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Aviation materials and technologies №1, 2017

Contents

  • V.I. Voronkov, K.E. Potapenko, P.A. Petrov, S.V. Vydumkina

    Obtaining specified data on plastic deformation resistance of aluminum alloys AD35 and AD31 at hot forging

    3-10
  • O.A. Tonysheva, N.M. Voznesenskaya, I.I. Shestakov, E.A. Yeliseyev

    Influence of modes of high-temperature thermomechanical processing on structure and properties of high-strength corrosion-resistant steel of austenitic-martensitic class 17Х13Н4К6САМ3ч

    11-16
  • A.A. Kosmin, S.A. Budinovskiy, S.A. Muboyadzhyan

    Heatand corrosion resistant coating for working turbine blades from promising high-temperature alloy VZhL21

    17-24
  • V.A. Kuznetsova, L.V. Semenova, G.G. Shapovalov

    Development trends in the field of anticorrosive polymeric systems for corrosion protection of fixing connections of contact couples of combined structures (review)

    25-31
  • L.V. Semenova, T.A. Novikova, N.I. Nefedov

    Study of removing ability of removers for paint systems removal

    32-37
  • A.S. Boychuk, A.S. Generalov, I.A. Dikov

    FRP parts and structures testing by phased array technique

    45-50
  • E.I. Oreshko, V.S. Erasov, A.N. Lutsenko, V.F. Terentev, A.K. Slizov

    Creation of the 3D stress-strain diagrams σ-ε-t

    61-68
  • V.V. Murashov, A.S. Generalov

    PCM products and multilayer glued structures testing by ultrasonic reflection methods

    69-74
  • N.S. Perov, A.I. Gulyaev

    About the importance of structure evolution control of polymer composite materials with the microheterogeneous matrix for service life forecasting

    75-85
Содержание номера
1.

DOI: 10.18577/2071-9140-2017-0-1-3-10

UDC: 620.178.6:669.715

Pages:: 3-10

V.I. Voronkov1, K.E. Potapenko1, P.A. Petrov1, S.V. Vydumkina2

[1] Federal state budgetary educational institution of higher professional education «Moscow State University of Mechanical Engineering (MAMI)»
[2] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Obtaining specified data on plastic deformation resistance of aluminum alloys AD35 and AD31 at hot forging

The way of obtaining data on resistance of aluminum alloys AD35 and AD31 to plastic deformation by the inverse method (the method of inverse modeling) is shown. The essence of the method of inverse problem statement is to reproduce mechanical tests through simulation, compare the calculated and experimental force diagrams and correct the data on resistance of the material to plastic deformation on the basis of this comparison. The work is executed within the implementation of the complex scientific direction 3.2. «Computer simulation including application of neural networks, processes of treatment by pressure with forecasting of structure, complex of mechanical and operational properties of products» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: resistance to plastic deformation,  mathematical model, strain rate, yield curve

Reference List

    1. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.

    2. Ospennikova O.G., Bubnov M.V., Kapitanenko D.V. Kompyuternoe modelirovanie processov obrabotki metallov davleniem [Computer modeling of metal working processes by pressure] //Aviacionnye materialy i tehnologii. 2012. №S. S. 141–147.

    3. 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.

    4. 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.

    5. Petrov P.A., Dubinchin A.V. Postroenie «izotermicheskoj» krivoj tekuchesti alyuminievogo splava AMg6 [Creation of «isothermal» curve flowability of Amg6 aluminum alloy] // Obrabotka materialov davleniem. 2008. №1 (19). S. 145–150.

    6. Petrov P.A. Postroenie «izotermicheskoj» krivoj tekuchesti alyuminievogo splava V95 [Creation of «isothermal» curve flowability of B95 aluminum alloy] // Obrabotka materialov davleniem. 2010. №2 (23). S. 88–93.

    7. Kalpin Yu.G., Perfilov V.I., Petrov P.A., Ryabov V.A., Filippov. Yu.K. Soprotivlenie deformacii i plastichnost metallov pri obrabotke davleniem: ucheb. posobie dlya vuzov [Resistance of deformation and plasticity of metals when processing by pressure: the manual for higher education institutions]. M.: MGTU MAMI, 2005. 113 s.

    8. Petrov P.A., Voronkov V.I., Krutina E.V., Ivanov V.A. Razrabotka tehnologii izotermicheskoj shtampovki detali «korpus mufty» iz alyuminievogo splava AD35 [Development of technology of isothermal punching of detail «the coupling body» from AD35 aluminum alloy] // Sb. dokl. Tretego Mezhdunarodnogo kongressa «Cvetnye metally–2011». Krasnoyarsk: Verso, 2011. S. 590–596.

