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(2018)
Effect of thermomechanical and heat treatment on the structure and properties of VZh177 alloy
(2010)
The new heat-resistant nickel alloy for gas turbine engines (GTE) and gas turbine devices (GTD), Materialovedenie
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Creation of modern heat - resistant materials and production technologies for aircraft engine building
(2010)
The new heat - resistant nickel alloy for gas turbine engines ( GTE ) and gas turbine devices ( GTD )
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Creation of modern heat-resistant materials and production technologies for aircraft engine building, Kryl’ya Rodiny
Strategy of development of special high - temperature alloys and steels , protective and thermal protective coatings , in 80 let
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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»Aviation Materials and Technologies
(2012)
Strategy of development of special high-temperature alloys and steels, protective and thermal protective coatings
O.G. Ospennikova (2012)
Strategy of development of special high-temperature alloys and steels, protective and thermal protective coatings, in 80 let. Aviatsionnye materialy i tekhnologii (The 80 Years—Aviation Materials and Technologies)
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Composition optimization of heatresistant nickel alloys, Aviats
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Calculation of the high-temperature strength of complexly alloyed nickel alloys using equations of the system of nonpolarized ionic radiiMetal Science and Heat Treatment, 37
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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,
E.V. Prikhod’ko (1984)
Zharoprochnye i zharostoikie stali na nikelevoi osnove (Heat Resistant Nickel-Based Steels and Alloys)
A. Buiakina, M. Letnikov, M. Bakradze, S. Shugaev (2016)
The effect of thermomechanical and heat treatment parameters on structure and mechanical properties of superalloy VZH177
Abstract—The results of development of new nickel-base superalloy having an operating temperature up to 800°C for gas turbine disks have been presented. Structures, mechanical properties, and phase transformations of six experimental compositions have been researched. Physical and chemical modeling has been used to make a right choice of an alloy; with parameters as composition equivalents (they were based on equations of nonpolarizing ionic radii). The highest level of strength, ductility, toughness, and heat resistance was exhibited at 750°C by the Ni–Co–Cr–W–Mo–Ta–Al–Ti–Nb experimental composition with the total of aluminum, titanium, and niobium equal to 10 wt % and containing 4 wt % of tantalum.
Inorganic Materials: Applied Research – Springer Journals
Published: Feb 7, 2019
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