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Dynamics Modelling and Simulating of Ultra-precision Fly-Cutting Machine Tool

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Abstract

Dynamics modelling and simulating are the significant process to improve the machining accuracy of the machine tool. This paper is aimed to model and simulate the ultra-precision fly-cutting machine tool (UFMT) and find the relations between structure parameters and machined surface. In this paper, the multi-rigid-flexible-body dynamics model of the UFMT is firstly built by using transfer matrix method for multibody systems. After deducing overall transfer equation, overall transfer matrix, eigenfrequency equation and dynamics equations, the vibration characteristics and dynamics response of tool-tip are simulated and validated by tests. The machined surface is simulated by transferring displacement between the fly-cutting tool-tip and the workpiece into 3D curve. According to the simulation results, both the air-bearing stiffness of the flying-cutting head and cutting process parameters have effects on the machined surface.

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Abbreviations

\( {\varvec{Z}}_{i,j} \) :

State vector in modal coordinates

\( {\varvec{z}}_{i,j} \) :

State vector in physical coordinates

\( x,y,z \) :

Translational displacement in x, y, z physics coordinate

\( X,Y,Z \) :

Translational displacement in x, y, z modal coordinate

\( \theta_{x} ,\theta_{y} ,\theta_{z} \) :

Angular displacement in x, y, z physics coordinate

\( \Theta_{x} ,\Theta_{y} ,\Theta_{z} \) :

Angular displacement in x, y, z modal coordinate

\( m_{x} ,m_{y} ,m_{z} \) :

Internal torque in x, y, z physics coordinate

\( M_{x} ,M_{y} ,M_{z} \) :

Internal torque in x, y, z modal coordinate

\( q_{x} ,q_{y} ,q_{z} \) :

Internal force in x, y, z physics coordinate

\( Q_{x} ,Q_{y} ,Q_{z} \) :

Internal force in x, y, z modal coordinate

\( {\varvec{U}}_{\text{all}} \) :

Overall transfer matrix

\( {\varvec{Z}}_{\text{all}} \) :

Overall state vector

\( {\varvec{T}} \) :

Successive premultiplication of the transfer matrix of each element in the transfer paths from each tip to the root of the system

\( {\varvec{G}} \) :

Successive premultiplication of the transfer matrix of each element in the transfer path from each tip to the k-th input end Ik of each body element which has multiple input ends

\( {\varvec{v}} \) :

The translational and angular displacement column matrix

\( {\varvec{M}},{\varvec{K}},{\varvec{C}} \) :

The mass, spring forces and damping forces matrix

\( {\varvec{f}} \) :

The column matrix of external forces torques

\( {\varvec{V}}^{k} \) :

Augmented eigenvector of k-order mode

\( q^{k} \) :

Generalized coordinate for k-order mode

\( \omega_{s} \) :

Natural frequency of s-order mode

\( \zeta_{s} \) :

Damping proportion of s-order mode

\( f_{z} \) :

The angular velocity of the spindle

R :

The radius of the fly-cutting head

\( z_{re} \) :

Relative displacements between the fly-cutting tool-tip and the workpiece surface in z-direction

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Acknowledgements

The research was supported by Science Challenge Project (No. TZ2016006-0104).

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Correspondence to Xiaoting Rui.

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Lu, H., Ding, Y., Chang, Y. et al. Dynamics Modelling and Simulating of Ultra-precision Fly-Cutting Machine Tool. Int. J. Precis. Eng. Manuf. 21, 189–202 (2020). https://doi.org/10.1007/s12541-019-00239-1

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