Number of the records: 1  

Neural network AE source location apart from structure size and material

  1. 1.
    SYSNO ASEP0349882
    Document TypeC - Proceedings Paper (int. conf.)
    R&D Document TypeConference Paper
    TitleNeural network AE source location apart from structure size and material
    Author(s) Chlada, Milan (UT-L) RID, ORCID
    Převorovský, Zdeněk (UT-L) RID
    Blaháček, Michal (UT-L)
    Number of authors3
    Source Title29th Europen Conference on Acoustic Emission Testing. - Vienna : TÚV Austria, 2010 - ISBN 978-3-200-01956-0
    Pagess. 1-8
    Number of pages8 s.
    Publication formCD-ROM - CD-ROM
    ActionEuropean Conference on Acoustic Emission Testing 2010 /29./
    Event date08.09.2010-10.09.2010
    VEvent locationVídeň
    CountryAT - Austria
    Event typeEUR
    Languageeng - English
    CountryAT - Austria
    KeywordsAE source location ; artificial neural networks ; arrival time profiles
    Subject RIVBI - Acoustics
    R&D ProjectsFR-TI1/274 GA MPO - Ministry of Industry and Trade (MPO)
    GAP104/10/1430 GA ČR - Czech Science Foundation (CSF)
    CEZAV0Z20760514 - UT-L (2005-2011)
    AnnotationAE localization procedures using artificial neural networks (ANN) represent extremely effective alternative to classical triangulation methods. Nevertheless, their application always requires full-scale, time consuming ANN training on each specific structure. Disadvantage of particularly trained ANN algorithm is in its non-transferability to any other object. A new ANN-based AE source location approach is proposed in this paper to overcome such limitation. The method replaces standard arrival time differences at the ANN inputs by so called signal arrival time profiles, independent on material and scale changes. The ANN training can be also performed theoretically on geometrical models and learned ANN is then applied on real structures with different dimensions and materials. Such approach enables considerable extension of ANN application possibilities. The use of new AE source location method is illustrated on experimental data obtained during aircraft structure part testing.
    WorkplaceInstitute of Thermomechanics
    ContactMarie Kajprová, kajprova@it.cas.cz, Tel.: 266 053 154 ; Jana Lahovská, jaja@it.cas.cz, Tel.: 266 053 823
    Year of Publishing2011
Number of the records: 1  

  This site uses cookies to make them easier to browse. Learn more about how we use cookies.