Source: http://viam-works.ru/en/articles?year=2015&num=12
Timestamp: 2019-04-20 02:58:10+00:00

Document:
Bazyleva O.A., Arginbaeva E.G., Shestakov A.V., Koljadov E.V.
The investigations of directional solidification parameters (rate and temperature gradient of crystallization) on microstructure, structural and phase parameters (lattices parameters of γꞌ- and γ-phases, misfit) and mechanical properties of intermetallic VIN alloys based on nickel were considered.
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The harmful influence of sulfur and phosphorus on heat resistant properties of ZhS36-VI alloy during stress rupture test on long base testing (500 and more hours) as well as on middle quantity of cycles to rupture upon MCF wasdetermined . The possibility to reduce the content of harmful influence of sulfur and phosphorus impurities or their neutralization through microalloing by lanthanum that positively influence on alloy properties recovery was investigated. The mechanism of lanthanum addition for neutralization of these impurities harmful influence was suggested whereby sulfur removes from the melt as refractory lanthanum sulfides by their adhesion on crucible walls during melting and on foam filter during casting. In contrast to sulfur the refractory phosphides with lanthanum don’t remove from the melt. The properties comparison of single crystal alloy cast on units of low- and high gradient direct solidification UVNK-9A and UVNS-5 is presented.
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27. Min P.G., Sidorov V.V. Rafinirovanie othodov zharoprochnogo nikelevogo splava ZhS32-VI ot primesi kremniya v usloviyah vakuumnoj indukcionnoj plavki [Refining of scraps of Ni-base superalloy ZhS32-VI to eliminate silicon impurity under conditions of vacuum induction melting] //Trudy VIAM. 2014. №9. St. 01 (viam-works.ru).
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Nazarkin R.M., Kolodochkina V.G., Ospennikova O.G., Orlov M.R.
The results of researches of single-crystal rotor blades from cast Ni-based superalloy ZhS32-VI in process of long-time life cycle testing of gas turbine engine (high-pressure turbine) are represented for microstructure and substructure. It is shown that precipitation of TCP-phases particles in the alloy during high-temperature testing is accompanied by the decreasing of crystal lattice constant of γ-solid solution. It is verified by data of x-ray diffraction analysis, x-Ray microanalysis and scanning electron microscopy. The point is proposed that decreasing of alloying element content in the γ-solid solution as result of TCP-phases precipitation (rich with the refractory elements) leads to the fall of the high-temperature resistance of the material. Also, a TCP-phases make negative influence on mechanical properties of the alloy due to the local destruction of coherency for interphase boundaries in zone of development of TCP-phases particles.
2. Ospennikova O.G. Strategiya razvitiya zharoprochnyh splavov i stalej specialnogo naznacheniya, zashhitnyh i teplozashhitnyh pokrytij [Strategy of development of hot strength alloys and steels special purpose, protective and heat-protective coverings] //Aviacionnye materialy i tehnologii. 2012. №S. S. 19–36.
3. Kablov E.N., Lomberg B.S., Ospennikova O.G. Sozdanie sovremennyh zharoprochnyh materialov i tehnologij ih proizvodstva dlya aviacionnogo dvigatelestroeniya [Creation of modern heat resisting materials and technologies of their production for aviation engine building] //Krylya Rodiny. 2012. №3–4. S. 34–38.
4. Orlov M.R. Strategicheskie napravleniya razvitiya Ispytatelnogo centra FGUP «VIAM» [Strategic directions of development of the Test center FSUE «VIAM»] //Aviacionnye materialy i tehnologii. 2012. №S. S. 387–393.
5. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharo-prochnye splavy novogo pokoleniya [Nickel foundry hot strength alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. C. 36–52.
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7. Kablov E.N. Fiziko-mehanicheskie i tehnologicheskie osobennosti sozdaniya zharoprochnyh splavov, soderzhashhih renij [Physicomechanical and technological features of creation of the hot strength alloys, containing reniye] //Vestnik Moskovskogo universiteta. Ser. 2: Himiya. 2005. T. 46. №3. S. 155–167.
8. 4. Kablov E.N., Muboyadzhyan S.A. Zharostojkie i teplozashhitnye pokrytiya dlja lopatok turbiny vysokogo davleniya perspektivnyh GTD [Heat resisting and heat-protective coverings for turbine blades of high pressure of perspective GTE] //Aviacionnye materialy i tehnologii. 2012. №S. S. 60–70.
9. Kablov E.N., Petrushin N.V., Bronfin M.B., Alekseev A.A. Osobennosti monokristallicheskih zharoprochnyh nikelevyh splavov, legirovannyh reniem [Features of the single-crystal heat resisting nickel alloys alloyed by rhenium] //Metally. 2006. №5. S. 47–57.
