozdaniju vysokotemperaturnyh zharostojkih pokrytij dlja rabochih lopatok aviacionnyh turbin [Application of analytical model of determination of elastic stresses in multi-layer system at the solution of tasks on creation of high-temperature heat resisting coverings for working blades of aviation turbines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 26–37.
7. Smirnov A.A., Budinovskij S.A. Analiz jevoljucii normal'nyh naprjazhenij v sisteme «splav–pokrytie» v oblasti temperatur do 1200°С [The analysis of evolution of normal stresses in splav-pokrytiye system in the field of temperatures to 1200°С] //Aviacionnye materialy i tehnologii. 2014. №2. S. 8–14.
8. Budinovskij S.A., Matveev P.V., Smirnov A.A. Issledovanie zharostojkosti litejnyh zharoprochnyh nikelevyh splavov v oblasti temperatur 1000–1200°С [Research of heat resistance of cast heat resisting nickel alloys in the field of temperatures 1000–1200°C] //Aviacionnaja promyshlennost'. 2014. №2. S. 48–52.
9. Budinovskij S.A., Mubojadzhjan S.A., Gajamov A.M., Stepanova S.V. Ionno-plazmennye zharostojkie pokrytija s kompozicionnym bar'ernym sloem dlja zashhity ot okislenija splava ZhS36-VI [Ion-plasma heat resisting coverings with composition barrier layer for protection against oxidation of alloy ZhS36-VI] //MiTOM. 2011. №1. S. 34–40.
10. Mubojadzhjan S.A., Budinovskij S.A., Gajamov A.M., Smirnov A.A. Poluchenie keramicheskih teplozashhitnyh pokrytij dlja rabochih lopatok turbin aviacionnyh GTD magnetronnym metodom [Receiving ceramic heat-protective coatings for working blades of turbines of aviation GTD magnetronny method] //Aviacionnye materialy i tehnologii. 2012. №4. S. 3–8.
11. Mubojadzhjan S.A., Budinovskij S.A., Gajamov A.M., Matveev P.V. Vysokotemperaturnye zharostojkie pokrytija i zharostojkie sloi dlja teplozashhitnyh pokrytij [High-temperature heat resisting coverings and heat resisting layers for heat-protective coverings] //Aviacionnye materialy i tehnologii. 2013. №1. S. 17–20.
12. Kablov E.N., Mubojadzhjan S.A. Zharostojkie i teplozashhitnye pokrytija dlja lopatok turbiny vysokogo davlenija perspektivnyh GTD [Heat resisting and heat-protective coverings for turbine blades of high pressure of perspective GTD] //Aviacionnye materialy i tehnologii. 2012. №S. S. 60–70.
13. Chubarov D.A., Matveev P.V. Novye keramicheskie materialy dlja teplozashhitnyh pokrytij rabochih lopatok GTD [New ceramic materials for heat-protective coverings of working blades of GTD] //Aviacionnye materialy i tehnologii. 2013. №4. S. 43–46.
14. Budinovskij S.A., Mubojadzhjan S.A., Gajamov A.M. Sovremennoe sostojanie i osnovnye tendencii razvitija vysokotemperaturnyh teplozashhitnyh pokrytij dlja rabochih lopatok turbin aviacionnyh GTD [Current state and the main tendencies of development of high-temperature heat-protective coverings for working blades of turbines of aviation GTD] //Aviacionnaja promyshlennost'. 2008. №4. S. 33–37.
15. Gajamov A.M., Budinovskij S.A., Mubojadzhjan S.A., Kos'min A.A. Vybor zharostojkogo pokrytija dlja zharoprochnogo nikelevogo renij-rutenijsoderzhashhego splava marki VZhM4 [Choice of heat resisting covering for heat resisting nickel reny -ruteniysoderzhashchy alloy of the VZhM4 brand] //Trudy VIAM. 2014. №1. St. 01 (viam-works.ru).
16. Budinovskij S.A., Mubojadzhjan S.A., Gajamov A.M., Matveev P.V. Razrabotka ionno-plazmennyh zharostojkih metallicheskih sloev teplozashhitnyh pokrytij dlja ohlazhdaemyh rabochih lopatok turbin [Development of ion-plasma heat resisting metal layers of heat-protective coverings for cooled working blades of turbines] //MiTOM. 2013. №11. S. 16–21.
