A non-contact calibration method of workpiece coordinate system for aero-engine blade-robotic grinding system

被引:0
|
作者
Chen, Ziyang [1 ]
Cai, Zhenhua [1 ]
Chen, Tingyang [2 ]
Deng, Chunming [3 ]
Niu, Shaopeng [3 ]
Wang, Chao [3 ]
Qu, Dongbo [1 ]
Ma, Zhenhua [1 ]
Hu, Yu [1 ]
机构
[1] Wuhan Univ Technol, Sch Automat, 122 Luoshi Rd, Wuhan 430070, Hubei, Peoples R China
[2] Wuhan Univ Technol, State Key Lab Silicate Mat Architectures, Wuhan, Peoples R China
[3] Guangdong Acad Sci, Inst New Mat, Guangzhou, Peoples R China
关键词
Workpiece calibration; aero-engine blade; robot grinding; hand-eye calibration; point cloud registration;
D O I
10.1177/09544054251315506
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Mounting error of the blade is an important factor that affects the grinding quality in aero-engine blade-robotic grinding system. In order to compensate for the mounting error, it is necessary to calibrate the pose of the workpiece coordinate system. However, most of the current workpiece calibration methods cannot meet the high accuracy requirements in the scenario of aero-engine blade grinding. Therefore, this paper proposes a new non-contact calibration method of workpiece coordinate system using scanner measurement, to solve the workpiece calibration problem in aero-engine blade-robotic grinding system. The method first calibrates the scanner based on the criterion sphere hand-eye calibration method and employs the Random Sample Consensus (RANSAC) algorithm to ensure the accuracy of the fitted sphere center coordinates. Then, the point cloud registration algorithms are used to align the scanned point cloud of the blade with the model point cloud. Finally, the space transformation matrix between the workpiece coordinate system and the base coordinate system is obtained through matrix calculation, achieving the accurate calibration of the workpiece coordinate system. The experimental validation of the proposed calibration method in this paper can maintain tiny and acceptable errors for grinding applications. Specifically, the hand-eye calibration error is less than 0.2 mm, and the point cloud registration error is less than 0.06 mm. Moreover, the calibrated blade exhibits excellent machining consistency after grinding, which can perfectly meet the requirements of actual machining accuracy.
引用
收藏
页数:13
相关论文
共 50 条
  • [41] An improved dynamic load-strength interference model for the reliability analysis of aero-engine rotor blade system
    Zhao, Bingfeng
    Xie, Liyang
    Zhang, Yu
    Ren, Jungang
    Bai, Xin
    Qin, Bo
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2021, 235 (11) : 1355 - 1373
  • [42] Dynamic modeling and vibration characteristics analysis of the aero-engine dual-rotor system with Fan blade out
    Yu, Pingchao
    Zhang, Dayi
    Ma, Yanhong
    Hong, Jie
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2018, 106 : 158 - 175
  • [43] Augmented reality material management system based on post-processing of aero-engine blade code recognition
    Zhang, Jie
    Wang, Shuxia
    He, Weiping
    Li, Jianghong
    Wu, Shixin
    Huang, Jiaxu
    Zhang, Qiang
    Wang, Manxian
    JOURNAL OF MANUFACTURING SYSTEMS, 2022, 65 : 564 - 578
  • [44] Dynamic blade tip clearance control of aero-engine by the integration of cooling air with fuel thermal management system
    Gou, Weilong
    Yang, Shiyu
    Lin, Yuanfang
    Shao, Faning
    Liang, Xingang
    Shi, Bo
    APPLIED THERMAL ENGINEERING, 2025, 261
  • [45] Dynamic Model and Theoretical Investigation for the Fan-Blade Out Event in the Flexible Rotor System of Aero-Engine
    Ma, Yanhong
    Wang, Yongfeng
    Hong, Jie
    PROCEEDINGS OF THE 10TH INTERNATIONAL CONFERENCE ON ROTOR DYNAMICS - IFTOMM, VOL. 4, 2019, 63 : 18 - 33
  • [46] A Robotic Polishing Trajectory Planning Method Combining Reverse Engineering and Finite Element Mesh Technology for Aero-Engine Turbine Blade TBCs
    Fan Yang
    Zhenhua Cai
    Yuepeng Chen
    Shujuan Dong
    Chunming Deng
    Shaopeng Niu
    Wei Zeng
    Shiping Wen
    Journal of Thermal Spray Technology, 2022, 31 : 2050 - 2067
  • [47] A Robotic Polishing Trajectory Planning Method Combining Reverse Engineering and Finite Element Mesh Technology for Aero-Engine Turbine Blade TBCs
    Yang, Fan
    Cai, Zhenhua
    Chen, Yuepeng
    Dong, Shujuan
    Deng, Chunming
    Niu, Shaopeng
    Zeng, Wei
    Wen, Shiping
    JOURNAL OF THERMAL SPRAY TECHNOLOGY, 2022, 31 (07) : 2050 - 2067
  • [48] Method to study kinetics of contact interaction in tool- workpiece system during grinding
    Linenko-Mel'nikov, Yu.P.
    Sverkhtverdye Materialy, 1991, (06): : 40 - 43
  • [49] Design of Non-contact Height Detecting System for a Marine Diesel Engine
    Pan, Xinglong
    He, Guo
    PROCEEDINGS OF THE 4TH INTERNATIONAL CONFERENCE ON MECHATRONICS, MATERIALS, CHEMISTRY AND COMPUTER ENGINEERING 2015 (ICMMCCE 2015), 2015, 39 : 875 - 880
  • [50] Orientation error compensation of turntable for calibration of a non-contact measurement system
    Huo, Ju
    Zhong, Xiao-Qing
    Yang, Ming
    Liu, Jia
    Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2010, 42 (01): : 100 - 105