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12. Morozova G.I. Zakonomernost formirovaniya himicheskogo sostava γ′/γ-matricy mnogokomponentnyh nikelevyh splavov [Pattern of forming of chemical composition γ′/γ-matrix multicomponent nickel alloys] //Doklady Akademii nauk. 1991. T. 320. №6. S. 1413–1416.
13. Kablov E.N., Petrushin N.V. Kompyuternyj metod konstruirovaniya litejnyh zharoprochnyh nikelevyh splavov [Computer method of designing of cast heat resisting nickel alloys] /V kn. Litejnye zharoprochnye splavy. Effekt S.T. Kishkina /Pod red. E.N. Kablova. M.: Nauka. 2006. S. 56–78.
14. Ospennikova O.G., Orlov M.R., Kolodochkina V.G., Nazarkin R.M. Strukturnye izmeneniya i povrezhdenie monokristallicheskih rabochih lopatok turbiny v processe resursnyh ispytanij aviacionnogo gazoturbinnogo dvigatelya [Structural changes and injury of single-crystal working turbine blades in the course of resource tests of the aviation gas turbine engine] //Deformaciya i razrushenie materialov. 2014. №8. S. 22–29.
15. Orlov M.R., Yakimova M.S., Letov A.F. Analiz rabotosposobnosti monokristallicheskih lopatok turbiny vysokogo davleniya v sostave nazemnyh gazoturbinnyh ustanovok [The analysis of operability of single-crystal turbine blades of high pressure as a part of land gas turbine units] //Aviacionnye materialy i tehnologii. 2012. №S. S. 399–407.
16. Samojlov A.I., Nazarkin R.M., Moiseeva N.S. Opredelenie misfita vo fragmentirovannyh monokristallah nikelevyh zharoprochnyh splavov [Definition miss-fit in fragmental single crystals of nickel hot strength alloys] //Trudy VIAM. 2013. №5. St. 02 (viam-works.ru).
17. Samojlov A.I., Nazarkin R.M., Moiseeva N.S. Misfit kak istochnik i kriterij rabotosposobnosti zharoprochnyh nikelevyh splavov [Misfit as source and criterion of operability of heat resisting nickel alloys] //Zavodskaya laboratoriya. Diagnostika materialov. 2013. T. 79. №6. S. 33–36.
18. Kablov E.N., Orlov M.R., Ospennikova O.G. Mehanizmy obrazovanija poristosti v monokristallicheskih lopatkah turbiny i kinetika ee ustranenija pri gorjachem izostaticheskom pressovanii [Mechanisms of formation of porosity in single-crystal turbine blades and kinetics of its elimination at hot isostatic pressing] //Aviacionnye materialy i tehnologii. 2012. №S. S. 117–129.
Belyaev M.S., Gorbovets M.A., Bakradze M.M.
The LCF behavior for Ni-base superalloy VZh175 was investigated for a given total strain, ratio R=0 and stain amplitude εa=0,4–0,6% at test temperatures 20 and 650°С. Parameters of elastic-plastic strain were observed in this article.
1. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharoprochnye splavy novogo pokoleniya [Nickel foundry heat resisting alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. C. 36–52.
2. Birger I.A., Balashov B.F., Dulnev R.A. i dr. Konstrukcionnaja prochnost materialov i detalej gazoturbinnyh dvigatelej [Constructional durability of materials and details of gas turbine engines]. M.: Mashinostroenie. 1981. 222 s.
4. Inozemtsev A.A., Ratchiev A.M., Nihamkin M.Sh. i dr. Malociklovaja ustalost i ciklicheskaya treshhinostojkost nikelevogo splava pri nagruzhenii, harakternom dlya diskov turbin [Low-cyclic fatigue and cyclic crack firmness of nickel alloy when loading, characteristic for disks of turbines] //Tuazheloe mashinostroenie. 2011. №4. S. 30–33.
5. Schijve J. Fatigue of structures and materials. Berlin Heidelberg: Springer-Verlag. 2009. 185 p.
6. Kablov E.N., Lomberg B.S., Ospennikova O.G. Sozdanie sovremennyh zharoprochnyh materialov i tehnologij ih proizvodstva dlya aviacionnogo dvigatelestroeniya [Creation of modern heat resisting materials and technologies of their production for aviation engine building] //Krylya Rodiny. 2012. №3–4. S. 34–38.
