Source: http://viam-works.ru/en/articles?year=2015&num=7
Timestamp: 2019-04-20 02:30:24+00:00

Document:
Muboyadzhyan S.A., Konnova V.I., Gorlov D.S., Aleksandrov D.A.
This article describes the experiments that were conducted to study fretting resistance steel EP866Sh. Strained bolt joints are made of the steel where the phenomenon of fretting occurs. Tests were conducted on a universal tribometer CETR UMT-3MT using R33HE1000 lower drive for reciprocating movement in the laboratory environment according to ASTM G204-10. During the experiments load intensity and the oscillation amplitude have changed. The method «pin-on-plate» was chosen to study the tribological properties of steel EP866. Estimated wear curves were conducted metallographic examination of samples.
1. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strate-gicheskih napravlenij razvitija materialov i tehnologij ih pererabotki na period do 2030 go-da» [Innovative development of VIAM Federal State Unitary Enterprise of GNTs Russian Federation on implementation «The strategic directions of development of materials and technologies of their processing for the period till 2030»] //Aviacionnye materialy i tehnologii. 2015. №1. S. 3–33.
2. Mubojadzhjan S.A., Aleksandrov D.A., Gorlov D.S., Egorova L.P., Bulavinceva E.E. Zashhitnye i uprochnjajushhie ionno-plazmennye pokrytija dlja lopatok i drugih ot-vetstvennyh detalej kompressora GTD [Protective and strengthening ion-plasma coverings for blades and other responsible details of the GTD compressor] //Aviacionnye materialy i tehnologii. 2012. №S. S. 71–81.
3. Mubojadzhjan S.A., Aleksandrov D.A., Gorlov D.S. Nanoslojnye uprochnjajushhie pokrytija dlja zashhity stal'nyh i titanovyh lopatok kompressora GTD [Nanolayer strength-ening coverings for protection of steel and titanic compressor blades of GTD] //Aviacionnye materialy i tehnologii. 2011. №3. S. 3–8.
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10. Markova E.S., Jakusheva N.A., Pokrovskaja N.G., Shal'kevich A.B. Tehnologicheskie osobenno-sti proizvodstva martensitostarejushhej stali VKS-180 [Technological features of production of maraging VKS-180 steel] //Trudy VIAM. 2013. №7. St. 01 (viam-works.ru).
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12. Galojan A.G., Mubojadzhjan S.A., Egorova L.P., Bulavinceva E.E. Korrozionnostojkoe pokrytie dlja zashhity detalej GTD iz vysokoprochnyh konstrukcionnyh martensitostare-jushhih stalej na rabochie temperatury do 450°С [Corrosion resistant coating for protection of details of GTD from high-strength constructional maraging staly on working tempera-tures to 450°С] //Trudy VIAM. 2014. №6. St. 03 (viam-works.ru).
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The article shows the characteristics of alloys based on magnesium, the effect of doping with rare earth elements (including Y, Nd, Sm, Tb and Sc) magnesium-based alloys the structure and mechanical, as well as performance characteristics. The effect of individual rare earth elements to magnesium-based alloys, and rare earth elements in the alloy more. The influence of alloying elements in the system Mg–Sm (Y)–Tb–Zr. It describes the effect of REE on the corrosion resistance of certain alloys doped with rare earth elements.
2. Kablov E.N. Aviakosmicheskoe materialovedenie [Aerospace materials science] //Vse ma-terialy. Jenciklopedicheskij spravochnik. 2008. №3. S. 2–14.
4. Chirkov E.F., Kononova L.A., Shmeljova V.S. Vlijanie jekviatomnogo soderzhanija Cu i Mg na processy starenija zharoprochnogo svarivaemogo konstrukcionnogo splava 1151 (Al–Cu–Mg) [Influence of the ekviatomny maintenance of Cu and Mg on processes of aging of heat resisting welded structural alloy 1151 (Al–Cu–Mg)] //Trudy VIAM. 2013. №2. St. 03 (viam-works.ru).
