Avtomaticheskaya Svarka (Automatic Welding), #4, 2022, pp. 41-49
Analysis of modern experience in development of sealing coatings for parts of gas turbine engines (Review)
Yu.S. Borysov, N.V. Vihilianska, O.M. Burlachenko, L.P. Olevska, V.M. Lopata
E.O. Paton Electric Welding Institute of the NAS of Ukraine.
11 Kazymyr Malevych Str., 03150, Kyiv, Ukraine. E-mail: office@paton.kiev.ua
In the work the experience in development of sealing thermal coatings for parts of gas turbine engines was analyzed. It was
found that the task of development of compositions and technologies of thermal spraying of sealing coatings intended to provide
the optimal radial gap between the elements of the stator and the rotor in order to reduce the consumption of technological
fuel and to increase the efficiency coefficient of engines, is relevant. The principles of optimization of the composition of the
material of the sealing coating were described. They consist mainly in combination of ease of fitting blades into the coating
with resistance to erosion wear, which provides the operation efficiency of the coating with its long life. The temperature modes
of operation of sealing coatings in different sections of a gas turbine engine were determined. For spraying of sealing coatings
applying thermal methods, composite powders are used, the composition of which corresponds to the concept purpose – solid
grease. As a metal component, Ni, AlSI, Ni- and Co-alloys are used and as a solid grease, graphite, hexagonal boron nitride,
betonite and polyester are used. For high-temperature sections of turbines, a combination of a stabilized zirconium oxide with
hexagonal boron nitride and polyester are used. The composition of these combinations determines the temperature zone of
their use related to the working conditions of the compressor or turbine. 29 Ref., 13 Fig.
Keywords: sealing coating, thermal spraying, matrix, solid grease, abrasion, erosion resistance, compressor, turbine
Received: 30.03.2022
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