    9. Petrov P.A. Razrabotka i issledovanie tehnologii tochnoj shtampovki detalej iz alyuminievyh splavov na osnove kompyuternogo modelirovaniya [Development and research of technology of exact punching of details from aluminum alloys on the basis of computer modeling] // Mater. Tretej nauch.-tehnich. konf. «Metallofizika, mehanika materialov, nanostruktury i processy deformirovaniya. Metalldeform–2009». Samara: SGAU, 2009. T. 2. S. 174–183.

    10. Grinberg I.V., Petrov P.A., Gnevashev D.A., Voronkov V.I. Fizicheskoe i matematicheskoe modelirovanie processa izgotovleniya tonkostennyh obolochek v shtampe dlya vydavlivaniya [Physical and mathematical modeling of process of manufacturing of thin-walled covers in stamp for extrusion] // Tehnologiya legkih splavov. 2010. №2. S. 101–106.

    11. Petrov P.A. Modelirovanie processov izotermicheskoj shtampovki alyuminievyh i magnievyh splavov [Modeling of processes of isothermal punching of aluminum and magnesium alloys] // Kuznechno-shtampovochnoe proizvodstvo. Obrabotka materialov davleniem. 2011. №12. S. 29–35.

    12. 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.

    13. Potapenko K.E., Penkov I.V., Voronkov V.I., Petrov P.A. Issledovanie kontaktnogo treniya pri goryachej plasticheskoj deformacii splava AMg6 [Research of contact friction at more hotly plastic strain of alloy AMg6] // Kuznechno-shtampovochnoe proizvodstvo. Obrabotka materialov davleniem. 2012. №2. S.16–19.

    14. Potapenko K.E., Pen\'kov I.V., Voronkov V.I., Petrov P.A., Shajhulov M.V. Issledovanie kontaktnogo treniya pri goryachej plasticheskoj deformacii splava AV [Research of contact friction at more hotly plastic strain of alloy of AV ] // Zagotovitelnye proizvodstva v mashinostroenii. 2012. №6. S. 18–21.

    15. Aleksandrov I.V., Chembarisova R.G., Latypov M.I. Analiticheskoe modelirovanie napryazheniya techeniya splava AL1570, podvergnutogo intensivnoj plasticheskoj deformacii [Analytical modeling of flow stress of alloy of AL1570 subjected to intensive plastic strain] // Vestnik UGATU. 2012. №3 (48). S. 120–123.

    16. Petrov P.A., Perfilov V.I. Issledovanie uprochneniya alyuminievogo splava AMg6 na nachalnom uchastke krivoj tekuchesti pri povyshennyh temperaturah [Research of hardening of Amg6 aluminum alloy on initial site of curve flowability at elevated temperatures] // Modelirovanie, programmnoe obespechenie i naukoemkie tehnologii v metallurgii: sb. tr. 2-j Vseros. nauch.-prakticheskoj konferencii. Novokuzneck, 2006. S. 205–207.

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2.

DOI: 10.18577/2071-9140-2017-0-1-11-16

UDC: 620.1

Pages:: 11-16

O.A. Tonysheva1, N.M. Voznesenskaya1, I.I. Shestakov1, E.A. Yeliseyev1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Influence of modes of high-temperature thermomechanical processing on structure and properties of high-strength corrosion-resistant steel of austenitic-martensitic class 17Х13Н4К6САМ3ч

Results of researches of influence of different modes of high-temperature thermomechanical processing (HTMP) on structure and mechanical properties of steel 17Х13Н4К6САМ3ч strengthened by carbon and nitrogen, containing rare earth metals such as yttrium, lanthanum, cerium and neodymium are given in the article.Working results show that increase in temperature of HTMP leads to formation of fine recrystallized grains of 9-10 points in melts of the steel containing the greatest total quantity of carbon and nitrogen: 0,25-0,30%. Fine recrystallized grains significantly increased impact strength of the steel (when testing Sharpy-samples) with saving of strength characteristics (tensile strength and yield strength) in comparison with the steel which has not been subjected by HTMP. The work is executed within the implementation of the complex scientific direction 8.2. «High-strength constructional and corrosion-resistant welded steels with high fracture toughness» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: high-strength corrosion-resistant steel, high-temperature thermomechanical processing, recrystallization

Reference List

    1. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.

    2. Kablov E.N., Ospennikova O.G., Lomberg B.S. Strategicheskie napravleniya razvitiya konstrukcionnyh materialov i tehnologij ih pererabotki dlya aviacionnyh dvigatelej nastoyashhego i budushhego [The strategic directions of development of constructional materials and technologies of their processing for aircraft engines of the present and the future] // Avtomaticheskaya svarka. 2013. №10. S. 23–32.

