High-Frequency Ultrasonic Methods for Determining Corrosion Layer Thickness of Hollow Metallic Components

High-Frequency Ultrasonic Methods for Determining Corrosion Layer Thickness of Hollow Metallic Components
Title:
High-Frequency Ultrasonic Methods for Determining Corrosion Layer Thickness of Hollow Metallic Components
Other Titles:
Ultrasonics
DOI:
10.1016/j.ultras.2018.05.006
Publication Date:
16 May 2018
Citation:
26. Hongwei Liu, Lei Zhang, Hong Fei Liu, Shuting Chen, Shihua Wang, Zheng Zheng Wong, and Kui Yao, “High-Frequency Ultrasonic Methods for Determining Corrosion Layer Thickness of Hollow Metallic Components,” Ultrasonics, https://doi.org/10.1016/j.ultras.2018.05.006, Vol. 89, pp.166–172, 2018.
Abstract:
Corrosion in internal cavity is one of the most common problems occurs in many hollow metallic components, such as pipes containing corrosive fluids and high temperature turbines in aircraft. It is highly demanded to non-destructively detect the corrosion inside hollow components and determine the corrosion extent from the external side. In this work, we present two high-frequency ultrasonic non-destructive testing (NDT) technologies, including piezoelectric pulse-echo and laser-ultrasonic methods, for detecting corrosion of Ni superalloy from the opposite side. The determination of corrosion layer thickness below ~100 micrometers has been demonstrated by both methods, in comparison with X-CT and SEM. With electron microscopic examination, it is found that with multilayer corrosion structure formed over a prolonged corrosion time, the ultrasonic NDT methods can only reliably reveal outer corrosion layer thickness because of the resulting acoustic contrast among the multiple layers due to their respective different mechanical parameters. A time-frequency signal analysis algorithm is employed to effectively enhance the high frequency ultrasonic signal contrast for the piezoelectric pulse-echo method. Finally, a blind test on a Ni superalloy turbine blade with internal corrosion is conducted with the high frequency piezoelectric pulser-receiver method.
License type:
http://creativecommons.org/licenses/by-nc-nd/4.0/
Funding Info:
This work was supported by the Aerospace Program of A*STAR, Singapore through the project IMRE/14–2P1114, and A*STAR Science and Engineering Research Council (SERC) Grant number 1421500068.
Description:
ISSN:
0041-624X
1874-9968
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