7. Kablov E.N., Ospennikova O.G., Lomberg B.S., Sidorov V.V. Prioritetnye napravleniya razvitiya tehnologij proizvodstva zharoprochnyh materialov dlya aviacionnogo dvigatelestroeniya [The priority directions of development of production technologies of heat resisting materials for aviation engine building] //Problemy chernoj metallurgii i materialovedenija. 2013. №3. S. 47–54.
8. Sposob polucheniya izdeliya iz deformiruemogo zharoprochnogo nikelevogo splava [Way of receiving product from deformable heat resisting nickel alloy]: pat. 2387733 Ros. Federaciya; opubl. 31.03.2009.
9. Golubovskij E.R., Svetlov I.L., Petrushin N.V., Cherkasova S.A., Volkov M.E. Malociklovaya ustalost monokristallov zharoprochnyh nikelevyh splavov pri povyshennyh temperaturah [Low-cyclic fatigue of single crystals of heat resisting nickel alloys at elevated temperatures] //Deformaciya i razrushenie materialov. 2009. № 8. S. 41–48.
10. Tobias J., Chlupova A., Petrenec M. et al. Low Cycle Fatigue and Analysis of the Cyclic Stress-Strain Response in Superalloy Inconel 738LC /In: 18-th International Conference «Engineering Mechanics 2012». Svratka. 2012. P. 1407–1411.
11. Nagesha A., Goyal Sunil, Nandagopal M. at al. Dynamic strain ageing in Inconel Alloy 783 under tension and low cycle fatigue //Mater. Sci. and Eng. A. 2012. V. 546. P. 34–39.
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15. Lomberg B.S., Ovsepyan S.V., Bakradze M.M., Mazalov I.S. Vysokotemperaturnye zharo-prochnye nikelevye splavy dlya detalej gazoturbinnyh dvigatelej [High-temperature heat resisting nickel alloys for details of gas turbine engines] //Aviacionnye materialy i tehnologii. 2012. №S. S. 52–57.
16. Bakradze M.M., Ovsepyan S.V., Shugaev S.A., Letnikov M.N. Vliyanie rezhimov zakalki na strukturu i svojstva shtampovok diskov iz zharoprochnogo nikelevogo splava EK151-ID [The influence of quenching on structure and properties nickel-based superalloy EK151-ID forgings] //Trudy VIAM. 2013. №9. St. 01 (viam-works.ru).
17. Lomberg B.S., Ovsepyan S.V., Bakradze M.M. Osobennosti legirovaniya i termicheskoj obrabotki zharoprochnyh nikelevyh splavov dlya diskov gazoturbinnyh dvigatelej novogo pokoleniya [Features of alloying and thermal processing of heat resisting nickel alloys for disks of gas turbine engines of new generation] //Aviacionnye materialy i tehnologii. 2010. №2. S. 3–8.
18. Kablov E.N., Ospennikova O.G., Lomberg B.S. Kompleksnaya innovacionnaya tehnologiya izotermicheskoj shtampovki na vozduhe v rezhime sverhplastichnosti diskov iz superzharoprochnyh splavov [Complex innovative technology of isothermal punching on air in mode of superplasticity of disks from superhot strength alloys] //Aviacionnye materialy i tehnologii. 2012. №S. S. 129–141.
19. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Litejnye zharoprochnye nikelevye splavy dlya perspektivnyh aviacionnyh GTD [Cast heat resisting nickel alloys for perspective aviation GTE] //Tehnologiya legkih splavov. 2007. №2. S. 6–16.
Kosmin A.A., Budinovskiy S.A., Matveev P.V., Smirnov A.A.
Comparative research of sulfide-oxide corrosion resistance of ZhS36 nickel superalloy with different advanced protective ion-plasma coatings is conducted. Results of accelerated comparative research method («salt shell method») tests of ZhS36 nickel superalloy with advanced protective ion-plasma coatings in comparison with standard SDP-6 coating in temperature range 850–900°С are presented.
1. Inozemtsev A.A., Nihamkin M.A., Sandrackij V.L. Osnovy konstruirovanija aviacionnyh dvigatelej i jenergeticheskih ustanovok [Bases of designing of aircraft engines and energy units]. M.: Mashinostroenie. 2008. T. 2. S. 159–192.
2. Kablov E.N., Sidorov V.V., Kablov D.E., Rigin V.E., Goryunov A.V. Sovremennye tehnologii polucheniya prutkovyh zagotovok iz litejnyh zharoprochnyh splavov novogo pokoleniya [Modern technologies of receiving the bar stock preparations from foundry heat resisting alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 97–105.
