Correction of the Technological Inheritance in Belt Grinding of Gas-Turbine Engine Blades

The optimal belt grinding conditions for gas-turbine engine blades are determined, and a method of preparing the control program of a CNC machine is created. The goal is to correct the technological inheritance: the error accumulated in the preceding operation. The method is based on controlling the...

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Bibliographic Details
Published in:Russian engineering research 2023-10, Vol.43 (10), p.1249-1253
Main Authors: Volkov, D. I., Koryazhkin, A. A., Kurochkin, A. V., Sutyagin, A. N., Il’in, I. V.
Format: Article
Language:English
Subjects:
Belt grinding
Blades
Engineering
Engineering Design
Error correction
Gas turbine engines
Grinding
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Summary:The optimal belt grinding conditions for gas-turbine engine blades are determined, and a method of preparing the control program of a CNC machine is created. The goal is to correct the technological inheritance: the error accumulated in the preceding operation. The method is based on controlling the rate of metal removal in different sections of the blade profile.
ISSN:1068-798X
1934-8088
DOI:10.3103/S1068798X23100337