SURFACE LAYER QUALITY IN COMPRESSOR TITANIUM BLADES AT MULTIAXES DEEP GRINDING
Authors:
1.
Soloviev Rybinsk State Aviation Technical University
(Rector’s advisor)
Rybinsk, Yaroslavl, Russian Federation
Rybinsk, Yaroslavl, Russian Federation
2.
PC “SPC ”Saturn”
(kandidat tehnicheskih nauk)
employee
Yaroslavl, Russian Federation
employee
Yaroslavl, Russian Federation
Type:
Article
Pages:
from 15
to 19
Status:
Published
Received:
09.12.2017
Accepted:
13.12.2017
Published:
13.12.2017
Subject area:
UDK 62 Инженерное дело. Техника в целом. Транспорт
Language:
English
Keywords:
deep grinding; compressor blades; residual stresses; titanium alloys
Abstract (English):
The investigation results of technological conditions impact at multiaxes deep grinding upon quality of titanium alloy blade surface layer in the compressors of gas turbine engines (GTE) are presented. The grinding mode impact upon a surface and a value of residual stresses in a surface layer of blades is defined and also conditions for defect occurrence as burns on blade surfaces under machining are detected.
The investigation results of technological conditions impact at multiaxes deep grinding upon quality of titanium alloy blade surface layer in the compressors of gas turbine engines (GTE) are presented. The grinding mode impact upon a surface and a value of residual stresses in a surface layer of blades is defined and also conditions for defect occurrence as burns on blade surfaces under machining are detected.
Keywords:
deep grinding; compressor blades; residual stresses; titanium alloys
deep grinding; compressor blades; residual stresses; titanium alloys
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3. Poletaev, V.A., Volkov, D.I. Turbine Blade Deep Grinding: Technologist’s Library. - M.: Mechanical Engineering, 2009. - pp. 272.
