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Exploring Vibrations of UAV Propellers: A Preliminary Study for Characterization and Fault Detection

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21260%2F24%3A00375277" target="_blank" >RIV/68407700:21260/24:00375277 - isvavai.cz</a>

  • Result on the web

    <a href="https://doi.org/10.23919/NTCA60572.2024.10517835" target="_blank" >https://doi.org/10.23919/NTCA60572.2024.10517835</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.23919/NTCA60572.2024.10517835" target="_blank" >10.23919/NTCA60572.2024.10517835</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Exploring Vibrations of UAV Propellers: A Preliminary Study for Characterization and Fault Detection

  • Original language description

    The propulsion systems of unmanned aircraft such as multicopters are very vulnerable to any kind of damage. Thus, the presented study introduces the possibility of using vibration sensing to determine the condition of the rotating propeller to detect possible damage or contamination. For the purpose of this study, a test stand was designed and a total of 3 different propeller damages were tested. These included minor and major damage to the tip of the propeller blade as well as disruption of the leading edge profile geometry. Propeller vibration was captured within the operating range of propeller (from 3 500 to 6000 RPM) in the axial X-axis and radial Y-axis. The measured data were processed by spectral analysis, i.e., by calculating the amplitude spectrum using a Fourier Transform. The outputs in the form of spectograms for each damage type and individual RPM were further processed by Principal Component Analysis (PCA). From the PCA, it was possible to identify the vibration frequency spectrum of the tested propeller and the individual damaged states.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

  • Continuities

    S - Specificky vyzkum na vysokych skolach

Others

  • Publication year

    2024

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    New Trends in Civil Aviation: Proceedings of the 24th International Conference on New Trends in Civil Aviation 2024

  • ISBN

    978-80-01-07181-6

  • ISSN

    2694-7854

  • e-ISSN

  • Number of pages

    5

  • Pages from-to

    247-251

  • Publisher name

    České vysoké učení technické v Praze

  • Place of publication

    Praha

  • Event location

    Praha

  • Event date

    Apr 25, 2024

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    001223424800024