Laser & Optoelectronics Progress, Volume. 60, Issue 15, 1514004(2023)

Controllability of Laser Removal of Aircraft Skin Paint Layer Based on Response Surface Analysis

Wenfeng Yang1、*, Dehui Lin1, Mian Zhong1, Shaolong Li1, Ziran Qian1, Guochun Liu1, Yu Cao2, Yi Xu1, Sai Zhang1, and Guo Li1
Author Affiliations
  • 1Civil Aircraft Composites Maintenance Research Center, Civil Aviation Flight University of China, Guanghan618307, Sichuan, China
  • 2Laser and Optoelectronic Intelligent Manufacturing Research Institute, Wenzhou University, Wenzhou 325035, Zhejiang, China
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    Figures & Tables(18)
    Laser processing equipment diagram and process diagram. (a) Laser processing equipment; (b) schematic diagram of the process
    Schematic of laser cleaning. (a) Cleaning area; (b) path of spot scanning
    Description of paint removal thickness measurement method
    Illustration of the Box-Behnken experimental design with three factors and three levels
    Effect of laser multiparameter coupling on T
    Interaction of laser power and number of scans on the thickness of paint removal. (a) Contour graph; (b) response graph
    Effect of laser multiparameter coupling on Sa
    Schematic diagram of the lap joint shape of the crater
    Interaction of laser power and number of scans on Sa. (a) Contour graph; (b) response graph
    Macro effect and measurements of the samples obtained in scheme 1. (a) Macro effect; (b) thickness of the paint layer removal; (c) surface roughness
    Macro effect and measurements of the samples obtained in scheme 2. (a) Macro effect; (b) thickness of the paint layer removal; (c) surface roughness
    • Table 1. Main parameters of the laser

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      Table 1. Main parameters of the laser

      Average power

      P /W

      Pulse frequency

      f /kHz

      Beam diameter

      D /μm

      Scan speed

      v /(mm·s-1

      Pulse duration

      τp /ns

      0—1201—200500—800060—350
    • Table 2. Test factor and level coding table

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      Table 2. Test factor and level coding table

      FactorExtreme value
      Low(-1)Medium(0)High(1)
      Power P /W243036
      Spot overlap rate α/%607080
      Number of scans N123
    • Table 3. Response surface experimental design matrix and experimental results

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      Table 3. Response surface experimental design matrix and experimental results

      No.ParameterResult
      P /Wα /%NT /μmSa /μm
      R12460211.593.13
      R23660224.394.16
      R3306019.822.10
      R43060329.943.02
      R5247016.852.21
      R63670316.742.47
      R72470318.532.43
      R83670265.502.99
      R93070223.053.34
      R103070224.933.31
      R113070227.613.16
      R123070227.593.00
      R133070223.303.87
      R142480218.092.95
      R153680253.843.50
      R163080115.932.31
      R173080360.862.15
    • Table 4. Analysis of variance for paint removal thickness model

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      Table 4. Analysis of variance for paint removal thickness model

      SourceSum of squareDegree of freedomMean squareFvalueProb>FSignificant
      Model4652.436775.40121.09<0.0001Yes
      A-α665.761665.76103.97<0.0001
      B-P1388.9111388.91216.90<0.0001
      C-N1968.4711968.47307.41<0.0001
      AB131.681131.6820.560.0011
      AC153.881153.8824.030.0006
      BC343.731343.7353.68<0.0001
      Residual64.03106.40
      Lack of fit44.2567.381.490.3640No
      Pure error19.7844.94
      Cor total4716.4616
    • Table 5. Analysis of variance for surface roughness model

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      Table 5. Analysis of variance for surface roughness model

      SourceSum of squareDegree of freedomMean squareFvalueProb>FSignificant
      Model5.2990.598.140.0057Yes
      A-α0.28010.2803.890.0890
      B-P0.72010.7209.960.0160
      C-N0.28010.2803.890.0892
      AB0.05810.0580.800.4017
      AC0.29010.2904.030.0846
      BC0.02210.0220.310.5943
      A21.012×10-311.012×10-30.0140.9092
      B20.05510.0550.760.4112
      C23.61013.61049.890.0002
      Residual0.51070.072
      Lack of fit0.07630.0250.24No
      Pure error0.43040.110
      Cor total5.80016
    • Table 6. Optimization criteria and weight

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      Table 6. Optimization criteria and weight

      NameCriteriaWeight
      GoalLowerUpper
      Spot overlap rate α /%In range60801
      Power P /WIn range24361
      Number of scans NEqual to 2131
      Paint layer removal thickness T /μmTarget(30/50)6.8565.501
      Surface roughnessSa /μmMaximize2.104.161
    • Table 7. Optimization results of parameter coupling and experimental verification

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      Table 7. Optimization results of parameter coupling and experimental verification

      TargetNo.T /μmError /μmSa /μmError /%TargetNo.T /μmError /μmSa /μmError /%
      30 μmPre30.003.9550 μmPre50.003.54
      L129.060.943.580.37T145.544.463.370.17
      L227.502.503.780.17T248.181.823.670.13
      L328.371.633.640.31T351.881.883.450.09
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    Wenfeng Yang, Dehui Lin, Mian Zhong, Shaolong Li, Ziran Qian, Guochun Liu, Yu Cao, Yi Xu, Sai Zhang, Guo Li. Controllability of Laser Removal of Aircraft Skin Paint Layer Based on Response Surface Analysis[J]. Laser & Optoelectronics Progress, 2023, 60(15): 1514004

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    Paper Information

    Category: Lasers and Laser Optics

    Received: May. 22, 2022

    Accepted: Jul. 7, 2022

    Published Online: Aug. 18, 2023

    The Author Email: Yang Wenfeng (ywfcyy@163.com)

    DOI:10.3788/LOP221882

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