Publication detail

Acquisition Module for Non-Destructive Testing of Aircraft Composite Structures

PHAM, N. LEUCHTER, J. HÁZE, J.

Original Title

Acquisition Module for Non-Destructive Testing of Aircraft Composite Structures

Type

article in a collection out of WoS and Scopus

Language

English

Original Abstract

This paper presents an acquisition module for nondestructive testing (NDT) of aircraft composite structures. The module was designed with multiple inputs, which allows data to be acquired in parallel in order to speed up the process of obtaining a large amount of data. The collected data are then sent to a computer for data processing and structural damage diagnosis. The design was described by using VHDL (Very high-speed integrated circuit Hardware Describe Language) and implemented in FPGA (Field Programmable Logic Array) Altera Cyclone II development board. The designed module is expected to monitor composite materials' structure health using the NDT technique of Electrical Impedance/Resistance Tomography (EIT/ERT).

Keywords

Non-Destructive Testing, Aircraft Composite Materials, Electrical Impedance Tomography, VHDL, FPGA.

Authors

PHAM, N.; LEUCHTER, J.; HÁZE, J.

Released

25. 4. 2023

Publisher

Brno University of Technology

Location

Brno

Pages from

129

Pages to

132

Pages count

4

URL

https://www.eeict.cz/eeict_download/archiv/sborniky/EEICT_2023_sbornik_1.pdf

BibTex

@inproceedings{BUT186984,
  author="Ngoc Nam {Pham} and Jan {Leuchter} and Jiří {Háze}",
  title="Acquisition Module for Non-Destructive Testing of Aircraft Composite Structures",
  year="2023",
  pages="129--132",
  publisher="Brno University of Technology",
  address="Brno",
  url="https://www.eeict.cz/eeict_download/archiv/sborniky/EEICT_2023_sbornik_1.pdf"
}