In situ non-destructive evaluation of an aircraft UHF antenna radome based on pulse-echo ultrasonic propagation imaging
Source abstract
Abstract
Abstract Most aircraft antennas are protected by radomes made of composite materials. However, antenna radome structures are easily damaged by external forces and internal manufacturing defects. To detect damage in the composite antenna radomes while in service, a full-field pulse-echo ultrasonic propagation imaging (PE UPI) system is proposed as an in situ non-destructive inspection technique, which is mobile inside a hangar. The radome is generally a double-curvature structure, and thus, a curvature compensation algorithm is also developed to increase damage visibility. The proposed hardware and software have been tested by detecting a resin rich region formed between the E-glass/epoxy plies. To visualize the damage, PE ultrasonic wave propagation imaging has been performed, and ultrasonic energy mapping has also been applied. A curvature compensating algorithm has been newly developed and compared for its performance in damage visibility improvement. To verify the size of the real defects of a UHF antenna radome, destructive testing has been performed by cutting the defect area, polishing the cross section and investigating the section using a 50× microscope. The results have shown the feasibility of the proposed PE UPI system and the inspection strategy as an in situ non-destructive evaluation technique for radome structures.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Structural Health Monitoring Techniques · Ultrasonics and Acoustic Wave Propagation · Non-Destructive Testing Techniques
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (14)
Show source-provided references
1. Radome health management based on synthesized impact detection, laser ultrasonic spectral imaging, and wavelet transformed ultrasonic propagation imaging methods10.1016/j.compositesb.2012.07.033 ↗
2. Aviation Maintenance Technician Handbook – Airframe, FAA (2012).
3. Baaran · 2009
4. J. Heida, D. Platenkamp, Evaluation of non-destructive inspection methods for composite. Aerospace structures 16th NDT in progress (2011) 1–12.
5. M.A.U. Khan, Non-destructive testing applications in commercial aircraft maintenance. ECNDT 98, 4(6) (1999) 1–10.
6. In-service flaw detection and quantification in the composite structures of aircraft10.2478/v10164-010-0003-0 ↗
7. G. Georgeson, Trends in R&D for nondestructive evaluation of in-service aircraft. In: 5th international symposium on NDT in aerospace (2013) 1-76.
8. Sounds ultra advanced, Web Exclusives: Aerospace Testing International. http://www.aerospacetestinginternational.com/articles.php?ArticleID=1185 (accessed 16.08.09).
9. S.C. Hong, J.R. Lee, Full-field pulse-echo ultrasonic wave propagation imaging for non-destructive composite inspection. In: 20th international conference on composite materials (2015) 1–6.
10. E.B. Flynn, J.R. Lee, G.J. Jarmer, G. Park, Frequency-wavenumber processing of laser-excited guided waves for imaging structural features and defects. In: 6th European workshop on structural health monitoring 2012 (2012) 1–8.
11. Structural imaging through local wavenumber estimation of guided waves10.1016/j.ndteint.2013.04.003 ↗
12. Spar disband visualization in in-service composite aircraft with ultrasonic propagation imager10.1016/j.ast.2015.05.010 ↗
13. Development of single channeled serial-connected piezo-electric sensor array and damage visualization based on multi-source wave propagation imaging
14. Identification of cracks in thin-walled structures by means of wavenumber filtering10.1016/j.ymssp.2014.05.041 ↗