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3D Shape Measurement of Aeroengine Blade Based on Fringe Projection Profilometer Improved by Multi-Layer Concentric Ring Calibration.
Chen, Ze; Ju, Yuhang; Sun, Chuanzhi; Wang, Yinchu; Liu, Yongmeng; Tan, Jiubin.
Affiliation
  • Chen Z; Center of Ultra-Precision Optoelectronic Instrument Engineering, Harbin Institute of Technology, Harbin 150080, China.
  • Ju Y; Key Lab of Ultra-Precision Intelligent Instrumentation Engineering, Harbin Institute of Technology, Ministry of Industry and Information Technology, Harbin 150080, China.
  • Sun C; Center of Ultra-Precision Optoelectronic Instrument Engineering, Harbin Institute of Technology, Harbin 150080, China.
  • Wang Y; Key Lab of Ultra-Precision Intelligent Instrumentation Engineering, Harbin Institute of Technology, Ministry of Industry and Information Technology, Harbin 150080, China.
  • Liu Y; Center of Ultra-Precision Optoelectronic Instrument Engineering, Harbin Institute of Technology, Harbin 150080, China.
  • Tan J; Key Lab of Ultra-Precision Intelligent Instrumentation Engineering, Harbin Institute of Technology, Ministry of Industry and Information Technology, Harbin 150080, China.
Sensors (Basel) ; 24(9)2024 Apr 28.
Article in En | MEDLINE | ID: mdl-38732915
ABSTRACT
The precision requirements for aeroengine blade machining are exceedingly stringent. This study aims to improve the accuracy of existing aeroengine blade measurement methods while achieving comprehensive measurement. Therefore, this study proposes a new concentric ring calibration method and designs a multi-layer concentric ring calibration plate. The effectiveness of this calibration method was verified through actual testing of standard ball gauges. Compared with the checkerboard-grid calibration method, the average deviation of the multilayer concentric ring calibration method for measuring the center distance of the standard sphere is 0.02352, which improves the measurement accuracy by 3-4 times. On the basis of multi-layer concentric ring calibration, this study builds a fringe projection profiler based on the three-frequency twelve-step phase shift method. Compared with the CMM, the average deviation of the blade chord length measured by this solution is 0.064, which meets the measurement index requirements of aeroengine fan blades.
Key words

Full text: 1 Collection: 01-internacional Database: MEDLINE Language: En Journal: Sensors (Basel) Year: 2024 Document type: Article Affiliation country: China Country of publication: Switzerland

Full text: 1 Collection: 01-internacional Database: MEDLINE Language: En Journal: Sensors (Basel) Year: 2024 Document type: Article Affiliation country: China Country of publication: Switzerland