17. Kos'min A.A., Budinovskij S.A., Mubojadzhjan S.A., Bulavinceva E.E. Zharostojkoe pokrytie dlja novogo perspektivnogo intermetallidnogo splava VIN3 [Heat resisting covering for new perspective intermetallidny alloy of VIN3] //Svarochnoe proizvodstvo. 2013. №6. S. 35–37.
18. Matveev P.V., Budinovskij S.A., Mubojadzhjan S.A., Kos'min A.A. Zashhitnye zharostojkie pokrytija dlja splavov na osnove intermetallidov nikelja [Protective heat resisting coverings for alloys on the basis of nickel intermetallic compound] //Aviacionnye materialy i teh-nologii. 2013. №2. S. 12–15.
19. Matveev P.V., Budinovskij S.A. Issledovanie svojstv zashhitnyh zharostojkih pokrytij dlja intermetallidnyh nikelevyh splavov tipa VKNA dlja rabochih temperatur do 1300°С [Research of properties of protective heat resisting coverings for intermetallidny nickel alloys of VKNA type for working temperatures to 1300°С] //Aviacionnye materialy i tehnologii. 2014. №3. S. 22–26.
20. Kablov E.N., Mubojadzhjan S.A., Budinovskij S.A., Lucenko A.N. Ionno-plazmennye zashhitnye pokrytija dlja lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] //Metally. 2007. №5. S. 23–34.
21. Muboyadzhyan S.A., Kablov E.N. Vacuum plasma technique of protective coatings pro-duction of complex alloys //MiTOM. 1995. №2. S. 15–18.
22. Kablov E.N., Mubojadzhjan S.A., Budinovskij S.A., Pomelov Ja.A. Ionno-plazmennye zash-hitnye pokrytija dlja lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] //Konversija v mashinostroenii. 1999. №2. S. 42–47.
It was determined that the maximum level of strength is achieved after full heat treatment (quenching and artificial ageing) after welding. Heat treatment of welded joints made by friction stir welding leads to structural heterogeneity alignment and removal of weakening of the heat affected zone. After-welding modes of heat treatment do not practically influence the protective properties of non-metallic inorganic coatings.
1. Kablov E.N., Lukin V.I., Ospennikova O.G. Perspektivnye aljuminievye splavy i tehnologii ih soedinenija dlja izdelij aviakosmicheskoj tehniki [Perspective aluminum alloys and technologies of their connection for products of aerospace equipment] /V sb. Tezisov dokladov II Mezhdunarodnoj konf. «Aljuminij–21/Svarka i pajka». 2012. S. 8.
3. Kablov E.N. Sovremennye materialy – osnova innovacionnoj modernizacii Rossii [Modern materials – basis of innovative modernization of Russia] //Metally Evrazii. 2012. №3. S. 10–15.
4. Panin V.E., Kablov E.N., Pochivalov Ju.I., Panin S.V., Kolobnev N.I. Vlijanie nanostrukturirovanija poverhnostnogo sloja aljuminij-litievogo splava 1424 na mehanizmy deformacii, tehnologicheskie harakteristiki i ustalostnuju dolgovechnost'. Povyshenie plastichnosti i tehnologicheskih harakteristik [Influence of nanostructuring surface layer aluminum-lithium alloy 1424 on deformation mechanisms, technical characteristics and fatigue life. Increase of plasticity and technical characteristics] //Fizicheskaja mezomehanika. 2012. T. 15. №6. S. 107–111.
6. Fridljander I.N., Chuistov K.V., Berezina A.L., Kolobnev N.I., Koval' Ju.N. Aljuminij-litievye splavy. Struktura i svojstva [Aluminum-lithium alloys. Structure and properties]. K.: Naukova dumka. 1992.
7. Fridlyander I.N., Sister V.G., Grushko O.E., Berstenev V.V., Sheveleva L.M., Ivanova L.A. Aluminum alloys: promising materials in the automotive industry //Metal Science and Heat Treatment. 2002. Т. 44. №9–10. P. 365–370.
9. Klochkov G.G., Grushko O.E., Klochkova Ju.Ju., Romanenko V.Ju. Promyshlennoe osvoenie vysokoprochnogo splava V-1469 sistemy Al–Cu–Li–Mg [Industrial development of V-1469 high-strength alloy of Al–Cu–Li–Mg system] //Trudy VIAM. 2014. №7. St. 01 (viam-works.ru).
