Fachinformationsdienst BAUdigital

A platform for research: civil engineering, architecture and urbanism

    ROTOR BLADE AIRFOIL FOR A TURBOMACHINE

    New search for: ALBERT BENEDIKT
    New search for: SIKORSKI SIEGFRIED

    A rotor blade airfoil (25) for a turbomachine (1) that is adapted for rotation about a longitudinal axis (2) of the turbomachine (1) is provided. The rotor blade airfoil (25) is built from an airfoil material reinforced with a fibrous material (30). At least a portion of the fibers of the fibrous material (30), in particular at least 20%, preferably at least 30% of the fibers, are oriented in a first fiber direction (31), and the first fiber direction (31) is tilted with respect to the stacking axis of the rotor blade airfoil (25).

    Access

    Download

    Access

    Download

    Page navigation

    Document information
    Similar titles

    Export, share and cite

    ROTOR BLADE AIRFOIL FOR A TURBOMACHINE

    New search for: ALBERT BENEDIKT
    New search for: SIKORSKI SIEGFRIED

    A rotor blade airfoil (25) for a turbomachine (1) that is adapted for rotation about a longitudinal axis (2) of the turbomachine (1) is provided. The rotor blade airfoil (25) is built from an airfoil material reinforced with a fibrous material (30). At least a portion of the fibers of the fibrous material (30), in particular at least 20%, preferably at least 30% of the fibers, are oriented in a first fiber direction (31), and the first fiber direction (31) is tilted with respect to the stacking axis of the rotor blade airfoil (25).

    Access

    Download

    ROTOR BLADE AIRFOIL FOR A TURBOMACHINE

    New search for: ALBERT BENEDIKT
    New search for: SIKORSKI SIEGFRIED

    A rotor blade airfoil (25) for a turbomachine (1) that is adapted for rotation about a longitudinal axis (2) of the turbomachine (1) is provided. The rotor blade airfoil (25) is built from an airfoil material reinforced with a fibrous material (30). At least a portion of the fibers of the fibrous material (30), in particular at least 20%, preferably at least 30% of the fibers, are oriented in a first fiber direction (31), and the first fiber direction (31) is tilted with respect to the stacking axis of the rotor blade airfoil (25).

    Access

    Download

    Access

    Download

    Page navigation

    Document information
    Similar titles

    Export, share and cite

    Document information
    Title:

    ROTOR BLADE AIRFOIL FOR A TURBOMACHINE

    Contributors:

    ALBERT BENEDIKT (author) / SIKORSKI SIEGFRIED (author)

    Publication date:

    2020-06-25

    Type of media:

    Patent

    Type of material:

    Electronic Resource

    Language:

    English

    Classification:

    IPC:  F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / C04B Kalk , LIME

    Similar titles

    Rotor blade airfoil for a turbomachine

    ALBERT BENEDIKT / SIKORSKI SIEGFRIED | European Patent Office | 2021

    Free access

    METHOD FOR MANUFACTURING A TURBOMACHINE BLADE

    DESNOYER VICTOR / MARBORUT MICHAEL / GILLOT CLEMENT et al. | European Patent Office | 2024

    Free access

    Issues of Simulation of Turbomachine Blade Vibration

    Pisarenko, G. S. / Vorob ev, Y. S. | British Library Online Contents | 2000

    The development of a GUI program for automated generating rotor blade airfoil performance table

    Kim, T. / Yee, K. / Oh, S. et al. | British Library Online Contents | 2009

    AUBE DE ROTOR POUR UNE TURBOMACHINE D’AERONEF

    CARIOU ROMAIN PIERRE / PAQUIN SYLVAIN / ROLLINGER ADRIEN BERNARD VINCENT et al. | European Patent Office | 2025

    Free access
    Back to top