    3. Kablov E.N., Ospennikova O.G., Vershkov A.V. Redkie metally i redkozemelnye elementy – materialy sovremennyh i budushhih vysokih tehnologij [Rare metals and rare earth elements – materials of modern and future high technologies] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2013. №2. St. 01. Available at: http://www.viam-works.ru (accessed: February 01, 2016).

    4. Krylov S.A., Evgenov A.G., Shherbakov A.I., Makarov A.A. Novaya elektroshlakovaya pech pod davleniem DEShP-0,1: osvoenie i perspektivy razvitiya [New pressure electroslag remelting furnace  PESR-0,1: development and prospects for improvement] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №5. St. 04. Available at: http://www.viam-works.ru (accessed: July 20, 2016). DOI: 10.18577/2307-6046-2016-0-5-4-4.

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    7. Shestakov I.I., Voznesenskaya N.M., Tonysheva O.A. Vliyanie vysokotemperaturnoj termomehanicheskoj obrabotki na strukturu i svojstva vysokoprochnoj korrozionnostojkoj stali marki 17H13N4K6SAM3ch [Influence of high-temperature thermomechanical treatment on the structure and properties of high-strength corrosion-resistant steel of grade 17H13N4К6SАМ3ch] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2016. №6. St. 02. Available at: http://www.viam-works.ru (accessed: August 01, 2016). DOI: 10.18577/2307-6046-2016-0-6-2-2.

    8. Tonysheva O.A., Voznesenskaja N.M., Shalkevich A.B., Petrakov A.F. Issledovanie vlijanija vysokotemperaturnoj termomehanicheskoj obrabotki na strukturu, tehnologicheskie, mehanicheskie i korrozionnye svojstva vysokoprochnoj korrozionnostojkoj stali pere-hodnogo klassa s povyshennym soderzhaniem azota [Research of influence of high-temperature thermomechanical processing on structure, technological, mechanical and corrosion properties of high-strength corrosion-resistant steel of transitional class with the raised content of nitrogen] // Aviacionnye materialy i tehnologii. 2012. №3. S. 31–36.

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3.

DOI: 10.18577/2071-9140-2017-0-1-17-24

UDC: 629.7.023

Pages:: 17-24

A.A. Kosmin1, S.A. Budinovskiy1, S.A. Muboyadzhyan1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Heatand corrosion resistant coating for working turbine blades from promising high-temperature alloy VZhL21

Coating and its application on turbine blades has been developed. Thermal fatigue tests of VZhL21 alloy rotor blades at a temperature of 480→770→480°С powered by 800 cycles before the first crack have been carried out on modes simulating the operation of engine TV3-117. It is shown that VZhL21 alloy rotor blades with a protective coating system SDP-1T+VSDP-13 were fully tested with no visible signs of damage. The influence of this coating on long-term durability and high-cycle fatigue of alloy VZhL21 has been evaluated. The positive effect of the coating on resistance to sulfide-oxide corrosion at the temperature range of 850-950°С, and also heat resistance at temperature up to 1050°С has been shown.

Keywords: coatings, heat resisting coatings, ion-plasma coatings, ion-plasma technology, heat resistance, protection of high-temperature alloys, coatings for turbine blades

Reference List

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    3. Kablov E.N., Startsev O.V., Medvedev I.M. Obzor zarubezhnogo opyta issledovanij korrozii i sredstv zashhity ot korrozii [Review of international experience on corrosion and corrosion protection] // Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 76–87. DOI: 10.18577/2071-9140-2015-0-2-76-87.

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    8. Kablov E.N., Krivonogov G.S. Rol granic zeren v ohrupchivanii vysokoprochnyh korrozionnostojkih stalej [Role of borders of grains in fragility high-strength corrosion-resistant the steels] // Metally. 2002. №1. S. 35–41.

    9. Galoyan A.G., Muboyadzhyan S.A., Egorova L.P., Bulavintseva E.E. Korrozionnostojkoe pokrytie dlya zashhity detalej GTD iz vysokoprochnyh konstrukcionnyh martensitostareyushhih stalej na rabochie temperatury do 450°C [Corrosion-resistant coating for protection of GTE details made of high-strength maraging constructional steel with operating temperature up to 450°C] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №6. St. 03. Available at: http://www.viam-works.ru (accessed: July 12, 2016). DOI: 10.18577/2307-6046-2014-0-6-3-3.

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    16. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.

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4.

DOI: 10.18577/2071-9140-2017-0-1-25-31

UDC: 678.026

Pages:: 25-31

V.A. Kuznetsova1, L.V. Semenova1, G.G. Shapovalov1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Development trends in the field of anticorrosive polymeric systems for corrosion protection of fixing connections of contact couples of combined structures (review)

Development trends in the field of anticorrosive polymeric systems for corrosion protection of fixing connections of contact couples of combined structures which provide operability of aircraft made of dissimilar materials, including carbon plastics, at operation of products in different climatic zones are considered. Scientific and technical documentation and titles of protection of leading countries of the world related to a problem of development of anticorrosive polymeric systems for corrosion protection of fixing connections of contact couples of combined structures are analized.