3. Kablov E.N., Svetlov I.L., Petrushin N.V. Nikelevye zharoprochnye splavy dlja litYa lopatok s napravlennoj i monokristallicheskoj strukturoj. Ch. ΙΙ [Nickel hot strength alloys for molding of blades with the directed and single-crystal structure. P. ΙΙ] //Materialovedenie. 1997. №5. S. 14–16.
4. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharoprochnye splavy novogo pokoleniya [Nickel foundry heat resisting alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. C. 36–52.
5. Kablov E.N., Svetlov I.L., Petrushin N.V. Nikelevye zharoprochnye splavy dlya litya lopatok s napravlennoj i monokristallicheskoj strukturoj. Ch. Ι [Nickel hot strength alloys for molding of blades with the directed and single-crystal structure. P. Ι] //Materialovedenie. 1997. №4. S. 32–39.
6. Kablov E.N., Bondarenko Yu.A., Echin A.B., Surova V.A., Kablov D.E. Razvitie processa napravlennoj kristallizatsii lopatok GTD iz zharoprochnyh i intermetallidnyh splavov s monokristallicheskoj strukturoj [Development of process of the directed crystallization of blades of GTE from heat resisting and intermetallic alloys with single-crystal structure] //Vestnik MGTU im. N.E. Baumana. Ser. «Mashinostroenie». 2011. №SP4. S. 20–25.
7. Zharoprochnyj splav na nikelevoj osnove dlya monokristallicheskogo litya [Heat resisting alloy on nickel basis for single-crystal molding]: pat. 2439184 Ros. Federatsiya; opubl. 05.10.2010.
8. Kablov E.N., Startsev 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.
9. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlya vysokoteplonagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for the high-heatloaded details of gas turbine engines] //Vestnik MGTU im. N.E. Baumana. Ser. «Mashinostroenie». 2011. №SP4. S. 13–19.
10. Kablov E.N., Muboyadzhyan S.A. Zharostojkie i teplozashhitnye pokrytiya dlya lopatok turbiny vysokogo davleniya perspektivnyh GTD [Heat resisting and heat-protective coverings for turbine blades of high pressure of perspective GTE] //Aviacionnye materialy i tehnologii. 2012. №S. S. 60–70.
11. Kablov E.N., Muboyadzhyan S.A., Budinovskij S.A., Pomelov Ya.A. Ionno-plazmennye zashhitnye pokrytiya dlya lopatok gazoturbinnyh dvigatelej [Ion-plasma protecting covers for blades of gas turbine engines] //Konversiya v mashinostroenii. 1999. №2. S. 42–47.
12. Matveev P.V., Budinovskij S.A. Issledovanie svojstv zashhitnyh zharostojkih pokrytij dlya intermetallidnyh nikelevyh splavov tipa VKNA dlya rabochih temperatur do 1300°C [Research of the properties of protective heat-resistant coating for intermetallic nickel alloys operating at temperatures up to 1300°C] //Aviacionnye materialy i tehnologii. 2014. №3. S. 22–26.
13. Kablov E.N., Muboyadzhyan 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.E. Baumana. Ser. «Mashinostroenie». 2011. №SP2. S. 149–163.
14. Kablov E.N., Muboyadzhyan S.A. Heat-resistant coatings for the high-pressure turbine blades of promising GTES //Russian metallurgy (Metally). 2012. V. 2012. №1. P. 1–7.
15. Matveev P.V., Budinovskij S.A., Muboyadzhyan S.A., Kosmin A.A. Zashhitnye zharostojkie pokrytiya dlya splavov na osnove intermetallidov nikelya [High-temperature coatings for intermetallic nickel-based alloys] //Aviacionnye materialy i tehnologii. 2013. №2. S. 12–15.
16. Muboyadzhyan S.A., Aleksandrov D.A., Gorlov D.S., Egorova L.P., Bulavinceva E.E. Zashhitnye i uprochnyayushhie ionno-plazmennye pokrytiya dlya lopatok i drugih otvetstvennyh detalej kompressora GTD [Protective and strengthening ion-plasma coverings for blades and other responsible details of the GTE compressor] //Aviacionnye materialy i tehnologii. 2012. №S. S. 71–81.
Iskhodzhanova I.V., Bondarenko Yu.A., Lapteva M.A.
The article presents a research on development of methods to assess the geometric characteristics and volume fraction of porosity, the geometric characteristics and volume fraction of eutectic (γ-γ)ʹ-phase, and the geometric characteristics of particles of the hardening γʹ-phase in monocrystalline Ni superalloys ZhS32U-VI. The results of investigations on proposed methods of quantitative metallographic analysis of blanks from the ZhS32U-VI superalloy, derived by directional solidification from the melt in different temperature gradient are presented.