10. Samorukov M.L. Analiticheskij podhod k matematicheskomu modelirovaniju temperaturnoj sostavljajushhej rotacionnoj svarki treniem [Analytical approach to mathematical modeling of temperature component of rotational friction bonding] //Trudy VIAM. 2013. №9. St. 03 (viam-works.ru).
11. Lukin V.I., Ospennikova O.G., Ioda E.N., Panteleev M.D. Svarka aljuminievyh splavov v aviakosmicheskoj promyshlennosti [Welding of aluminum alloys in the aerospace industry] //Svarka i diagnostika. 2013. №2. S. 47–52.
12. Lukin V.I., Ioda E.N., Bazeskin A.V. i dr. Povyshenie nadezhnosti svarnyh soedinenij iz vysokoprochnogo aljuminievo-litievogo splava V-1461 [Increase of reliability of welded connections from high-strength aluminum-lithium alloy V-1461] //Svarochnoe proizvodstvo. 2010. №11. S. 14–17.
13. Petrovic M., Veljic D., Rakin M., Radovic N., Sedmak A., Bajic N. Friction-stir welding of high-strength aluminium alloys and a numerical simulation of plunge stage //Materials in technology. 2012. V. 46. №3. P. 215–221.
14.	Silis M.I., Eliseev A.A., Silis V.Je. i dr. Osobennosti struktury svarnyh soedinenij aljuminievyh splavov, poluchennyh frikcionnoj svarkoj [Features of structure of welded compounds of the aluminum alloys received by frictional welding] //MiTOM. 2009. №4. S. 34–39.
15.	Lukin V.I., Ioda E.N., Bazeskin A.V. i dr. Osobennosti formirovanija svarnogo soedinenija pri svarke treniem s peremeshivaniem aljuminievogo splava V-1469 [Features of forming of welded connection at friction bonding with V-1469 aluminum alloy hashing] //Svarochnoe proizvodstvo. 2012. №6. S. 30–36.
16.	Antipov V.V., Kolobnev N.I., Hohlatova L.B. Razvitie aljuminijlitievyh splavov i mnogostupenchatyh rezhimov termicheskoj obrabotki [Development of alyuminiylitiyevy alloys and multistage modes of thermal processing] //Aviacionnye materialy i tehnologii. 2012. №S. S. 183–195.
17.	Oglodkov M.S., Hohlatova L.B., Kolobnev N.I. i dr. Vlijanie termomehanicheskoj obrabotki na svojstva i strukturu splava sistemy Al–Cu–Mg–Li–Zn [Influence of thermomechanical processing on properties and Al–Cu–Mg–Li–Zn system alloy structure] //Aviacionnye materialy i tehnologii. 2010. №4. S. 7–11.
18. Zhilikov V.P., Karimova S.A., Leshko S.S., Chesnokov D.V. Issledovanie dinamiki korrozii aljuminievyh splavov pri ispytanii v kamere solevogo tumana (KST) [Research of dynamics of corrosion of aluminum alloys when testing in the salt spray chamber (KST)] //Aviacionnye materialy i tehnologii. 2012. №4. S. 18–22.
The article considers advantages and disadvantages of currently used ZrO2–(7–8)%Y2O3 (yttrium-stabilized zirconia – YSZ) ceramic layer, widely used now in serial coatings to protect turbine blades of gas turbine engines. The systems and some properties of new ceramic materials based on zirconium oxide with the addition of one or more rare earth elements which are currently being developed abroad are represented. The ceramic layers developed by VIAM brought on by magnetron midrange targets sputtering based on zirconium alloys with rare earth metals with following plasma chemical ceramics deposition in the argon oxygen environment are shown. The microstructure of the surface of the deposited layers, thermal conductivity and the prospects of their use in the development of a new thermal barrier coating (TBC) generation are investigated.
1. Budinovskij S.A., Mubojadzhjan S.A., Gajamov A.M. Sovremennoe sostojanie i osnovnye tendencii razvitija vysokotemperaturnyh teplozashhitnyh pokrytij dlja rabochih lopatok turbin aviacionnyh GTD [Current state and the main tendencies of development of high-temperature heat-protective coverings for working blades of turbines of aviation GTD] //Aviacionnaja promyshlennost'. 2008. №4. S. 33–37.
2. Kuznecov V.P., Lesnikov V.P., Konakova I.P. i dr. Struktura i fazovyj sostav monokristallicheskogo splava VZhM4 s gazocirkuljacionnym zashhitnym pokrytiem [Structure and phase composition of VZhM4 single-crystal alloy with gazotsirkulyatsionny protecting cover] //MiTOM. 2011. №3. S. 28–32.