5. Kablov E.N., Ospennikova O.G., Vershkov A.K. 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).
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1. Kablov E.N., Bondarenko Ju.A., Echin A.B., Surova V.A. Razvitie processa napravlennoj kristallizacii lopatok GTD iz zharoprochnyh splavov s monokristallicheskoj i kompozicionnoj strukturoj [Development of process of the directed crystallization of blades of GTD from hot strength alloys with single-crystal and composition structure] //Aviacionnye materialy i tehnologii. 2012. №1. S. 3–8.
4. Kablov E.N., Gerasimov V.V., Visik E.M., Demonis I.M. Rol' napravlennoj kristallizacii v resursosberegajushhej tehnologii proizvodstva detalej GTD [Role of the directed crystallization in the resource-saving production technology of details of GTD] //Trudy VIAM. 2013. №3. St. 05 (viam-works.ru).
5. 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).
6. Min P.G., Sidorov V.V. Opyt pererabotki litejnyh othodov splava ZhS32-VI na nauchno-proizvodstvennom komplekse VIAM po izgotovleniju lityh prutkovyh (shihtovyh) zagotovok [Experience of processing of foundry waste of alloy ZhS32-VI on VIAM scientific-industrial complex on manufacturing of cast bar (blend) preparations] //Aviacionnye materialy i tehnologii. 2013. №4. S. 20–25.
7. Lomberg B.S., Ovsepjan S.V., Bakradze M.M., Mazalov I.S. Vysokotemperaturnye zharoprochnye nikelevye splavy dlja detalej gazoturbinnyh dvigatelej [High-temperature heat resisting nickel alloys for details of gas turbine engines] //Aviacionnye materialy i tehnologii. 2012. №S. S. 52–57.
8. Kablov E.N., Sidorov V.V., Kablov D.E., Rigin V.E., Gorjunov A.V. Sovremennye tehnologii poluchenija prutkovyh zagotovok iz litejnyh zharoprochnyh splavov novogo pokolenija [Modern technologies of receiving bar preparations from foundry hot strength alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 97–105.
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Lukin V.I., Rylnikov V.S., Loshinin U.V., Nischev K.N.
The article is about investigating of heat effects taking place while drying and sintering of silver containing paste, used to get low temperature joints in system of «Si on Mo» for semiconductor elements. It was investigated the modifications in form and size of silver particles taking place during drying at different temperatures. The relationship between micro hardness of sintered layers and temperature was investigated.
1. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitija materialov i tehnologij ih pererabotki na period do 2030 go-da» [Innovative development of VIAM Federal State Unitary Enterprise of GNTs Russian Federation on implementation «The strategic directions of development of materials and technologies of their processing for the period till 2030»] //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 3–33.
2. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharoprochnye splavy novogo pokolenija [Nickel foundry hot strength alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 36–51.
3. Kablov E.N., Antipov V.V., Senatorova O.G., Lukina N.F. Novyj klass sloistyh aljumostekloplastikov na osnove aljuminijlitievogo splava 1441 s ponizhennoj plotnost'ju [New class layered alyumostekloplastikov on basis aluminum-lithium alloy 1441 with lowered density] //Vestnik MGTU im. N.Je. Baumana. 2011. №SP2. S. 174–183.
4. Kablov E.N., Bondarenko Ju.A., Echin A.B., Surova V.A. Razvitie processa napravlennoj kristallizacii lopatok GTD iz zharoprochnyh splavov s monokristallicheskoj i kompozicionnoj strukturoj [Development of process of the directed crystallization of blades of GTD from hot strength alloys with single-crystal and composition structure] //Aviacionnye materialy i tehnologii. 2012. №1. S. 3‒8.
5. 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.
6. 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).
7. Lukina N.F., Dement'eva L.A., Petrova A.P., Serezhenkov A.A. Konstrukcionnye i termostojkie klei [Constructional and heat-resistant glues] //Aviacionnye materialy i tehnologii. 2012. №S. S. 328–335.
