28 September 2016 The FEM simulation of the thin walled aircraft engine corpus deformation during milling
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Proceedings Volume 10031, Photonics Applications in Astronomy, Communications, Industry, and High-Energy Physics Experiments 2016; 100310B (2016) https://doi.org/10.1117/12.2249048
Event: Photonics Applications in Astronomy, Communications, Industry, and High-Energy Physics Experiments 2016, 2016, Wilga, Poland
Abstract
This paper discusses the results of the experimental research performed with the support of finite element method. The deformation of the thin walled aircraft engine corpus was analyzed based on a geometric model. Then, the boundary of the outer side of the part was loaded by the components of a cutting force during milling. The material model of the part was also defined in the simulation software. The analysis allowed to optimize feed rate in order to decrease the deformation of the part.
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A. Matras, A. Matras, M. Plaza, M. Plaza, } "The FEM simulation of the thin walled aircraft engine corpus deformation during milling ", Proc. SPIE 10031, Photonics Applications in Astronomy, Communications, Industry, and High-Energy Physics Experiments 2016, 100310B (28 September 2016); doi: 10.1117/12.2249048; https://doi.org/10.1117/12.2249048
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