Laser & Optoelectronics Progress, Volume. 55, Issue 4, 041201(2018)
Three-Dimensional Measurement Method of Aero-Engine Blades Based on Projected Fringe Order Identification
Fig. 1. Structure diagram of structured light three-dimensional reconstruction system
Fig. 10. (a) Three-dimensional form and (b) gray-scale form of discontinuous wrapping phase
Fig. 11. (a) Unwrapping phase diagram with the method of point by point; (b) unwrapping phase diagram with discontinuous path integral algorithm based on quality graph guidance
Fig. 14. Trend of the phase of point P with the change of u. (a) Change law of real phase; (b) change law of wrapped phase
Fig. 16. Images of standard measured mass surface with projected fringe. (a) 0 phase shift; (b) π/2 phase shift; (c) π phase shift; (d) 3π/2 phase shift
Fig. 17. (a) Initial restoration result and (b) stitching restoration result of standard measured mass
Fig. 18. (a) Physical map of inlet guide vane; (b) extraction result of the area of vane
Fig. 19. Images of inlet guide vane surface with projected fringe. (a) 0 phase shift; (b) π/2 phase shift; (c) π phase shift; (d) 3π/2 phase shift
Fig. 22. (a) Initial restoration result, (b) preliminary stitching restoration result and (c) stitching result using the iterative nearest point algorithm of inlet guide vane
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Long Ma, Hongyue Xu, Yanmin Hu, Jianchun Wang, Chao Huang, Xin Pei. Three-Dimensional Measurement Method of Aero-Engine Blades Based on Projected Fringe Order Identification[J]. Laser & Optoelectronics Progress, 2018, 55(4): 041201
Category: Instrumentation, measurement, and metrology
Received: Aug. 26, 2017
Accepted: --
Published Online: Sep. 11, 2018
The Author Email: Long Ma (malong9904@aliyun.com)