A vane has an airfoil shell and a spar within the shell. The vane has an outboard shroud at an outboard end of the shell and an inboard platform at an inboard end of the shell. The spar has a first chamber essentially along the suction side and a second chamber along the pressure side opposite the first chamber.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Ceramic matrix composite turbine engine vane


    Beteiligte:
    Shi, Jun (Autor:in) / Ochs, Stuart S. (Autor:in) / Green, Kevin E. (Autor:in) / Jarmon, David C. (Autor:in) / Sahm, Michael K. (Autor:in) / Prill, Lisa A. (Autor:in)

    Erscheinungsdatum :

    18.11.2008


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Turbine vane ceramic endwall

    HAYES, C. W. / ZABIEREK, D. | AIAA | 1975


    COMPOSITE COMPRESSOR VANE OF AN AXIAL TURBINE ENGINE

    ENGLEBERT ERIC | Europäisches Patentamt | 2017

    Freier Zugriff

    Gas Turbine Ceramic Vane Testing

    Nessler, C. G. | SAE Technical Papers | 1974


    Gas turbine engine outlet guide vane assembly

    BREEZE-STRINGFELLOW ANDREW / KHALID SYED ARIF | Europäisches Patentamt | 2022

    Freier Zugriff