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Optimizing the Accuracy and Method of Detecting Lightning Damage to Aerospace Composite Material Using Electrical Impedance Analysis

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26220%2F26%3A0198703" target="_blank" >RIV/00216305:26220/26:0198703 - isvavai.cz</a>

  • Alternative codes found

    RIV/00216275:25510/25:39922899

  • Result on the web

    <a href="https://ieeexplore.ieee.org/document/10966217" target="_blank" >https://ieeexplore.ieee.org/document/10966217</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1109/TAES.2025.3561727" target="_blank" >10.1109/TAES.2025.3561727</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Optimizing the Accuracy and Method of Detecting Lightning Damage to Aerospace Composite Material Using Electrical Impedance Analysis

  • Original language description

    In line with the trends of reducing emissions in transport, the aviation industry has adopted significant use of composite materials in aircraft design. The use of composite materials for construction can also enhance material resistance to lightning strikes, where it is necessary to improve electrical conductivity and structural integrity. This article presents the results of research to use electrical impedance tomography (EIT) to measure the properties of structural aviation materials with the aim of achieving higher accuracy and reliability in detecting material failure caused by electrical voltage discharges. Procedures for diagnosing the state of glass fiber reinforced polymer composite materials in the event of a possible lightning strike and the possibilities of automatic diagnostics based on measuring conductive layers of the material by impedance methods are presented. Our approach to reduce measurement uncertainty in detecting material failures by high-voltage discharges is discussed, which can be used to determine which material designs have better resistance to lightning strikes. The results of our modeling and analysis were verified practically in a high-voltage laboratory to demonstrate the potential use of EIT in aircraft design.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • OECD FORD branch

    20201 - Electrical and electronic engineering

Result continuities

  • Project

  • Continuities

    S - Specificky vyzkum na vysokych skolach

Others

  • Publication year

    2025

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Name of the periodical

    IEEE Transactions on Aerospace and Electronic Systems

  • ISSN

    0018-9251

  • e-ISSN

    1557-9603

  • Volume of the periodical

    61

  • Issue of the periodical within the volume

    4

  • Country of publishing house

    US - UNITED STATES

  • Number of pages

    17

  • Pages from-to

    10349-10365

  • UT code for WoS article

    001550830000028

  • EID of the result in the Scopus database

    2-s2.0-105002773071