Design of test Platform for Robot Drilling and Cutting Force Simulation

DOI

10.2991/icmii-15.2015.57How to use a DOI?

Keywords

End-effector; dynamic simulation; cutting force; drilling vibrations; robots.

Abstract

In view of the requirements of aircraft parts automatic drilling processing, based on the analysis of the working process of the automatic drilling end-effector, through the steady-state design and the system structure modeling with CATIA, design a set of testing, drilling, pressure riveting, suck crumbs as one of the compound system of drilling end-effector. For building the structure design, virtual assembly and motion simulation for the integration of 3D virtual platform, it can realize the motion simulation of the multiple working procedures in the drilling operation. Adopted the large dynamic simulation software ADAMS and ABAQUS to analyze the cutting mechanism of robot drilling, the influence factors of the cutting force and clamping force of the robot are analyzed in the simulation, theoretical analysis of the accuracy error of process parameters to reduce the range of the robot system drilling. Finite element simulation study showed that dynamics simulation calculation can effectively solve the problem of process parameters settings for the robot system distributed, to provide theoretical reference for improving the drilling efficiency and assembly quality of aircraft components.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Ying Xu
AU  - Renbin He
AU  - Jianqiang Chen
AU  - Benshuang Zhang
AU  - Zhaolei Li
AU  - Yanyu Deng
PY  - 2015/10
DA  - 2015/10
TI  - Design of test Platform for Robot Drilling and Cutting Force Simulation
BT  - Proceedings of the 3rd International Conference on Mechatronics and Industrial Informatics
PB  - Atlantis Press
SP  - 319
EP  - 323
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmii-15.2015.57
DO  - 10.2991/icmii-15.2015.57
ID  - Xu2015/10
ER  -