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Analysis of material removal on radial compressor wheel of aircraft engine after finishing production operations using CMM

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F18%3A00325212" target="_blank" >RIV/68407700:21220/18:00325212 - isvavai.cz</a>

  • Result on the web

    <a href="http://www.mmscience.eu/november-2018.html#201818" target="_blank" >http://www.mmscience.eu/november-2018.html#201818</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.17973/MMSJ.2018_11_201818" target="_blank" >10.17973/MMSJ.2018_11_201818</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Analysis of material removal on radial compressor wheel of aircraft engine after finishing production operations using CMM

  • Original language description

    This paper deals with the dimensional analysis of the turboprop aircraft engine radial compressor wheel. The radial compressor wheel is very complex component. This part is manufactured by turning and five-axis milling technology. Due to the high stress of this part in service life, the residual stress in the surface layer is important. Desirable are the compressive stress levels to prevent cracks. For this reason, research is being carried out on technologies that influence the surface layer. They are the finishing technologies vibrational tumbling and superfinishing. The article describes the method used to measure the thickness variation of blade of the compressor wheel after vibrational tumbling and superfinishing. In terms of shape complexity a coordinate measuring machine with a rotary table was used.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>SC</sub> - Article in a specialist periodical, which is included in the SCOPUS database

  • CEP classification

  • OECD FORD branch

    20301 - Mechanical engineering

Result continuities

  • Project

    <a href="/en/project/TH01011405" target="_blank" >TH01011405: Life extension and repair process development of Ti6Al4V compressor blades used in turboprop engines</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2018

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    MM Science Journal

  • ISSN

    1803-1269

  • e-ISSN

    1805-0476

  • Volume of the periodical

    4_2018

  • Issue of the periodical within the volume

    4

  • Country of publishing house

    CZ - CZECH REPUBLIC

  • Number of pages

    5

  • Pages from-to

    2521-2525

  • UT code for WoS article

  • EID of the result in the Scopus database

    2-s2.0-85057342204