Prospects for the domestic production of large-sized cast blades and vanes for industrial gas turbines


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Abstract

Russian experience in the production of large-sized cast blades and vanes for industrial gas turbines is analyzed for the past decades. It is noted that the production of small- and medium-sized blades and vanes made of Russian alloys using technologies for aviation, marine, and gas-pumping turbines cannot be scaled for industrial gas turbines. It is shown that, in order to provide manufacturability under large-scale casting from domestic nickel alloys, it is necessary to solve complex problems in changing their chemical composition, to develop new casting technologies and to optimize the heat treatment modes. An experience of PAO NPO Saturn in manufacturing the blades and vanes made of ChS88U-VI and IN738-LC foundry nickel alloys for the turbines of the GTE-110 gas turbine unit is considered in detail. Potentialities for achieving adopted target parameters for the mechanical properties of working blades cast from ChS88UM-VI modified alloy are established. For the blades made of IN738-LC alloy manufactured using the existing foundry technology, a complete compliance with the requirements of normative and technical documentation has been established. Currently, in Russia, the basis of the fleet of gas turbine plants is composed by foreign turbines, and, for the implementation of the import substitution program, one can use the positive experience of PAO NPO Saturn in casting blades from IN738-LC alloy based on a reverse engineering technique. A preliminary complex of studies of the original manufacturer’s blades should be carried out, involving, first of all, the determination of geometric size using modern measurement methods as well as the studies on the chemical compositions of the used materials (base metal and protective coatings). Further, verifying the constructed calculation models based on the obtained data, one could choose available domestic materials that would meet the operating conditions of the blades according to their heat resistance and corrosion resistance.

About the authors

D. A. Kazanskiy

All Russia Thermal Engineering Institute

Author for correspondence.
Email: d.a.kazanskiy@gmail.com
Russian Federation, Moscow, 115280

E. A. Grin

All Russia Thermal Engineering Institute

Email: d.a.kazanskiy@gmail.com
Russian Federation, Moscow, 115280

A. N. Klimov

Gas Turbine Technologies Engineering Center

Email: d.a.kazanskiy@gmail.com
Russian Federation, Moscow, 115280

A. I. Berestevich

PAO NPO Saturn

Email: d.a.kazanskiy@gmail.com
Russian Federation, Rybinsk, Yaroslavl oblast, 152903


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