3. Kos'min A.A., Budinovskij S.A., Mubojadzhjan S.A., Bulavinceva E.E. Zharostojkoe pokrytie dlja novogo perspektivnogo intermetallidnogo splava VIN3 [Heat resisting covering for new perspective intermetallidny alloy of VIN3] //Svarochnoe proizvodstvo. 2013. №6. S. 35–37.
4. Budinovskij S.A., Kablov E.N., Mubojadzhjan S.A. Primenenie analiticheskoj modeli opredelenija uprugih naprjazhenij v mnogoslojnoj sisteme pri reshenii zadach po sozdaniju vysokotemperaturnyh zharostojkih pokrytij dlja rabochih lopatok aviacionnyh turbin [Application of analytical model of determination of elastic stresses in multi-layer system at the solution of tasks on creation of high-temperature heat resisting coverings for working blades of aviation turbines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 26–37.
5. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlja vysokoteplonagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for the high-heatloaded details of gas turbine engines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 13–19.
6. Kablov E.N., Mubojadzhjan S.A. Ionnoe travlenie i modificirovanie poverhnosti otvetstvennyh detalej mashin v vakuumno-dugovoj plazme [Ion etching and modifying of surface of responsible details of machines in vacuum and arc plasma] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 149–163.
7. Kablov E.N., Mubojadzhjan S.A., Budinovskij S.A., Pomelov Ja.A. Ionno-plazmennye zashhitnye pokrytija dlja lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] //Konversija v mashinostroenii. 1999. №2. S. 42–47.
8. Muboyadzhyan S.A., Kablov E.N. Vacuum plasma technique of protective coatings production of complex alloys//MiTOM. 1995. №2. S. 15–18.
9. Kablov E.N., Ospennikova O.G., Vershkov A.V. Redkie metally i redkozemel'nye jelementy – materialy sovremennyh i budushhih vysokih tehnologij [Rare metals and rare earth elements – materials of modern and future high technologies] //Trudy VIAM. 2013. №2. St. 01 (viam-works.ru).
10. Matveev P.V., Budinovskij S.A., Mubojadzhjan S.A., Kos'min A.A. Zashhitnye zharostojkie pokrytija dlja splavov na osnove intermetallidov nikelja [Protective heat resisting coverings for alloys on the basis of nickel intermetallic compound] //Aviacionnye materialy i teh-nologii. 2013. №2. S. 12–15.
11. Budinovskij S.A., Mubojadzhjan S.A., Gajamov A.M., Matveev P.V. Razrabotka ionno-plazmennyh zharostojkih metallicheskih sloev teplozashhitnyh pokrytij dlja ohlazhdaemyh rabochih lopatok turbin [Development of ion-plasma heat resisting metal layers of heat-protective coverings for cooled working blades of turbines] //MiTOM. 2013. №11. S. 16–21.
12. Budinovskij S.A., Mubojadzhjan S.A., Gajamov A.M., Stepanova S.V. Ionno-plazmennye zharostojkie pokrytija s kompozicionnym bar'ernym sloem dlja zashhity ot okislenija splava ZhS36-VI [Ion-plasma heat resisting coverings with composition barrier layer for protection against oxidation of alloy ZhS36-VI] //MiTOM. 2011. №1. S. 34–40.
13. Kablov E.N., Mubojadzhjan S.A., Budinovskij S.A., Lucenko A.N. Ionno-plazmennye zashhitnye pokrytija dlja lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] //Metally. 2007. №5. S. 23–34.
14. Gajamov A.M., Budinovskij S.A., Mubojadzhjan S.A., Kos'min A.A. Vybor zharostojkogo po-krytija dlja zharoprochnogo nikelevogo renij-rutenijsoderzhashhego splava marki VZhM4 [Choice of heat resisting covering for heat resisting nickel reny-ruteniysoderzhashchy alloy of the VZhM4 brand] //Trudy VIAM. 2014. №1. St. 01 (viam-works.ru).
15. Budinovskij S.A. Primenenie analiticheskoj modeli opredelenija uprugih mehanicheskih i termicheskih naprjazhenij v mnogoslojnoj sisteme v reshenii zadach po sozdaniju zharostojkih aljuminidnyh pokrytij [Application of analytical model of determination of elastic mechanical and thermal stresses in multi-layer system in the solution of tasks on creation of heat resisting alyuminidny coverings] //Uprochnjajushhie tehnologii i pokrytija. 2013. №3. S. 3–11.
