This paper deals with the development of a new mathematical model that characterizes the structure-process interaction for a complex milling system. The structure is divided into a work piece and a machine part, which are represented by different models. While the machine dynamics is characterized by a standard multi-body system, the work piece is described as a linear thermo-elastic continuum. The coupling of both parts is carried out by an empirical process model permitting an estimate of heat and coupling forces occurring during milling. This work reports the derivation of the governing equations emphasizing the coupling and summarizes the numerical algorithms being applied to solve the coupled equation system. The results of numerical s...
AbstractThin-walled components, i.e. fuselage frames of airplanes, are prone to an unstable process ...
This article presents an overview of current simulation methods describing the interaction of grindi...
Thin-walled components, i.e. fuselage frames of airplanes, are prone to an unstable process behavior...
This paper deals with the development of a new mathematical model that characterizes the structure-p...
This paper deals with a new mathematical model to characterize the interaction between machine and ...
This paper deals with a new mathematical model to characterise the interaction between machine and ...
AbstractIn the machining of large structural components such as those used in the construction of ai...
AbstractDuring the finishing milling process of thin-walled workpieces, deformations occur due to th...
Controlling the thermo-elastic behavior of tooling machines can only be achieved by systematic analy...
The article is focused on the thermal behaviour of a spindle of a milling centre. This is a typical ...
AbstractDuring roughing in NC milling, heat is introduced into the workpiece. For the manufacturing ...
In high-speed dry milling of thin-walled parts, the cutter-workpiece temperature rises asymptoticall...
This paper presents a method for a NC-Simulation based prediction of shape errors caused by thermal ...
In practice, different cutting processes are encountered, each process having different characterist...
AbstractBased on the method of adaptive finite elements (FEM) a correction approach has been conside...
AbstractThin-walled components, i.e. fuselage frames of airplanes, are prone to an unstable process ...
This article presents an overview of current simulation methods describing the interaction of grindi...
Thin-walled components, i.e. fuselage frames of airplanes, are prone to an unstable process behavior...
This paper deals with the development of a new mathematical model that characterizes the structure-p...
This paper deals with a new mathematical model to characterize the interaction between machine and ...
This paper deals with a new mathematical model to characterise the interaction between machine and ...
AbstractIn the machining of large structural components such as those used in the construction of ai...
AbstractDuring the finishing milling process of thin-walled workpieces, deformations occur due to th...
Controlling the thermo-elastic behavior of tooling machines can only be achieved by systematic analy...
The article is focused on the thermal behaviour of a spindle of a milling centre. This is a typical ...
AbstractDuring roughing in NC milling, heat is introduced into the workpiece. For the manufacturing ...
In high-speed dry milling of thin-walled parts, the cutter-workpiece temperature rises asymptoticall...
This paper presents a method for a NC-Simulation based prediction of shape errors caused by thermal ...
In practice, different cutting processes are encountered, each process having different characterist...
AbstractBased on the method of adaptive finite elements (FEM) a correction approach has been conside...
AbstractThin-walled components, i.e. fuselage frames of airplanes, are prone to an unstable process ...
This article presents an overview of current simulation methods describing the interaction of grindi...
Thin-walled components, i.e. fuselage frames of airplanes, are prone to an unstable process behavior...