1. Litye lopatki gazoturbinnyh dvigatelej: splavy, tehnologii, pokrytiya [Cast blades of gas turbine engines: alloys, technologies, coverings] /Pod obshh. red. E.N. Kablova. 2-e izd. M.: Nauka. 2006. 632 s.
2. 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.
3. Kablov E.N., Petrushin N.V., Svetlov I.L. Kompyuternoe konstruirovanie zharoprochnogo nikelevogo splava IV pokoleniya dlya monokristallicheskih lopatok gazovyh turbin [Computer designing of heat resisting nickel alloy IV of generation for single-crystal blades of gas turbines] /V kn. Litejnye zharoprochnye splavy. Effekt S.T. Kishkina. M.: Nauka. 2006. S. 98–116.
5. Bondarenko Yu.A., Kablov E.N., Morozova G.I. Vliyanie vysokogradientnoj napravlennoj kristallizacii na strukturu i fazovyj sostav zharoprochnogo splava tipa Rene N5 [Influence of the high-gradient directed crystallization on structure and phase composition of hot strength alloy of the Rene N5 type] //MiTOM. 1999. №2. S. 15–18.
6. Bondarenko Yu.A., Kablov E.N. Napravlennaya kristallizaciya zharoprochnyh splavov s povyshennym temperaturnym gradientom [The directed crystallization of heat resisting alloys with the raised temperature gradient] //MiTOM. 2002. №7. S. 20–23.
7. Bondarenko Yu.A., Echin A.B., Surova V.A., Narskij A.R. Vliyanie temperaturnogo gradienta na fronte rosta na strukturu zharoprochnogo splava pri napravlennoj kristallizacii [Influence of temperature gradient at the front growth on hot strength alloy structure at the directed crystallization] //Litejshhik Rossii. 2014. №5. S. 24–27.
8. Kablov E.N., Bondarenko Yu.A., Kablov D.E. Osobennosti struktury i zharoprochnyh svojstv monokristallov <001> vysokorenievogo nikelevogo zharoprochnogo splava, poluchennogo v usloviyah vysokogradientnoj napravlennoj kristallizacii [Features of structure and heat resisting properties of single crystals of <001> high-rhenium nickel hot strength alloys received in the conditions of high-gradient directed crystallization] //Aviacionnye materialy i tehnologii. 2011. №4. S. 25–31.
9. Kablov E.N., Orlov M.R., Ospennikova O.G. Mehanizmy obrazovaniya poristosti v monokristallicheskih lopatkah turbiny i kinetika ee ustraneniya pri goryachem izostaticheskom pressovanii [Mechanisms of formation of porosity in single crystals turbine blades and kinetics of its elimination at hot isostatic pressing] //Aviacionnye materialy i tehnologii. 2012. №S. S. 117–129.
10. Zharoprochnyj splav na osnove nikelja [Heat resisting alloy on the basis of nickel]: pat. 2148099 Ros. Federaciya; opubl. 18.01.99. Byul. №12.
11. Chabina E.B., Alekseev A.A., Filonova E.V., Lukina E.A. Primenenie metodov analiticheskoj mikroskopii i rentgenostrukturnogo analiza dlya issledovaniya strukturno-fazovogo sostoyaniya materialov [Application of methods of analytical microscopy and x-ray of the structural analysis for research of structural and phase condition of materials] //Trudy VIAM. 2013. №5. St. 06 (viam-works.ru).
12. Svetlov I.L., Ishodzhanova I.V., Evgenov A.G., Naprienko S.A. Issledovanie vysokotemperaturnoj polzuchesti i defektnosti struktury monokristallov nikelevogo zharoprochnogo splava posle gorjachego izostaticheskogo pressovaniya [Research of high-temperature creep and deficiency of structure of single crystals of nickel hot strength alloy after hot isostatic pressing] //Deformaciya i razrushenie materialov. 2011. №3. S. 28–32.
13. Nejman A.V., Filonova E. V., Ishodzhanova I. V. O lokalnoj rekristallizacii v monokristallah nikelevyh zharoprochnyh splavov [About local re crystallization in monocrystals of nickel hot strength alloys] //Metallurgiya i mashinostroenie. 2013. №1. S. 19–22.
14. Sidorov V.V., Ishodzhanova I.V., Rigin V.E., Folomejkin Yu.I. Ocenka effektivnosti filtracii pri razlivke slozhnolegirovannogo nikelevogo rasplava [Assessment of efficiency of filtering at razlivka complex-alloyed nickel rasplava] //Elektrometallurgiya. 2011. №11. S. 17–21.
