A new double spiral scanning method for CFRP step blind hole drilling by nanosecond UV laser

被引:0
作者
Lu, Ya [1 ,2 ,3 ]
Wu, Hongbo [1 ,2 ]
Rong, Youmin [1 ,2 ]
Chen, Long [1 ,2 ]
Li, Wenyuan [1 ,2 ]
Zhang, Guojun [1 ,2 ,3 ]
Huang, Yu [1 ,2 ,3 ]
Liu, Pengrui [4 ]
Bao, Tianjiao [4 ]
机构
[1] Huazhong Univ Sci & Technol, Natl Key Lab Intelligent Mfg Equipment & Technol, Wuhan, Peoples R China
[2] Huazhong Univ Sci & Technol, Sch Mech Sci & Engn, Wuhan, Peoples R China
[3] Guangdong HUST Ind Technol Res Inst, Guangdong Prov Key Lab Mfg Equipment Digitizat, Dongguan, Peoples R China
[4] AECC Beijing Inst Aeronaut Mat, Beijing, Peoples R China
基金
中国博士后科学基金; 中国国家自然科学基金;
关键词
Laser drilling; CFRP; Double spiral scanning; High-quality ablation; Processing efficiency; COMPOSITES; IR;
D O I
10.1016/j.optlastec.2025.112704
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Carbon fiber reinforced polymer (CFRP) composites used in aerospace under extreme conditions will inevitably leads to the occurrence of delamination, pits, and other defects. High-precision step blind hole drilling is the key process for eliminating damaged defects and preparing for subsequent repairs. A new double spiral scanning mode (DSSM) method was proposed to achieve five-layer step blind hole drilling with low damage and high efficiency. By analyzing the morphologies at the bottom of the blind hole under different laser frequencies, scanning intervals and scanning angles, it was found that the material between the scanning tracks was mainly removed by thermal ablation and expansion impact of the plasma plume, and the stable removal scanning intervals were related to the fiber arrangement angles. When the scanning interval was too large, the sector residue (SR) appeared on the ablative surface. When the traditional scanning method was used, there was no SR when the spacing was less than 0.04 mm. When the spacing was greater than 0.04 mm, the SR increased with the spacing. By changing the scanning angle, the curve mapping relationship between the scanning angle and the maximum scanning interval without SR was obtained. Compared with SSM, the variable curvature characteristic of the DSSM reduced the influence of the beam occlusion effect on processing. The maximum scanning spacing corresponding to no SR was increased to 0.12 mm, and the removal rate of single-layer blind hole material was increased by 34.77 % (2.045 mm3/s to 2.756 mm3/s). The processing efficiency was increased by 26.91 % (7.985 s to 5.836 s). Finally, DSSM was used to achieve high-precision drilling of five-layer equal-depth step blind hole structure with single layer depth of 125 +/- 15 mu m.
引用
收藏
页数:15
相关论文
共 39 条
  • [1] The fatigue of carbon fibre reinforced plastics - A review
    Alam, Parvez
    Mamalis, Dimitrios
    Robert, Colin
    Floreani, Christophe
    Bradaigh, Conchur M. O.
    [J]. COMPOSITES PART B-ENGINEERING, 2019, 166 : 555 - 579
  • [2] Chen L., 2023, Measurement, V221, P10
  • [3] Bonding quality monitoring of Carbon Fiber Reinforced Plastics bonded structures by fiber Bragg gratings
    Di Palma, Pasquale
    Leone, Marco
    Russo, Marialessandra
    Iadicicco, Agostino
    Cavaccini, Giovanni
    Consales, Marco
    Cusano, Andrea
    Campopiano, Stefania
    [J]. OPTICS AND LASER TECHNOLOGY, 2023, 161
  • [4] El-Hofy M., 2017, Abrasive Water Jet Machining of Multidirectional CFRP Laminates, P535
  • [5] Laser beam machining of carbon fiber reinforced composites: a review
    El-Hofy, M. H.
    El-Hofy, H.
    [J]. INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2019, 101 (9-12) : 2965 - 2975
  • [6] Fan Yuqing, 2009, Acta Aeronautica et Astronautica Sinica, V30, P534
  • [7] Experimental and numerical analysis of step drill bit performance when drilling woven CFRPs
    Feito, N.
    Diaz-Alvarez, J.
    Lopez-Puente, J.
    Miguelez, M. H.
    [J]. COMPOSITE STRUCTURES, 2018, 184 : 1147 - 1155
  • [8] Identification of crack and disbond fronts in repaired aircraft structural panels with bonded FRP composite patches
    Fujimoto, Shin-etsu
    Sekine, Hideki
    [J]. COMPOSITE STRUCTURES, 2007, 77 (04) : 533 - 545
  • [9] Geier N., 2023, Compos Pt B-Eng., V254, P21
  • [10] Effect of laser cleaning in Laser Assisted Joining of CFRP and PC sheets
    Genna, S.
    Lambiase, F.
    Leone, C.
    [J]. COMPOSITES PART B-ENGINEERING, 2018, 145 : 206 - 214