8. Kucevich K.E., Dement'eva L.A., Lukina N.F., Chursova L.V. Svojstva i naznachenie kleja VK-36RM dlja aviacionnoj tehniki [Properties and glue assignment VK-36RM of aviation engineering] //Klei. Germetiki. Tehnologii. 2013. №8. S. 5–6.
9. Lukina N.F., Dement’eva L.A., Serezhenkov A.A. et al. Adhesive prepregs and composite matirials on their bases //Russian J. of General Chemistry. 2011. V. 81. №5. P. 1022–1024.
10. Lukina N.F., Dement'eva L.A., Serezhenkov A.A. i dr. Kleevye prepregi i kompozicionnye materialy na ih osnove [Glue prepregs and composite materials on their basis] //Rossijskij himicheskij zhurnal. 2010. T. LIV. №1. S. 53–56.
11. Zhang Zhiye (Zach), Lu Guo-Quan. Pressure-Assisted Low-Temperatuze Sintering of Silver Paste as an Alternative Die-Attach Solution to Soldez Reflow //Trans. Jnd. Applicat. 2002. V. 25. №4. Р. 279–283.
12. Lukin V.I., Ryl'nikov V.S., Afanas'ev-Hodykin A.N., Kucevich K.E., Nishhev K.N. Metod opredelenija prochnosti sceplenija serebrjanogo pokrytija s kremnievoj podlozhkoj s ispol'zovaniem kleja [Method of determination of durability of coupling of silver covering with silicon substrate with glue use] //Klei. Germetiki. Tehnologii. 2014. №6. S. 34‒36.
One of the difficult-defined number of alloying elements in high-temperature nickel alloys, while alloys in the presence of interfering elements molybdenum, tantalum, zir-conium, hafnium, et al. Is niobium. Creation of a new series of heat-resistant nickel alloys (ZHNS) for gas turbine engines (GTE) for the latest generation of power plants with cooling vanes, allowing to increase the temperature of the gas to 2100–2200 К, requires the development of new technologies for the production of the required alloys and semi-finished products, allowing to solve tasks. In order to control the content of niobium in these heat-resistant nickel alloys developed a method for determination of niobium in the concentration range of 1–15% by weight. alloys at a content of up to 30% by weight. Molybdenum spectrophotometric method with a reagent piridilazorezortsinom.
1. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharoprochnye splavy novogo pokolenija [Nickel foundry hot strength alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 36–52.
2. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategicheskih napravlenij razvitija materialov i tehnologij ih pererabotki na period do 2030 goda» [Innovative development of VIAM Federal State Unitary Enterprise of GNTs Russian Federation on implementation «The strategic directions of development of materials and technologies of their processing for the period to 2030»] //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 3–33.
3. Kablov E.N., Sidorov V.V., Kablov D.E., Rigin V.E., Gorjunov A.V. Sovremennye tehnologii poluchenija prutkovyh zagotovok iz litejnyh zharoprochnyh splavov novogo pokolenija [Modern technologies of receiving bar preparations from foundry hot strength alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 97–105.
5. Lomberg B.S., Ovsepjan S.V., Bakradze M.M. Novyj zharoprochnyj nikelevyj splav dlja diskov gazoturbinnyh dvigatelej (GTD) i gazoturbinnyh ustanovok (GTU) [New heat resisting nickel alloy for disks of gas turbine engines (GTD) and gas turbine units (GTU)] //Materialovedenie. 2010. №7. S. 24–28.
6. Mubojadzhjan S.A., Aleksandrov D.A., Gorlov D.S., Egorova L.P., Bulavinceva E.E. Zashhitnye i uprochnjajushhie ionno-plazmennye pokrytija dlja lopatok i drugih otvetstvennyh detalej kompressora GTD [Protective and strengthening ion-plasma coverings for blades and other responsible details of the GTD compressor] //Aviacionnye materialy i tehnologii. 2012. №S. S. 71–81.
7. 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.