15. Klark E.R., Eberhardt K.N. Mikroskopicheskie metody issledovaniya materialov [Microscopic methods of research of materials]. M.: Tehnosfera. 2007. 376 s.
16. Gulyaev A.I., Ishodzhanova I.V., Zhuravleva P.L. Primenenie metoda opticheskoj mikroskopii dlya kolichestvennogo analiza struktury PKM [Application of optical microscopy method for the quantitative analysis of polymer composite material structure] //Trudy VIAM. 2014. №7. St. 07 (viam-works.ru).
Karachevtsev F.N., Zagvozdkina T.N., Dvoretskov R.M.
In various types of nickel alloys silicon is present in a wide concentration range from a few hundredths of a percent in the heat resisting nickel alloys to whole percent in the nickel-based solders. The paper describes a method of measuring the mass fraction of silicon in the nickel-based alloys by atomic emission spectrometry with inductively coupled plasma (ICP-AES) in combination with microwave sample preparation. Compositions of dissolution mixtures and parameters of microwave digestion were selected. Limits of relative measurement error for Si content from 0,01 to 8% don't exceed 2% (±δ, at P=0,95).
1. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharo-prochnye splavy novogo pokoleniya [Nickel foundry heat resisting alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. C. 36–52.
2. Kablov E.N., Ospennikova O.G., Petrushin N.V., Visik E.M. Monokristallicheskij zharoprochnyj nikelevyj splav novogo pokoleniya s nizkoj plotnostyu [Single-crystal nickel-based superalloy of a new generation with low-density] //Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 14–25.
4. Shmotin Yu.N., Starkov R.Yu., Danilov D.V., Ospennikova O.G., Lomberg B.S. Novye materialy dlya perspektivnogo dvigatelya OAO «NPO „Saturn”» [New materials for the perspective engine of JSC «NPO „Saturn”»] //Aviacionnye materialy i tehnologii. 2012. №2. S. 6–8.
5. Kablov E.N., Ospennikova O.G., Petrushin N.V. Novyj monokristallicheskij intermetallidnyj (na osnove γʹ-fazy) zharoprochnyj splav dlya lopatok GTD [New single crystal heat-resistant intermetallic γʹ-based alloy for GTE blades] //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 34–40.
6. Kablov E.N. Fiziko-himicheskie i tehnologicheskie osobennosti sozdaniya zharoprochnyh splavov, soderzhashhih renij [Physical and chemical and technological features of creation of the heat resisting alloys containing rhenium] //Vestnik Moskovskogo universiteta. Ser. 2: Himiya. 2005. T. 46. №3. S. 155–167.
7. Kablov E.N., Petrushin N.V., Bronfin M.B., Alekseev A.A. Osobennosti monokristallicheskih zharoprochnyh nikelevyh splavov, legirovannyh reniem [Features of the single-crystal heat resisting nickel alloys alloyed by rhenium] //Metally. 2006. №5. S. 47–57.
8. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Litejnye zharoprochnye nikelevye splavy dlya perspektivnyh aviacionnyh GTD [Foundry heat resisting nickel alloys for perspective aviation GTE] //Tehnologiya legkih splavov. 2007. №2. S. 6–16.
9. Kablov E.N., Sidorov V.V., Kablov D.E., Rigin V.E., Goryunov A.V. Sovremennye tehnologii polucheniya prutkovyh zagotovok iz litejnyh zharoprochnyh splavov novogo pokoleniya [Modern technologies of receiving the bar stock preparations from foundry heat resisting alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 97–105.
10. Sidorov B.B., Ishodzhanova I.B., Rigin B.E., Folomejkin Yu.I. Ocenka effektivnosti filtratsii pri razlivke slozhnolegirovannogo nikelevogo rasplava [Assessment of efficiency of a filtration when pouring of difficult alloyed nickel fusion] //Elektrometallurgiya. 2011. №11. S. 17–21.
11. Sidorov V.V., Rigin V.E., Goryunov A.V., Min P.G., Kablov D.E. Poluchenie Re–Ru-soderzhashhego splava s ispolzovaniem nekondicionnyh othodov [Receiving Re–Ru the containing alloy with use of sub-standard waste] //Metallurgiya mashinostroeniya. 2012. №3. S. 15–17.
12. Pripoj na osnove nikelya [Solder on the basis of nickel]: pat. 2452600 Ros. Federacya; opubl. 22.06.2011.
13. Pupyshev A.A., Danilova D.A. Ispolzovanie atomno-emissionnoj spektrometrii s induktivno-svyazannoj plazmoj dlya analiza materialov i produktov chernoj metallurgii [Use of nuclear and issue spectrometry with the inductive and connected plasma for the analysis of materials and products of ferrous metallurgy] //Analitika i kontrol. 2007. T. 11. №2–3. S. 131–181.
