Articles
This paper studied metallurgic features of the high-strength beryllium-containing steel VNS-32-VI obtaining including smelting in the vacuum induction furnaces, forging and rolling processes, heat treatment modes of hot-rolled bars with diameter 10–27 mm and forged to 50 mm, intended for hardwearing elements of fuel control apparatus. There were optimized temperature-time parameters of deformation and thermal treatment of bars working. These parameters provided the stability of the mechanical properties and low level of non-metallic inclusions. There were identified the ways of δ-ferrite embrit-tlement phase content decreasing in the steel.
2. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlja vysokoteplonagruzhen-nyh detalej gazoturbinnyh dvigatelej [Materials for high-thermal components of gas turbine engines] //Vestnik MGTU im. N.Je. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 13–19.
3. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [Strategic directions of development of materials and technolo-gies to process them for the period up to 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.
4. Kablov E.N. Sovremennye materialy – osnova innovacionnoj modernizacii Rossii [Modern materials – the basis of innovative modernization of Russia] //Metally Evrazii. 2012. №3. S. 10–15.
5. Ospennikova O.G. Strategija razvitija zharoprochnyh splavov i stalej special'nogo naznachenija, zashhitnyh i teplozashhitnyh pokrytij [The development strategy of sup-eralloys and special steel, protective and thermal barrier coatings] //Aviacionnye mate-rialy i tehnologii. 2012. №S. S. 19–36.
6. Tonysheva O.A., Voznesenskaja N.M., Shal'kevich A.B., Petrakov A.F. Issledovanie vlijanija vysokotemperaturnoj termomehanicheskoj obrabotki na strukturu, tehnolog-icheskie, mehanicheskie i korrozionnye svojstva vysokoprochnoj korrozionnostojkoj stali perehodnogo klassa s povyshennym soderzhaniem azota [Investigation of the influence of high-temperature thermomechanical treatment on the structure, process, mechanical and corrosion properties of high-grade stainless steel transition with a high content of nitrogen] //Aviacionnye materialy i tehnologii. 2012. №3. S. 31–36.
7. Salahova R.K. Korrozionnaja stojkost' stali 30HGSA s «trehvalentnym» hromovym pokrytiem v estestvennyh i iskusstvennyh sredah [The corrosion resistance of steel with 30KhGSA «trivalent» chromium plated in natural and artificial environments] //Aviacionnye materialy i tehnologii. 2012. №2. S. 59–66.
8. Bratuhin A.G. Demchenko O.F., Dolzhenkov N.N., Krivonogov G.S. Vysokoprochnye korrozionnostojkie stali sovremennoj aviacii [High-strength corrosion-resistant steel of modern aviation]. M.: MAI. 2006. S. 112–121, 130–143.
9. Solncev St.S., Rozenenkova V.A., Mironova N.A., Kas'kov V.S. Kompleksnaja sistema zashhity berillija ot okislenija [Comprehensive system protection against oxidation of beryllium] //Aviacionnye materialy i tehnologii. 2010. №1. S. 12–16.
10. Erasov V.S., Grinevich A.V., Senik V.Ja., Konovalov V.V., Trunin Ju.P., Nesterenko G.I. Raschetnye znachenija harakteristik prochnosti aviacionnyh materialov [Calculated values of the strength characteristics of aircraft materials] //Aviacionnye materialy i tehnologii. 2012. №2. S. 14–16.
11. Voznesenskaja N.M., Izotov V.I., Ul'janova N.V., Popova L.S., Potak Ja.M. Struktura i svojstva vysokoprochnoj nerzhavejushhej stali 1H15N4AM3 [Structure and properties of high strength stainless steel 1H15N4AM3] //MiTOM. 1971. №1. S. 32–35.
12. Savvina N.A., Kosarina E.I., Miroshin K.G., Stepanov A.V. Teoreticheskij raschet i prakticheskie sposoby opredelenija verojatnosti obnaruzhenija defektov v aviacionnyh materialah [Theoretical calculation and practical ways to determine the probability of detection of defects in aircraft materials] //Aviacionnye materialy i tehnologii. 2005. №1. S. 16–22.
13. Krivonogov G.S., Kablov E.N. Granicy zeren i ih rol' v ohrupchivanii vysokoprochnyh korrozionnostojkih stalej [Grain boundaries and their role in the embrittlement of high-strength stainless steels] //Metally. 2002. №1. S. 35–45.
