Mechanics Model and Machining Distortion Analysis for High Speed Milling of Titanium Alloy Aircraft Monolithic Component

Yong Yang; Chang He Li; Fa Zhan Yang

doi:10.4028/www.scientific.net/AMM.29-32.354

Paper Titles

Influence of Different Sliding Velocity on the Thermo-Mechanical Coupling of the Rough Surface Contact
p.332

Nodal Evolutionary Computation Enhanced Level Set Algorithm for Structural Topology Optimization
p.337

Hierarchical ANFIS Identification of Magneto-Rheological Dampers
p.343

The Research on Software of the Temperature Control of Motor Speed System
p.349

Mechanics Model and Machining Distortion Analysis for High Speed Milling of Titanium Alloy Aircraft Monolithic Component
p.354

Mechanics Modeling and Three-Dimensional Finite Element Simulating for High Speed Milling of Titanium Alloy
p.360

Study on “Single Factor” Material Model Used in Finite Element Simulation of High Speed Cutting of Mo-Cr Cast Iron
p.365

Study on one Special-Shaped Long-Span Arch Bridge Using Wind Tunnel Test
p.370

Comparative Analysis on Aerostatic Coefficients of Bridge Deck Based on Wind Tunnel Test
p.377

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 29-32Mechanics Model and Machining Distortion Analysis...

Mechanics Model and Machining Distortion Analysis for High Speed Milling of Titanium Alloy Aircraft Monolithic Component

Abstract:

A physics-based material processing simulation is approached to research the machining distortion for high speed milling of titanium alloy aircraft monolithic component by the finite element method (FEM). Several mechanics models, such as material constitutive model, material removal model, and cutting loads application model, have been implemented to improve the accuracy of finite element simulation. The distortion result of aircraft monolithic component resulting from FEM show a good agreement with the experiment result. The research result shows that the distortion law of titanium alloy aircraft monolithic component is bending distortion and protruding upward, and the maximum distortion dimension lies in the middle of monolithic component.