10. Gundobin N.V., Titov V.I., Pilipenko L.V., Dvoreckov R.M. Spektrofotometricheskoe opredelenie niobija v zharoprochnyh nikelevyh splavah, soderzhashhih tantal [Spectropho-tometric definition of niobium in the heat resisting nickel alloys containing tantalum] //Trudy VIAM. 2014. №8. St. 10 (viam-works.ru).
11. Elinson S.V., Petrov K.I. Analiticheskaja himija cirkonija i gafnija [Analytical chemistry of zirconium and hafnium]. M.: Nauka. 1965. 267 s.
Panarin A.V., Ilyin V.A., Salakhova R.K., Smirnova T.B.
The work presents research results of microstructure deposited on aluminum casting alloys AL25 & AL26 pyrolytic chrome-carbide coating (PCCC). As an etchant was used Murakami’s reagent. Quantitative composition of selected etchant & modes of microsections etching optimized. Chrome-carbide coating's microstructure dependence from conditions of the deposition process showed. Chemical and phase compositions of PCCC identified.
1. Kablov E.N. Innovacionnye razrabotki FGUP «VIAM» GNC RF po realizacii «Strategi-cheskih napravlenij razvitija materialov i tehnologij ih pererabotki na period do 2030 goda» [Innovative development of VIAM Federal State Unitary Enterprise of GNTs Russian Federation on implementation «The strategic directions of development of materials and technologies of their processing for the period to 2030»] //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 3–33.
2. Kablov E.N., Starcev O.V., Medvedev I.M., Panin S.V. Korrozionnaja agressivnost' pri-morskoj atmosfery. Ch. 1. Faktory vlijanija (Obzor) [Corrosion aggression of the seaside atmosphere. P.1. Factors of influence (review)] //Korrozija: materialy, zashhita. 2013. №12. S. 6–18.
3. Kablov E.N. Aviacionnoe materialovedenie XXI v veke. Perspektivy i zadachi [Aviation materials science of XXI in century. Perspectives and tasks] /V kn. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2002: Jubilejnyj nauch.-tehnich. sb. M.: MISiS–VIAM. 2002. S. 23–47.
4. Kablov E.N. Aviakosmicheskoe materialovedenie [Aerospace materials science] //Vse ma-terialy. Jenciklopedicheskij spravochnik. 2008. №3. S. 26.
6. Antipov V.V., Senatorova O.G., Tkachenko E.A., Vahromov R.O. Aljuminievye deform-iruemye splavy [Aluminum deformable alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 167–182.
7. Fridljander I.N., Sister V.G., Grushko O.E., Berstenev V.V., Sheveleva L.M., Ivanova L.A. Aljuminievye splavy – perspektivnyj material v avtomobilestroenii [Aluminum alloys – perspective material in automotive industry] //MiTOM. 2002. №9. S. 3–9.
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The paper presents some results on the effect of assisted deposition (PA-PVD) on reinforcing properties of ion-plasma coatings, such as phase composition, lattice parameter, erosion resistance. The results metallophysical research, testing on erosion resistance of monolayer and multilayercoatings.
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The results of the tensile strength of the flexible samples cut off from the VTI-16TM material in the longitudinal and cross direction, are presented in this paper. The aim of the investigation is to find out if the anisotropy presents in the material after rolling.
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In this article features of application high-level programming languages for calculation radio engineering parameters are considered. Described programs for calculation radio engineering parameters of materials developed in VIAM. It is provided structure of the program for calculation factor of reflection the electromagnetic wave at normal falling on a nonmetallic single-layered isotropic material (located on metal).
3. Romanov A.M., Beljaev A.A., Shirokov V.V. Osobennosti optimizacii rezonansnyh radiopogloshhajushhih materialov nemagnitnogo tipa [Features of optimization of resonance radio absorbing materials of non-magnetic type] //Trudy VIAM. 2014. №11. St. 05 (viam-works.ru).
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The article contains the sequence of operations for modeling of manufacturing by infusion composite arched element. Described are phenomenological processes arising from the formation and critical characteristics that must be taken into account in the simulation.
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