Keywords: elastic polymeric anticorrosive structure, epoxy oligomer, corrosion resistance, moisture resistance, adhesion, modifier, hardener

Reference List

    1. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.

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    10. Kondrashov E.K., Kuznetsova V.A., Semenova L.V., Lebedeva T.A., Malova N.E. Razvitie aviacionnyh lakokrasochnyh materialov [Development of aviation paint and varnish materials] // Vse materialy. Enciklopedicheskij spravochnik. 2012. №5. S. 49–54.

    11. Goldberg M.M., Koryukin A.V., Kondrashov E.K. Pokrytiya dlya polimernyh materialov [Coverings for polymeric materials]. M.: Himiya, 1980. 287 s.

    12. Kondrashov E.K., Kuznecova V.A., Semenova L.V., Lebedeva T.A. Osnovnye napravleniya povysheniya ekspluatacionnyh, tehnologicheskih i ekologicheskih harakteristik lakokrasochnyh pokrytij dlya aviacionnoj tehniki [The main directions of increase of utilization, technical and ecological properties of paint coatings for aviation engineering] // Rossijskij himicheskij zhurnal. 2010. T. LIV. №1. S. 96–102.

    13. Semenova L.V., Nefedov N.I. Primenenie epoksidnyh modificirovannyh gruntovok v sistemah LKP [Application of modified epoxy primers in the painting systems] // Aviacionnye materialy i tehnologii. 2014. №3. S. 38–44. DOI: 10.18577/2071-9140-2014-0-3-38-44.

    14. Kuznetsova V.A., Deev I.S., Kondrashov E.K., Kuznetsov G.V. Vliyanie otverditelej na mikrostrukturu i svojstva modificirovannogo epoksidnogo svyazuyushhego dlya toplivostojkogo pokrytiya [Influence of hardeners on microstructure and property of the modified epoxy resistant covering binding for fuel] // Vse materialy. Enciklopedicheskij spravochnik. 2012. №11. S. 38–41.

    15. Kuznetsova V.A., Kondrashov E.K., Semenova L.V., Kuznetsov G.V. O vliyanii formy chastic oksida cinka na ekspluatacionnye svojstva polimernyh pokrytij [About influence of particle shape of zinc oxide on operational properties of polymer coatings] // Materialovedenie. 2012. №12. S. 12–14.

    16. Semenova L.V., Rodina N.D., Nefedov N.I. Vliyanie sherohovatosti sistem lakokrasochnyh pokrytij na ekspluatacionnye svojstva samoletov [An effect of roughness of paint and varnish coating systems on service properties of aircraft] // Aviacionnye materialy i tehnologii. 2013. №2. S. 37–40.

    17. Kuznetsova V.A., Deev I.S., Kuznecov G.V., Kondrashov E.K. Vliyanie napolnitelya na ustalostnuyu prochnost i mikrostrukturu svobodnyh polimernyh plenok pokrytij pri ciklicheskom rastyazhenii [Influence of filler on fatigue resistance and microstructure of free polymer films of coverings at cyclic stretching] // Zavodskaya laboratoriya. 2014. №5. S. 35–39.

    18. Fang Wang, Junjun Liu, Yuefei Li, Ruibin Fan, Yanni Li. Complex Barrier Layer of Triazinedithoil Prepared by Electrodeposition and Initiated Polymerization on aluminum Alloy towards Corrosion Protection // International Journal of Electrochemical Science. 2012. No. 7. P. 3672–3680.

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DOI: 10.18577/2071-9140-2017-0-1-32-37

UDC: 667.691

Pages:: 32-37

L.V. Semenova1, T.A. Novikova1, N.I. Nefedov1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

Study of removing ability of removers for paint systems removal

The present paper describes the results of study of removing ability of Russian paint remover brands АРS-А36, APS-А38 and SVP-4 for paint-and-lacquer coatings removal. The effect of paint removers both on the coating itself and the substrate was investigated. The maximum allowable time of application of special composition on the coating was determined. As a result of the research the repair technology of paint coatings on the outer surface of aircraft has been developed, including different methods of removing corrosion products, optimal treatment of the surface by chemical compositions and application of high-efficiency coatings

Keywords: paint coatings, paint, remover, corrosion, repair technology

Reference List

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    4. Semenova L.V., Rodina N.D., Nefedov N.I. Vliyanie sherohovatosti sistem lakokrasochnyh pokrytij na ekspluatacionnye svojstva samoletov [An effect of roughness of paint and varnish coating systems on service properties of aircraft] // Aviacionnye materialy i tehnologii. 2013. №2. S. 37–40.

