FIELD: turbines.
SUBSTANCE: present invention relates to a method for repairment of section (22) of an end part of turbine blade (10), having a structural defect. The method includes areas of a damaged section with a structural defect at section (22) of the end part and provision of pre-sintered mold (60) including first section (62) with the first composition and second section (64) with the second composition. Pre-sintered mold (60) is configured for coupling with an upper surface of a remained section of turbine blade (10). Pre-sintered mold (60) contains superalloy material and solder material, and it is subjected to a soldering process to melt solder material and fill the structural defect. First section (62) can be a bandage shelf of an end part of the blade, and second section (64) can be a section with whistling profiling. Boron is used in solder material to decrease a temperature, at which soldering is performed.
EFFECT: elimination of the need for welding repairment and elimination of the need for excessive heat treatment, need for qualified welders, and cracks in an area of heat impact.
18 cl, 5 dwg
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Authors
Dates
2022-12-02—Published
2019-03-29—Filed