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High-Temperature Cermet Material Based on Intermetallic Nickel Matrix

  • MATERIALS FOR AVIATION AND SPACE TECHNOLOGIES
  • Published:
Inorganic Materials: Applied Research Aims and scope

Abstract

A method for synthesis of an intermetallic nickel matrix reinforced with particles of different refractory compounds added at different concentrations is considered. Prepared materials are based on two variants of a Ni3Al–Cr–W–Mo–Ti–Hf alloy: type VKNA-1V alloy and type VKNA-1V alloy with increased tungsten content (VKNA-1V(W)). The intermetallic matrix is reinforced with nanoparticles of the oxides Al2O3, Al2O3 ⋅ Y2O3, and Al2O3 ⋅ Y2O3 ⋅ HfO2, with the content of reinforcing component at 2 and 5 vol %. Samples are compacted by spark plasma sintering. The microstructure of prepared cermet materials (CMs) is investigated using scanning electron microscopy. The impact viscosity and flexural strength are determined. We establish the effect that the content and composition of the reinforcing component has on the physicomechanical properties of the high-temperature CMs based on an intermetallic matrix dispersion-hardened with refractory metal particles. Our findings show that the optimal combination of flexural strength and impact viscosity at room temperature is achieved in the CM sample in which the intermetallic matrix is based on VKNA-1V(W) alloy and the reinforcing component is represented by ternary oxide Al2O3 ⋅ Y2O3 ⋅ HfO2 added at a concentration of 2%.

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REFERENCES

  1. Kablov, E.N., Innovative developments of the All-Russian Scientific Research Institute of Aviation Materials within the project “Strategic development of materials and technologies of their recycling until 2030,” Aviats. Mater. Tekhnol., 2015, no. 1, pp. 3–33. https://doi.org/10.18577/2071-9140-2015-0-1-3-33

  2. Kablov, E.N., Strategic development of the materials and technologies for their recycling until 2030, Aviats. Mater. Tekhnol., 2012, suppl., pp. 7–17.

  3. Kablov, E.N., Lomberg, B.S., and Ospennikova, O.G., Creation of modern heat-resistant materials and production technologies for aircraft engine building, Kryl’ya Rodiny, 2012, nos. 3–4, pp. 34–38.

  4. Ospennikova, O.G., The development strategy of heat-resistant alloys and special steel, protective and thermal-proof coatings, Aviats. Mater. Tekhnol., 2012, suppl., pp. 19–36.

  5. Kablov, E.N., Petrushin, N.V., Svetlov, I.L., and Demonis, I.M., Ni-based casting superalloys of the new generation, Aviats. Mater. Tekhnol., 2012, suppl., pp. 36–52.

  6. Kablov, E.N. and Toloraiya, V.N., The All-Russian Scientific Research Institute of Aviation Materials is a pioneer in the national technology of casting of monocrystalline turbine blades for gas-turbine engines and devices, Aviats. Mater. Tekhnol., 2012, suppl., pp. 105–117.

  7. Grinberg, B.A. and Ivanov, M.A., Intermetallidy Ni3Al i TiAl: mikrostruktura, deformatsionnoe povedenie (Ni3Al and TiAl Intermetallics: Microstructure and Deformation Properties), Yekaterinburg: Ural. Otd., Ross. Akad. Nauk, 2002.

  8. Povarova, K.B., Kazanskaya, N.K., Drozdov, A.A., and Morozov, A.E., Physicochemical laws of the interaction of nickel aluminides with alloying elements: II. Interaction of nickel aluminides with alloying elements and/or interstitial phases, Russ. Metall. (Engl. Transl.), 2007, vol. 2007, no. 5, pp. 380–386.

  9. Povarova, K.B., Bannykh, O.A., Kazanskaya, N.K., and Antonova, A.V., Heat-resistant composites with a metal or intermetallic matrix, strengthened by particles or fibers of oxides, borides, carbides, Metally, 2001, no. 5, pp. 68–78.

  10. Bolshakova, A.N., Efimochkin, I.Yu., and Basargin, O.V., Laboratory high-temperature test for four-point bending of composite material samples based on metal-ceramic matrix, Vse Mater., 2017, no. 4, pp. 50–52.

  11. Basargin, O.V., Kolyshev, S.G., Shchetanov, B.V., and Shcheglova, T.M., Some features of high-temperature bend tests of Nb-based CM specimens, Tr. Vseross. Nauchno-Issled. Inst. Aviats. Mater., 2015, no. 5, pp. 11–19. http://www.viam-works.ru/ru/articles?art_id=818. https://doi.org/10.18577/2307-6046-2015-0-5-11-11

  12. Sidorov, V.V., Kablov, D.E., and Rigin, V.E., Metallurgiya liteynykh zharoprochnykh splavov: tekhnologiya i oborudovanie (Metallurgy of Casted Heat-Resistant Alloys), Moscow: Vseross. Nauchno-Issled. Inst. Aviats. Mater., 2016.

  13. Bazyleva, O.A., Buntushkin, V.P., Kablov, E.N., and Sidorov, V.V., RF Patent 2349663, Byull. Izobret., 2009, no. 8.

  14. Bazyleva, O.A., Buntushkin, V.P., Bondarenko, Yu.A., Morozova, G.I., et al., RF Patent 1607422, 2001.

  15. Morozova, G.I., Compensation of imbalance of alloying of refractory nickel alloys, Met. Sci. Heat Treat., 2013, vol. 54, nos. 11–12, pp. 667–671.

  16. Karachevtsev, F.N., Letov, A.F., Protsenko, O.M., and Yakimova, M.S., Development and application of certified reference materials of airborne advanced alloys, Tr. Vseross. Nauchno-Issled. Inst. Aviats. Mater., 2016, no. 10 (46), p. 8. http://www.viam-works.ru.

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Funding

This work was carried out within complex scientific discipline 12: Metal Matrix and Hybrid Composite Materials (“Strategic Areas in the Development of Materials and Technologies for their Recycling to 2030”) [1, 2].

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Correspondence to I. Yu. Efimochkin, E. G. Arginbayeva or A. N. Bolshakova.

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Translated by A. Kukharuk

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Efimochkin, I.Y., Bazyleva, O.A., Arginbayeva, E.G. et al. High-Temperature Cermet Material Based on Intermetallic Nickel Matrix. Inorg. Mater. Appl. Res. 11, 297–303 (2020). https://doi.org/10.1134/S2075113320020094

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  • DOI: https://doi.org/10.1134/S2075113320020094

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