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    8. Chebotarevskij V.V., Kondrashov E.K. Tehnologiya lakokrasochnyh pokrytij v mashinostroenii [Technology of paint coatings in mechanical engineering]. M.: Mashinostroenie, 1978. S. 214–220.

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    11. Semyonova L.V., Bejder E.Ya., Petrova G.N., Nefedov N.I. Elektroizolyacionnye svojstva polimernyh pokrytij [Electro-insulative properties of polymer coatings] // Trudy VIAM elektron. nauch.-tehnich. zhurn. 2014. №8. St. 07. Available at: http://www.viam-works.ru (accessed: December 07, 2016). DOI: 10.18577/2307-6046-2014-0-8-7-7.

    12. Lakokrasochnye pokrytiya. Istoriya aviacionnogo materialovedeniya: VIAM – 75 let poiska, tvorchestva, otkrytij / pod obshh. red. E.N. Kablova [Paint coatings. History of aviation materials science: VIAM – 75 years of search, creativity, opening / gen. ed. by. E.N. Kablov]. M.: Nauka, 2007. S. 326.

    13. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.

    14. Kondrashov E.K., Kuznetsova V.A., Semenova L.V., Lebedeva T.A., Malova N.E.  Razvitie aviacionnyh lakokrasochnyh materialov [Development of aviation paint and varnish materials] // Vse materialy. Enciklopedicheskij spravochnik. 2012. №5. S. 49–54.

    15. Kondrashov E.K., Kuznetsova V.A., Semenova L.V., Lebedeva T.A. Osnovnye napravleniya povysheniya ekspluatacionnyh, tehnologicheskih i ekologicheskih harakteristik lakokrasochnyh pokrytij dlya aviacionnoj tehniki [The main directions of increase of utilization, technical and ecological properties of paint coatings for aviation engineering] // Rossijskij himicheskij zhurnal. 2010. T. LIV. №1. S. 96–102.

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    17. Beider E.Ya., Donskoi A.A., Zhelezina G.F., Kondrashov E.K., Sytyi Y.V., Surnin E.G. An experience of using fluoropolymer materials in aviation engineering // Russian Journal of General Chemistry. 2009. Vol. 79. No. 3. P. 548–564.

    18. Semenova L.V., Malova N.E., Kuznetsova V.A., Pozhoga A.A. Lakokrasochnye materialy i pokrytiya [Paint and varnish materials and coatings] // Aviacionnye materialy i tehnologii. 2012. №S. S. 315–327.

    19. Semenova L.V., Nefedov N.I. Primenenie epoksidnyh modificirovannyh gruntovok v sistemah LKP [Application of modified epoxy primers in the painting systems] // Aviacionnye materialy i tehnologii. 2014. №3. S. 38–44. DOI: 10.18577/2071-9140-2014-0-3-38-44.

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DOI: 10.18577/2071-9140-2017-0-1-45-50

UDC: 620.179:678.8

Pages:: 45-50

A.S. Boychuk1, A.S. Generalov1, I.A. Dikov1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

FRP parts and structures testing by phased array technique

The application of phased array (PA) technique for critical FRP parts and structures testing in production and service conditions is shown in the article. The most dangerous production and service types of defects and ways of its obtaining in laboratory on FRP specimens are discribed. The experience of PA application for delaminations, inclusions, impact damages, lightning stroke damages detection with sensitivity equivalent to assured detection of 5 mm diameter flat bottom hole is described. The way of nondestructive testing of FRP parts and structures with curved surface and also stringer panel radii zone with the use of PA is proposed. Work is executed within implementation of the complex scientific direction 2.3. «Methods of nondestructive researches and control» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: carbon fiber reinforced plastics (CFRP), fiber reinforced plastics (FRP), nondestructive testing (NDT), ultrasound testing (UT), phased array (PA)

Reference List

    1. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.

    2. Trostyanskaya E.B., Mihajlin Yu.A., Buharov S.V. Tendencii primeneniya i razvitiya kompozicionnyh materialov v samoletostroenii [Tendencies of application and development of composite materials in aircraft construction] // Aviacionnaya promyshlennost. 2002. №2. S. 18–22.

    3. Donetskij K.I., Kogan D.I., Hrulkov A.V. Svojstva polimernyh kompozicionnyh materialov, izgotovlennyh na osnove pletenyh preform [Properties of the polymeric composite materials made on the basis of braided preforms] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №3. St. 05. Available at: http://www.viam-works.ru (accessed: April 10, 2015). DOI: 10.18577/2307-6046-2014-0-3-5-5.