14. Dvoretskov R.M., Karachevcev F.N., Zagvozdkina T.N., Mehanik E.A. Opredelenie himicheskogo sostava vysokolegirovannyh nikelevyh splavov aviacionnogo naznacheniya metodom AES-ISP v sochetanii s mikrovolnovoj probopodgotovkoj [Definition of a chemical composition of the high-alloyed nickel alloys of aviation appointment as the AES-ISP method in combination with microwave preparation of tests] //Zavodskaya laboratoriya. Diagnostika materialov. 2013. T. 79. №9. S. 6–9.
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Alexeev E.B., Nochovnaya N.A., Panin P.V., Novak A.V.
The article presents research results on technological parameters of deformation, structure and phase composition of a pilot intermetallic ortho alloy Ti–13Al–40Nb–5(Zr+V+Mo+W)–0,5(Si+C) determination. It has been resolved that no strain strengthening effect throughout hot working process is observed at a temperature of 1000°С. Temperature intervals of the following phase areas have been determined for the pilot alloy: (О+βA2)→(О+β(A2+В2)+α2)→(β(A2+В2)+α2)→β(A2+В2). Also it has been shown that technological plasticity (degree of strain) decrease at deformation temperatures lower than 1000°С and prolonged duration is caused by phase transformations: in these conditions decomposition of β-phase takes place together with the ordered intermetallic O- and α2-phases precipitation.
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4. 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.
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8. Kashapov O.S., Novak A.V., Nochovnaya N.A., Pavlova T.V. Sostoyanie, problemy i perspektivy sozdaniya zharoprochnyh titanovyh splavov dlya detalej GTD [Condition, problems and perspectives of creation of heat resisting titanium alloys for GTE details] //Trudy VIAM. 2013. №3. St. 02 (viam-works.ru).
9. Nochovnaya N.A., Ivanov V.I., Alekseev E.B., Kochetkov A.S. Puti optimizacii ekspluatacionnyh svojstv splavov na osnove intermetallidov titana [Ways of optimization of operational properties of alloys on the basis of titanium intermetallic compound] //Aviacionnye materialy i tehnologii. 2012. №S. S. 196–206.
10. Nochovnaya N.A., Panin P.V., Kochetkov A.S., Bokov K.A. Sovremennye zharoprochnye splavy na osnove gamma-alyuminida titana: perspektivy razrabotki i primeneniya [Modern hot strength alloys on the basis of titanium gamma aluminide: development and application perspectives] //MiTOM. 2014. №7. S. 23–27.
11. Nochovnaya N.A., Skvortsova S.V., Anishchuk D.S., Alekseev E.B., Panin P.V., Umarova O.Z. Otrabotka tehnologii opytnogo zharoprochnogo splava na osnove intermetallida Ti2AlNb [Working off of technology of pilot hot strength alloy on the basis of Ti2AlNb intermetallic compound] //Titan. 2013. №4 (42). S. 33–38.
12. Nochovnaya N.A., Alekseev E.B., Yasinskij K.K., Kochetkov A.S. Specifika plavki i sposoby polucheniya slitkov intermetallidnyh titanovyh splavov s povyshennym soderzhaniem niobiya [Specifics of melting and ways of receiving ingots of intermetallic titanium alloys with the raised content of niobium] //Vestnik MGTU im. N.E. Baumana. Ser. «Mashinostroenie». 2011. №SP2. C. 53–59.
13. Kablov D.E., Panin P.V., Shiryaev A.A., Nochovnaya N.A. Opyt ispolzovaniya vakuumno-dugovoj pechi ALD VAR L200 dlya vyplavki slitkov zharoprochnyh splavov na osnove aljuminidov titana [The use of ADL VAR L200 vacuum-arc furnace for ingots fabrication of high-temperature titanium aluminides base alloys] //Aviacionnye materialy i tehnologii. 2014. №2. S. 27–33.
14. Alekseev E.B., Nochovnaja N.A., Skvorcova S.V., Grushin I.A., Agarkova E.O. Vliyanie termicheskoj obrabotki na strukturno-fazovyj sostav i mehanicheskie svojstva titanovogo splava na osnove orto-fazy [Influence of thermal processing on structural and phase structure and mechanical properties of titanium alloy on the basis of orto-phase] //Titan. 2014. №4 (46). S. 45–49.
