ZHANG Xiandong1, BU Kun1, LIU Lianxi2, DOU Yangliu1. Comparison of Bending and Torsion Deformation Algorithms for Ceramic Core of Hollow Turbine Blade. Aeronautical Manufacturing Technology, 2016, 59(21): 63-68.
ZHANG Xiandong1, BU Kun1, LIU Lianxi2, DOU Yangliu1. Comparison of Bending and Torsion Deformation Algorithms for Ceramic Core of Hollow Turbine Blade. Aeronautical Manufacturing Technology, 2016, 59(21): 63-68. DOI: 10.16080/j.issn1671-833x.2016.21.063.
Ceramic core is used to form the cooling channel of hollow turbine blade in investment casting process. The bending and torsion deformations of ceramic core have direct influence on the wall thickness dimension accuracy of turbine blade. To study bending and torsion deformation of ceramic core generating in manufacturing process
firstly
based on the definition of bending and torsion deformations for airfoil and the structure characteristics of ceramic core
the algorithms for computing bending and torsion deformations of ceramic core are studied
including contour-based methods: Snake-model
spline-fitting method and point-based methods: Convex-hull
2D-registration
distance-weight method. Secondly
through computing a simulated known bending and twist deformation
these five methods are compared. The comparing results indicate that the accuracy and stability of spline-fitting method is better than other methods.