Aspects of application of high-strength and high-modulus fiber metal composite materials for aeronautical purpose (review)

Grishina O.I., Kochetov V.N., Shavnev A.A., Serpova V.M.
Grishina O.I., Kochetov V.N., Shavnev A.A., Serpova V.M. Aspects of application of high-strength and high-modulus fiber metal composite materials for aeronautical purpose (review) // Proceedings of VIAM. 2014. No. 10. DOI: 10.18577/2307-6046-2014-0-10-5-5. URL: https://test.viam.ru/en/journal/2014/10/5
Abstract

A review of metal composite materials based on aluminum and titanium matrixes, rein-forced with high-strength fibers of refractory compounds for application in constructions of aerotechnics and space transport systems is presented.

Reference list
  1. Kablov E.N. Strategicheskie napravlenija razvitija materialov i tehnologij ih pererabotki na period do 2030 goda [Strategic directions of development of materials and technologies to process them for the period up to 2030] //Aviacionnye materialy i tehnologii. 2012. №S. S. 7–17.
  2. 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.
  3. Kablov E.N. Razrabotki VIAM dlja gazoturbinnyh dvigatelej i ustanovok [VIAM development for gas turbine engines and systems] //Kryl'ja Rodiny. 2010. №4. S. 31–33.
  4. Kablov E.N., Ospennikova O.G., Bazyleva O.A. Materialy dlja vysokonagruzhennyh detalej gazoturbinnyh dvigatelej [Materials for highly loaded parts of gas turbine engines] //Vestnik MGTU im. N.Je. Baumana. 2011. №SP2. S. 13–19.
  5. Kablov E.N., Gerasimov V.V., Visik E.M., Demonis I.M. Rol' napravlennoj kristallizacii v resursosberegajushhej tehnologii proizvodstva detalej GTD [The role of directional solidification in the resource-saving technology of production of gas-turbine] //Trudy VIAM. 2013. №3. St. 01 (viam-works.ru).
  6. Metallicheskie kompozicionnye materialy [Metal composite materials] /V kn. Istorija aviacionnogo materialovedenija. VIAM – 80 let: gody i ljudi /Pod obshh. red. E.N. Kablova. M.: VIAM. 2012. S. 373–380.
  7. Tarasov Ju.M., Antipov V.V. Novye materialy VIAM − dlja perspektivnoj aviacionnoj tehniki proizvodstva OAO «OAK» [New materials VIAM – for promising aviation equipment produced by OJC «UAC»] //Aviacionnye materialy i tehnologii. 2012. №2. S. 5–6.
  8. Shmotin Ju.N., Starkov R.Ju., Danilov D.V., Ospennikova O.G., Lomberg B.S. Novye materialy dlja perspektivnogo dvigatelja OAO «NPO „Saturn”» [New materials for advanced engine OJC «SPA „Saturn”»] //Aviacionnye materialy i tehnologii. 2012. №2. S. 6–8.
  9. Doroshenko N.I., Chursova L.V. Jevoljucija materialov dlja lopastej vertoletov [Evolution of materials for helicopter blades] //Aviacionnye materialy i tehnologii. 2012. №2. S. 16–18.
  10. Kablov E.N., Shhetanov B.V., Ivahnenko Ju.A., Balinova Ju.A. Perspektivnye armirujushhie vysokotemperaturnye volokna dlja metallicheskih i keramicheskih kompozicionnyh materialov [Promising reinforcing fibers for high temperature metal and ceramic composite materials] //Trudy VIAM. 2013. №2. St. 05 (viam-works.ru).
  11. Kablov E.N. Aviakosmicheskoe materialovedenie [Aerospace materials] //Vse materialy. Jenciklopedicheskij spravochnik. 2008. №3. S. 2–14.
  12. 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 [The development process of directional solidification of gas turbine engine blades with a single-crystal superalloys and composite structure] //Aviacionnye materialy i tehnologii. 2012. №1. S. 3–8.
  13. Belov N.A. Jekonomnolegirovannye zharoprochnye aljuminievye splavy: principy optimizacii fazovogo sostava [Ehkonomnolegirovannye heat-resistant aluminum alloys: principles of optimization phase composition] //Aviacionnye materialy i tehnologii. 2011. №2. S. 6–11.