16. Mubojadzhjan S.A., Budinovskij S.A., Gajamov A.M., Matveev P.V. Vysokotemperaturnye zharostojkie pokrytija i zharostojkie sloi dlja teplozashhitnyh pokrytij [High-temperature heat resisting coverings and heat resisting layers for heat-protective coverings] //Aviacionnye materialy i tehnologii. 2013. №1. S. 17–20.
17. Chubarov D.A., Matveev P.V. Novye keramicheskie materialy dlja teplozashhitnyh pokrytij rabochih lopatok GTD [New ceramic materials for heat-protective coverings of working blades of GTD] //Aviacionnye materialy i tehnologii. 2013. №4. S. 43–46.
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22. Kablov E.N., Mubojadzhjan S.A. Teplozashhitnye pokrytija dlja lopatok turbiny vysokogo davlenija perspektivnyh GTD [Heat-protective coverings for turbine blades of high pressure of perspective GTD] //Metally. 2012. №1. S. 5–13.
23. Kablov E.N., Mubojadzhjan S.A. Zharostojkie i teplozashhitnye pokrytija dlja lopatok turbiny vysokogo davlenija perspektivnyh GTD [Heat resisting and heat-protective coverings for turbine blades of high pressure of perspective GTD] //Aviacionnye materialy i tehnologii. 2012. №S. S. 60–70.
24. Mubojadzhjan S.A., Budinovskij S.A., Gajamov A.M., Smirnov A.A. Poluchenie keramich-eskih teplozashhitnyh pokrytij dlja rabochih lopatok turbin aviacionnyh GTD magnetronnym metodom [Receiving ceramic heat-protective coatings for working blades of turbines of aviation GTD magnetronny method] //Aviacionnye materialy i tehnologii. 2012. №4. S. 3–8.
Shchepilov A.V., Muboyadzhyan S.A., Gorlov D.S., Konnova V.I.
The possibility of using ion-plasma coatings deposited by high energy vacuum-plasma technology to reduce the free end oscillations amplitude of VT6 titanium alloy samples during testing on vibrodynamic bench at resonance conditions by the first bending mode is hereby shown. The coatings based on pure Ti, Zr, Cr, Ni, Al, Cu metals deposited on the MAP-3 unit under modes enabling the coating growth in the range of 19–73 g/m2 while the tempera-ture of ion and radiation heating does not exceed tempering temperature of the VT6 titanium alloy is investigated. The tests on the damping capacity of applied coatings were performed. It is established that aluminum coating has the best properties.
1. Muravchenko F.M., Sheremet'ev A.V. Aktual'nye problemy dinamiki, prochnosti i nadezhnosti sovremennyh aviadvigatelej [Actual problems of dynamics, durability and reliability of modern aircraft engines] //Vibracii v tehnike i tehnologijah. 2001. №4(20). S. 2–5.
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6. Sposob poluchenija litogo trubnogo katoda iz splavov na osnove aljuminija dlja ionno-plazmennogo nanesenija pokrytij [Way of receiving the cast pipe cathode from alloys on the basis of aluminum for ion-plasma drawing coverings]: pat. 2340426 Ros. Federacija; opubl. 16.04.2007.
7. Sposob poluchenija lityh trubnyh izdelij iz splavov na osnove nikelja i/ili kobal'ta [Way of receiving cast tubular goods from alloys on the basis of nickel and/or cobalt]: pat. 2344019 Ros. Federacija; opubl. 16.04.2007.
8. Kablov E.N. Strategicheskie napravlenija razvitija 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 till 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.
9. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlja vysokoteplonagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for the high-heatloaded details of gas turbine engines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 13–19.
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11. Kashapov O.S., Pavlova T.V., Nochovnaja N.A. Vlijanie rezhimov termicheskoj obrabotki na strukturu i svojstva zharoprochnogo titanovogo splava dlja lopatok KVD [Influence of modes of thermal processing on structure and property of heat resisting titanium alloy for KVD blades] //Aviacionnye materialy i tehnologii. 2010. №2. S. 8–14.
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Kablov E.N., Beider E.Ya., Petrova G.N., Stolyankov Yu.V., Rumyantseva T.V.
