• DocumentCode
    1735052
  • Title

    Optimization of PECT system for defect detection on aircraft riveted structures

  • Author

    Xiangchao, Hu ; Feilu, Luo

  • Author_Institution
    Coll. of Mechatron. & Autom., Nat. Univ. of Defense Technol., Changsha, China
  • Volume
    2
  • fYear
    2011
  • Firstpage
    996
  • Lastpage
    999
  • Abstract
    Pulsed eddy current non-destructive testing (PECT) has been proved to be the most effective method for defect detection on aircraft riveted structures. In this paper, a study of PECT system optimization was made using “Method of Phase-shift and Logic-operation” (MPL) and DDS technique on the basis of analysis about the effects that system parameters exert upon the inspecting results. A novel auto-differentially rotary sensor for defect detection on riveted structures was proposed and presented from structure designing and working principle. The advantages and key performances of the optimized system were analyzed and PECT experiments on the specimen of rivet structures are carried out. The experimental results testify the availability of the optimized system and the necessity to optimize the PECT system parameters.
  • Keywords
    aircraft; inspection; nondestructive testing; sensors; structural engineering; DDS technique; PECT system optimization; PECT system parameters; aircraft riveted structures; auto-differentially rotary sensor; defect detection; inspection; method of phase-shift and logic-operation; pulsed eddy current nondestructive testing; Availability; Auto-differentially Rotary Sensor; Method of Phase-shift and Logic-operation; PECT Introduction (Heading 1); Riveted Structure; System Parameter Optimization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Science and Network Technology (ICCSNT), 2011 International Conference on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4577-1586-0
  • Type

    conf

  • DOI
    10.1109/ICCSNT.2011.6182129
  • Filename
    6182129