  14. Kovtunov A.I., Mjamin S.V. Issledovanie tehnologicheskih i mehanicheskih svojstv sloistyh titanoaljuminievyh kompozicionnyh materialov, poluchennyh zhidkofaznym sposobom [Investigation of processing and mechanical properties titanoalyuminievyh layered composite material obtained by the liquid phase method] //Aviacionnye materialy i tehnologii. 2013. №1. S. 9–12.
  15. Kablov E.N., Shhetanov B.V., Grashhenkov D.V., Shavnev A.A., Njafkin A.N. Metallomatrichnye kompozicionnye materialy na osnove Al–SiC [Metal matrix composites based on Al–SiC] //Aviacionnye materialy i tehnologii. 2012. №S. S. 373–380.
  16. Kablov E.N., Chibirkin V.V., Vdovin S.M. Izgotovlenie, svojstva i primenenie teplootvodjashhih osnovanij iz MMK Al–SiC v silovoj jelektronike i preobrazovatel'noj tehnike [Manufacture, properties and applications of heat-removing bases from MMK Al–SiC in power electronics and converter equipment] //Aviacionnye materialy i tehnologii. 2012. №2. S. 20–22.
  17. Pratt and Whitney Composite Rotor Test //Interavia Air Letter. 1973. V. 7. №7881.
  18. Р. 5–6.
  19. Niema I.T., Garett R.A. Eutecnic Bonding of Boron-Aluminum Structural Components //Welding Journal. 1974. V. 53. №4. P. 351–360.
  20. Possibility of Composite Compressor Blades Seen in Germany //Interavia Air Letter. 1975. №8188. Р. 8–9.
  21. Garibotey G.F. Trends in Aerospace Materials //Astronautic and Aeronautics. 1978. V. 16. №7–8. P. 70–81.
  22. Adsit N.R. Composites for Space Application //ASTM Standartisation News. 1984. Dec.
  23. FDL Вegins Aluminum Matrix Composite Structure Program //Light Metal Age. 1981. V. 39. №11. P. 36.
  24. Knoell A.G. Evaluation of Boron-Aluminum Tubes in Compossion //J. Spacecraft and Rockets. 1975. V. 12. №10. Р. 635–637.
  25. Weisinger M.D. Boron-Aluminum Tube Struts for NASA Space Shuttle //Metals Abstracts. 1979. P. 69–72.
  26. Stenger C.G. Keramick als Versterking van meltellen //Metal en Techn. 1986. V. 31. №5. P. 9–12.
  27. Gorshkov L.A., Karimbaev T.D., Nozhnickij Ju.A. Voprosy sozdanija konstrukcij GTD iz KM [Questions to create structures of GTD KM] /V sb. Novye tehnologicheskie processy i nadezhnost' GTD. M.: ONTI VIAM. 1976. Vyp. 3. S. 3–10.
  28. National Research Council Advanced Fibers for High-Temperature Ceramic Composites: Advanced Materials for the Twenty-First Century /In: Nat. Academy Press. Washington D.C. 1998. P. 37–38.
  29. Vienna University of Technology, Institute of Materials Science and Technology. www.mmc-assess.tuwien.ac.at
  30. MMC VIII-Metallic Composites and Foams. London: Royal Society. 2001.
  31. Shalin R.E., Il'chenko V.M. Titanovye splavy v aviacionnom priborostroenii [Titanium alloys in aircraft instrumentation]. http://www.titanmet.ru.
  32. Smarsly W. Aero Engine Materials /In: Seminar, Faculty of Mechanical Engineering, Cracow University of Technology. Poland MTU Aero engines GmbH (2006), http://www.mtu.de/en/technologies/engineering_news.
  33. Miracle D.B. Aeronautical Applications of Metal-Matrix Composites. Air Force Research Laboratory. 2000. P. 1043–1049.
  34. Hemptenmacher J., Schurmann H., Weber K., Peters P.W.M. Gefügeuntersuchungen und mechanische Eigenschaften der SiC (SCS-6) faserverstärkten Titanlegierung Ti–22Al–25Nb. Deutsches Zentrum für Luft- und Raumfahrt, DLR, Institut für Werkstoff-Forschung, Köln; Symposium: Verbundwerkstoffe und Werkstoffverbunde, Kassel. 2005.
  35. NASA TM-2001-211343, NASA Reference Publication. 1361 р.