The physical, mechanical and thermo-physical properties of the domestic foamed elastic VPP-1 and rigid plate-type VPP-5 polymer materials produced to substitute the foreign foamed elastic «Solimide» (USA) and rigid plate-type «Rohacell» (Germany) polyimide materials are described in the article. Properties of the domestic foamed VPP-1 and VPP-5 polyimide materials are compared with foreign foamed polyimide analogue materials. The description of the manufacturing method for the foamed polyimide test specimens on the foamed polymeric materials mechanical treatment equipment developed in VIAM is provided. The recommendations on application of the domestic foamed polyimide materials VPP-1 and VPP-5 are given as well.
3. Kablov E.N. Razrabotki VIAM dlja gazoturbinnyh dvigatelej i ustanovok [Development of VIAM for gas turbine engines and installations] //Kryl'ja Rodiny. 2010. №4. S. 31–33.
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5. Stoljankov Ju.V., Ishodzhanova I.V., Antjufeeva N.V. K voprosu o defektah obrazcov dlja ispytanij ugleplastikov [To question of defects of test pieces ugleplastikov] //Trudy VIAM. 2014. №10. St. 10 (viam-works.ru).
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15. Bejder Je.Ja., Petrova G.N., Izotova T.F., Gureeva E.V. Kompozicionnye termoplastichnye materialy i penopoliimidy [Composite thermoflexible materials and penopoliimidy] //Trudy VIAM. 2013. №11. St. 01 (viam-works.ru).
16. Stoljankov Ju.V., Bejder Je.Ja., Platonov M.M., Petrova G.N. Ustrojstvo dlja mehanicheskoj obrabotki vspenennyh polimernyh materialov [The device for machining of frothed polymeric materials] //Trudy VIAM. 2015 (v pechati).
17. Ustrojstvo dlja mehanicheskoj obrabotki vspenennyh polimernyh materialov [The device for machining of frothed polymeric materials]: pat. №145916. Ros. Federacija; opubl. 27.09.2014.
Karimova S.A., Avdushkina L.I., Efimova E.A., Nizamov Т.I., Aliyev A.A.
In this work the anti-corrosion properties of polyesterurethane compound in conditions of high humidity (WKL-100) and the salt spray chamber (KCT-35) on samples of 30KhGSA steel and D16-T, 1163-AT and 1163-T aluminum alloys were determined. The results were compared with properties of well-known Cor Ban 35, PINS AT (TU38.401-58-120–95) and Dinitrol AV-40 protecting compounds. The fulfilled tests have shown high protective properties of pilot batch of PEUK compound for application in technological processes for enhanced parts and units protection in aviation hardware.
3. Kablov E.N., Starcev O.V., Krotov A.S., Kirillov V.N. Klimaticheskoe starenie kompozicionnyh materialov aviacionnogo naznachenija. II. Relaksacija 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] //Deformacija i razrushenie materialov. 2012. №6. S. 17–19.
4. Kablov E.N., Starcev O.V., Krotov A.S., Kirillov V.N. Klimaticheskoe starenie kompozicionnyh materialov aviacionnogo naznachenija. I. Mehanizmy starenija [Climatic aging of composite materials of aviation assignment. I. Aging mechanisms] //Deformacija i razrushenie materialov. 2010. №11. S. 19–27.
5. Kablov E.N., Petrova A.P., Narskij A.R. G.V. Akimov – sozdatel' otechestvennoj nauki o kor-rozii [G.V. Akimov – the creator of domestic science about corrosion] //Istorija nauki i tehniki. 2009. №11. S. 12–15.
6. Kirillov V.N., Starcev O.V., Efimov V.A. Klimaticheskaja stojkost' i povrezhdaemost' polimernyh kompozicionnyh materialov, problemy i puti reshenija [Climatic firmness and damageability of polymeric composite materials, problems and solutions] //Aviacionnye materialy i tehnologii. 2012. №S. S. 412–423.
7. Kirillov V.N., Efimov V.A., Shvedkova A.K., Nikolaev E.V. Issledovanie vlijanija klimaticheskih faktorov i mehanicheskogo nagruzhenija na strukturu i mehanicheskie svojstva PKM [Research of influence of climatic factors and mechanical loading on structure and the PKM mechanical properties] //Aviacionnye materialy i tehnologii. 2011. №4. S. 41–45.
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9. Semenova L.V., Nefedov N.I. Pokrytija dlja zashhity gidroagregatov [Coverings for protection of hydraulic units] //Trudy VIAM. 2014. №2. St. 05. (viam-works.ru).