    4. Lukina N.F., Dementeva L.A., Kutsevich K.E. Kleevye prepregi na osnove tkanej Porcher – perspektivnye materialy dlya detalej i agregatov iz PKM [Adhesive prepregs based on tissue Porsher – perspective materials for parts and units out of polymeric composite materials] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №6. St. 10. Available at: http://www.viam-works.ru (accessed: April 10, 2015). DOI: 10.18577/2307-6046-2014-0-6-10-10.

    5. Poliimidnoe svyazuyushhee dlya armirovannyh plastikov, prepreg na ego osnove i izdelie, vypolnennoe iz nego: pat. 2394857 Ros. Federaciya [Polyimide binding for the reinforced plastics, prepreg on its basis and the product which has been executed of it: pat. 2394857 Rus. Federation]; opubl. 07.05.09.

    6. Epoksidnoe svyazuyushhee, prepreg na ego osnove i izdelie, vypolnennoe iz nego: pat. 2424259 Ros. Federaciya [Epoxy binding, prepreg on its basis and the product which has been executed of it: stalemate. 2424259 Rus. Federation]; opubl. 22.10.09.

    7. Timoshkov P.N., Hrulkov A.V. Sovremennye tehnologii pererabotki polimernyh kompozitsionnyh materialov, poluchaemyh metodom propitki rasplavnym svyazuyushchim [Modern technologies of hotmelt polymer composite materials processing] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №8. St. 04. Available at: http://www.viam-works.ru (accessed: April 10, 2015). DOI: 10.18577/2307-6046-2014-0-8-4-4.

    8. Dementeva L.A., Serezhenkov A.A., Lukina N.F., Kutsevich K.E. Svoistva i naznachenie kompozitsionnyh maerialov na osnove kleevyh prepregov [Properties and appointment of composite materials based on adhesive prepregs] // Trudy VIAM: elektron. nauch.-tehnich. zhurn. 2014. №8. St. 06. Available at: http://www.viam-works.ru (accessed: April 10, 2015). DOI: 10.18577/2307-6046-2014-0-8-6-6.

    9. Kablov E.N., Kondrashov S.V., Yurkov G.Yu. Perspektivy ispolzovaniya uglerodsoderzhashhih nanochastic v svyazuyushhih dlya polimernyh kompozicionnyh materialov [Perspectives of use of carbon-containing nanoparticles in binding for polymeric composite materials] // Rossijskie nanotehnologii. 2013. T. 8. №3–4. S. 24–42.

    10. Kablov E.N., Kirillov V.N., Zhirnov A.D., Startsev O.V., Vapirov Yu.M. Centry dlya klimaticheskih ispytanij aviacionnyh PKM [The centers for climatic tests of aviation PCM] // Aviacionnaya promyshlennost. 2009. №4. S. 36–46.

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    12. Boychuk A.S., Generalov A.S., Stepanov A.V., Yuhackova O.V. Nerazrushayushhij kontrol PKM s ispolzovaniem ultrazvukovyh fazirovannyh reshetok [Non-destructive testing of PCM with use of the ultrasonic phased grids] // Promyshlennye ASU i kontrollery. 2013. №2. S. 54–58.

    13. Boychuk A.S., Stepanov A.V, Kosarina E.I., Generalov A.S. Primenenie tehnologii ultrazvukovyh fazirovannyh reshetok v nerazrushayushhem kontrole detalej i konstrukcij aviacionnoj tehniki, izgotavlivaemyh iz PKM [Application of ultrasonic phased lattice technique for nondestructive testing of aviation FRP parts structures] // Aviacionnye materialy i tehnologii. 2013. №2. S. 41–46.

    14. Boychuk A.S., Stepanov A.V., Generalov A.S. Ultrazvukovoj kontrol krivolinejnyh poverhnostej konstrukcij sovremennyh samoletov iz polimernyh kompozicionnyh materialov s pomoshh\'yu preobrazovatelya na fazirovannoj reshetke i special\'nyh prisposoblenij [Ultrasonic control of curvilinear surfaces of designs of modern airplanes from polymeric composite materials by means of the converter on the phased grid and special adaptations] // Sb. tez. dokl. XIX Mezhdunar. konf. «Sovremennye metody i sredstva nerazrushayushhego kontrolya i tehnicheskoj diagnostiki». Gurzuf. 2011. S. 129–130.

    15. Boychuk A.S., Generalov A.S., Stepanov A.V. UZK detalej i konstrukcij iz PKM s krivolinejnoj poverhnostyu pri ispolzovanii fazirovannyh reshetok [USC of details and designs from PCM with curvilinear surface when using the phased grids] // Sb. tez. dokl. XX Mezhdunar. nauch.-tehnich. konf. studentov i aspirantov «Radioelektronika, elektrotehnika i energetika». M., 2014. T. 2. S. 102.