14. Wagatsuma K., Hirokawa Kh. Observation of ion nitriding on Fe–Cr, Fe–Ni and Ni–Cr alloy surfaces in a glow discharge plasma //Surface and interface analisis. 2012. V. 8. №1. P. 37–42.
15. Potak Ja.M., Sagalevich E.A. Strukturnaja diagramma deformiruemyh nerzhavejushhih stalej [Structure diagram deformable stainless steels] //MiTOM. 1971. №9. S. 12–16.
16. Krivonogov G.S., Kablov E.N. Matematicheskaja model' strukturnoj diagrammy malouglerodistyh korrozionnostojkih stalej i ee primenenie pri razrabotke novyh mate-rialov [Mathematical model of the structural diagram of low carbon stainless steels and its application in the development of new materials] //Metally. 2001. №5. S. 42–48.
17. Tonysheva O.A., Voznesenskaja N.M., Eliseev Je.A., Shal'kevich A.B. Novaja vysoko-prochnaja jekonomnolegirovannaja azotsoderzhashhaja stal' povyshennoj nadezhnosti [New high ehkonomnolegirovannyh nitrogen-containing steel increased reliability] //Aviacionnye materialy i tehnologii. 2012. №S. S. 84–88.
18. Smoljakova M.Ju., Vershinin D.S., Tregubov I.M. Issledovanie vlijanija nizkotempera-turnogo azotirovanija na strukturno-fazovyj sostav i svojstva austenitnoj stali [Investiga-tion of the influence of low-temperature nitridation on the structural and phase composi-tion and properties of austenitic steel] /V sb. dokladov 9-oj Mezhdunarodnoj konf. «Vzaimodejstvie izluchenij s tverdym telom». Minsk. 2011. S. 176–177.
19. Kosolapov G.F., Gerasimov S.A. O strukture α-fazy azotirovannogo sloja stali 38H2MJuA i 10H13 [The structure of α-phase steel nitrided layer 38H2MYUA and 10X13] //MiTOM. 2011. №5. S. 71–73.
20. Gerasimov S.A., Kuksenova L.I., Lapteva V.G. Struktura i iznosostojkost' azotiro-vannyh konstrukcionnyh stalej i splavov [Structure and wear resistance of nitrided structural steels and alloys]. M.: MGTU im. N.Je. Baumana. 2012. S. 508–509.
In the present work residual stress analysis has been accomplished for welded junc-tions of the VT20 (Ti–6Al–2Zr–1V–1Mo), VT6 (Ti–6Al–4V), and VT23 (Ti–5.5Al–4.5V–2Mo–1Cr–0.5Fe) alloys wherein macrostress values and distribution thereof along the cross-section of welded junctions were in focus. It has been shown that tension stresses occur in the center of weld joints while compression stresses are detected in heat-affected zones independently of argon-arc or electron-beam welding method applied. For the studied alloys the following regula-rity has been revealed: the relative tension stress level decreases with the -stabilizing coefficient increase.
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A method for determination of silicon carbide and aluminum nitride in uplotnitel′nom material based on nickel. Error of definition of these components does not exceed 5% RH.
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Fine-dispersed metal powders of the heat resisting alloy brand EP648-VI for laser metal deposition (LMD), obtained by method of atomization at a facility HERMI-GA10/100 VI are investigated. It is shown, that the obtained fine-dispersed powders when spraying by cold and hot gas have low oxygen content, the spherical form, the expressed dendritic structure in all range of the granulometric distribution. Adaptive laser metal deposition with application metal powder of the heat resisting alloy EP648-VI of the granulometric distribution 40–80 microns on working off technology of recovery of geometry extreme combs on the bandage shelf of working blades of the second step guarantees high quality of welding material (availability of defects of typemicrocracks, lack of penetrations is not revealed).
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The design of vacuum induction installations including the modern vacuum induction furnace VIM 12 III HMC ALD production (Germany) was considered. The VIM 12 III HMC installation has all necessary units and devices including transduceres for oxidized melt measure and conforms to modern requirements for a vacuum equipment. The installation permits to design the new effective basic processes of last generation cast supperalloys melting for single crystal casting and thereby to increase their operationale performances.
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In given article a method of measurement of honeycomb glass fiber plastics permit-tivity in free space is considered. On the measured complex transiting ratio of the hon-eycomb glass fiber plastics sample its permittivity is calculated. The estimation of influ-ence rereflection between the sample and close located reception aerial is spent. Also comparisons of results of measurements in free space with results of measurements a waveguide method are resulted.
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