10. Karimova S.A., Pavlovskaja T.G. Razrabotka sposobov zashhity ot korrozii konstrukcij, rabotajushhih v uslovijah kosmosa [Development of ways of corrosion protection of the designs working in the conditions of space] //Trudy VIAM. 2013. №4. St. 02. (viam-works.ru).
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17. Antipov V.V., Senatorova O.G., Tkachenko E.A., Vahromov R.O. Aljuminievye deformiruemye splavy [Aluminum deformable alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 167–182.
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Iskhodzhanova I.V., Orlov M.R., Grigorenko V.B., Lapteva M.A.
On the investigations examples of aircraft gas turbine engines corrosive damages after 5 years exposure on the open experimental ground of the FSUE «VIAM» G.V. Akimov Gelendzhik climatic test center (VIAM GCTC) the possibilities of confocal laser imaging microscopy are represented. The 3D-models were built and quantitative assessment of surface topography by statistical data processing of the roughness using standard software was undertaken.
2. Kablov E.N. Strategicheskie napravlenija razvitija 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 till 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.
4. Orlov M.R. Strategicheskie napravlenija razvitija Ispytatel'nogo centra FGUP «VIAM» [Strategic directions of development of the Test center VIAM Federal State Unitary Enterprise] //Aviacionnye materialy i tehnologii. 2012. №S. S. 387–393.
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6. Fridljander I.N., Chuistov K.V., Berezina A.L., Kolobnev N.I., Koval' Ju.N. Aljuminij-litievye splavy. Struktura i svojstva [Aluminum - lithium alloys. Structure and properties]. K.: Naukova dumka. 1992.
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9. Abraimov N.V., Orlov M.R., Shkretov Ju.P. Nekotorye aspekty vysokotemperaturnogo okis-lenija splava na osnove γʹ-Ni3Al [Some aspects of high-temperature oxidation of alloy on basis γʹ-Ni3Al] //Korrozija: materialy, zashhita. 2010. №8. S. 1–11.
10. Orlov M.R., Ospennikova O.G., Gromov V.I. Zamedlennoe razrushenie stali 38HN3MA v processe dlitel'noj jekspluatacii [Steel 38ХН3МА delayed fracture in the course of long operation] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 5–12.
11. Orlov M.R., Jakimova M.S. Zamedlennoe razrushenie monokristallicheskih lopatok iz zharo-prochnogo splava ZhS26-VI v processe jekspluatacii GTU [Delayed fracture of single-crystal blades from ZhS26-VI hot strength alloy in use GTU] //Gazoturbinnye tehnologii. 2011. №8. S. 10–15.
12. Ishodzhanova I.V. Primenenie konfokal'noj lazernoj skanirujushhej mikroskopii dlja reshenija materialovedcheskih zadach [Application of konfokalny laser scanning microscopy for the solution of materialovedchesky tasks] /V sb. materialov VII Evrazijskoj nauch.-praktich. konf. «Prochnost' neodnorodnyh struktur». M.: MISiS. 2014. S. 138.
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14. Klevcov G.V., Merson E.D. O vozmozhnosti ispol'zovanija konfokal'nogo lazernogo skanirujushhego mikroskopa dlja issledovanija mikrorel'efa poverhnosti razrushenija metallicheskih materialov [About possibility of use of konfokalny laser scanning microscope for research of microrelief of surface of destruction of metal materials] //Fundamental'nye issledovanija. 2012. №11. S. 1185–1189.
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29. Semenychev V.V. Korrozionnaja stojkost' listov splava D16ch.-T v morskih subtropikah [Corrosion resistance of sheets of alloy Д16ч.-T in sea subtropics] //Trudy VIAM. 2014. №7. St. 11 (viam-works.ru).
Lukin V.I., Rylnikov V.S., Afanasiev-Khodykin A.N., Kutsevich K.E., Nischev K.N.
The method of determining the adhesion strength of silver coating to the silicon substrate was developed for defining the quality of contact connections in semiconductor elements. It is shown hereby that the best option is to use high-adhesive membranous glue VK-51 and a special tooling with molybdenum heat compensators.
3. Petrova A.P., Lukina N.F. Klei dlja mnogorazovoj kosmicheskoj sistemy [Glues for reusable space system] //Trudy VIAM. 2013. №4. St. 04 (viam-works.ru).
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