Conceptual Design and Performance Evaluation of a Hybrid Flexible Manufacturing System for Large Scale Aeronautic Components

被引:0
|
作者
Zhang J. [1 ]
Tang T. [1 ]
Fang H. [1 ]
机构
[1] School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou
关键词
Circumferential guideway; Flexible manufacturing system; Parallel kinematic machine; Workspace;
D O I
10.7652/xjtuxb201901001
中图分类号
学科分类号
摘要
To realize efficient manufacturing and quick assembling of the arc-shaped aeronautic structural component with large scale, a hybrid flexible manufacturing system consisting of a double circumferential guideway and two parallel kinematic machine (PKM) modules is proposed. A conceptual design of the flexible manufacturing system is carried out with the virtual prototype technology, a kinematic model is established to conduct an inverse kinematic description, and the singularity of the PKM is analyzed. Then the reachable workspace of the system is predicted by using a 'sliced partition' searching algorithm, and an elasto-static model is developed to calculate the gravity-caused elastic displacements of the system by the substructure synthesis technique. The results are validated by numerical simulations on ANSYS Workbench. An index of average displacement is suggested to evaluate the influence of configuration parameter on the system elasto-static performance throughout the entire reachable workspace. The investigations manifest that the flexible manufacturing system claims the merits of a large workspace generated by the serial mechanism and high rigidity and loading capacity coming from the PKM module. The gravity-caused structural deformations must be paid enough attentions during the design stage of the flexible manufacturing system. Additionally, to facilitate its applications, the designers must enhance the bending resistance along x-direction and torsion resistance about y-direction of the hybrid flexible manufacturing system. © 2019, Editorial Office of Journal of Xi'an Jiaotong University. All right reserved.
引用
收藏
页码:1 / 10
页数:9
相关论文
共 19 条
  • [1] Shang M., Butterfield J., Armstrong C., Et al., A flexible fixture for aircraft wing assembly based on a parallel kinematic machine (Exechon), SAE International Journal of Aerospace, 4, 2, pp. 839-849, (2011)
  • [2] Summers M., Robot capability test and development of industrial robot positioning system for the aerospace industry, Journal of the Egyptian Medical Association, 5-6, pp. 121-124, (2005)
  • [3] Xu G., Automatic assembly technology for large aircraft, Acta Aeronautica et Astronautica Sinica, 29, 3, pp. 734-740, (2008)
  • [4] Eguti C.C.A., Trabasso L.G., Design of a robotic orbital driller for assembling aircraft structures, Mechatronics, 24, 5, pp. 533-545, (2014)
  • [5] He X., Tian W., Zeng Y., Et al., Robot positioning error and residual error compensation for aircraft assembly, Acta Aeronautica et Astronautica Sinica, 38, 4, pp. 287-297, (2017)
  • [6] Wang H., Shen J., Tian W., Et al., Design and implementation of robot flexible drilling control system, Journal of Nanjing University of Aeronautics & Astronautics, 44, pp. 65-68, (2012)
  • [7] Hennes N., Staimer D., Application of PKM in aerospace manufacturing-high performance machining centers ECOSPEED, ECOSPEED-F and ECOLINER, Proceedings of the 4th Chemnitz Parallel Kinematics Seminar, pp. 557-577, (2004)
  • [8] Neumann K.E., Tricept applications, Proceedings of the 3rd Chemnitz Parallel Kinematics Seminar, pp. 547-551, (2002)
  • [9] Neumann K.E., Exechon parallel kinematics, simplified machining and assembly: SAE Technical Paper 2009-01-3092, (2009)
  • [10] Zhang J., Zhao Y.Q., Ceccarelli M., Elastodynamic model-based vibration characteristics prediction of a three prismatic-revolute-spherical parallel kinematic machine, ASME Journal of Dynamic Systems, Measurement, and Control, 138, 4, (2016)