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    18. Boychuk A.S., Generalov A.S., Lozhkova D.S., Stepanov A.V. Ocenka veroyatnosti obnaruzheniya defektov v ugleplastikah pri ultrazvukovoj defektoskopii s ispolzovaniem fazirovannyh reshetok [Assessment of probability of detection of defects in carbon plastics at ultrasonic defect’s scope with use of the phased grids] // Sb. tez. dokl. XIX Mezhdunar. nauch.-tehnich. konf. studentov i aspirantov «Radioelektronika, elektrotehnika i energetika». M.: NIU MEI, 2013. S. 106.

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DOI: 10.18577/2071-9140-2017-0-1-61-68

UDC: 620.1

Pages:: 61-68

E.I. Oreshko1, V.S. Erasov1, A.N. Lutsenko1, V.F. Terentev2, A.K. Slizov3

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»
[2] Institute of Metallurgy and Materials Science A.A. Baykova of Russian academy of sciences
[3] Joint Stock Company «Kamov»

Creation of the 3D stress-strain diagrams σ-ε-t

The paper focuses on the interplay of the main tensile test factors: strain, stress and time. The advantages of representation of testing processes and their results in 3D coordinate system (stress, strain and time) are demonstrated. For creation of three-dimensional charts of deformation of material the ANSYS Mechanical program is proposed, allowing to build exact geometry of object, both by means of the convenient graphic interface of the user and parametric programming language APDL. Construction technique of 3D stress-strain diagrams is described. The work is executed within the implementation of the complex scientific direction 3.1. «Computer designing and modeling of compositions of cast and wrought alloys and steels, including natural composites and intermetallic compounds, technologies of their manufacturing and processing» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: mechanical tests, static stretching, time, elastic deformation, plastic deformation, soft loading, hard loading, strain rate, 3D coordinate system «stress, strain, time»

Reference List

    1. 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. DOI: 10.18577/2071-9140-2015-0-1-3-33.

    2. Kablov E.N., Grinevich A.V., Erasov V.S. Harakteristiki prochnosti metallicheskih aviacionnyh materialov i ih raschetnye znacheniya [Characteristics of durability of metal aviation materials and their calculated values] // 75 let. Aviacionnye materialy. Izbrannye trudy «VIAM» 1932–2007: yubileiny nauch.-tehnich. sb. M.: VIAM, 2007. S. 370–379.

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    4. Erasov V.S. Fiziko-mehanicheskie harakteristiki kak osnovnye integralnye pokazateli kachestva aviacionnyh konstrukcionnyh materialov: metod. posobie [Physicomechanical characteristics as main integral figures of merit of aviation constructional materials: methodical grant]. M.: VIAM, 2011. 16 s.

    5. Erasov V.S., Yakovlev N.O., Nuzhnyj G.A. Kvalifikatsionnye ispytaniya i issledovaniya prochnosti aviatsionnyh materialov [Qualification tests and researches of durability of aviation materials] // Aviacionnye materialy i tehnologii. 2012. №S. S. 440–448.

    6. Erasov V.S., Bajramukov R.R. Rol faktora vremeni pri provedenii mehanicheskih ispytanij, obrabotke dannyh i predstavlenii rezultatov [Role of factor of time at carrying out mechanical tests, data processing and representation of results] // Aviacionnye materialy i tehnologii. 2013. №S2.S. 62–67.

    7. Erasov V.S., Bajramukov R.R., Nuzhnyj G.A. Opredelenie skorosti plasticheskoj deformacii pri ispytanii na rastyazhenie [Speed sensing of plastic strain at tension test] // Zavodskaya laboratoriya. Diagnostika materialov. 2014. T. 80. №5. S. 61–63.

    8. Erasov V.S., Oreshko E.I., Lutsenko A.N. Povrezhdaemost materialov pri staticheskom rastyazhenii [Damageability of materials in tension testing] // Aviacionnye materialy i tehnologii. 2015. №4 (37). S. 91–94. DOI: 10.18577/2071-9140-2015-0-4-91-94.

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    14. Kolobnev N.I., Hohlatova L.B., Oglodkov M.S., Klochkova Yu.Yu. Vysokoprochnye splavy sistemy Al–Cu–Li s povyshennoj vyazkost\'yu razrusheniya dlya samoletnyh konstrukcij [High-strength alloys of Al–Cu–Li system with the increased fracture toughness for aircraft designs] // Tsvetnye metally. 2013. №9. S. 66–70.

    15. Kolobnev N.I., Hohlatova L.B., Yakovlev N.O., Oglodkov M.S. Alyuminij-litievyj splav V-1461 sistemy Al–Cu–Li dlya kriogennyh temperatur [Aluminum-lithium alloy V-1461 of Al–Cu–Li system for cryogenic temperatures] // Metallurgiya mashinostroeniya. 2014. №5. S. 29–33.

