| International Journal of Advanced Robotic Systems | |
| Mechanical performance research of friction stir welding robot for aerospace applications | |
| article | |
| Haitao Luo1  Fengqun Zhao3  Siwei Guo4  Changshuai Yu1  Guangming Liu1  Tingke Wu4  | |
| [1] State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences;Department of Space Automation Technology and Systems, Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences;School of Mechanical Engineering, Shenyang Ligong University;Institute of Mechanical Engineering and Automation, Northeastern University | |
| 关键词: Friction stir welding; welding robot; typical working conditions; load analysis; boundary conditions; | |
| DOI : 10.1177/1729881421996543 | |
| 学科分类:社会科学、人文和艺术(综合) | |
| 来源: InTech | |
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【 摘 要 】
The friction stir welding robot for aerospace applications developed by the research group is subject to the effects of size, working conditions, and other conditions during the operation. The load conditions of the friction stir welding robot are harsh, and the strength and stiffness tests of the whole machine need to be carried out. Five typical working conditions of the friction stir welding robot are analyzed. By analyzing the system composition and configuration of the robot, the loading conditions of the robot stirring head during the welding process are accurately simulated, and this is used as the stiffness and strength check. The boundary conditions of the robot are simulated and analyzed under typical working conditions. The results show that the data of each part of the robot under load are obtained for a given size of the rocket cap welding. After analysis, the maximum normal displacement of the friction stir welding robot reached 0.6424 mm and the maximum stress was 79.21 MPa under the condition of melon flap welding.
【 授权许可】
CC BY
【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| RO202108130004903ZK.pdf | 1458KB |
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