Email this article Development and research of a rhenium-free high-temperature nickel superalloy for the turbine rotor blades in aviation GTE
- Authors: Shmotin Y.N.1, Logunov A.V.1, Leshchenko I.A.1, Danilov D.V.1
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Affiliations:
- OAO NPO SATURN
- Issue: Vol 2016, No 13 (2016)
- Pages: 1214-1220
- Section: Processes of Manufacture of Ferrous and Nonferrous Metals
- URL: https://journals.rcsi.science/0036-0295/article/view/171114
- DOI: https://doi.org/10.1134/S0036029516130188
- ID: 171114
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Abstract
The studies directed on designing an advanced rhenium-free nickel superalloy, which is an analog of ZhS32VI alloy, are performed. The chemical composition of the alloy has been found and an experimental alloy batch has been melted (10 kg). Microstructural and metallographic studies and strength tests are carried out. The new single-crystal superalloy has a long-term strength σ1000100= 238–248 MPa at a density of 8.87 g/cm3.
About the authors
Yu. N. Shmotin
OAO NPO SATURN
Email: vladimir.pavlov@npo-saturn.ru
Russian Federation, pr. Lenina 163, Rybinsk, Yaroslavl’ oblast, 152903
A. V. Logunov
OAO NPO SATURN
Author for correspondence.
Email: vladimir.pavlov@npo-saturn.ru
Russian Federation, pr. Lenina 163, Rybinsk, Yaroslavl’ oblast, 152903
I. A. Leshchenko
OAO NPO SATURN
Email: vladimir.pavlov@npo-saturn.ru
Russian Federation, pr. Lenina 163, Rybinsk, Yaroslavl’ oblast, 152903
D. V. Danilov
OAO NPO SATURN
Email: vladimir.pavlov@npo-saturn.ru
Russian Federation, pr. Lenina 163, Rybinsk, Yaroslavl’ oblast, 152903