    16. Oreshko E.I., Erasov V.S., Podjivotov N.Yu. Vybor shemy raspolozheniya vysokomodulnyh sloev v mnogoslojnoj gibridnoj plastine dlya ee naibolshego soprotivleniya potere ustojchivosti [Arrangement of high-modular layers in a multilayer hybrid plate for its greatest resistance to stability loss] // Aviacionnye materialy i tehnologii. 2014. №S4. S. 109–117. DOI: 10.18577/2071-9140-2014-0-S4-109-117.

    17. Oreshko E.I., Erasov V.S., Lutsenko A.N. Matematicheskoe modelirovanie deformirovaniya konstrukcionnogo ugleplastika pri izgibe [Mathematical modeling of deformation constructional carbon fiber at a bend] // Aviacionnye materialy i tehnologii. 2016. №2 (41). S. 50–59. DOI: 10.18577/2071-9140-2016-2-50-59.

    18. Oreshko E.I., Erasov V.S., Lutsenko A.N. Osobennosti raschetov ustojchivosti sterzhnej i plastin [Features of calculations of stability of rods and plates] // Aviacionnye materialy i tehnologii. 2016. №4. S. 74–79. DOI: 10.18577/2071-9140-2016-0-4-74-79.

    19. Dimitrienko Yu.I., Gubareva E.A., Sborshhikov S.V., Bazyleva O.A., Lucenko A.N., Oreshko E.I. Modelirovanie uprugoplasticheskih harakteristik monokristallicheskih intermetallidnyh splavov  na osnove mikrostrukturnogo chislennogo analiza [Modeling of elasto-plastic characteristics of single-crystal intermetallidny alloys on the basis of the microstructural numerical analysis] // Matematicheskoe modelirovanie i chislennye metody. 2015. №2. S. 3–22.

    20. Dimitrienko Yu.I., Lucenko A.N., Gubareva E.A., Oreshko E.I., Bazyleva O.A., Sborshhikov S.V. Raschet mekhanicheskikh kharakteristik zharoprochnykh intermetallidnykh splavov na osnove nikelya metodom mnogomasshtabnogo modelirovaniya struktury [Calculating of mechanical characteristics of heat resistant intermetallic alloys on the basis of nickel by method of multi-scale modeling of structure] // Aviacionnye materialy i tehnologii. 2016. №3 (42). S. 33–48. DOI: 10.18577/2071-9140-2016-0-3-33-48.

    21. Oreshko E.I., Erasov V.S., Podzhivotov N.Yu., Lutsenko A.N. Raschet na prochnost gibridnoj paneli kryla na baze listov i profilej iz vysokoprochnogo alyuminij-litievogo splava i sloistogo alyumostekloplastika [Strength calculation of hybrid wing panel on the basis of sheets and profiles from high-strength aluminum lithium alloy and laminated aluminum fiberglass] // Aviacionnye materialy i tehnologii. 2016. №1 (40). S. 53–61. DOI: 10.18577/2071-9140-2016-0-1-53-61.

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10.

DOI: 10.18577/2071-9140-2017-0-1-69-74

UDC: 621.721.5:620.179.1

Pages:: 69-74

V.V. Murashov1, A.S. Generalov1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

PCM products and multilayer glued structures testing by ultrasonic reflection methods

The physical basis of ultrasonic reflection methods is considered. Advantages and disadvantages of these methods for identification of defects in PCM products and multilayer glued structures are given. The efficiency of spectrum analysis of echo pulses, passed through a glue layer or reflected from zone of violation of glued joint is shown. Work is executed within implementation of the complex scientific direction 2.3. «Methods of nondestructive researches and control» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: ultrasonic methods of reflection, products from PCM, multilayer glued structures, violations of glued joint, spectrum analysis of echo pulses

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DOI: 10.18577/2071-9140-2017-0-1-75-85

UDC: 541.64:539.2

Pages:: 75-85

N.S. Perov1, A.I. Gulyaev1

[1] Federal state unitary enterprise «All-Russian Scientific-Research Institute of Aviation Materials» of National Research Center «Kurchatov Institute»

About the importance of structure evolution control of polymer composite materials with the microheterogeneous matrix for service life forecasting

Validity of application of the damage additive accumulation model for polymer composite materials service life forecasting at the tests simulating different operating conditions is considered. Molecular mobility and structure of new promising carbon fiber polycyanurate composite are studied in different natural and artificial environments. Results of researches of the composite polymeric matrix relaxation properties and microstructure show that the morphology and quantitative characteristics of microstructure depend on type and duration of exposure. Work is executed within implementation of the complex scientific direction 18.3. «Modeling and forecasting of climatic firmness» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

Keywords: carbon fiber polymer composite, climatic tests, structural heterogenity, microphase separation, relaxation properties, degradation, aging

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