Abstract
The finishing of the flow sections of compressor blades is considered. A sequence of operations for this purpose in an automated cycle is proposed. The development of control programs for the grinding of flow sections of the blades is discussed, with allowance for the nonuniform distribution of the margin over the blade surface.
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Poletaev, V.A., Tekhnologiya avtomatizirovannogo proizvodstva lopatok gazoturbinnykh dvigatelei (Technology of Automated Production of the Blades of Gas Turbine Engines), Moscow: Mashinostroenie, 2006.
Poletaev, V.A., Mikhryutin, V.V., and Koryazhkin, A.A., Belt grinding of large blades of gas turbine engines on CNC machines, Spravochnik. Inzh. Zh., 2005, no. 12, pp. 10–15.
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Translated by Bernard Gilbert
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Poletaev, V.A., Volkov, D.I. Automated Belt Grinding of Axial-Compressor Blades in Gas-Turbine Engines. Russ. Engin. Res. 39, 594–597 (2019). https://doi.org/10.3103/S1068798X19070177
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DOI: https://doi.org/10.3103/S1068798X19070177