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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2022, Vol. 43 ›› Issue (7): 425426-425426.doi: 10.7527/S1000-6893.2021.25426

• Material Engineering and Mechanical Manufacturing • Previous Articles     Next Articles

Special defect inspection of composite aramid paper honeycomb sandwich structure

HAO Wei, LI Ming, WANG Jue, XU Ying   

  1. Shenyang Aircraft Industry(Group) Co., LTD, Shenyang 110034, China
  • Received:2021-03-01 Revised:2021-04-29 Published:2021-04-29

Abstract: In the practical test of the composite aramid paper honeycomb sandwich structure, a large ultrasonic attenuation is found in water-squirting through-transmission ultrasonic C-scan detection, while no defects are detected by the pulse echo ultrasonic A-scan method and only a few detects can be identified by the Digital Radiography (DR) method. In this paper, various nondestructive testing methods (such as immersion focused pulse echo ultrasonic C-scan detection, air-coupled through-transmission ultrasonic C-scan detection, reflection infrared detection, shearography, X-ray Computed Tomography (X-CT), etc.) are used to detect the area of large ultrasonic attenuation caused by the through-transmission ultrasonic method. Qualitative localization analyses of most defects are carried out by X-CT detection. The sectional profile of the samples shows that two types of defects in the honeycomb core are the main causes of ultrasonic attenuation in the penetrating method:collapse defects and lattices bubbling defects. These defects are difficult to be detected by X-ray penetrating detection, but they can cause obvious attenuation in ultrasonic propagation. The ultrasonic detecting results are verified by testing the pieces with defects.

Key words: aramid paper honeycomb, through-transmission ultrasonic, pulse echo ultrasonic, X-CT, honeycomb collapse, honeycomb cell bubblinghttp

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