Design of an advanced automatic inspection system for aircraft parts based on fluorescent penetrant inspection analysis

被引:10
|
作者
Zheng, J. [1 ]
Xie, W. F. [1 ]
Viens, M. [2 ]
Birglen, L. [3 ]
Mantegh, I. [4 ]
机构
[1] Concordia Univ, Dept Mech & Ind Engn, Montreal, PQ H3G 1M8, Canada
[2] Ecole Technol Super, Dept Genie Mecan, Montreal, PQ H3C 1K3, Canada
[3] Polytech Montreal, Dept Mech Engn, Montreal, PQ H3T 1G4, Canada
[4] CNRC Aerosp Mfg Technol Ctr, Montreal, PQ H3S 2S4, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
turbine blades; discontinuities; FPI; image processing; pattern recognition;
D O I
10.1784/insi.2014.57.1.18
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
Non-destructive testing (NDT) of aircraft parts has become increasingly important in improving the safety and reliability of the aerospace industry, especially in the testing of high-temperature and high-pressure turbine engine parts. Among the various types of NDT methods available, fluorescent penetrant inspection (FPI) is comparably more cost-efficient and is widely used in NDT on aircraft parts. However, current FPI still requires considerable labour forces in its processing, inspection and analysis procedures. In this paper, we have developed an advanced automatic inspection system (AAIS) that uses image processing and pattern recognition techniques to aid human inspectors. The system can automatically detect, measure and classify discontinuities from the FPI images of aircraft parts. Tests have been performed on the sample images provided by our industrial partners to evaluate our developed AAIS. The test results demonstrate that the developed system has significantly improved the efficiency of FPI with satisfactory accuracy.
引用
收藏
页码:18 / 34
页数:17
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