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17. Alekseev E.B., Nochovnaya N.A., Panin P.V. Issledovanie struktury i fazovogo sostava opytnogo zharoprochnogo splava na osnove intermetallida Ti2AlNb v deformirovannom sostoyanii [Research of structure and phase composition of pilot hot strength alloy on the basis of Ti2AlNb intermetallic compound in the deformed condition] //Titan. 2014. №4 (46). S. 12–17.
18. Alekseev E.B., Nochovnaya N.A., Ivanov V.I., Panin P.V., Novak A.V. Issledovanie vliyaniya alyuminiya na fazovyj sostav i svojstva deformirovannyh polufabrikatov iz intermetallidnogo titanovogo splava VTI-4 [Research of influence of aluminum on phase structure and properties of the deformed semi-finished products from intermetallic VTI-4 titanium alloy] //Tehnologiya legkih splavov. 2015. №1. S. 57–61.
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The article contains the review and analysis of methods of increasing in fire safety of fibrous thermal insulation. Permanent growing requirements to service properties of heat-insulating materials are caused by the progress in such areas of the industry, as transport, aviation, energy, chemical, oil-extracting and others, and also need of providing operation safety of machines and mechanisms. A number of new heat-insulating systems is developed for implementation of fire safety requirements of new aviation rules. New types of protective coatings meeting the modern requirements of aviation rules are developed.
3. Strelnikov S.V., Zastrogina O.B., Veshkin E.A., Shvets N.I. K voprosu o sozdanii vysokoeffektivnyh tehnologij izgotovleniya panelej interera v krupnoserijnom proizvodstve [To a question of creation of highly effective manufacturing techniques of panels of an interior in a large-lot production] //Aviacionnye materialy i tehnologii. 2011. №4. S. 18–24.
4. Ivahnenko Yu.A., Babashov V.G., Zimichev A.M., Tinyakova E.V. Vysokotemperaturnye teploizolyacionnye i teplozashhitnye materialy na osnove volokon tugoplavkih soedinenij [High-temperature heat insulating and heat-protective materials on the basis of fibers of high-melting connections] //Aviacionnye materialy i tehnologii. 2012. №S. S. 380–386.
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7. Varrik N.M. Termostojkie volokna i teplozvukoizolyacionnye ognezashhitnye materialy [Heat-resistant fibers and heat and sound insulating fireproof materials] //Trudy VIAM. 2014. №6. St. 07 (viam-works.ru).
8. Burn through resistant systems for transportation, especially aircraft: pat. 6565040 US; publ. 20.05.2003.
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17. Babashov V.G., Warrik N.M. Vysokotemperaturnyj gibkij voloknistyj teploizolyacionnyj material [High-temperature flexible fibrous insulation material] //Trudy VIAM. 2015. №1. St. 03 (viam-works.ru).
18. Ivahnenko Yu.A., Kuzmin V.V., Bespalov A.S. Sostoyanie i perspektivy razvitiya teplozvukoizolyacionnyh pozharobezopasnyh materialov [Condition and perspectives of development of heat sound-proof fireproof materials] //Problemy bezopasnosti poletov. 2014. №7. S. 27–30.
19. Zimichev A.M., Warrik N.M. K voprosu primeneniya diskretnyh volokon iz tugoplavkih oksidov dlya formirovaniya serdechnika termostojkih uplotnitelnyh shnurov [On the issue of application of discrete fibers of refractory oxides to form cores of heat-resistant sealing cords] //Trudy VIAM. 2015. №2. St. 07 (viam-works.ru).
The epoxy polymer based on Ethal-247 resin and cycloaliphatic Ethal-45M curing agent was exposed to Gelendzhik and Saransk atmosphere. The color characteristics of the specimens were measured and it was shown that colorimetric property such as a color difference of the polymer surface is sensitive to initial stages of weathering. It was shown that the natural UV-radiation is a dominant factor for polymer degradation. The application of solar radiation doze provides more reliable results.
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Processes of sorption and desorption of moisture by epoxy polymeric matrix and layered carbon fiber on its basis are considered. Moisture diffusion factors are estimated on stages of sorption and desorption. The conclusion is drawn on nature of diffusion in epoxy matrix and in polymeric composite material, on the basis of this matrix. The qualitative analysis of epoxy matrix, in the course of moisture sorption, is carried out by FTIR Spectroscopy. The structure and energy of molecule of epoxy matrix is calculated, at absence and presence of the bonded moisture in its composition. Researches of mechanical properties of polymeric composite materials are conducted at different values of moisture content. Changes of thermophysical properties of layered carbon fiber in the course of moisture sorption and desorption are investigated.
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