Laser & Optoelectronics Progress, Volume. 55, Issue 4, 041201(2018)

Three-Dimensional Measurement Method of Aero-Engine Blades Based on Projected Fringe Order Identification

Long Ma*, Hongyue Xu, Yanmin Hu, Jianchun Wang, Chao Huang, and Xin Pei
Author Affiliations
  • Sino-European Institute of Aviation Engineering, Civil Aviation University of China, Tianjin 300300, China
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    Figures & Tables(24)
    Structure diagram of structured light three-dimensional reconstruction system
    Object graph of structured light three-dimensional reconstruction system
    Control interface of upper computer
    Structure of measurement system
    Schematic of calibration on Z axis
    Schematic of rotation axis calibration
    Result of center fitting
    Fitted circle and axis of rotation
    Fringe projection pattern
    (a) Three-dimensional form and (b) gray-scale form of discontinuous wrapping phase
    (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
    Result of feature point extraction and matching
    Flow chart of stripe recognition method basedon active binocular vision
    Trend of the phase of point P with the change of u. (a) Change law of real phase; (b) change law of wrapped phase
    Stitching flow chart of three-dimensional restoration result
    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
    (a) Initial restoration result and (b) stitching restoration result of standard measured mass
    (a) Physical map of inlet guide vane; (b) extraction result of the area of vane
    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
    (a) Wrapped phase and (b) unwrapped phase on inlet guide vane surface
    Height diagram of inlet guide vane surface
    (a) Initial restoration result, (b) preliminary stitching restoration result and (c) stitching result using the iterative nearest point algorithm of inlet guide vane
    Blade section of inlet guide vane
    • Table 1. Error comparison of fitting results of two models

      View table

      Table 1. Error comparison of fitting results of two models

      No.Altitude /mmPhasedifference /radTrianglemodel /mmPolynomialmodel /mm
      11.2200-0.6504-0.02150.0066
      22.4400-1.3169-0.00920.0059
      33.6600-1.9803-0.0218-0.0164
      44.8800-2.64060.00180.0001
      56.1000-3.2862-0.0060-0.0122
      67.3200-3.94630.02020.0119
      78.5400-4.60580.0064-0.0012
      89.7600-5.27790.01650.0120
      910.9800-5.95750.00240.0036
      1012.2000-6.6316-0.0193-0.0101
      Average error /mm0.01250.0080
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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

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    Paper Information

    Category: Instrumentation, measurement, and metrology

    Received: Aug. 26, 2017

    Accepted: --

    Published Online: Sep. 11, 2018

    The Author Email: Long Ma (malong9904@aliyun.com)

    DOI:10.3788/LOP55.041201

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